diff --git a/ale/drivers/nh_drivers.py b/ale/drivers/nh_drivers.py
index f7d96edab2f15554faa5e319144a4e90b5b4ec77..7740a92a59f3ce08895841e4539ea3a27feceabf 100644
--- a/ale/drivers/nh_drivers.py
+++ b/ale/drivers/nh_drivers.py
@@ -11,6 +11,7 @@ from ale.base.type_distortion import NoDistortion
from ale.base.data_naif import NaifSpice
from ale.base.label_isis import IsisLabel
from ale.base.type_sensor import Framer
+from ale.base.type_sensor import LineScanner
class NewHorizonsLorriIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Driver):
"""
@@ -65,3 +66,125 @@ class NewHorizonsLorriIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoD
@property
def sensor_name(self):
return self.label['IsisCube']['Instrument']['SpacecraftName']
+
+
+class NewHorizonsLeisaIsisLabelNaifSpiceDriver(LineScanner, IsisLabel, NaifSpice, NoDistortion, Driver):
+ """
+ Driver for reading New Horizons LEISA ISIS3 Labels.
+ """
+
+ @property
+ def instrument_id(self):
+ """
+ Returns an instrument id for uniquely identifying the instrument, but often
+ also used to be piped into Spice Kernels to acquire IKIDs. Therefore they
+ the same ID the Spice expects in bods2c calls.
+
+ Returns
+ -------
+ : str
+ instrument id
+ """
+ id_lookup = {
+ "LEISA" : "NH_RALPH_LEISA"
+ }
+ return id_lookup[super().instrument_id]
+
+ @property
+ def ikid(self):
+ """
+ Overridden to grab the ikid from the Isis Cube since there is no way to
+ obtain this value with a spice bods2c call. Isis sets this value during
+ ingestion, based on the original fits file.
+
+ Returns
+ -------
+ : int
+ Naif ID used to for identifying the instrument in Spice kernels
+ """
+ return self.label['IsisCube']['Kernels']['NaifFrameCode'][0]
+
+
+ @property
+ def ephemeris_start_time(self):
+ """
+ Returns the ephemeris start time of the image.
+ Expects spacecraft_id to be defined. This should be the integer
+ Naif ID code for the spacecraft.
+
+ Returns
+ -------
+ : float
+ ephemeris start time of the image
+ """
+ return spice.scs2e(self.spacecraft_id, self.spacecraft_clock_start_count)
+
+ @property
+ def ephemeris_stop_time(self):
+ """
+ ISIS doesn't preserve the spacecraft stop count that we can use to get
+ the ephemeris stop time of the image, so compute the ephemeris stop time
+ from the start time and the exposure duration.
+ """
+ return self.ephemeris_start_time + self.exposure_duration * self.image_lines
+
+ @property
+ def detector_center_line(self):
+ """
+ Returns the center detector line. Expects ikid to be defined. This should
+ be an integer containing the Naif Id code of the instrument.
+
+ Returns
+ -------
+ : float
+ Detector line of the principal point
+ """
+ return 0
+
+ @property
+ def detector_center_sample(self):
+ """
+ Returns the center detector sample. Expects ikid to be defined. This should
+ be an integer containing the Naif Id code of the instrument.
+
+ Returns
+ -------
+ : float
+ Detector sample of the principal point
+ """
+ return 0
+
+ @property
+ def sensor_name(self):
+ """
+ Returns the name of the instrument. Need to over-ride isis_label because
+ InstrumentName is not defined in the ISIS label for NH Leisa cubes.
+
+ Returns
+ -------
+ : str
+ Name of the sensor
+ """
+ return self.instrument_id
+
+ @property
+ def sensor_model_version(self):
+ """
+ Returns
+ -------
+ : int
+ ISIS sensor model version
+ """
+ return 1
+
+ @property
+ def exposure_duration(self):
+ """
+ The exposure duration of the image, in seconds
+
+ Returns
+ -------
+ : float
+ Exposure duration in seconds
+ """
+ return self.label['IsisCube']['Instrument']['ExposureDuration']
diff --git a/notebooks/KernelSlice.ipynb b/notebooks/KernelSlice.ipynb
index df22e8fc113bad2782e41400c26496594507fb63..f8276f043b998d040573670745a089793095be24 100644
--- a/notebooks/KernelSlice.ipynb
+++ b/notebooks/KernelSlice.ipynb
@@ -18,10 +18,9 @@
"\n",
"\n",
"# These should be provided when running this script. \n",
- "cube = \"/home/acpaquette/B10_013341_1010_XN_79S172W.cub\"\n",
- "output_dir = \"/Users/jmapel/ale/nb_test\" # Output dir for created kernel files\n",
- "data_dir = \"/usgs/cpkgs/isis3/data/\" # Dir of where to pull original kernels from\n",
- "ckslicer_loc = \"/Users/jmapel/ale/ckslicer\"\n",
+ "cube = \"leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced.cub\"\n",
+ "output_dir = \"leisa/lsb_0296962438_0x53c_eng/\" # Output dir for created kernel files\n",
+ "data_dir = \"isis3/isis_data/\" # Dir of where to pull original kernels from\n",
"\n",
"def merge_intervals(intervals):\n",
" \"\"\"\n",
@@ -48,7 +47,7 @@
" merged[-1] = (merged[-1][0], interval[1])\n",
" return merged\n",
"\n",
- "def add_light_time_correction(cube_info, padding=5):\n",
+ "def add_light_time_correction(cube_info, padding=120):\n",
" \"\"\"\n",
" Compute the time intervals for the image and any light time correction\n",
" \n",
@@ -65,18 +64,18 @@
" A sorted list of the intervals as (start_et, stop_et)\n",
" \"\"\"\n",
" image_start_et = spice.scs2e(cube_info['SpacecraftID'], cube_info['SpacecraftClockCount'])\n",
+ " \n",
" image_end_et = image_start_et + cube_info['ExposureDuration'] * cube_info['Lines']\n",
- " \n",
- " inst_state, inst_lt = spice.spkez(cube_info['SpacecraftID'], image_start_et, 'J2000', 'LT+S', 0)\n",
- " target_state, target_lt = spice.spkez(cube_info['TargetID'], image_start_et, 'J2000', 'LT+S', 0)\n",
- " sun_state, sun_lt = spice.spkez(10, image_start_et, 'J2000', 'LT+S', cube_info['TargetID'])\n",
+ "\n",
+ " inst_state, inst_lt = spice.spkez(cube_info['SpacecraftID'], image_start_et, 'J2000', 'NONE', 0)\n",
+ " target_state, target_lt = spice.spkez(cube_info['TargetID'], image_start_et, 'J2000', 'NONE', 0)\n",
+ " sun_state, sun_lt = spice.spkez(10, image_start_et, 'J2000', 'NONE', cube_info['TargetID'])\n",
" \n",
" intervals = [\n",
" (image_start_et - padding, image_end_et + padding),\n",
" (image_start_et - padding - inst_lt, image_end_et + padding - inst_lt),\n",
" (image_start_et - padding - target_lt, image_end_et + padding - target_lt),\n",
" (image_start_et - padding - sun_lt, image_end_et + padding - sun_lt)]\n",
- "\n",
" return merge_intervals(intervals)"
]
},
@@ -107,9 +106,8 @@
" \n",
"# Save other necesary info in cube_info dict\n",
"cube_info.update(Lines = cube_pvl['IsisCube']['Core']['Dimensions']['Lines'])\n",
- "cube_info.update(Lines = 400)\n",
- "cube_info.update(SpacecraftClockCount = cube_pvl['IsisCube']['Instrument']['SpacecraftClockCount'])\n",
- "cube_info.update(ExposureDuration = cube_pvl['IsisCube']['Instrument']['LineExposureDuration'].value * 0.001)\n",
+ "cube_info.update(SpacecraftClockCount = cube_pvl['IsisCube']['Instrument']['SpacecraftClockStartCount'])\n",
+ "cube_info.update(ExposureDuration = cube_pvl['IsisCube']['Instrument']['ExposureDuration'])\n",
"cube_info.update(TargetID = spice.bods2c(cube_pvl['IsisCube']['Instrument']['TargetName']))\n",
"cube_info.update(SpacecraftID = spice.bods2c(cube_pvl['IsisCube']['Instrument']['SpacecraftName']))\n",
"\n",
@@ -127,9 +125,8 @@
" output_comments = output_basename + '.cmt'\n",
" start_sclk = spice.sce2s(cube_info['SpacecraftID'], interval[0])\n",
" end_sclk = spice.sce2s(cube_info['SpacecraftID'], interval[1])\n",
- "\n",
" # Create new sliced ck kernel\n",
- " ckslicer_command = [ckslicer_loc, \n",
+ " ckslicer_command = [\"ckslicer\", \n",
" '-LSK {}'.format(cube_info['LeapSecond'][0]), \n",
" '-SCLK {}'.format(cube_info['SpacecraftClock'][0]), \n",
" '-INPUTCK {}'.format(ck), \n",
@@ -190,7 +187,7 @@
],
"metadata": {
"kernelspec": {
- "display_name": "Python 3",
+ "display_name": "Python 3 (ipykernel)",
"language": "python",
"name": "python3"
},
@@ -204,7 +201,7 @@
"name": "python",
"nbconvert_exporter": "python",
"pygments_lexer": "ipython3",
- "version": "3.7.1"
+ "version": "3.10.2"
}
},
"nbformat": 4,
diff --git a/notebooks/write_NHLeisaIsisLabelNaifSpiceDriver.ipynb b/notebooks/write_NHLeisaIsisLabelNaifSpiceDriver.ipynb
new file mode 100644
index 0000000000000000000000000000000000000000..1ccc7dd83519ac6c866b27d07001f5660e7120e3
--- /dev/null
+++ b/notebooks/write_NHLeisaIsisLabelNaifSpiceDriver.ipynb
@@ -0,0 +1,97 @@
+{
+ "cells": [
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": [
+ "fileName = 'ale/leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced.cub'\n",
+ "\n",
+ "import os\n",
+ "os.environ[\"ISISDATA\"] = \"isis3/isis_data\"\n",
+ "os.environ[\"ISISTESTDATA\"] = \"isis_testData\"\n",
+ "os.environ[\"ISISROOT\"] = \"isis/ISIS3/build\"\n",
+ "\n",
+ "import ale \n",
+ "from ale.drivers.nh_drivers import NewHorizonsLeisaIsisLabelNaifSpiceDriver\n",
+ "from ale.formatters.formatter import to_isd\n",
+ "import spiceypy as spice\n",
+ "from ale.drivers import AleJsonEncoder"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": [
+ "from ale.util import generate_kernels_from_cube\n",
+ "kernels = generate_kernels_from_cube(fileName, expand=True, format_as='list')"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {
+ "scrolled": false
+ },
+ "outputs": [],
+ "source": [
+ "with NewHorizonsLeisaIsisLabelNaifSpiceDriver(fileName, props = {\"kernels\": kernels}) as driver:\n",
+ " isisString = to_isd(driver)"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": [
+ "isisString"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": [
+ "import json\n",
+ "\n",
+ "isis_dict = isisString\n",
+ "\n",
+ "json_file = os.path.splitext(fileName)[0] + '.json'\n",
+ "\n",
+ "with open(json_file, 'w') as fp:\n",
+ " json.dump(isis_dict, fp, cls = AleJsonEncoder)\n",
+ " \n",
+ "with open(json_file, 'r') as fp:\n",
+ " isis_dict = json.load(fp)\n",
+ " \n",
+ "isis_dict.keys()"
+ ]
+ }
+ ],
+ "metadata": {
+ "kernelspec": {
+ "display_name": "Python 3 (ipykernel)",
+ "language": "python",
+ "name": "python3"
+ },
+ "language_info": {
+ "codemirror_mode": {
+ "name": "ipython",
+ "version": 3
+ },
+ "file_extension": ".py",
+ "mimetype": "text/x-python",
+ "name": "python",
+ "nbconvert_exporter": "python",
+ "pygments_lexer": "ipython3",
+ "version": "3.10.2"
+ }
+ },
+ "nbformat": 4,
+ "nbformat_minor": 2
+}
diff --git a/tests/pytests/data/isds/nhleisa_isd.json b/tests/pytests/data/isds/nhleisa_isd.json
new file mode 100644
index 0000000000000000000000000000000000000000..2644264aa125ce595732aa3f938578952241dd97
--- /dev/null
+++ b/tests/pytests/data/isds/nhleisa_isd.json
@@ -0,0 +1 @@
+{"isis_camera_version": 1, "image_lines": 368, "image_samples": 256, "name_platform": "NEW HORIZONS", "name_sensor": "NH_RALPH_LEISA", "reference_height": {"maxheight": 1000, "minheight": -1000, "unit": "m"}, "name_model": "USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL", "interpolation_method": "lagrange", "line_scan_rate": [[0.5, -157.50400000810623, 0.856]], "starting_ephemeris_time": 487928588.0336103, "center_ephemeris_time": 487928745.5376103, "radii": {"semimajor": 1188.3, "semiminor": 1188.3, "unit": "km"}, "body_rotation": {"time_dependent_frames": [10019, 1], "ck_table_start_time": 487928588.0336103, "ck_table_end_time": 487928903.0416103, "ck_table_original_size": 5, "ephemeris_times": [487928588.0336103, 487928666.7856103, 487928745.5376103, 487928824.28961027, 487928903.0416103], "quaternions": [[-0.2447405651322848, 0.2727488147412229, -0.6923053902236965, -0.6216296216423436], [-0.24501922793442102, 0.27243841475512237, -0.6924275986998515, -0.6215198377098623], [-0.2452978414907075, 0.27212796001179584, -0.6925496680060897, -0.6214099288589402], [-0.24557640574494083, 0.2718174505738702, -0.6926715981177864, -0.6212998951117484], [-0.24585492064113273, 0.27150688650375393, -0.6927933890104353, -0.6211897364904025]], "angular_velocities": [[-7.719038104508623e-06, 8.279682752122315e-06, -1.2223224358447397e-06], [-7.719038104508623e-06, 8.279682752122315e-06, -1.22232243584474e-06], [-7.719038104508622e-06, 8.279682752122315e-06, -1.222322435844739e-06], [-7.719038104508623e-06, 8.279682752122315e-06, -1.2223224358447393e-06], [-7.719038104508623e-06, 8.279682752122316e-06, -1.2223224358447386e-06]], "reference_frame": 1}, "instrument_pointing": {"time_dependent_frames": [-98000, 1], "ck_table_start_time": 487928588.0336103, "ck_table_end_time": 487928903.0416103, "ck_table_original_size": 5, "ephemeris_times": [487928588.0336103, 487928666.7856103, 487928745.5376103, 487928824.28961027, 487928903.0416103], "quaternions": [[-0.6894448798229785, -0.13288333554010637, -0.30018901711893975, 0.645673548182655], [-0.687721087896909, -0.13374109956420746, -0.29978054587038167, 0.6475219284834335], [-0.6859672573646195, -0.13441668765411288, -0.2995880589786557, 0.6493289388446816], [-0.6843925306207158, -0.13520640845056833, -0.2991531939769342, 0.6510249286147723], [-0.68280490039217, -0.13588350538291064, -0.2989481901333484, 0.6526431801384941]], "angular_velocities": [[-6.0016600701510346e-05, -3.4315085391481984e-05, 3.616461098110838e-05], [-2.9998984431665234e-05, -2.9941950083650682e-05, 5.4011064302860286e-05], [-5.7451833433989726e-05, -2.640886089874711e-05, 3.345134823897179e-05], [-2.2375968791183237e-05, -2.5852223731490175e-05, 5.491960013111816e-05], [-1.3816947750491701e-05, -3.320701389161546e-05, 5.328198819154163e-05]], "reference_frame": 1, "constant_frames": [-98901, -98201, -98000], "constant_rotation": [-0.001805871124864633, 0.0037494052664166673, 0.9999913403573196, 0.018161770046999218, 0.9998281559785996, -0.0037159953166251633, -0.999833430596437, 0.01815490216391774, -0.001873656632970122]}, "naif_keywords": {"BODY999_RADII": [1188.3, 1188.3, 1188.3], "BODY_FRAME_CODE": 10019, "BODY_CODE": 999, "FRAME_-98901_CLASS": 4.0, "INS-98901_TRANSX": [0.0, 0.04, 0.0], "INS-98901_TRANSY": [0.04, 0.0, 0.04], "TKFRAME_-98901_UNITS": "DEGREES", "INS-98901_PIXEL_PITCH": 0.04, "INS-98901_FOCAL_LENGTH": 644.486, "FRAME_-98901_NAME": "ISIS_NH_RALPH_LEISA", "INS-98901_ITRANSL": [-1.0, 0.0, 25.0], "FRAME_-98901_CLASS_ID": -98901.0, "INS-98901_ITRANSS": [0.0, 25.0, 0.0], "TKFRAME_-98901_ANGLES": [0.0, 90.0, 0.0], "TKFRAME_-98901_AXES": [1.0, 2.0, 3.0], "TKFRAME_-98901_SPEC": "ANGLES", "FRAME_-98901_CENTER": -98.0, "TKFRAME_-98901_RELATIVE": "NH_RALPH_LEISA", "BODY999_PM": [302.695, 56.3625225, 0.0], "BODY999_POLE_RA": [132.993, 0.0, 0.0], "BODY999_POLE_DEC": [-6.163, 0.0, 0.0], "BODY999_LONG_AXIS": 0.0}, "detector_sample_summing": 1, "detector_line_summing": 1, "focal_length_model": {"focal_length": 644.486}, "detector_center": {"line": 0, "sample": 0}, "starting_detector_line": 0, "starting_detector_sample": 0, "focal2pixel_lines": [-1.0, 0.0, 25.0], "focal2pixel_samples": [0.0, 25.0, 0.0], "optical_distortion": {"radial": {"coefficients": [0.0, 0.0, 0.0]}}, "instrument_position": {"spk_table_start_time": 487928588.0336103, "spk_table_end_time": 487928903.0416103, "spk_table_original_size": 5, "ephemeris_times": [487928588.0336103, 487928666.7856103, 487928745.5376103, 487928824.28961027, 487928903.0416103], "positions": [[-341893.24779512954, 29580910.11543975, 7720840.361930893], [-341880.7808565185, 29579860.06353102, 7720567.900988498], [-341868.3126599601, 29578810.0127891, 7720295.440004236], [-341855.84320573055, 29577759.963213038, 7720022.97897548], [-341843.3724940212, 29576709.914803796, 7719750.517901289]], "velocities": [[0.15829834503568418, -13.333661290526594, -3.4597333648983915], [0.15831431122399225, -13.333646475303395, -3.4597338961260395], [0.15833027850391226, -13.333631661980828, -3.459734446767892], [0.1583462468689395, -13.333616850568019, -3.4597350168341365], [0.15836221629776992, -13.333602041080965, -3.4597356063085027]], "reference_frame": 1}, "sun_position": {"spk_table_start_time": 487928745.5376103, "spk_table_end_time": 487928745.5376103, "spk_table_original_size": 1, "ephemeris_times": [487928745.5376103], "positions": [[-1185193768.8247254, 4445753700.58781, 1744608601.9356186]], "velocities": [[-5.384652174342424, -0.7983186588678509, 1.3987335963733494]], "reference_frame": 1}}
\ No newline at end of file
diff --git a/tests/pytests/data/isds/newhorizons_isd.json b/tests/pytests/data/isds/nhlorri_isd.json
similarity index 100%
rename from tests/pytests/data/isds/newhorizons_isd.json
rename to tests/pytests/data/isds/nhlorri_isd.json
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/leisaAddendum002.ti b/tests/pytests/data/lsb_0296962438_0x53c_eng/leisaAddendum002.ti
new file mode 100644
index 0000000000000000000000000000000000000000..e9f519cec11183bc729e6e1f3eddfda52c1bd10c
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/leisaAddendum002.ti
@@ -0,0 +1,65 @@
+\begintext
+Leisa's pixel pitch is currently set to the size of the pixels (assuming that it is measured in mm,) so assuming no space in-between.
+
+Leisa's focal length is the same as MVIC's because the light is
+focused onto a shared focal plane. This is also in mm. But there is
+some anamorphism, so we are choosing the value that works best for the
+scan direction. It doesn't work as well for the orthogonal axis, but
+distortions along that axis are much easier to correct later.
+
+INS-98901_FOCAL_LENGTH=644.486
+INS-98201_TRANSX = (0.0,0.040,0.0)
+INS-98201_TRANSY = ( 0.0, 0.0, 0.040 )
+INS-98201_ITRANSS = ( 0.0, 25.0, 0.0 )
+INS-98201_ITRANSL = ( 0.0, 0.0, 25.0)
+INS-98201_PIXEL_PITCH=0.040
+
+\begintext
+ISIS requires the +Z or -Z axis to be along the boresight of
+the telescope. So we rotate the -98201 axes by 90deg about +Y
+
+Create a new naif id for the new rotated frame in ISIS:
+(Naif Frame ID = -98201 -> Isis Frame ID = -98901)
+
+\begindata
+ FRAME_ISIS_NH_RALPH_LEISA = -98901
+ FRAME_-98901_NAME = 'ISIS_NH_RALPH_LEISA'
+ FRAME_-98901_CLASS = 4
+ FRAME_-98901_CLASS_ID = -98901
+ FRAME_-98901_CENTER = -98
+ TKFRAME_-98901_RELATIVE = 'NH_RALPH_LEISA'
+ TKFRAME_-98901_SPEC = 'ANGLES'
+ TKFRAME_-98901_ANGLES = ( 0.0 90.0 0.0 )
+ TKFRAME_-98901_AXES = ( 1, 2, 3 )
+ TKFRAME_-98901_UNITS = 'DEGREES'
+
+ INS-98901_PIXEL_PITCH=0.040
+ INS-98901_FOCAL_LENGTH=644.486
+
+\begintext
+ The following affine coefficients are useful for band 1 of the ISIS cube. Without
+ a constant term in the Y and Line there is no offset in the line direction to
+ correctly transform band 2-256. All lines in band 1 come from line 1 of the
+ 256x256 array, all lines of band 2 come from line 2 and so on.
+ INS-98901_TRANSX = ( 0.0,0.040,0.0 )
+ INS-98901_TRANSY = ( 0.0, 0.0, 0.040 )
+
+ INS-98901_ITRANSS = ( 0.0, 25.0, 0.0 )
+ INS-98901_ITRANSL = ( 0.0, 0.0, 25.0 )
+
+
+\begintext
+The following affine coefficents are not to be used as is. They are used as the
+starting/base values. The constant term is multiplied by the band_number-1 to get the
+correct Y and Line constant terms. The other coefficients are used as is for all bands.
+\begindata
+ INS-98901_TRANSX = ( 0.0, 0.040, 0.0 )
+ INS-98901_TRANSY = ( 0.04, 0.0, 0.040 )
+
+ INS-98901_ITRANSS = ( 0.0, 25.0, 0.0 )
+ INS-98901_ITRANSL = ( -1.0, 0.0, 25.0 )
+
+
+
+
+
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_0.xsp b/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..55714947098a16c12081a541d37afe3cb3b1fff6
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_0.xsp
@@ -0,0 +1,278 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 78
+'PLUXXX '
+'1D14F27612CEC4^8'
+'1D14F5039B4171^8'
+'3E7'
+'9'
+'1'
+'3'
+78
+'1D12CC4^8'
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+'42F3C0FA12A944^3'
+'1BDAC4B5462D41^3'
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+'98FE41E4214228^1'
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+'38C432C86EDE08^0'
+'2634EA39F2B5C6^-1'
+'-131F42B491D0CA^-1'
+'1C67D5060E6D04^2'
+'413A373E24A6CC^3'
+'718B6A66CABDE4^2'
+'-36DECE593AD076^3'
+'-1D588101F97149^2'
+'755F5CE39BDBC8^2'
+'269D9E2CEA1A3A^1'
+'-6B4C14B59E36B8^1'
+'-188760B9185E34^0'
+'372A0B69692586^0'
+'79E8C0294A62^-2'
+'-126D74121DFA78^-1'
+'-1FA25019224FB9^3'
+'127595BBEE4AA^3'
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+'20AEF968581FF4^3'
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+'-2B792C295BB7B8^2'
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+'EB79092CADE36^-1'
+'-BB39D76A1AE19^-1'
+'-3EC4A0CF21DAE^-2'
+'-1101565EC0CCE6^-1'
+'F4DC1CC21737E8^-2'
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+'-CDE00B861B2D1^-2'
+'11940FF3697026^-1'
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+'FBB3CA7E0B277^-4'
+'C13408BAD6B628^-5'
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+'0^0'
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+'0^0'
+'1D0ED7C^8'
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+'4A^2'
+'1^1'
+END_ARRAY 1 78
+BEGIN_ARRAY 2 24
+'DE-0433LE-0433 '
+'1D14F27612CEC4^8'
+'1D14F5039B4171^8'
+'9'
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+END_ARRAY 2 24
+BEGIN_ARRAY 3 39
+'DE-0433LE-0433 '
+'1D14F27612CEC4^8'
+'1D14F5039B4171^8'
+'A'
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+'1'
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+'1D0AE34^8'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+BEGIN_ARRAY 4 73
+'pvshort.nio '
+'1D14F27612CEC4^8'
+'1D14F5039B4171^8'
+'-62'
+'9'
+'1'
+'1'
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+'1D154FC17F697A^8'
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+'81F9D4A4B3EAA8^4'
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+'F3E2^-11'
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+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'50BF99DF629A0C^-8'
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+'-18BBC15B5536E3^-C'
+'-C42ABE51ACA8C8^-E'
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+'-2099CC^-10'
+'0^0'
+'0^0'
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+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'179C2867A7C457^-8'
+'-4DBF8F4D526A38^-A'
+'-55947A28B0B3A^-D'
+'-331FF6B5684184^-E'
+'-13E595CFBDDD9B^-F'
+'-93915^-11'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
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+'0^0'
+'0^0'
+'0^0'
+'6^1'
+'5^1'
+'5^1'
+'5^1'
+'1D151AE^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /ale/leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_0.bsp LOG FILE
+
+; Created 2022-06-10/14:57:03.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Volumes/pkgs/isis3/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /ale/leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_0.bsp
+SOURCE_SPK_KERNEL = isis3/isis_data/newhorizons/kernels/spk/nh_recon_pluto_od122_v01.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 999, 9, 10, -98
+ BEGIN_TIME = 2015 JUN 18 15:06:26.889
+ END_TIME = 2015 JUN 18 15:17:20.422
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_1.xsp b/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..fd278adc3e819a340258925f91f1be9d02aba0b9
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_1.xsp
@@ -0,0 +1,278 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 78
+'PLUXXX '
+'1D1532940890FD^8'
+'1D1534BF0A9D44^8'
+'3E7'
+'9'
+'1'
+'3'
+78
+'1D12CC4^8'
+'3F48^5'
+'6FA86E00B05604^2'
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+'38C432C86EDE08^0'
+'2634EA39F2B5C6^-1'
+'-131F42B491D0CA^-1'
+'1C67D5060E6D04^2'
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+'718B6A66CABDE4^2'
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+'755F5CE39BDBC8^2'
+'269D9E2CEA1A3A^1'
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+'79E8C0294A62^-2'
+'-126D74121DFA78^-1'
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+END_ARRAY 1 78
+BEGIN_ARRAY 2 24
+'DE-0433LE-0433 '
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+END_ARRAY 2 24
+BEGIN_ARRAY 3 39
+'DE-0433LE-0433 '
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+'1D0AE34^8'
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+'1^1'
+END_ARRAY 3 39
+BEGIN_ARRAY 4 73
+'pvshort.nio '
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+'1D1534BF0A9D44^8'
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+73
+'1D154C57AAC4C6^8'
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+'4^1'
+'5^1'
+'4^1'
+'1D154C57AAC4C6^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /ale/leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_1.bsp LOG FILE
+
+; Created 2022-06-10/14:57:07.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced_1.bsp
+SOURCE_SPK_KERNEL = /newhorizons/kernels/spk/nh_recon_pluto_od122_v01.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 999, 9, 10, -98
+ BEGIN_TIME = 2015 JUN 18 19:40:00.849
+ END_TIME = 2015 JUN 18 19:49:15.857
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng_isis.lbl b/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng_isis.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..a45ffcd14afcad6af25f304dfb4238c3046072b5
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng_isis.lbl
@@ -0,0 +1,163 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 256
+ TileLines = 368
+
+ Group = Dimensions
+ Samples = 256
+ Lines = 368
+ Bands = 256
+ End_Group
+
+ Group = Pixels
+ Type = SignedWord
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = "NEW HORIZONS"
+ InstrumentId = LEISA
+ TargetName = Pluto
+ SpacecraftClockStartCount = 0296962438:00000
+ ExposureDuration = 0.856
+ StartTime = 2015-06-18T19:42:00.8491479
+ StopTime = 2015-06-18T19:47:02.849148
+ FrameRate = 1.16822 <Hz>
+ End_Group
+
+ Group = Archive
+ MidObservationTime = 487928739.0336103 <s past J2000>
+ ObservationDuration = 302.0
+ Detector = LEISA
+ ScanType = LEISA
+ End_Group
+
+ Group = BandBin
+ Center = (2.4892, 2.4808, 2.4723, 2.4639, 2.4555, 2.4471, 2.4386,
+ 2.4302, 2.4218, 2.4134, 2.4050, 2.3966, 2.3883, 2.3799,
+ 2.3715, 2.3632, 2.3548, 2.3465, 2.3382, 2.3299, 2.3216,
+ 2.3134, 2.3051, 2.2969, 2.2886, 2.2804, 2.2722, 2.2641,
+ 2.2559, 2.2478, 2.2397, 2.2316, 2.2235, 2.2155, 2.2074,
+ 2.1994, 2.1915, 2.1835, 2.1756, 2.1676, 2.1598, 2.1519,
+ 2.1441, 2.1362, 2.1285, 2.1207, 2.1130, 2.1053, 2.0976,
+ 2.0899, 2.0823, 2.0747, 2.0671, 2.0596, 2.0520, 2.0446,
+ 2.0371, 2.0297, 2.0223, 2.0149, 2.0075, 2.0002, 1.9929,
+ 1.9857, 1.9784, 1.9712, 1.9641, 1.9569, 1.9498, 1.9427,
+ 1.9357, 1.9287, 1.9217, 1.9147, 1.9078, 1.9009, 1.8940,
+ 1.8871, 1.8803, 1.8735, 1.8668, 1.8600, 1.8533, 1.8466,
+ 1.8400, 1.8334, 1.8268, 1.8202, 1.8137, 1.8072, 1.8007,
+ 1.7942, 1.7878, 1.7814, 1.7750, 1.7687, 1.7623, 1.7560,
+ 1.7498, 1.7435, 1.7373, 1.7311, 1.7249, 1.7188, 1.7126,
+ 1.7065, 1.7004, 1.6944, 1.6884, 1.6823, 1.6763, 1.6704,
+ 1.6644, 1.6585, 1.6526, 1.6467, 1.6409, 1.6350, 1.6292,
+ 1.6234, 1.6176, 1.6119, 1.6061, 1.6004, 1.5947, 1.5890,
+ 1.5833, 1.5777, 1.5720, 1.5664, 1.5608, 1.5552, 1.5497,
+ 1.5441, 1.5386, 1.5331, 1.5276, 1.5221, 1.5166, 1.5112,
+ 1.5057, 1.5003, 1.4949, 1.4895, 1.4841, 1.4788, 1.4734,
+ 1.4681, 1.4628, 1.4575, 1.4522, 1.4469, 1.4417, 1.4365,
+ 1.4312, 1.4260, 1.4208, 1.4157, 1.4105, 1.4054, 1.4003,
+ 1.3952, 1.3901, 1.3850, 1.3800, 1.3749, 1.3699, 1.3649,
+ 1.3600, 1.3550, 1.3501, 1.3452, 1.3403, 1.3355, 1.3306,
+ 1.3258, 1.3210, 1.3163, 1.3116, 1.3069, 1.3022, 1.2975,
+ 1.2929, 1.2883, 1.2838, 1.2793, 1.2748, 1.2704, 1.2660,
+ 1.2616, 1.2573, 1.2530, 1.2487, 1.2446, 1.2404, 1.2363,
+ 1.2322, 1.2282, 1.2243, 1.2204, 2.2623, 2.2589, 2.2555,
+ 2.2521, 2.2488, 2.2454, 2.2421, 2.2387, 2.2354, 2.2321,
+ 2.2288, 2.2255, 2.2222, 2.2189, 2.2156, 2.2124, 2.2091,
+ 2.2059, 2.2026, 2.1994, 2.1962, 2.1930, 2.1898, 2.1866,
+ 2.1834, 2.1803, 2.1771, 2.1740, 2.1708, 2.1677, 2.1646,
+ 2.1615, 2.1584, 2.1553, 2.1522, 2.1491, 2.1461, 2.1430,
+ 2.1400, 2.1370, 2.1339, 2.1309, 2.1279, 2.1249, 2.1220,
+ 2.1190, 2.1160, 2.1131, 2.1101, 2.1072, 2.1043, 2.1014,
+ 2.0985, 2.0956, 2.0927, 2.0898)
+ Width = (0.011228, 0.011190, 0.011152, 0.011114, 0.011076,
+ 0.011038, 0.011000, 0.010962, 0.010924, 0.010886, 0.010848,
+ 0.010810, 0.010772, 0.010735, 0.010697, 0.010659, 0.010622,
+ 0.010584, 0.010547, 0.010509, 0.010472, 0.010435, 0.010397,
+ 0.010360, 0.010323, 0.010286, 0.010249, 0.010212, 0.010176,
+ 0.010139, 0.010102, 0.010066, 0.010029, 0.009993, 0.009957,
+ 0.009921, 0.009885, 0.009849, 0.009813, 0.009777, 0.009742,
+ 0.009706, 0.009671, 0.009636, 0.009601, 0.009566, 0.009531,
+ 0.009496, 0.009461, 0.009427, 0.009392, 0.009358, 0.009324,
+ 0.009290, 0.009256, 0.009222, 0.009189, 0.009155, 0.009122,
+ 0.009088, 0.009055, 0.009022, 0.008989, 0.008957, 0.008924,
+ 0.008891, 0.008859, 0.008827, 0.008795, 0.008763, 0.008731,
+ 0.008699, 0.008668, 0.008636, 0.008605, 0.008574, 0.008543,
+ 0.008512, 0.008481, 0.008451, 0.008420, 0.008390, 0.008360,
+ 0.008329, 0.008299, 0.008270, 0.008240, 0.008210, 0.008181,
+ 0.008151, 0.008122, 0.008093, 0.008064, 0.008035, 0.008006,
+ 0.007978, 0.007949, 0.007921, 0.007892, 0.007864, 0.007836,
+ 0.007808, 0.007780, 0.007753, 0.007725, 0.007697, 0.007670,
+ 0.007643, 0.007615, 0.007588, 0.007561, 0.007534, 0.007508,
+ 0.007481, 0.007454, 0.007428, 0.007401, 0.007375, 0.007349,
+ 0.007322, 0.007296, 0.007270, 0.007245, 0.007219, 0.007193,
+ 0.007167, 0.007142, 0.007116, 0.007091, 0.007065, 0.007040,
+ 0.007015, 0.006990, 0.006965, 0.006940, 0.006915, 0.006890,
+ 0.006865, 0.006841, 0.006816, 0.006792, 0.006767, 0.006743,
+ 0.006719, 0.006694, 0.006670, 0.006646, 0.006622, 0.006598,
+ 0.006574, 0.006550, 0.006527, 0.006503, 0.006479, 0.006456,
+ 0.006432, 0.006409, 0.006386, 0.006362, 0.006339, 0.006316,
+ 0.006293, 0.006270, 0.006247, 0.006224, 0.006202, 0.006179,
+ 0.006157, 0.006134, 0.006112, 0.006090, 0.006068, 0.006046,
+ 0.006024, 0.006002, 0.005980, 0.005959, 0.005937, 0.005916,
+ 0.005895, 0.005874, 0.005853, 0.005832, 0.005811, 0.005791,
+ 0.005770, 0.005750, 0.005730, 0.005710, 0.005691, 0.005671,
+ 0.005652, 0.005633, 0.005614, 0.005595, 0.005576, 0.005558,
+ 0.005540, 0.005522, 0.005505, 0.005321, 0.005313, 0.005305,
+ 0.005297, 0.005289, 0.005281, 0.005273, 0.005265, 0.005257,
+ 0.005249, 0.005242, 0.005234, 0.005226, 0.005218, 0.005211,
+ 0.005203, 0.005195, 0.005188, 0.005180, 0.005173, 0.005165,
+ 0.005158, 0.005150, 0.005143, 0.005135, 0.005128, 0.005120,
+ 0.005113, 0.005105, 0.005098, 0.005091, 0.005083, 0.005076,
+ 0.005069, 0.005062, 0.005054, 0.005047, 0.005040, 0.005033,
+ 0.005026, 0.005019, 0.005012, 0.005005, 0.004998, 0.004990,
+ 0.004984, 0.004977, 0.004970, 0.004963, 0.004956, 0.004949,
+ 0.004942, 0.004935, 0.004928, 0.004922, 0.004915)
+ OriginalBand = (1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17,
+ 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32,
+ 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47,
+ 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62,
+ 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77,
+ 78, 79, 80, 81, 82, 83, 84, 85, 86, 87, 88, 89, 90, 91, 92,
+ 93, 94, 95, 96, 97, 98, 99, 100, 101, 102, 103, 104, 105,
+ 106, 107, 108, 109, 110, 111, 112, 113, 114, 115, 116, 117,
+ 118, 119, 120, 121, 122, 123, 124, 125, 126, 127, 128, 129,
+ 130, 131, 132, 133, 134, 135, 136, 137, 138, 139, 140, 141,
+ 142, 143, 144, 145, 146, 147, 148, 149, 150, 151, 152, 153,
+ 154, 155, 156, 157, 158, 159, 160, 161, 162, 163, 164, 165,
+ 166, 167, 168, 169, 170, 171, 172, 173, 174, 175, 176, 177,
+ 178, 179, 180, 181, 182, 183, 184, 185, 186, 187, 188, 189,
+ 190, 191, 192, 193, 194, 195, 196, 197, 198, 199, 200, 201,
+ 202, 203, 204, 205, 206, 207, 208, 209, 210, 211, 212, 213,
+ 214, 215, 216, 217, 218, 219, 220, 221, 222, 223, 224, 225,
+ 226, 227, 228, 229, 230, 231, 232, 233, 234, 235, 236, 237,
+ 238, 239, 240, 241, 242, 243, 244, 245, 246, 247, 248, 249,
+ 250, 251, 252, 253, 254, 255, 256)
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -98901 <SPICE ID>
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 48300033
+ Bytes = 639
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 48300672
+ Bytes = 15636
+End_Object
+End
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/merged_nhpc_2015_v001_0_sliced_-98000.xc b/tests/pytests/data/lsb_0296962438_0x53c_eng/merged_nhpc_2015_v001_0_sliced_-98000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..d4a1a23e82f95b6caf99f27db5b2cb8f391c8848
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/merged_nhpc_2015_v001_0_sliced_-98000.xc
@@ -0,0 +1,272 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' < DAFCAT: CK CONCATENATION > '
+BEGIN_ARRAY 1 251
+'nhpc '
+'D80E7C1A2B9^B'
+'D80E9B43DEE^B'
+'-17ED0'
+'1'
+'3'
+'1'
+251
+'3536D4A2608602^0'
+'-29AB656AED380E^0'
+'F3E3BD6BF39D1^0'
+'268BAA59B2B614^0'
+'-5F75E3AA506038^-3'
+'-123AF9CE3662F8^-3'
+'-3A542857CF0DFA^-3'
+'-352F3827D9383^0'
+'29A28A3EF253FC^0'
+'-F3E7BA86658408^0'
+'-26868016D0B576^0'
+'-82C0538D1CC428^-3'
+'-18A49BABD84A6^-3'
+'-46FCECC45E0BAC^-3'
+'-35108FF659909C^0'
+'2990FD1F8BC5A^0'
+'-F3F592671A61B8^0'
+'-266C0A2F053C62^0'
+'D3C20457EAF4C^-4'
+'-15DF9019083673^-3'
+'E69034D58495E^-4'
+'-34FE0B623E43C2^0'
+'2981AB8FDF16F4^0'
+'-F3FFBC11880928^0'
+'-2655994B7F4184^0'
+'-9E9ACECFB61CB8^-4'
+'-185F0F37D58582^-3'
+'-2A7C58A7C158C4^-4'
+'-34F1E8BF568724^0'
+'297C710955AB02^0'
+'-F40449E34D1A8^0'
+'-264F0989F5B2C6^0'
+'6355B3E7304C6^-3'
+'-1026FC2FD48CDC^-3'
+'196CDABF760789^-3'
+'-34D3FB58CD7944^0'
+'2963E3DA9B6F9A^0'
+'-F414BEC1E038C^0'
+'-262A00A6812DFA^0'
+'-25250160846212^-3'
+'-1E2AB179B0606D^-3'
+'-12B2B01F5E8502^-3'
+'-34D2DB468F8348^0'
+'294FF146BECB64^0'
+'-F41FA4D7F4E53^0'
+'-25FB5A2B0DD0BE^0'
+'-22B5863FD33DB6^-3'
+'153C7130168C4^-3'
+'-3445B9072B644^-4'
+'-34DDD9F4691B6^0'
+'2949818E36378E^0'
+'-F42231CB92F608^0'
+'-25E2A0C9E35364^0'
+'-DA4BBF082686E^-4'
+'A4B6CACF239E2^-4'
+'B37F3F06231BF8^-4'
+'-34E6867A7F6B2C^0'
+'2944DB688303C8^0'
+'-F424024BCB9688^0'
+'-25CFDFFA951CB4^0'
+'-3BE8FAD1558B3A^-3'
+'FB00BCC150927^-4'
+'-3635EDF6D35012^-4'
+'-34EF7E2F8066CE^0'
+'29431205306FE8^0'
+'-F424C561E4DEF^0'
+'-25C0577B778E4A^0'
+'-318A696375E852^-4'
+'15989031B79A95^-3'
+'250B64796131AC^-3'
+'-34F12EE270C1EC^0'
+'29415139DB33FA^0'
+'-F4257BB4AB5FE8^0'
+'-25BB47BCAE21E2^0'
+'-B800E9966100A8^-4'
+'-3AA569D1A44A02^-4'
+'D0C5D56F395C8^-4'
+'-34FFE2AEEB1686^0'
+'293692A69CCA9A^0'
+'-F4271D30034A8^0'
+'-25A7CF46D53FC6^0'
+'-42B2187FA6815C^-3'
+'14C3F09CE693C8^-3'
+'-1D47BCBBFBED1D^-3'
+'-35115DADD01B58^0'
+'292BA954EE1F6E^0'
+'-F4214F0D21351^0'
+'-25C0BB931E0A92^0'
+'AE0C7AAE68AFC^-3'
+'2B54C0591BB212^-3'
+'E310658FE3F1A^-4'
+'-3518972D6EC968^0'
+'2926D7CE6853F4^0'
+'-F41F6F18BFED7^0'
+'-25C7F2E7101B18^0'
+'452C4B26C02C58^-3'
+'26FEA9301FC82E^-3'
+'3A0B508047DDCE^-5'
+'-352693A9BA53F2^0'
+'2916BD73EA7548^0'
+'-F41CEED0BE3CB^0'
+'-25D5F5A4AD2A0C^0'
+'-207C0507EA219E^-3'
+'11AEB79DE4565D^-3'
+'-300E20BE034DAE^-3'
+'-35357CB7A38716^0'
+'2912F79C7F94F8^0'
+'-F415C976B7B28^0'
+'-25F3282CBB6FEE^0'
+'6391D3ED35975^-4'
+'1C6790B9244604^-3'
+'-234EE2C49EE4C^-3'
+'-35446F6F5C55D8^0'
+'291BB9EFA694EE^0'
+'-F40C08EF2C9AE^0'
+'-26135E1EB7EE58^0'
+'7ECC1BD1735C9C^-4'
+'1006333AD8A63E^-3'
+'98CB00F0790FF^-4'
+'-3544DA2D3D5D1E^0'
+'291E152A69388^0'
+'-F40A79BEF6E0F^0'
+'-261A3B65B93326^0'
+'7BC8677F4D786C^-3'
+'203D8D6745B1A8^-3'
+'176ADC19576831^-3'
+'-355096FD7FAFEE^0'
+'292ABF1D791808^0'
+'-F400A1B1ABB528^0'
+'-263B213D47DECC^0'
+'612E8549D6E7E4^-3'
+'1AD9CB47D1C2DA^-4'
+'13047AC271D146^-3'
+'-35610C2E5273FA^0'
+'293D437803A3C6^0'
+'-F3F30C8F374C4^0'
+'-2666CA30A57CA6^0'
+'A13F94A847A5E^-3'
+'30306BFB6A0252^-3'
+'310091428D03E6^-3'
+'-35688473F2D826^0'
+'293E910DDF04C^0'
+'-F3F0189769A94^0'
+'-266DC2B65147BC^0'
+'-4BA4A5CD0FA75^-3'
+'6540D9C2D5EFE^-4'
+'-1C9C97C45A7CAE^-3'
+'-356EF279F2882A^0'
+'294AB4988DE67C^0'
+'-F3E893577EF0D8^0'
+'-26877D20DE864E^0'
+'6F38ACB098D7D^-3'
+'1CC775C74323C7^-3'
+'2B065FAF07760C^-3'
+'-3577B380D86966^0'
+'295CA1F1E3E164^0'
+'-F3E44215744658^0'
+'-268371FEC06182^0'
+'-7F30B04E4686D^-3'
+'-AF806E9BCA66F8^-4'
+'-48D068AE51B5C4^-4'
+'-357C42440E8694^0'
+'297C7241FFEA5C^0'
+'-F3DFCD249D3568^0'
+'-26771D10AD410E^0'
+'4C9777D097CBBC^-3'
+'B0F2B34209DC7^-5'
+'42C66B8DAC6A6^-3'
+'-357D352D00B2DC^0'
+'297C444A476652^0'
+'-F3E00A07F4E718^0'
+'-26747ABD75C0C6^0'
+'-8E7BC4E606C4E8^-4'
+'7E7BBA07CB7098^-4'
+'280D1A9D216D34^-3'
+'-35812EE696E2C^0'
+'2999AFD1279456^0'
+'-F3DCD3D0C9AE88^0'
+'-2663851BD3CC86^0'
+'D6BB66E85B1038^-4'
+'19F67C68007ACD^-4'
+'46CB10F90DD2E^-3'
+'-358611D60E30BC^0'
+'29B1C79C2F5498^0'
+'-F3DA6BC71FFAF8^0'
+'-2651D726732B78^0'
+'2B35543C8D3462^-3'
+'6546D612E5CAA^-4'
+'2237B1FD243B22^-3'
+'-358BD05DCD8D92^0'
+'29B89FFF162C64^0'
+'-F3D918FFB7C83^0'
+'-264AC899E51016^0'
+'-411E84CC007B7^-3'
+'1939DEC1A13A^-4'
+'F81ADEE065A9C^-4'
+'-3590516D3CBAB8^0'
+'29BD143E99B3FA^0'
+'-F3D7C9FEAECCA8^0'
+'-2647F68A2FA132^0'
+'-71DF76A900B988^-3'
+'-40217175A9E204^-4'
+'-11BCADBE7DA2EB^-3'
+'-3598557EE6EF08^0'
+'29CE9056AEA60C^0'
+'-F3D1C3AA1196B8^0'
+'-2650090CF68AF^0'
+'596E58E6C07AC^-3'
+'19344A79B2307B^-3'
+'461FB98946D6A4^-3'
+'359BDF6D2B0A06^0'
+'-29D56AAF946778^0'
+'F3CF54CF529E98^0'
+'2653163D7BEC18^0'
+'6F14AF87C0203^-3'
+'1F046241E76C15^-3'
+'47A6611E64AC7C^-3'
+'D80E7C1A2B9^B'
+'D80E7CE83B^B'
+'D80E7FC4A7^B'
+'D80E81885^B'
+'D80E82A113^B'
+'D80E857D7F^B'
+'D80E8859EB^B'
+'D80E897EE3^B'
+'D80E8A5A9D^B'
+'D80E8B3657^B'
+'D80E8B7F95^B'
+'D80E8CA48D^B'
+'D80E8DBD5^B'
+'D80E8E12C3^B'
+'D80E8EE248^B'
+'D80E8FBE02^B'
+'D80E90E2FA^B'
+'D80E90EF2F^B'
+'D80E9207F2^B'
+'D80E932CEA^B'
+'D80E93CB9B^B'
+'D80E9451E2^B'
+'D80E9576DA^B'
+'D80E969BD2^B'
+'D80E96A807^B'
+'D80E97C0CA^B'
+'D80E98E5C2^B'
+'D80E998473^B'
+'D80E99FE85^B'
+'D80E9ADA3F^B'
+'D80E9B43DEE^B'
+'D80E7C1A2B9^B'
+'1^1'
+'1F^2'
+END_ARRAY 1 251
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /ale/leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/merged_nhpc_2015_v001_1_sliced_-98000.xc b/tests/pytests/data/lsb_0296962438_0x53c_eng/merged_nhpc_2015_v001_1_sliced_-98000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..ff0d1b3f7b65a46a9ab2917739c6f00b66bd101b
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/merged_nhpc_2015_v001_1_sliced_-98000.xc
@@ -0,0 +1,3431 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' < DAFCAT: CK CONCATENATION > '
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+'D8119820E4^B'
+'D811982D19^B'
+'D81198394E^B'
+'D811984583^B'
+'D8119851B8^B'
+'D811985DED^B'
+'D811986A22^B'
+'D811987657^B'
+'D81198828C^B'
+'D811988EC1^B'
+'D811989AF6^B'
+'D81198A72B^B'
+'D81198B36^B'
+'D81198BF95^B'
+'D81198CBCA^B'
+'D81198D7FF^B'
+'D81198E434^B'
+'D81198F069^B'
+'D81198FC9E^B'
+'D8119908D3^B'
+'D811991508^B'
+'D81199213D^B'
+'D811992D72^B'
+'D8119939A7^B'
+'D8119945DC^B'
+'D811995211^B'
+'D811995E46^B'
+'D811996A7B^B'
+'D8119976B^B'
+'D8119982E5^B'
+'D811998F1A^B'
+'D811999B4F^B'
+'D81199A784^B'
+'D81199B3B9^B'
+'D81199BFEE^B'
+'D81199CC23^B'
+'D81199D858^B'
+'D81199E48D^B'
+'D81199F0C2^B'
+'D81199FCF7^B'
+'D8119A092C^B'
+'D8119A1561^B'
+'D8119A2196^B'
+'D8119A2DCB^B'
+'D8119A3A^B'
+'D8119A4635^B'
+'D8119A526A^B'
+'D8119A5E9F^B'
+'D8119A6AD4^B'
+'D8119A7709^B'
+'D8119A833E^B'
+'D8119A8F73^B'
+'D8119A9BA8^B'
+'D8119AA7DD^B'
+'D8119AB412^B'
+'D8119AC047^B'
+'D8119ACC7C^B'
+'D8119AD8B1^B'
+'D8119AE4E6^B'
+'D8119AF11B^B'
+'D8119AFD5^B'
+'D8119B0985^B'
+'D8119B15BA^B'
+'D8119B21EF^B'
+'D8119B2E24^B'
+'D8119B3A59^B'
+'D8119B468E^B'
+'D8119B52C3^B'
+'D8119B5EF8^B'
+'D8119B6B2D^B'
+'D8119B7762^B'
+'D8119B8397^B'
+'D8119B8FCC^B'
+'D8119B9C01^B'
+'D8119BA836^B'
+'D8119BB46B^B'
+'D8119BC0A^B'
+'D8119BCCD5^B'
+'D8119BD90A^B'
+'D8119BE53F^B'
+'D8119BF174^B'
+'D8119BFDA9^B'
+'D8119C09DE^B'
+'D8119C1613^B'
+'D8119C2248^B'
+'D8119C2E7D^B'
+'D8119C3AB2^B'
+'D8119C46E7^B'
+'D8119C531C^B'
+'D8119C5F51^B'
+'D8119C6B86^B'
+'D8119C77BB^B'
+'D8119C83F^B'
+'D8119C9025^B'
+'D8119C9C5A^B'
+'D8119CA88F^B'
+'D8119CB4C4^B'
+'D8119CC0F9^B'
+'D8119CCD2E^B'
+'D8119CD963^B'
+'D8119CE598^B'
+'D8119CF1CD^B'
+'D8119CFE02^B'
+'D8119D0A37^B'
+'D8119D166C^B'
+'D8119D22A1^B'
+'D8119D2ED6^B'
+'D8119D3B0B^B'
+'D8119D474^B'
+'D8119D5375^B'
+'D8119D5FAA^B'
+'D8119D6BDF^B'
+'D8119D7814^B'
+'D8119D8449^B'
+'D8119D907E^B'
+'D8119D9CB3^B'
+'D8119DA8E8^B'
+'D8119DB51D^B'
+'D8119DC152^B'
+'D8119DCD87^B'
+'D8119DD9BC^B'
+'D8119DE5F1^B'
+'D8119DF226^B'
+'D8119DFE5B^B'
+'D8119E0A9^B'
+'D8119E16C5^B'
+'D8119E22FA^B'
+'D8119E2F2F^B'
+'D8119E3B64^B'
+'D8119E4799^B'
+'D8119E53CE^B'
+'D8119E6003^B'
+'D8119E6C38^B'
+'D8119E786D^B'
+'D8119E84A2^B'
+'D8119E90D7^B'
+'D8119E9D0C^B'
+'D8119EA941^B'
+'D8119EB576^B'
+'D8119EC1AB^B'
+'D8119ECDE^B'
+'D8119EDA15^B'
+'D8119EE64A^B'
+'D8119EF27F^B'
+'D8119EFEB4^B'
+'D8119F0AE9^B'
+'D8119F171E^B'
+'D8119F2353^B'
+'D8119F2F88^B'
+'D8119F3BBD^B'
+'D8119F47F2^B'
+'D8119F5427^B'
+'D8119F605C^B'
+'D8119F6C91^B'
+'D8119F78C6^B'
+'D8119F84FB^B'
+'D8119F913^B'
+'D8119F9D65^B'
+'D8119FA99A^B'
+'D8119FB5CF^B'
+'D8119FC204^B'
+'D8119FCE39^B'
+'D8119FDA6E^B'
+'D8119FE6A3^B'
+'D8119FF2D8^B'
+'D8119FFF0D^B'
+'D811A00B42^B'
+'D811A01777^B'
+'D811A023AC^B'
+'D811A02FE1^B'
+'D811A03C16^B'
+'D811A0484B^B'
+'D811A0548^B'
+'D811A060B5^B'
+'D811A06CEA^B'
+'D811A0791F^B'
+'D811A08554^B'
+'D811A09189^B'
+'D811A09DBE^B'
+'D811A0A9F3^B'
+'D811A0B628^B'
+'D811A0C25D^B'
+'D811A0CE92^B'
+'D811A0DAC7^B'
+'D811A0E6FC^B'
+'D811A0F331^B'
+'D811A0FF66^B'
+'D811A10B9B^B'
+'D811A117D^B'
+'D811A12405^B'
+'D811A19E17^B'
+'D811A21829^B'
+'D811A2923B^B'
+'D811A4AB57^B'
+'D811A52569^B'
+'D811A53EE6^B'
+'D81191EDFA^B'
+'D81196B2AE^B'
+'D8119B7762^B'
+'D811A03C16^B'
+'D8118AC7E6^B'
+'1^1'
+'1A9^3'
+END_ARRAY 1 3407
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /ale/leisa/lsb_0296962438_0x53c_eng/lsb_0296962438_0x53c_eng-spiced.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/naif0012.tls b/tests/pytests/data/lsb_0296962438_0x53c_eng/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/naif0012.tls
@@ -0,0 +1,152 @@
+KPL/LSK
+
+
+LEAPSECONDS KERNEL FILE
+===========================================================================
+
+Modifications:
+--------------
+
+2016, Jul. 14 NJB Modified file to account for the leapsecond that
+ will occur on December 31, 2016.
+
+2015, Jan. 5 NJB Modified file to account for the leapsecond that
+ will occur on June 30, 2015.
+
+2012, Jan. 5 NJB Modified file to account for the leapsecond that
+ will occur on June 30, 2012.
+
+2008, Jul. 7 NJB Modified file to account for the leapsecond that
+ will occur on December 31, 2008.
+
+2005, Aug. 3 NJB Modified file to account for the leapsecond that
+ will occur on December 31, 2005.
+
+1998, Jul 17 WLT Modified file to account for the leapsecond that
+ will occur on December 31, 1998.
+
+1997, Feb 22 WLT Modified file to account for the leapsecond that
+ will occur on June 30, 1997.
+
+1995, Dec 14 KSZ Corrected date of last leapsecond from 1-1-95
+ to 1-1-96.
+
+1995, Oct 25 WLT Modified file to account for the leapsecond that
+ will occur on Dec 31, 1995.
+
+1994, Jun 16 WLT Modified file to account for the leapsecond on
+ June 30, 1994.
+
+1993, Feb. 22 CHA Modified file to account for the leapsecond on
+ June 30, 1993.
+
+1992, Mar. 6 HAN Modified file to account for the leapsecond on
+ June 30, 1992.
+
+1990, Oct. 8 HAN Modified file to account for the leapsecond on
+ Dec. 31, 1990.
+
+
+Explanation:
+------------
+
+The contents of this file are used by the routine DELTET to compute the
+time difference
+
+[1] DELTA_ET = ET - UTC
+
+the increment to be applied to UTC to give ET.
+
+The difference between UTC and TAI,
+
+[2] DELTA_AT = TAI - UTC
+
+is always an integral number of seconds. The value of DELTA_AT was 10
+seconds in January 1972, and increases by one each time a leap second
+is declared. Combining [1] and [2] gives
+
+[3] DELTA_ET = ET - (TAI - DELTA_AT)
+
+ = (ET - TAI) + DELTA_AT
+
+The difference (ET - TAI) is periodic, and is given by
+
+[4] ET - TAI = DELTA_T_A + K sin E
+
+where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
+heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
+small-period fluctuations, is accurate to about 0.000030 seconds.
+
+The eccentric anomaly E is given by
+
+[5] E = M + EB sin M
+
+where M is the mean anomaly, which in turn is given by
+
+[6] M = M + M t
+ 0 1
+
+where t is the number of ephemeris seconds past J2000.
+
+Thus, in order to compute DELTA_ET, the following items are necessary.
+
+ DELTA_TA
+ K
+ EB
+ M0
+ M1
+ DELTA_AT after each leap second.
+
+The numbers, and the formulation, are taken from the following sources.
+
+ 1) Moyer, T.D., Transformation from Proper Time on Earth to
+ Coordinate Time in Solar System Barycentric Space-Time Frame
+ of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
+ 33-56 and 57-68.
+
+ 2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
+ Reference System on Algorithms for Computing Time Differences
+ and Clock Rates, JPL IOM 314.5--942, 1 October 1985.
+
+The variable names used above are consistent with those used in the
+Astronomical Almanac.
+
+\begindata
+
+DELTET/DELTA_T_A = 32.184
+DELTET/K = 1.657D-3
+DELTET/EB = 1.671D-2
+DELTET/M = ( 6.239996D0 1.99096871D-7 )
+
+DELTET/DELTA_AT = ( 10, @1972-JAN-1
+ 11, @1972-JUL-1
+ 12, @1973-JAN-1
+ 13, @1974-JAN-1
+ 14, @1975-JAN-1
+ 15, @1976-JAN-1
+ 16, @1977-JAN-1
+ 17, @1978-JAN-1
+ 18, @1979-JAN-1
+ 19, @1980-JAN-1
+ 20, @1981-JUL-1
+ 21, @1982-JUL-1
+ 22, @1983-JUL-1
+ 23, @1985-JUL-1
+ 24, @1988-JAN-1
+ 25, @1990-JAN-1
+ 26, @1991-JAN-1
+ 27, @1992-JUL-1
+ 28, @1993-JUL-1
+ 29, @1994-JUL-1
+ 30, @1996-JAN-1
+ 31, @1997-JUL-1
+ 32, @1999-JAN-1
+ 33, @2006-JAN-1
+ 34, @2009-JAN-1
+ 35, @2012-JUL-1
+ 36, @2015-JUL-1
+ 37, @2017-JAN-1 )
+
+\begintext
+
+
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/new_horizons_1454.tsc b/tests/pytests/data/lsb_0296962438_0x53c_eng/new_horizons_1454.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..be0e263b66f0f9259b3d80f4ec4d78b550115ac8
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/new_horizons_1454.tsc
@@ -0,0 +1,1696 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "new_horizons_1454.tsc"
+MISSION_NAME = "NEW HORIZONS"
+SPACECRAFT_NAME = "NEW HORIZONS"
+DATA_SET_ID = "NH-J/P/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "new_horizons_1454.tsc"
+PRODUCT_CREATION_TIME = 2017-04-30T00:00:00
+PRODUCER_ID = "APL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = {
+ JUPITER,
+ PLUTO,
+ "SOLAR SYSTEM"
+ }
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "NH spacecraft clock kernel"
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+\begintext
+
+FILENAME = "new-horizons_1454.tsc"
+CREATION_DATE = "03-Apr-2017"
+
+
+NEW HORIZONS Spacecraft Clock Kernel (SCLK)
+===========================================================================
+
+ This file is a SPICE spacecraft clock (SCLK) kernel containing
+ information required for time conversions involving the on-board
+ NEW HORIZONS spacecraft clock.
+
+Version
+--------------------------------------------------------
+
+ NEW HORIZONS SCLK Kernel Version:
+
+ Version 1.04 -- March 1, 2011 -- Stan Cooper
+ Following processing of all ACO4 data in Partition #2, manually
+ added the first Partition #3 record (for October 31, 2010), to
+ accommodate the Timekeeping System ground software.
+
+ Version 1.03 -- December 16, 2010 -- Stan Cooper
+ Partition #2 start shifted ten seconds earlier per request by Eric
+ Melin. Start time was set too late.
+
+ Version 1.02 -- November 15, 2010 -- Stan Cooper
+ Partition #3 created in response to unplanned November 1st
+ resynchronization of software MET to BC hardware MET. Effectively,
+ the software MET has jumped one second back.
+
+ Version 1.01 -- August 12, 2010 -- Stan Cooper
+ Paritition #2 created in response to July 2nd loss of software
+ MET synchronization with BC hardware MET. Software MET is now
+ one second larger than BC hardware MET. Effectively, the
+ software MET has jumped one second ahead.
+
+ Version 1.0 -- December 14, 2005 -- Stan Cooper
+ Initial (seed) time coefficients triplet set for a launch time
+ of 2006-011-14:11:00 EST, which equals 2006-011-19:11:00 UTC.
+ Note that this was set using the new value of 33 leap seconds
+ that comes into effect a few days before launch.
+
+ Version 0.4 -- November 15, 2005 -- Stan Cooper
+ Corrected the statement "SPICE uses linear interpolation" to
+ "SPICE uses linear extrapolation". This was confirmed earlier
+ with Scott Turner as noted in the MESSENGER SCLK kernels.
+
+ Version 0.3 -- May 11, 2005 -- Stan Cooper
+ Modified file header to avoid loss of header text when kernel
+ is automatically updated. Also, added FILENAME and
+ CREATION_DATE fields that are automatically updated.
+
+ Version 0.2 -- June 25, 2003 -- Scott Turner
+
+ The number of digits representing fractional seconds present
+ in the TDT component of the SCLK coefficient triples were
+ inadequate for NEW HORIZONS' requirements. The field now
+ contains 6 digits instead of 3.
+
+ Version 0.1 -- June 24, 2003 -- Scott Turner
+
+ This kernel was created as an initial input to the NEW HORIZONS
+ SCLK update process. It provides values for the fields
+ required to handle the SCLK string format, as well as the
+ baseline units of the clock correlation coefficients that
+ the update process is to introduce or correct. The initial
+ clock rate established in this file assumes no drift from
+ the parallel time system (TDT). Further the clock coefficients
+ indicate the clock starts on the following epoch:
+
+ 1/0:0 (SCLK)
+ 01-JAN-2003-00:01:04.184 (TDT)
+
+ The end of the first partition is currently defined as the value
+ in ticks of the rollover of the spacecraft clock.
+
+Usage
+--------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that
+ make use of this SCLK kernel must 'load' the kernel, normally
+ during program initialization. Loading the kernel associates
+ the data items with their names in a data structure called the
+ 'kernel pool'. The SPICELIB routine FURNSH loads text kernel
+ files, such as this one, into the pool as shown below:
+
+ FORTRAN:
+
+ CALL FURNSH ( SCLK_kernel_name )
+
+ C:
+
+ furnsh_c ( SCLK_kernel_name );
+
+ Once loaded, the SCLK time conversion routines will be able to
+ access the necessary data located in this kernel for their
+ designed purposes.
+
+References
+--------------------------------------------------------
+
+ 1. "SCLK Required Reading"
+
+Inquiries
+--------------------------------------------------------
+
+ If you have any questions regarding this file or its usage,
+ contact:
+
+ Scott Turner
+ (443)778-1693
+ Scott.Turner@jhuapl.edu
+
+Kernel Data
+--------------------------------------------------------
+
+ The first block of keyword equals value assignments define the
+ type, parallel time system, and format of the spacecraft clock.
+ These fields are invariant from SCLK kernel update to SCLK
+ kernel update.
+
+ The NEW HORIZONS spacecraft clock is represented by the SPICE
+ type 1 SCLK kernel. It uses TDT, Terrestrial Dynamical Time,
+ as its parallel time system.
+
+\begindata
+
+SCLK_KERNEL_ID = ( @2017-04-03T10:00:49 )
+SCLK_DATA_TYPE_98 = ( 1 )
+SCLK01_TIME_SYSTEM_98 = ( 2 )
+
+
+\begintext
+
+ In a particular partition of the NEW HORIZONS spacecraft clock,
+ the clock read-out consists of two separate stages:
+
+ 1/18424652:24251
+
+ The first stage, a 32 bit field, represents the spacecraft
+ clock seconds count. The second, a 16 bit field, represents
+ counts of 20 microsecond increments of the spacecraft clock.
+
+ The following keywords and their values establish this structure:
+
+\begindata
+
+SCLK01_N_FIELDS_98 = ( 2 )
+SCLK01_MODULI_98 = ( 4294967296 50000 )
+SCLK01_OFFSETS_98 = ( 0 0 )
+SCLK01_OUTPUT_DELIM_98 = ( 2 )
+
+
+\begintext
+
+ This concludes the invariant portion of the SCLK kernel data. The
+ remaining sections of the kernel may require updates as the clock
+ correlation coefficients evolve in time. The first section below
+ establishes the clock partitions. The data in this section consists
+ of two parallel arrays, which denote the start and end values in
+ ticks of each partition of the spacecraft clock.
+
+ SPICE utilizes these two arrays to map from spacecraft clock ticks,
+ determined with the usual modulo arithmetic, to encoded SCLK--the
+ internal, monotonically increasing sequence used to tag various
+ data sources with spacecraft clock.
+
+\begindata
+
+SCLK_PARTITION_START_98 = ( 0.00000000000000e+00
+ 7.01906790000000e+12
+ 7.54337430000000e+12 )
+
+SCLK_PARTITION_END_98 = ( 7.01906785000000e+12
+ 7.54337435000000e+12
+ 2.14748364799999e+14 )
+
+\begintext
+
+ The remaining section of the SCLK kernel defines the clock correlation
+ coefficients. Each line contains a 'coefficient triple':
+
+ Encoded SCLK at which Rate is introduced.
+ Corresponding TDT Epoch at which Rate is introduced.
+ Rate in TDT (seconds) / most significant clock count (~seconds).
+
+ SPICE uses linear extrapolation to convert between the parallel time
+ system and encoded SCLK. The triples are stored in the array defined
+ below.
+
+ The first time triplet below was entered manually and represents the
+ approximate time (in TDT) at which MET is set to zero. The plan for
+ New Horizons is that MET will be set to roll over to zero at the
+ beginning of the daily launch window. Note that the conversion from
+ UTC to TDT used 33 leap seconds.
+
+\begindata
+
+SCLK01_COEFFICIENTS_98 = (
+
+ 0 @19-JAN-2006-18:09:05.184000 1.00000000000
+ 2766250000 @20-JAN-2006-09:31:12.483494 1.00000000905
+ 5196350000 @20-JAN-2006-23:01:14.483934 1.00000000931
+ 9606650000 @21-JAN-2006-23:31:20.484755 1.00000000939
+ 13926500000 @22-JAN-2006-23:31:17.485566 1.00000000919
+ 18246400000 @23-JAN-2006-23:31:15.486360 1.00000000938
+ 22566350000 @24-JAN-2006-23:31:14.487170 1.00000000892
+ 26885950000 @25-JAN-2006-23:31:06.487941 1.00000000954
+ 31206000000 @26-JAN-2006-23:31:07.488765 1.00000001357
+ 44169100000 @29-JAN-2006-23:32:09.492284 1.00000007324
+ 48495750000 @30-JAN-2006-23:34:22.498622 0.99999993415
+ 52805100000 @31-JAN-2006-23:30:49.492947 1.00000001019
+ 57124700000 @01-FEB-2006-23:30:41.493827 1.00000001790
+ 91701750000 @09-FEB-2006-23:36:22.506207 0.99999998303
+ 104645200000 @12-FEB-2006-23:30:51.501814 1.00000000852
+ 108962750000 @13-FEB-2006-23:30:02.502550 1.00000000833
+ 117603550000 @15-FEB-2006-23:30:18.503989 1.00000000799
+ 134885300000 @19-FEB-2006-23:30:53.506750 1.00000000804
+ 139201550000 @20-FEB-2006-23:29:38.507444 1.00000000759
+ 143531500000 @21-FEB-2006-23:32:57.508101 1.00000000759
+ 151982150000 @23-FEB-2006-22:29:50.509384 1.00000000729
+ 165123050000 @26-FEB-2006-23:30:08.511299 1.00000000724
+ 169440450000 @27-FEB-2006-23:29:16.511924 1.00000000698
+ 173760250000 @28-FEB-2006-23:29:12.512527 1.00000000697
+ 182401100000 @02-MAR-2006-23:29:29.513731 1.00000000679
+ 195001700000 @05-MAR-2006-21:29:41.515442 1.00000000641
+ 203280050000 @07-MAR-2006-19:29:08.516504 1.00000000611
+ 212639700000 @09-MAR-2006-23:29:01.517648 1.00000000607
+ 229381150000 @13-MAR-2006-20:29:30.519679 1.00000000572
+ 246746750000 @17-MAR-2006-20:58:02.521664 1.00000000530
+ 276812450000 @24-MAR-2006-19:59:56.524853 1.00000000473
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diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_pcnh_006.tpc b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_pcnh_006.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..25e9b327f000090b0c72f1080223a43aa32cfc92
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_pcnh_006.tpc
@@ -0,0 +1,116 @@
+nh_pcnh_006.tpc
+
+PCK containing radii for Pluto, Charon, Nix, Hydra
+
+\begindata
+
+BODY999_RADII = ( 1188.3 1188.3 1188.3 )
+BODY901_RADII = ( 606.0 606.0 606.0 )
+BODY902_RADII = ( 24.1 16.4 15.2 )
+BODY903_RADII = ( 25.65 17.9 16.1 )
+BODY904_RADII = ( 10 10 10 )
+BODY905_RADII = ( 3.5 3.5 3.5 )
+
+BODY902_POLE_RA = ( 350.1179532 0.0 0.0 )
+BODY902_POLE_DEC = ( -38.6337107 0.0 0.0 )
+BODY902_PM = ( 81.9449154 197.01579 0.0 )
+BODY902_JED_EPOCH = ( 2457217.83654080 )
+BODY902_CONSTANTS_REF_FRAME = ( 1 )
+
+
+BODY903_POLE_RA = ( 349.1 0.0 0.0 )
+BODY903_POLE_DEC = ( 37.69 0.0 0.0 )
+BODY903_PM = ( 176.3895140 837.7607 0.0 )
+BODY903_JED_EPOCH = ( 2457217.83654080 )
+BODY903_CONSTANTS_REF_FRAME = ( 1 )
+
+\begintext
+
+ID Body Radii 1-sigma comments
+
+999 Pluto 1188.3km +/-1.6km Nimmo et al., 2016 (3)
+901 Charon 606.0km +/-1.0km Nimmo et al., 2016 (3)
+904 Kerberos 10 km Weaver et al. 2016 (4)
+905 Styx 3.5km Weaver et al. 2016 (4)
+
+
+902 Nix Porter et al., 2017 (5), updated via email:
+ Tri-axial diameters = 48.3 x 32.8 x 30.4 km
+ ra = 350.1179532deg
+ dec = -38.6337107deg
+ pm = 81.9449154deg
+ period = 1.8272647d/360deg
+ = 1d/197.01579deg
+ et0 = 490133077.125s past J2000 epoch
+ = 5672.83654090 JED past JED 2451545.0
+ = 2457217.8365407987 JED
+ Rotation model reference frame is J2000 (SPICE Frame ID 1)
+
+
+903 Hydra, Porter et al., 2017 (5):
+ Tri-axial diameters = 50.3 x 35.8 x 32.2 km
+ ra = 82.4457646deg
+ dec = 6.5129206deg
+ pm = 176.3895140
+ period = 0.4297170d/360deg
+ = 1d/837.760665740deg
+ et0 = 490133077.125s past J2000 epoch
+ = 5672.83654090 JED past JED 2451545.0
+ = 2457217.8365407987 JED
+ Rotation model reference frame is J2000 (SPICE Frame ID 1)
+
+
+
+Notes
+=====
+
+(1) Nimmo et al. Mean radius and shape of Pluto and Charon from New
+ Horizons images, 2016. http://arxiv.org/abs/1603.00821
+
+(2) Based on embargoed materials presented at New Horizons Science Team
+ Meeting, 29.-31.July, 2015
+
+(3) Francis Nimmo, Orkan Umurhan, Carey M. Lisse, Carver J. Bierson,
+ Tod R. Lauer, Marc W. Buie, Henry B. Throop, Josh A. Kammer,
+ James H. Roberts, William B. McKinnon, Amanda M. Zangari, Jeffrey
+ M. Moore, S. Alan Stern, Leslie A. Young, Harold A. Weaver, Cathy B.
+ Olkin, Kim Ennico, Mean radius and shape of Pluto and Charon from
+ New Horizons images, Icarus, Available online 12 July 2016, ISSN
+ 0019-1035, http://dx.doi.org/10.1016/j.icarus.2016.06.027.
+
+(4) Weaver, H. A.; Buie, M. W.; Buratti, B. J.; Grundy, W. M.; Lauer, T. R.;
+ Olkin, C. B.; Parker, A. H.; Porter, S. B.; Showalter, M. R.; Spencer,
+ J. R.; Stern, S. A.; Verbiscer, A. J.; McKinnon, W. B.; Moore, J. M.;
+ Robbins, S. J.; Schenk, P.; Singer, K. N.; Barnouin, O. S.; Cheng, A.
+ F.; Ernst, C. M.; Lisse, C. M.; Jennings, D. E.; Lunsford, A. W.;
+ Reuter, D. C.; Hamilton, D. P.; Kaufmann, D. E.; Ennico, K.; Young, L.
+ A.; Beyer, R. A.; Binzel, R. P.; Bray, V. J.; Chaikin, A. L.; Cook, J.
+ C.; Cruikshank, D. P.; Dalle Ore, C. M.; Earle, A. M.; Gladstone, G. R.;
+ Howett, C. J. A.; Linscott, I. R.; Nimmo, F.; Parker, J. Wm.; Philippe,
+ S.; Protopapa, S.; Reitsema, H. J.; Schmitt, B.; Stryk, T.; Summers, M.
+ E.; Tsang, C. C. C.; Throop, H. H. B.; White, O. L.; Zangari, A. M., The
+ small satellites of Pluto as observed by New Horizons, Science, Volume
+ 351, Issue 6279, id.aae0030 (2016),
+ http://dx.doi.org/10.1126/science.aae0030.
+
+(5) Porter, S.B. et al., 2017. Shapes and Poles of Nix and Hydra. Presented
+ at the 2017 Asteroids, Comets, and Meteors Meeting.
+
+
+History
+=======
+
+BTCarcich 2017-04-26 Version 006, Updated Nix and Hydra radii, added
+ Kerberos and Styx radii; added Nix and
+ Hydra pole positions.
+BTCarcich 2016-09-13 Version 005, Restored 1-sigma uncertainties for Pluto
+ and Charon from online abstract.
+BTCarcich 2016-09-13 Version 005, Added new Pluto and Charon values,
+ removed 1-sigma uncertainties
+BTCarcich 2016-05-31 Version 004, cleaning up typos; no substantive change
+BTCarcich 2016-05-28 Version 003, updated Pluto and Charon radii
+ per direction by Ross Beyer, Leslie
+ Young, via NH-GGI email list
+BTCarcich 2015-08-05 Version 002, updated Charon radii per Alan Stern
+BTCarcich 2015-07-30 Version 001
+
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_ralph_v100u.ti b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_ralph_v100u.ti
new file mode 100644
index 0000000000000000000000000000000000000000..21ac6064d32874a8ad86cd2df834770f8773b892
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_ralph_v100u.ti
@@ -0,0 +1,783 @@
+KPL/IK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "nh_ralph_v100u.ti"
+MISSION_NAME = "NEW HORIZONS"
+SPACECRAFT_NAME = "NEW HORIZONS"
+DATA_SET_ID = "NH-J/P/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = IK
+PRODUCT_ID = "nh_ralph_v100u.ti"
+PRODUCT_CREATION_TIME = 2018-10-18T00:00:00
+PRODUCER_ID = APL
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "NEW HORIZONS"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = {
+ JUPITER,
+ PLUTO,
+ "SOLAR SYSTEM"
+ }
+INSTRUMENT_NAME = "LINEAR ETALON IMAGING SPECTRAL ARRAY"
+NAIF_INSTRUMENT_ID = {
+ -98209,
+ -98208,
+ -98207,
+ -98206,
+ -98205,
+ -98204,
+ -98203,
+ -98202,
+ -98201,
+ }
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = INSTRUMENT
+ DESCRIPTION = "NH RALPH instrument kernel "
+END_OBJECT = SPICE_KERNEL
+END
+\endlabel
+
+
+RALPH Instrument Kernel
+==============================================================================
+
+ This instrument kernel (I-kernel) contains references to the mounting
+ alignment, internal and FOV geometry for the New Horizons Visible/IR
+ integrated imaging and spectroscopy remote sensing package (RALPH).
+
+Version and Date
+----------------------------------------------------------
+
+ The TEXT_KERNEL_ID stores version information of loaded project text
+ kernels. Each entry associated with the keyword is a string that consists
+ of four parts: the kernel name, version, entry date, and type. For example,
+ the RALPH I-kernel might have an entry as follows:
+
+ TEXT_KERNEL_ID += 'NEWHORIZONS_RALPH V1.0.0 22-FEBRUARY-2007 IK'
+ | | | |
+ | | | |
+ KERNEL NAME <-------+ | | |
+ | | V
+ VERSION <-------+ | KERNEL TYPE
+ |
+ V
+ ENTRY DATE
+
+ RALPH I-Kernel Version:
+
+ \begindata
+
+ TEXT_KERNEL_ID += 'NEWHORIZONS_RALPH V1.0.0 22-FEBRUARY-2007 IK'
+
+ NAIF_BODY_NAME += ( 'NH_RALPH' )
+ NAIF_BODY_CODE += ( -98200 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_FT' )
+ NAIF_BODY_CODE += ( -98203 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_PAN2' )
+ NAIF_BODY_CODE += ( -98204 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_PAN1' )
+ NAIF_BODY_CODE += ( -98205 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_RED' )
+ NAIF_BODY_CODE += ( -98206 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_BLUE' )
+ NAIF_BODY_CODE += ( -98207 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_METHANE' )
+ NAIF_BODY_CODE += ( -98208 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_MVIC_NIR' )
+ NAIF_BODY_CODE += ( -98209 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_LEISA' )
+ NAIF_BODY_CODE += ( -98201 )
+
+ NAIF_BODY_NAME += ( 'NH_RALPH_SIA' )
+ NAIF_BODY_CODE += ( -98202 )
+
+ \begintext
+
+
+ Version 1.0.0 -- February 22, 2007 -- Lillian Nguyen, JHU/APL
+
+ -- Removed the NH_RALPH_MVIC field of view definition and
+ added a NH_RALPH instrument boresight.
+ -- Removed the NH_RALPH_MVIC pixel size and IFOV definitions
+ and replaced them with the identical definitions for each
+ of the MVIC arrays.
+ -- Promoting to version 1.0.0 denoting approval of kernel set
+ by instrument teams.
+
+ Version 0.0.3 -- February 13, 2007 -- Lillian Nguyen, JHU/APL
+
+ -- Updated the MVIC FOV, LEISA FOV, and LEISA IFOV.
+ -- Added fields of view for the Frame Transfer and TDI arrays.
+
+ Version 0.0.2 -- October 4, 2006 -- Lillian Nguyen, JHU/APL
+
+ -- Removed the 3-letter frames NH_MVI, NH_LEI.
+
+ Version 0.0.1 -- June 15, 2006 -- Lillian Nguyen
+
+ -- Pixel size and IFOV added for MVIC and LEISA.
+
+ Version 0.0.0 -- December 28, 2005 -- Lillian Nguyen
+
+ -- Draft Version. NOT YET APPROVED BY INSTRUMENT TEAM.
+
+
+References
+----------------------------------------------------------
+
+ 1. Slides from Ralph Instrument Acceptance Review,
+ April 13, 2005.
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. New Horizons Spacecraft to PERSI/RALPH Interface
+ Control Document, Rev B, 7399-9201.
+
+ 4. APL New Horizons web site,
+ http://pluto.jhuapl.edu/spacecraft/overview.html.
+
+ 5. New Horizons Spacecraft Frames Kernel.
+
+ 6. New Horizons Mission Science Definitions (MSD),
+ NH7399-9000v1.6.
+
+ 7. RALPH Mechanical Interface Control Drawing (MICD), Rev B,
+ 574995_b.
+
+ 8. ALICE Instrument Kernel.
+
+ 9. Ralph Instrument Specification, Rev. A ECR SWRI 5310-001.
+
+ 10. LEISA to Ralph Interface Control Document.
+
+ 11. Document titled "RalphArrayPositions.doc", received from
+ Cathy Olkin by e-mail, Mar. 23, 2006, and e-mail exchange
+ concerning the document, Apr. 3-4, 2006.
+
+ 12. "RalphAlignWriteup03.doc", received from Allen Lunsford
+ 2/7/2007.
+
+ 13. E-mail from Cathy Olkin regarding the removal of the
+ NH_RALPH_MVIC frame and the introduction of the NH_RALPH
+ frame, received 2/22/2007.
+
+Contact Information
+----------------------------------------------------------
+
+ Lillian Nguyen, JHU/APL, (443)-778-5477, Lillian.Nguyen@jhuapl.edu
+
+
+Implementation Notes
+----------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make use of
+ this instrument kernel must ``load'' the kernel, normally during program
+ initialization. Loading the kernel associates data items with their names
+ in a data structure called the ``kernel pool''. The SPICELIB routine FURNSH,
+ CSPICE routine furnsh_c, and IDL routine cspice_furnsh load SPICE kernels
+ as shown below:
+
+ FORTRAN (SPICELIB)
+
+ CALL FURNSH ( 'kernel_name' )
+
+ C (CSPICE)
+
+ furnsh_c ( "kernel_name" )
+
+ ICY (IDL)
+
+ cspice_furnsh, 'kernel_name'
+
+ In order for a program or subroutine to extract data from the pool, the
+ SPICELIB routines GDPOOL, GCPOOL, and GIPOOL are used. See [2] for details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Naming Conventions
+----------------------------------------------------------
+
+ All names referencing values in this I-kernel start with the characters
+ `INS' followed by the NAIF New Horizons spacecraft ID number (-98)
+ followed by a NAIF three digit ID code for the RALPH instrument.
+
+ The remainder of the name is an underscore character followed by the unique
+ name of the data item. For example, the Ralph boresight direction in the
+ Ralph LEISA frame (``NH_RALPH_LEISA'' -- see [5] ) is specified by:
+
+ INS-98201_BORESIGHT
+
+ The upper bound on the length of the name of any data item is 32
+ characters.
+
+ If the same item is included in more than one file, or if the same item
+ appears more than once within a single file, the latest value supersedes
+ any earlier values.
+
+
+RALPH description
+----------------------------------------------------------
+
+ From [4]:
+
+ ``Ralph: Visible and infrared imager/spectrometer; provides color,
+ composition and thermal maps.
+ .
+ .
+ .
+ Ralph's main objectives are to obtain high resolution color maps and
+ surface composition maps of the surfaces of Pluto and Charon. The
+ instrument has two separate channels: the Multispectral Visible Imaging
+ Camera (MVIC) and the Linear Etalon Imaging Spectral Array (LEISA). A
+ single telescope with a 3-inch (6-centimeter) aperture collects and
+ focuses the light used in both channels.
+
+ MVIC operates at visible wavelengths - using the same light by which we
+ see - and has 4 different filters for producing color maps. One filter is
+ tailored to measure the methane frost distribution over the surface, while
+ the others are more generic and cover blue, red and near-infrared colors,
+ respectively. MVIC also has two panchromatic filters, which pass
+ essentially all visible light, for when maximum sensitivity to faint light
+ levels is required. In all cases, the light passes from the telescope
+ through the filters and is focused onto a charge coupled device (CCD).
+ (Although the MVIC CCD is a unique, sophisticated device, virtually all
+ consumer digital cameras use CCDs.)
+
+ LEISA operates at infrared wavelengths (it uses heat radiation), and its
+ etalon acts like a prism to bend different wavelengths of light by
+ different amounts so that each wavelength can be analyzed separately.
+ Since quantum physics teaches us that different molecules emit and absorb
+ light at different wavelengths, analysis of the different components of
+ the light by LEISA can be used to identify the unique "fingerprints" of
+ these molecules. LEISA will be used to map the distribution of frosts of
+ methane (CH4), molecular nitrogen (N2), carbon monoxide (CO), and water
+ (H2O) over the surface of Pluto and the water frost distribution over the
+ surface of Charon. LEISA data may also reveal new constituents on the
+ surfaces that have not yet been detected.''
+
+ From [10]:
+
+ ``Ralph is a visible and infrared remote sensing camera comprised of MVIC
+ and LEISA. MVIC is the multispectral visible imaging camera. LEISA is the
+ infrared spectral imaging focal plane. The Ralph common telescope is based
+ on a standard off-axis three mirror anastigmat design, which directs the
+ image to a beamsplitter, sending the image to both the MVIC detector and
+ LEISA.
+ .
+ .
+ .
+ The Ralph telescope is an all aluminum three-mirror "anastigmat"
+ telescope. It has a 75 mm aperture and a 650 mm effective focal length
+ when at its operating temperature of 220 K, or -53 degrees C. Its large,
+ flat focal plane is shared by a beamsplitter that transmits the infrared
+ light to the LEISA detector, while reflecting the visible and near-IR
+ light to the MVIC detector. The field of view is 5.7 by 0.9 degrees for
+ the visible, and 0.91 degrees square for the IR. The mirrors are to be
+ made of aluminum, diamond turned, with uncoated aluminum surfaces.''
+
+ From [9]:
+
+ ``MVIC shall provide imaging science data in five spectral bands at visible
+ and near-infrared wavelengths. MVIC shall also provide Optical Navigation
+ (OPNAV) imaging data for spacecraft navigation and orientation. The LEISA
+ instrument shall provide high spectral resolution imaging science data at
+ short-wave infrared wavelengths. MVIC will use optical filters to provide
+ spectral band discrimination. LEISA will use a linear variable etalon
+ filter to provide spectral discrimination. MVIC and the LEISA instrument
+ shall use a common light collection telescope. The common telescope shall
+ use a beamsplitter to direct light into two individual optical paths for
+ the MVIC and LEISA detectors. MVIC shall obtain two dimensional science
+ imaging data using time-delayed integration (TDI) data acquisition
+ synchronized to one dimensional spacecraft rotation. MVIC will also obtain
+ science imaging data using frame transfer data acquisition. The LEISA
+ instrument shall obtain two-dimensional imaging data in push broom mode.
+ MVIC shall use optical filters to provide the spectral band discrimination.
+ MVIC shall have five spectral bands, for data obtained using TDI data
+ acquisition, with wavelength ranges as described in Table 1 [reproduced
+ below].
+
+ --------------- ------------------------------
+ Spectral Band Nominal Wavelength Range (nm)
+ --------------- ------------------------------
+ Blue 400 - 550
+ Red 550 - 700
+ NIR 780 - 960
+ Methane 875 - 915
+ Panchromatic 400 - 960
+ --------------- ------------------------------
+
+ MVIC
+ ----
+ MVIC shall have a field of view (FOV) in the cross-track direction of 5.7d.
+ MVIC shall have a FOV that is determined by the TDI data acquisition range
+ in the in-track direction.
+ MVIC will have a FOV of 5.7 deg. x 0.15 deg.for images obtained using frame
+ transfer.
+ MVIC will use a front-side illuminated CCD silicon detector array.
+ MVIC will possess one TDI sensor for each of the blue, red, NIR, and
+ methane bands.
+ MVIC will possess one frame transfer sensor.
+ MVIC will possess two TDI sensors for the panchromatic band, to be referred
+ to as Pan1 and Pan2.
+ The detector shall be sensitive to light at wavelengths from 400 to 960 nm.
+ The CCD detector shall have pixels of size 13 X 13 microns +/- 0.1 microns.
+ Each TDI sensor shall have 32 x 5000 photosensitive pixels.
+ The frame transfer sensor shall possess 128 x 5000 photosensitive pixels.
+
+ LEISA
+ -----
+ The LEISA detector shall be a 256x256 HgCdTe array with 40 micron square
+ pixels.
+ The detector shall be sensitive to light from 1.25-2.50 microns.
+
+ Definitions/Glossary of Terms
+ -----------------------------
+ Cross-Track Direction - In spacecraft coordinates, motion that includes a
+ component in the +Z or -Z directions where the Z-axis is the axis of
+ rotation for the spacecraft in scan mode.
+ In-Track Direction - In spacecraft coordinates, motion in the X-Y plane
+ associated with spacecraft rotation about the Z-axis.
+ Instantaneous Field of View - The field of view imaged by the full detector
+ array with the spacecraft in staring mode.
+ OpNav Imaging Mode - For the MVIC sensor, this mode is used to take data to
+ meet OpNav requirements. 2D imaging for OpNav imaging mode is acquired
+ through frame transfer with the spacecraft in staring mode.
+ Scan Mode - In spacecraft coordinates, spacecraft rotation about the
+ Z-axis. Scan mode is used to acquire data for 2D images through
+ synchronized physical scanning and detector array readout. In scan mode,
+ the field of view in the in-track direction is determined by the length of
+ observation, IFOV, and the scan rate.
+ Science Imaging Mode - For the MVIC sensor, this mode is used to take data
+ to meet science requirements. 2D imaging for science imaging mode is
+ acquired through synchronized operation with 1D spacecraft maneuvers. The
+ detector readout occurs in TDI mode.
+ Single Pixel Instantaneous Field of View - The field of view for a single
+ pixel in a detector array.
+ Staring Mode - The spacecraft is pointed at a specific point and does not
+ have rotation about the Z-axis of the spacecraft. Staring mode is used to
+ acquire data for 2D images through frame transfer techniques for 2D
+ detector arrays.
+ TDI Mode Data Acquisition - For TDI data acquisition, a 2D image is
+ obtained by scanning around the Z axis. Looking down on the spacecraft from
+ above the ecliptic, in the nominal flight configuration (+Z pointing up,
+ -X pointing at Pluto or Charon), the spacecraft scans from left to right
+ clockwise.
+ TDI FOV - This indicates that the field of view for an image is variable
+ because it is related to spacecraft motion. Roughly, TDI FOV is the total
+ angle scanned by the spacecraft for a single observation. The TDI FOV is
+ comprised of multiples of the single pixel instantaneous field of view. For
+ a single observation by the FOV in the cross track direction.
+ LEISA Data Acquisition - For LEISA data acquisition, a 2D spectral image
+ is obtained by scanning around the Z axis in either the clockwise or
+ counterclockwise direction.''
+
+ RALPH Field of View Parameters
+----------------------------------------------------------
+
+ The detectors that constitute Ralph are MVIC, LEISA, and SIA. MVIC
+ has several focal plane arrays.
+
+ -- Multispectral Visible Imaging Camera (MVIC)
+
+ -- MVIC Frame Transfer Array (FT)
+
+ -- MVIC Pan 1 Array (PAN1)
+
+ -- MVIC Pan 2 Array (PAN2)
+
+ -- MVIC Red Array (RED)
+
+ -- MVIC Blue Transfer Array (BLUE)
+
+ -- MVIC Methane Array (METHANE)
+
+ -- MVIC NIR Array (NIR)
+
+ -- Linear Etalon Imaging Spectral Array (LEISA)
+
+ -- Solar Illumination Aperture (SIA)
+
+ The field of view sizes for the above detectors/arrays are given in [11],
+ with the exception of the PAN1, PAN2, RED, BLUE, METHANE, and NIR vertical
+ (along-scan) directions. Each of those arrays has 32 pixels per row [11].
+ The fields of view for those arrays were calculated using the following
+ formula:
+
+ along-scan FOV size = ( rows * IFOV ) deg
+
+ = ( 32 * 19.8/1000000 rad ) * ( 180/pi ) deg
+
+ = 0.036 deg
+
+ The cross-scan FOV size is 5.67 deg for each of the MVIC arrays [11].
+
+ The field of view sizes are given in the tables below.
+
+ Rectangular FOVs (coordinates in parenthesis are in the
+ spacecraft frame):
+
+ ---------- ---------------- ---------------- ----------------
+ Detector Horizontal Vertical Cone Axis
+ (cross scan)
+ ---------- ---------------- ---------------- ----------------
+ FT 5.67 deg (in Z) 0.145 deg (in Y) boresight (-X)
+
+ PAN1 5.67 deg (in Z) 0.036 deg (in Y) boresight (-X)
+
+ PAN2 5.67 deg (in Z) 0.036 deg (in Y) boresight (-X)
+
+ RED 5.67 deg (in Z) 0.036 deg (in Y) boresight (-X)
+
+ BLUE 5.67 deg (in Z) 0.036 deg (in Y) boresight (-X)
+
+ METHANE 5.67 deg (in Z) 0.036 deg (in Y) boresight (-X)
+
+ NIR 5.67 deg (in Z) 0.036 deg (in Y) boresight (-X)
+
+ LEISA 0.89 deg 0.89 deg boresight (-X)
+ ---------- ---------------- ---------------- ----------------
+
+ Circular FOV:
+
+ ---------- ---------------- ----------------
+ Detector Diameter Cone Axis
+ ---------- ---------------- ----------------
+ SIA 5.0 degrees near +Y
+ ---------- ---------------- ----------------
+
+ The SIA cone axis is nominally aligned with the ALICE Solar Occultation
+ Channel (SOC) [3], whose boresight is aligned to a line in the spacecraft
+ YZ plane right-hand rotated by 2 degrees around the X axis from the REX
+ boresight (spacecraft Y axis) [8]. The ALICE SOC FOV is illustrated in [8].
+
+ The MVIC and LEISA boresights are nominally aligned to the spacecraft -X
+ axis.
+
+ The INS[ID]_FOV_FRAME, INS[ID]_FOV_SHAPE, INS[ID]_BORESIGHT, and FOV
+ ANGLES specification keywords defined below are used to describe the
+ instrument field of view. Since the SIA detector has a circular field
+ of view, and the MVIC arrays and LEISA have rectangular ones, the
+ INS[ID]_FOV_SHAPE will either be 'CIRCLE' or 'RECTANGLE'. For SIA, GETFOV
+ returns a single vector that lies along the edge of the circular cone, and
+ for the MVIC arrays and LEISA, GETFOV returns four boundary corner vectors.
+
+ Note that a field of view is not defined for the instrument boresight. The
+ SPICE routine GDPOOL may be used to get the NH_RALPH boresight.
+
+
+Multispectral Visible Imaging Camera (MVIC) FOV Definitions
+
+ There is no single field of view definition for the Ralph instrument [13],
+ but the instrument boresight is by definition the center of the frame
+ transfer array. That boresight is the -X axis of the NH_RALPH frame:
+
+ N.B. This incomplete FOV frame has been disabled to satisfy a lien from
+ the PDS review of Release 0002 of this data set in August, 2014.
+
+ \begin_disabled_data
+
+ INS-98200_FOV_FRAME = 'NH_RALPH'
+ INS-98200_BORESIGHT = ( -1.0, 0.0, 0.0 )
+
+ \begintext
+
+ Each of the MVIC arrays, LEISA, and SIA have a field of view defined. Those
+ definitions are below.
+
+ Since the MVIC frame transfer array's angular separation in Y is 0.145
+ degrees, looking down the Z axis in the instrument frame we have: (Note
+ we are arbitrarily choosing vectors that terminate in the X=-1 plane.)
+
+
+ ^ Y
+ | inst
+ |
+ |. |
+ | `. |
+ | `. |
+ | o`. |
+ .0725 `. |
+ <---------------o
+ -X | ,' Z (out)
+ inst | ,' inst
+ | ,'
+ | ,'
+ |'
+
+ |--- 1.0 ---|
+ Plane Z = 0
+
+ And since the MVIC frame transfer array's angular separation in Z is 5.67
+ degrees, looking up the Y axis in the instrument frame, we have: (Note we
+ are arbitrarily choosing vectors that terminate in the X=-1 plane.)
+
+
+ ^ Z
+ | inst
+ |
+ |. |
+ | `. |
+ | `. |
+ | o`. |
+ 2.835 `. |
+ <---------------x
+ -X | ,' Y (in)
+ inst | ,' inst
+ | ,'
+ | ,'
+ |'
+
+ |--- 1.0 ---|
+ Plane Y = 0
+
+ These FOV values for the MVIC frame transfer array are given in the
+ keywords below:
+
+ \begindata
+
+ INS-98203_FOV_FRAME = 'NH_RALPH_MVIC_FT'
+ INS-98203_FOV_SHAPE = 'RECTANGLE'
+ INS-98203_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98203_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98203_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98203_FOV_REF_ANGLE = ( 0.0725 )
+ INS-98203_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98203_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
+ The angular separation in Y for each of the TDI arrays is 0.036 degrees.
+ Looking down the Z axis in the TDI frame we have: (Note we are arbitrarily
+ choosing vectors that terminate in the X=-1 plane.)
+
+
+ ^ Y
+ | inst
+ |
+ |. |
+ | `. |
+ | `. |
+ | o`. |
+ 0.018 `. |
+ <---------------o
+ -X | ,' Z (out)
+ inst | ,' inst
+ | ,'
+ | ,'
+ |'
+
+ |--- 1.0 ---|
+ Plane Z = 0
+
+ Which leads to the following field of view definitions:
+
+ \begindata
+
+ INS-98204_FOV_FRAME = 'NH_RALPH_MVIC_PAN2'
+ INS-98204_FOV_SHAPE = 'RECTANGLE'
+ INS-98204_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98204_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98204_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98204_FOV_REF_ANGLE = ( 0.018 )
+ INS-98204_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98204_FOV_ANGLE_UNITS = 'DEGREES'
+
+ INS-98205_FOV_FRAME = 'NH_RALPH_MVIC_PAN1'
+ INS-98205_FOV_SHAPE = 'RECTANGLE'
+ INS-98205_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98205_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98205_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98205_FOV_REF_ANGLE = ( 0.018 )
+ INS-98205_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98205_FOV_ANGLE_UNITS = 'DEGREES'
+
+ INS-98206_FOV_FRAME = 'NH_RALPH_MVIC_RED'
+ INS-98206_FOV_SHAPE = 'RECTANGLE'
+ INS-98206_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98206_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98206_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98206_FOV_REF_ANGLE = ( 0.018 )
+ INS-98206_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98206_FOV_ANGLE_UNITS = 'DEGREES'
+
+ INS-98207_FOV_FRAME = 'NH_RALPH_MVIC_BLUE'
+ INS-98207_FOV_SHAPE = 'RECTANGLE'
+ INS-98207_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98207_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98207_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98207_FOV_REF_ANGLE = ( 0.018 )
+ INS-98207_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98207_FOV_ANGLE_UNITS = 'DEGREES'
+
+ INS-98208_FOV_FRAME = 'NH_RALPH_MVIC_METHANE'
+ INS-98208_FOV_SHAPE = 'RECTANGLE'
+ INS-98208_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98208_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98208_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98208_FOV_REF_ANGLE = ( 0.018 )
+ INS-98208_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98208_FOV_ANGLE_UNITS = 'DEGREES'
+
+ INS-98209_FOV_FRAME = 'NH_RALPH_MVIC_NIR'
+ INS-98209_FOV_SHAPE = 'RECTANGLE'
+ INS-98209_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98209_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98209_FOV_REF_VECTOR = ( 0.0, +1.0, 0.0 )
+ INS-98209_FOV_REF_ANGLE = ( 0.018 )
+ INS-98209_FOV_CROSS_ANGLE = ( 2.835 )
+ INS-98209_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
+
+ From [11], the MVIC pixels are 13 microns wide with a single pixel FOV of
+ 19.8 microradians. These values are captured for each of the MVIC arrays
+ in the keywords below.
+
+ \begindata
+
+ INS-98203_PIXEL_SIZE = ( 13.0 )
+ INS-98203_IFOV = ( 19.8 )
+
+ INS-98204_PIXEL_SIZE = ( 13.0 )
+ INS-98204_IFOV = ( 19.8 )
+
+ INS-98205_PIXEL_SIZE = ( 13.0 )
+ INS-98205_IFOV = ( 19.8 )
+
+ INS-98206_PIXEL_SIZE = ( 13.0 )
+ INS-98206_IFOV = ( 19.8 )
+
+ INS-98207_PIXEL_SIZE = ( 13.0 )
+ INS-98207_IFOV = ( 19.8 )
+
+ INS-98208_PIXEL_SIZE = ( 13.0 )
+ INS-98208_IFOV = ( 19.8 )
+
+ INS-98209_PIXEL_SIZE = ( 13.0 )
+ INS-98209_IFOV = ( 19.8 )
+
+ \begintext
+
+
+Linear Etalon Imaging Spectral Array (LEISA) FOV Definition
+
+ Since LEISA's angular separation in Y is 0.89 degrees, looking down the
+ Z axis in the spacecraft frame we have: (Note we are arbitrarily choosing
+ vectors that terminate in the X=-1 plane.)
+
+
+ ^ Y
+ | sc
+ |
+ |. |
+ | `. |
+ | `. |
+ | o`. |
+ |.445 `. |
+ <---------------o
+ -X | ,' Z (out)
+ sc | ,' sc
+ | ,'
+ | ,'
+ |'
+
+ |--- 1.0 ---|
+ Plane Z = 0
+
+ Since LEISA's field of view is square, a similar computation yields the
+ Z component.
+
+ These FOV values for MVIC are given in the keywords below:
+
+ \begindata
+
+ INS-98201_FOV_FRAME = 'NH_RALPH_LEISA'
+ INS-98201_FOV_SHAPE = 'RECTANGLE'
+ INS-98201_BORESIGHT = ( -1.0, 0.0, 0.0 )
+ INS-98201_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98201_FOV_REF_VECTOR = ( 0.0, 1.0, 0.0 )
+ INS-98201_FOV_REF_ANGLE = ( 0.445 )
+ INS-98201_FOV_CROSS_ANGLE = ( 0.445 )
+ INS-98201_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
+ From [11], the LEISA pixels are 40 microns wide with a single pixel FOV of
+ 61 microradians. These values are captured in the keywords below.
+
+ INS-98201_PIXEL_SIZE = ( 40.0 )
+ INS-98201_IFOV = ( 61.0 )
+
+ The above IFOV is nominal and has been adjusted in-flight to the value
+ below [12]. The pixel size in microns is the nominal value:
+
+ \begindata
+
+ INS-98201_PIXEL_SIZE = ( 40.0 )
+ INS-98201_IFOV = ( 62.065 )
+
+ \begintext
+
+
+Solar Illumination Aperture (SIA) FOV Definition
+
+ The SIA frame is defined such that the boresight is the instrument
+ Z axis. The field of view is circular with a 5 degree angular separation.
+ A cross section is illustrated below. (Note we are arbitrarily choosing
+ vectors that terminate in the Z=1 plane.)
+
+ Y ^
+ sc |
+ |
+ |
+ |
+ | _.-|
+ | _.-' o|
+ |_.-' 2.5 |
+ x-------------->
+ X (in)`~._ | Z
+ sc `~._ | ins
+ `~.|
+
+ |--- 1.0 ---|
+
+ Plane X = 0
+
+
+ Because the SIA field of view is circular, the FOV reference vector (keyword
+ FOV_REF_VECTOR) is any vector with a component that lies in a plane normal
+ to the field of view boresight. We chose the +Y axis of the instrument
+ frame. These FOV values are given in the keywords below:
+
+ \begindata
+
+ INS-98202_FOV_FRAME = 'NH_RALPH_SIA'
+ INS-98202_FOV_SHAPE = 'CIRCLE'
+ INS-98202_BORESIGHT = ( 0.0, 0.0, 1.0 )
+ INS-98202_FOV_CLASS_SPEC = 'ANGLES'
+ INS-98202_FOV_REF_VECTOR = ( 0.0, 1.0, 0.0 )
+ INS-98202_FOV_REF_ANGLE = ( 2.5 )
+ INS-98202_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_soc_misc_v002.tf b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_soc_misc_v002.tf
new file mode 100644
index 0000000000000000000000000000000000000000..6c5765387ec7ae416e0c1b8d3688de18408829f7
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_soc_misc_v002.tf
@@ -0,0 +1,217 @@
+KPL/FK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "nh_soc_misc_v002.tf"
+MISSION_NAME = "NEW HORIZONS"
+SPACECRAFT_NAME = "NEW HORIZONS"
+DATA_SET_ID = "NH-J/P/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = FK
+PRODUCT_ID = "nh_soc_misc_v002.tf"
+PRODUCT_CREATION_TIME = 2016-04-30T00:00:00
+PRODUCER_ID = "SWRI"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = {
+ JUPITER,
+ PLUTO,
+ "SOLAR SYSTEM"
+ }
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = FRAMES
+ DESCRIPTION = "NH frames kernel. Provides supplemental
+name-to-ID mapping for misc bodies (Asteroid APL; target KBO 2014 MU69
+of proposed NH extended mission; etc.) "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+KPL/FK
+
+New Horizons Science Operations Center-specific Target Frames Kernel
+===============================================================================
+
+ This frame kernel contains the NAIF body name/code translation
+ for miscellaneous targets that will show up in some NH FITS file
+ headers due to targets added that are not in the project Frames
+ Kernel (nh_vXXX.tf) or other project SPICE kernels.
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ The TEXT_KERNEL_ID stores version information of loaded project text
+ kernels. Each entry associated with the keyword is a string that comprises
+ four parts: kernel name; kernel version; entry date; kernel type. For
+ example, the NH I-kernel might have an entry as follows:
+
+ TEXT_KERNEL_ID += 'NEWHORIZONS V2.0.0 30-APRIL-2016 IK'
+ | | | |
+ | | | |
+ KERNEL NAME <-------+ | | |
+ | | V
+ VERSION <-------+ | KERNEL TYPE
+ |
+ V
+ ENTRY DATE
+
+ New Horizons Science Operations Center-specific Frames Kernel Version:
+
+ \begindata
+
+ TEXT_KERNEL_ID += 'NEWHORIZONS_SOC_FRAMES V0.0.1 21-AUG-2008 FK'
+
+ \begintext
+
+ Version 0.0.0 -- August 21, 2008 -- Brian Carcich, SWRI Consultant
+
+ -- Initial version: Provide NAIF body name/code translation
+ for asteroid 2002 JF56, aka (132524) APL
+
+ Version 0.0.1 -- August 21, 2008 -- Brian Carcich, SWRI Consultant
+
+ -- Initial version: Moved name 2002_JF56 last so it is
+ preferred output of BODC2N().
+
+ Version 0.0.2 -- April, 30 2016 - Brian Carcich, SWRI Consultant
+
+ -- Added 2014 MU69/3713011 name/ID mapping
+ -- Fixed email
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``SPICE NAIF_IDS Required Reading''
+
+ 2. ``SPICE PCK Required Reading''
+
+ 3. ``SPICE Kernel Pool Required Reading''
+
+ 4. ``SPICE FRAMES Required Reading''
+
+ 5. ``SPK Required Reading''
+
+ 6. ``BRIEF User's Guide''
+
+ 7. Minor Planet Center - Minor Planet Names:
+ http://cfa-www.harvard.edu/iau/lists/MPNames.html
+ - dated 2008-Jul-17
+
+ 8. http://en.wikipedia.org/wiki/132524_APL
+ - as of 2008-Jul-21
+
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Brian Carcich, SWRI Consultant, BrianTCarcich<AT>gmail.com
+
+ - replace <AT> with ASCII 64 character
+
+
+Implementation Notes
+-------------------------------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make use of
+ this instrument kernel must ``load'' the kernel, normally during program
+ initialization. Loading the kernel associates data items with their names
+ in a data structure called the ``kernel pool''. The SPICELIB routine FURNSH,
+ CSPICE routine furnsh_c, and IDL routine cspice_furnsh load SPICE kernels
+ as shown below:
+
+ FORTRAN (SPICELIB)
+
+ CALL FURNSH ( 'kernel_name' )
+
+ C (CSPICE)
+
+ furnsh_c ( "kernel_name" )
+
+ ICY (IDL)
+
+ cspice_furnsh, 'kernel_name'
+
+ In order for a program or subroutine to extract data from the pool, the
+ SPICELIB routines GDPOOL, GCPOOL, and GIPOOL are used. See [3] for details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+NAIF Body Code for asteroid APL (formerly 2002 JF56)
+-------------------------------------------------------------------------------
+
+ This file provides the SPICE toolkit with the NAIF Body Code for asteroid
+ 2002 JF56 with various forms of its name. See [1] for more details.
+
+ The NAIF Body Code of 3127862 is included in the SP-Kernel provided
+ by the New Horizons project to the Science Operation Center (SOC).
+ in SP-Kernel originally named 'sb-2002jf56-2.bsp'
+
+ The output of the NAIF diagnostic program BRIEF on that SP-Kernel was
+ used to determine the NAIF Body Code of the asteroid; that output is
+ included here:
+
+ Brief. Version: 2.2.0 (SPICE Toolkit N0058)
+
+
+ Summary for: /home/soc/spice/kernels/recon/spk/sb-2002jf56-2.bsp
+
+ Body: 3127862
+ Start of Interval (ET) End of Interval (ET)
+ -------------------------------- --------------------------------
+ 2006 JAN 19 00:00:00.000 2006 OCT 02 00:00:00.000
+
+ See [5] and [6] for details.
+
+ Since no pole solution exists for 2002 JF56, no frame information will be
+ provided (e.g. BODY3127862_POLE_RA, &c; see [2] and [4] for details).
+
+ Note that, according to the NAIF_IDS Required Reading [1], the ID of this
+ asteroid in the JPL Asteroid and Comet Catalog is probably 1127862, while
+ this asteroid also has an ID of 132524 assigned by the Minor Planet Center
+ published in various places (e.g. see [7] and [8]).
+
+ Several names will be provided, with and without spaces, all referring
+ to the same object.
+
+\begindata
+
+NAIF_BODY_NAME += ( 'APL'
+ , '132524_APL'
+ , '(132524) APL'
+ , '(132524) 2002 JF56'
+ , '2002 JF56'
+ , '2002_JF56'
+ , '132524 APL'
+ )
+NAIF_BODY_CODE += ( 2132524
+ , 2132524
+ , 2132524
+ , 2132524
+ , 2132524
+ , 2132524
+ , 2132524
+ )
+
+NAIF_BODY_NAME += ( '2014 MU69'
+ , '2014_MU69'
+ )
+NAIF_BODY_CODE += ( 3713011
+ , 3713011
+ )
+
+\begintext
+
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_stars_kbo_centaur_v002.tpc b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_stars_kbo_centaur_v002.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..68496f4adc1ff5a54ccabbdc8f262951bf06ba2f
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_stars_kbo_centaur_v002.tpc
@@ -0,0 +1,1243 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "nh_stars_kbo_centaur_v002.tpc"
+MISSION_NAME = "NEW HORIZONS"
+SPACECRAFT_NAME = "NEW HORIZONS"
+DATA_SET_ID = "NH-J/P/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = PCK
+PRODUCT_ID = "nh_stars_kbo_centaur_v002.tpc"
+PRODUCT_CREATION_TIME = 2017-04-30T00:00:00
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = {
+ JUPITER,
+ PLUTO,
+ "SOLAR SYSTEM"
+ }
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = TARGET_CONSTANTS
+ DESCRIPTION = "PCK/Pinpoint input/Synthetic body constants"
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+########################################################################
+Start of comments
+
+This SPICE text kernel file is a catchall to provide
+
+- NAME/ID translations for bodies for which none existed within SPICE
+ at the time this file was created, including stars.
+
+- a non-rotating synthetic rotation state for all such bodies and
+ stars such that the body-fixed frames are aligned with the J2000
+ inertial frame.
+
+- Input to the SPICE pinpoint utility to model stars as objects moving
+ parallel to the spacecraft at a distance of 1km and positioned in the
+ same inertial direction (RA and DEC) w.r.t. the spacecraft as the star
+ being modelled. This is an oversimplified model for stars but its
+ accuracy is sufficient for the purpose intended.
+
+- A finite list of bodies (kernel pool variable - KPV - NH_TARGET_BODIES)
+ to check against New Horizons spacecraft pointing commands, parsed from
+ command sequence products, to heuristically determine the target for
+ any given observation.
+
+ - N.B. There may be duplicate entries in this list in some versions
+ of this kernel. The NH_TARGET_BODIES KPV is used internally
+ by the New Horizons (NH) project. NH project software makes
+ allowances for this duplication, and so such duplication is not
+ an error in this kernel.
+
+########################################################################
+
+During New Horizons long cruise phase, budgets and resources were limited,
+and the time of personnel who did planning and command sequencing so much
+so that is was not possible to put a process in place where the
+sequencing personnel would document the target and/or intent of
+observations in a usable way. Instead, the Science Operations Center
+(SOC) developed software to parse command sequencing products and
+determine the targets heuristically either from Chebyshev
+coefficient-based trajectory models, or from inertial pointing
+directions, which had been simulated on the ground before being uploaded
+to the spacecraft.
+
+########################################################################
+BODYnnn_PM
+BODYnnn_POLE_DEC
+BODYnnn_POLE_RA
+BODYnnn_RADII
+
+ The BODYnnn_... kernel pool variables, with the nnn substrings indicating
+ SPICE ID codes, provide synthetic body-fixed frames and radii for all
+ possible targets.
+
+
+NAIF_BODY_CODE
+NAIF_BODY_NAME
+
+ The NAIF_BODY_... kernel pool variables provide translation between
+ SPICE text names and SPICE numeric IDs
+
+
+NH_TARGET_BODIES
+
+ The NAIF_TARGET_BODIES kernel pool variable provides a set of bodies
+ that may be tested against uplink commands with Chebyshev
+ coefficient-based ephememeris models and spacecraft attitude pointing
+ to identify potential targets.
+
+
+SITEnnn_CENTER
+SITEnnn_FRAME
+SITEnnn_IDCODE
+SITES
+SITEnnn_XYZ
+
+ The SITEnnn_... and SITES kernel pool variables are inputs to the
+ NAIF/SPICE pinpoint utility to create bodies that stay in a fixed
+ position with respect to the New Horizons spacecraft; the nh_stars.bsp
+ SPK is the product of these inputs and the pinpoint utility
+
+########################################################################
+
+The set of bodies defined in this kernel comprise stars, asteoids, KBOs
+and plutonian satellites. Except for the stars, all the bodies have
+ephemerides in SPKs provided by this data set.
+
+Stars identified in this kernel have KPVs used by the pinpoint SPICE
+utility; that is, an SP-kernel for the stars may be created using this
+text kernel as an input to the pinpoint SPICE utility. Non-stars
+identified in this kernel to not have associated KPVs for pinpoint.
+
+The 8888nnn schema for assigning SPICE IDs to stars is an ad hoc
+convention adopted for the NH project; within the NH project and within
+this data set it does not conflict with any other SPICE IDs. No such
+claim is made beyond that scope; it is up to the user of this file to
+check whether it conflicts with any NH-external kernels that may be
+FURNSHed within the same application.
+
+The following is a list of the stars and other bodies: the first token
+in each line is an integer SPICE ID; the rest of each line contains the
+primary name for the body; see the rest of the kernel for alternate
+names used for the bodies.
+
+The alternate names used in this kernel, e.g. JR1 for 15810 ARAWN (1994
+JR1), will almost certainly be ambiguous or non-unique if this kernel is
+used outside the scope of New Horizons data. Again, it is up to the
+user of this file to resolve any conflicts with NH-external kernels that
+may be FURNSHed within the same application.
+
+
+Stars:
+ 8888000 zet Pup
+ 8888001 Vega
+ 8888002 gam Gru
+ 8888003 rho Leo
+ 8888004 M7
+ 8888005 Spica
+ 8888006 HD 93521
+ 8888007 Interplanetary Medium (IPM)
+ 8888008 NGC 3532
+ 8888009 Arcturus
+ 8888010 HD 214168
+ 8888011 Bellatrix
+ 8888012 M 1
+ 8888013 HD 205905
+ 8888014 HD 37962
+ 8888015 Cyg A
+ 8888016 Cas A
+ 8888017 M 87
+
+
+Solar system bodies: asteroids; KBOs; plutonian satelllites.
+ 2010199 10199 CHARIKLO
+ 2136472 136472 MAKEMAKE
+ 2136108 136108 HAUMEA
+ 904 KERBEROS
+ 905 STYX
+ 2015810 15810 ARAWN (1994 JR1)
+ 3523335 2010 JJ124
+ 2002060 2060 CHIRON
+ 2028978 28978 IXION (2001 KX76)
+ 2307261 ASTEROID 307261 (2002 MS4)
+ 2050000 50000 QUAOAR (2002 LM60)
+ 3713011 ASTEROID 486958 (2014 MU69)
+
+
+End of comments; the rest of this file is a string from a Python script.
+########################################################################
+
+This is a SPICE text kernel, created via script
+ uplinkdb_objects.py
+in directory
+ /home/brian/pipeline/uplinkdb/nh_targets
+
+The preamble that follows is the __doc__ string from that script, which
+contains crucial information for the use of this kernel, i.e. the
+integer SPICE ID codes of the bodies for which ephemerides will be
+checked when Chebychev-based trajectories are found in SASFs/SSFs/CMDs.
+========================================================================
+Preamble for uplinkdb_objects.py
+
+This was originally the __doc__ string in file uplinkdb_objects.py
+
+You may be reading it in a SPICE text kernel e.g.
+
+ nh_stars_kbo_centaur_ppinp.tpc
+
+This script creates that SPICE text kernel for use by PINPOINT to
+create a SPICE SP-Kernel with several stars.
+
+That kernel also provide name/ID mappings (NAIF_BODY_CODE/NAME) for
+those stars, plus KBOs Makemake and Haumea, and Centaur asteroid
+Chariklo, via this __doc__ string as a SPICE meta-kernel by defining
+kernel pool variable NH_TARGET_BODIES.
+
+Usage:
+
+ N.B. Usually called via the Makefile in the same directory
+
+ python uplinkdb_objects.py > nh_stars_kbo_centaur_ppinp.tpc
+
+ e.g. followed by
+
+ rm -f spk/nh_stars.bsp
+
+ pinpoint -def nh_stars_kbo_centaur_ppinp.tpc -spk spk/nh_stars.bsp -batch
+
+########################################################################
+########################################################################
+### N.B. This triple-quoted __doc__ string can be read in this file as a
+### SPICE text kernel; for use in this script, the backslash-b
+### characters (backspace, ASCII 8) are replaced by '\b', a
+### two-character string, so f.write will output the correct
+### backslash-begindata/text codes to the output file.
+########################################################################
+########################################################################
+
+ 506 is HIMALIA
+ 507 is ELARA
+ 517 is CALLIRHOE
+
+NH_TARGET_BODIES is a SPICE kernel pool variable (KPV) that lists the IDs
+of bodies the ephemerides of which will be checked against
+Chebyshev polynomial-based trajectories in New Horizons SASFs/SSFs/CMDs
+
+N.B. There may be duplicate entries in this list in some versions
+ of this kernel. The NH_TARGET_BODIES KPV is used internally
+ by the New Horizons (NH) project. NH project software makes
+ allowances for this duplication, and so such duplication is not
+ an error in this kernel.
+
+\begindata
+
+NH_TARGET_BODIES = ( 10 3
+ 501 502 503 504 505 506 507 517 599
+ 7 8
+ 901 902 903 904 905 999
+ )
+
+\begintext
+========================================================================
+End of preamble
+
+zet Pup
+['SIMBAD:', '* zet Pup', '120.89603141', '-40.00314780', 'Variable of BY Dra type']
+
+\begindata
+NAIF_BODY_NAME += ( 'zet Pup' )
+NAIF_BODY_CODE += ( 8888000 )
+NH_TARGET_BODIES += ( 8888000 )
+BODY8888000_POLE_RA = ( 0. 0. 0. )
+BODY8888000_POLE_DEC = ( 90. 0. 0. )
+BODY8888000_PM = ( 270. 0. 0. )
+BODY8888000_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star zet Pup:
+\begindata
+SITES += ( 'SITE8888000' )
+SITE8888000_FRAME = 'J2000'
+SITE8888000_IDCODE = 8888000
+SITE8888000_XYZ = ( -0.393332 0.657313 -0.642830 )
+SITE8888000_CENTER = -98
+\begintext
+
+Vega
+['SIMBAD:', '* alf Lyr', '279.23473479', '+38.78368896', 'Variable Star of delta Sct type']
+
+\begindata
+NAIF_BODY_NAME += ( 'Vega' )
+NAIF_BODY_CODE += ( 8888001 )
+NH_TARGET_BODIES += ( 8888001 )
+BODY8888001_POLE_RA = ( 0. 0. 0. )
+BODY8888001_POLE_DEC = ( 90. 0. 0. )
+BODY8888001_PM = ( 270. 0. 0. )
+BODY8888001_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Vega:
+\begindata
+SITES += ( 'SITE8888001' )
+SITE8888001_FRAME = 'J2000'
+SITE8888001_IDCODE = 8888001
+SITE8888001_XYZ = ( 0.125096 -0.769413 0.626382 )
+SITE8888001_CENTER = -98
+\begintext
+
+gam Gru
+['SIMBAD:', '* gam Gru', '328.48219248', '-37.36485527', 'Star']
+
+\begindata
+NAIF_BODY_NAME += ( 'gam Gru' )
+NAIF_BODY_CODE += ( 8888002 )
+NH_TARGET_BODIES += ( 8888002 )
+BODY8888002_POLE_RA = ( 0. 0. 0. )
+BODY8888002_POLE_DEC = ( 90. 0. 0. )
+BODY8888002_PM = ( 270. 0. 0. )
+BODY8888002_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star gam Gru:
+\begindata
+SITES += ( 'SITE8888002' )
+SITE8888002_FRAME = 'J2000'
+SITE8888002_IDCODE = 8888002
+SITE8888002_XYZ = ( 0.677538 -0.415486 -0.606888 )
+SITE8888002_CENTER = -98
+\begintext
+
+RHOLEO (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'RHOLEO' )
+NAIF_BODY_CODE += ( 8888003 )
+\begintext
+
+rho Leo
+['SIMBAD:', '* rho Leo', '158.20279865', '+09.30658596', 'Blue supergiant star']
+
+\begindata
+NAIF_BODY_NAME += ( 'rho Leo' )
+NAIF_BODY_CODE += ( 8888003 )
+NH_TARGET_BODIES += ( 8888003 )
+BODY8888003_POLE_RA = ( 0. 0. 0. )
+BODY8888003_POLE_DEC = ( 90. 0. 0. )
+BODY8888003_PM = ( 270. 0. 0. )
+BODY8888003_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star rho Leo:
+\begindata
+SITES += ( 'SITE8888003' )
+SITE8888003_FRAME = 'J2000'
+SITE8888003_IDCODE = 8888003
+SITE8888003_XYZ = ( -0.916282 0.366435 0.161717 )
+SITE8888003_CENTER = -98
+\begintext
+
+M6M7 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'M6M7' )
+NAIF_BODY_CODE += ( 8888004 )
+\begintext
+
+M 7 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'M 7' )
+NAIF_BODY_CODE += ( 8888004 )
+\begintext
+
+M7
+['SIMBAD:', 'NGC 6475', '268.463', '-34.793', 'Open (galactic) Cluster']
+
+\begindata
+NAIF_BODY_NAME += ( 'M7' )
+NAIF_BODY_CODE += ( 8888004 )
+NH_TARGET_BODIES += ( 8888004 )
+BODY8888004_POLE_RA = ( 0. 0. 0. )
+BODY8888004_POLE_DEC = ( 90. 0. 0. )
+BODY8888004_PM = ( 270. 0. 0. )
+BODY8888004_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star M7:
+\begindata
+SITES += ( 'SITE8888004' )
+SITE8888004_FRAME = 'J2000'
+SITE8888004_IDCODE = 8888004
+SITE8888004_XYZ = ( -0.022027 -0.820923 -0.570613 )
+SITE8888004_CENTER = -98
+\begintext
+
+Spica
+['SIMBAD:', '* alf Vir', '201.29824736', '-11.16131949', 'Variable Star of beta Cep type']
+
+\begindata
+NAIF_BODY_NAME += ( 'Spica' )
+NAIF_BODY_CODE += ( 8888005 )
+NH_TARGET_BODIES += ( 8888005 )
+BODY8888005_POLE_RA = ( 0. 0. 0. )
+BODY8888005_POLE_DEC = ( 90. 0. 0. )
+BODY8888005_PM = ( 270. 0. 0. )
+BODY8888005_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Spica:
+\begindata
+SITES += ( 'SITE8888005' )
+SITE8888005_FRAME = 'J2000'
+SITE8888005_IDCODE = 8888005
+SITE8888005_XYZ = ( -0.914080 -0.356353 -0.193572 )
+SITE8888005_CENTER = -98
+\begintext
+
+HD93521 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'HD93521' )
+NAIF_BODY_CODE += ( 8888006 )
+\begintext
+
+HD 93521
+['SIMBAD:', 'HD 93521', '162.09796404', '+37.57030340', 'Star']
+
+\begindata
+NAIF_BODY_NAME += ( 'HD 93521' )
+NAIF_BODY_CODE += ( 8888006 )
+NH_TARGET_BODIES += ( 8888006 )
+BODY8888006_POLE_RA = ( 0. 0. 0. )
+BODY8888006_POLE_DEC = ( 90. 0. 0. )
+BODY8888006_PM = ( 270. 0. 0. )
+BODY8888006_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star HD 93521:
+\begindata
+SITES += ( 'SITE8888006' )
+SITE8888006_FRAME = 'J2000'
+SITE8888006_IDCODE = 8888006
+SITE8888006_XYZ = ( -0.754231 0.243639 0.609734 )
+SITE8888006_CENTER = -98
+\begintext
+
+Interplanetary Medium (IPM); 51.3; 44.8; ECLIPJ2000; RADEC
+
+\begindata
+NAIF_BODY_NAME += ( 'Interplanetary Medium (IPM)' )
+NAIF_BODY_CODE += ( 8888007 )
+NH_TARGET_BODIES += ( 8888007 )
+BODY8888007_POLE_RA = ( 0. 0. 0. )
+BODY8888007_POLE_DEC = ( 90. 0. 0. )
+BODY8888007_PM = ( 270. 0. 0. )
+BODY8888007_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Interplanetary Medium (IPM):
+\begindata
+SITES += ( 'SITE8888007' )
+SITE8888007_FRAME = 'J2000'
+SITE8888007_IDCODE = 8888007
+SITE8888007_XYZ = ( 0.443654 0.227787 0.866767 )
+SITE8888007_CENTER = -98
+\begintext
+
+NGC3532 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'NGC3532' )
+NAIF_BODY_CODE += ( 8888008 )
+\begintext
+
+NGC 3532
+['SIMBAD:', 'NGC 3532', '166.413', '-58.753', 'Open (galactic) Cluster']
+
+\begindata
+NAIF_BODY_NAME += ( 'NGC 3532' )
+NAIF_BODY_CODE += ( 8888008 )
+NH_TARGET_BODIES += ( 8888008 )
+BODY8888008_POLE_RA = ( 0. 0. 0. )
+BODY8888008_POLE_DEC = ( 90. 0. 0. )
+BODY8888008_PM = ( 270. 0. 0. )
+BODY8888008_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star NGC 3532:
+\begindata
+SITES += ( 'SITE8888008' )
+SITE8888008_FRAME = 'J2000'
+SITE8888008_IDCODE = 8888008
+SITE8888008_XYZ = ( -0.504212 0.121861 -0.854939 )
+SITE8888008_CENTER = -98
+\begintext
+
+Arcturus
+['SIMBAD:', '* alf Boo', '213.91530029', '+19.18240916', 'Red Giant Branch star']
+
+\begindata
+NAIF_BODY_NAME += ( 'Arcturus' )
+NAIF_BODY_CODE += ( 8888009 )
+NH_TARGET_BODIES += ( 8888009 )
+BODY8888009_POLE_RA = ( 0. 0. 0. )
+BODY8888009_POLE_DEC = ( 90. 0. 0. )
+BODY8888009_PM = ( 270. 0. 0. )
+BODY8888009_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Arcturus:
+\begindata
+SITES += ( 'SITE8888009' )
+SITE8888009_FRAME = 'J2000'
+SITE8888009_IDCODE = 8888009
+SITE8888009_XYZ = ( -0.783787 -0.526987 0.328577 )
+SITE8888009_CENTER = -98
+\begintext
+
+HD214168 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'HD214168' )
+NAIF_BODY_CODE += ( 8888010 )
+\begintext
+
+HD 214168
+['SIMBAD:', '* 8 Lac B', '338.96711542', '+39.62813397', 'Star']
+
+\begindata
+NAIF_BODY_NAME += ( 'HD 214168' )
+NAIF_BODY_CODE += ( 8888010 )
+NH_TARGET_BODIES += ( 8888010 )
+BODY8888010_POLE_RA = ( 0. 0. 0. )
+BODY8888010_POLE_DEC = ( 90. 0. 0. )
+BODY8888010_PM = ( 270. 0. 0. )
+BODY8888010_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star HD 214168:
+\begindata
+SITES += ( 'SITE8888010' )
+SITE8888010_FRAME = 'J2000'
+SITE8888010_IDCODE = 8888010
+SITE8888010_XYZ = ( 0.718885 -0.276428 0.637802 )
+SITE8888010_CENTER = -98
+\begintext
+
+10199 CHARIKLO; 2010199
+
+\begindata
+NAIF_BODY_NAME += ( '10199 CHARIKLO' )
+NAIF_BODY_CODE += ( 2010199 )
+NH_TARGET_BODIES += ( 2010199 )
+BODY2010199_POLE_RA = ( 0. 0. 0. )
+BODY2010199_POLE_DEC = ( 90. 0. 0. )
+BODY2010199_PM = ( 270. 0. 0. )
+BODY2010199_RADII = ( 100. 100. 100. )
+\begintext
+
+136472 MAKEMAKE; 2136472
+
+\begindata
+NAIF_BODY_NAME += ( '136472 MAKEMAKE' )
+NAIF_BODY_CODE += ( 2136472 )
+NH_TARGET_BODIES += ( 2136472 )
+BODY2136472_POLE_RA = ( 0. 0. 0. )
+BODY2136472_POLE_DEC = ( 90. 0. 0. )
+BODY2136472_PM = ( 270. 0. 0. )
+BODY2136472_RADII = ( 100. 100. 100. )
+\begintext
+
+136108 HAUMEA; 2136108
+
+\begindata
+NAIF_BODY_NAME += ( '136108 HAUMEA' )
+NAIF_BODY_CODE += ( 2136108 )
+NH_TARGET_BODIES += ( 2136108 )
+BODY2136108_POLE_RA = ( 0. 0. 0. )
+BODY2136108_POLE_DEC = ( 90. 0. 0. )
+BODY2136108_PM = ( 270. 0. 0. )
+BODY2136108_RADII = ( 100. 100. 100. )
+\begintext
+
+KERBEROS; 904
+
+\begindata
+NAIF_BODY_NAME += ( 'P4' 'KERBEROS' )
+NAIF_BODY_CODE += ( 904 904 )
+NH_TARGET_BODIES += ( 904 )
+BODY904_POLE_RA = ( 0. 0. 0. )
+BODY904_POLE_DEC = ( 90. 0. 0. )
+BODY904_PM = ( 270. 0. 0. )
+BODY904_RADII = ( 100. 100. 100. )
+\begintext
+
+STYX; 905
+
+\begindata
+NAIF_BODY_NAME += ( 'P5' 'STYX' )
+NAIF_BODY_CODE += ( 905 905 )
+NH_TARGET_BODIES += ( 905 )
+BODY905_POLE_RA = ( 0. 0. 0. )
+BODY905_POLE_DEC = ( 90. 0. 0. )
+BODY905_PM = ( 270. 0. 0. )
+BODY905_RADII = ( 100. 100. 100. )
+\begintext
+
+Bellatrix
+['SIMBAD:', '* gam Ori', '081.28276356', '+06.34970326', 'Variable Star']
+
+\begindata
+NAIF_BODY_NAME += ( 'Bellatrix' )
+NAIF_BODY_CODE += ( 8888011 )
+NH_TARGET_BODIES += ( 8888011 )
+BODY8888011_POLE_RA = ( 0. 0. 0. )
+BODY8888011_POLE_DEC = ( 90. 0. 0. )
+BODY8888011_PM = ( 270. 0. 0. )
+BODY8888011_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Bellatrix:
+\begindata
+SITES += ( 'SITE8888011' )
+SITE8888011_FRAME = 'J2000'
+SITE8888011_IDCODE = 8888011
+SITE8888011_XYZ = ( 0.150628 0.982385 0.110597 )
+SITE8888011_CENTER = -98
+\begintext
+
+Tau A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Tau A' )
+NAIF_BODY_CODE += ( 8888012 )
+\begintext
+
+Tau-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Tau-A' )
+NAIF_BODY_CODE += ( 8888012 )
+\begintext
+
+Taurus A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Taurus A' )
+NAIF_BODY_CODE += ( 8888012 )
+\begintext
+
+Taurus-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Taurus-A' )
+NAIF_BODY_CODE += ( 8888012 )
+\begintext
+
+M 1
+['SIMBAD:', 'M 1', '083.63308', '+22.01450', 'SuperNova Remnant']
+
+\begindata
+NAIF_BODY_NAME += ( 'M 1' )
+NAIF_BODY_CODE += ( 8888012 )
+NH_TARGET_BODIES += ( 8888012 )
+BODY8888012_POLE_RA = ( 0. 0. 0. )
+BODY8888012_POLE_DEC = ( 90. 0. 0. )
+BODY8888012_PM = ( 270. 0. 0. )
+BODY8888012_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star M 1:
+\begindata
+SITES += ( 'SITE8888012' )
+SITE8888012_FRAME = 'J2000'
+SITE8888012_IDCODE = 8888012
+SITE8888012_XYZ = ( 0.102810 0.921371 0.374841 )
+SITE8888012_CENTER = -98
+\begintext
+
+HD205905 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'HD205905' )
+NAIF_BODY_CODE += ( 8888013 )
+\begintext
+
+HD 205905
+['SIMBAD:', 'HD 205905', '324.79229796', '-27.30657448', 'Pre-main sequence Star']
+
+\begindata
+NAIF_BODY_NAME += ( 'HD 205905' )
+NAIF_BODY_CODE += ( 8888013 )
+NH_TARGET_BODIES += ( 8888013 )
+BODY8888013_POLE_RA = ( 0. 0. 0. )
+BODY8888013_POLE_DEC = ( 90. 0. 0. )
+BODY8888013_PM = ( 270. 0. 0. )
+BODY8888013_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star HD 205905:
+\begindata
+SITES += ( 'SITE8888013' )
+SITE8888013_FRAME = 'J2000'
+SITE8888013_IDCODE = 8888013
+SITE8888013_XYZ = ( 0.726017 -0.512295 -0.458752 )
+SITE8888013_CENTER = -98
+\begintext
+
+HD37962 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'HD37962' )
+NAIF_BODY_CODE += ( 8888014 )
+\begintext
+
+HD 37962
+['SIMBAD:', 'HD 37962', '085.21652848', '-31.35110766', 'High proper-motion Star']
+
+\begindata
+NAIF_BODY_NAME += ( 'HD 37962' )
+NAIF_BODY_CODE += ( 8888014 )
+NH_TARGET_BODIES += ( 8888014 )
+BODY8888014_POLE_RA = ( 0. 0. 0. )
+BODY8888014_POLE_DEC = ( 90. 0. 0. )
+BODY8888014_PM = ( 270. 0. 0. )
+BODY8888014_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star HD 37962:
+\begindata
+SITES += ( 'SITE8888014' )
+SITE8888014_FRAME = 'J2000'
+SITE8888014_IDCODE = 8888014
+SITE8888014_XYZ = ( 0.071215 0.851021 -0.520281 )
+SITE8888014_CENTER = -98
+\begintext
+
+Cygnus-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Cygnus-A' )
+NAIF_BODY_CODE += ( 8888015 )
+\begintext
+
+Cygnus A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Cygnus A' )
+NAIF_BODY_CODE += ( 8888015 )
+\begintext
+
+Cyg-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Cyg-A' )
+NAIF_BODY_CODE += ( 8888015 )
+\begintext
+
+Cyg A
+['SIMBAD:', 'NAME Cyg A', '299.86815263', '+40.73391583', 'Seyfert 2 Galaxy']
+
+\begindata
+NAIF_BODY_NAME += ( 'Cyg A' )
+NAIF_BODY_CODE += ( 8888015 )
+NH_TARGET_BODIES += ( 8888015 )
+BODY8888015_POLE_RA = ( 0. 0. 0. )
+BODY8888015_POLE_DEC = ( 90. 0. 0. )
+BODY8888015_PM = ( 270. 0. 0. )
+BODY8888015_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Cyg A:
+\begindata
+SITES += ( 'SITE8888015' )
+SITE8888015_FRAME = 'J2000'
+SITE8888015_IDCODE = 8888015
+SITE8888015_XYZ = ( 0.377363 -0.657099 0.652547 )
+SITE8888015_CENTER = -98
+\begintext
+
+Cass A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Cass A' )
+NAIF_BODY_CODE += ( 8888016 )
+\begintext
+
+Cass-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Cass-A' )
+NAIF_BODY_CODE += ( 8888016 )
+\begintext
+
+Cas-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Cas-A' )
+NAIF_BODY_CODE += ( 8888016 )
+\begintext
+
+Cas A
+['SIMBAD:', 'NAME Cassiopeia A', '350.850000', '+58.815000', 'SuperNova Remnant']
+
+\begindata
+NAIF_BODY_NAME += ( 'Cas A' )
+NAIF_BODY_CODE += ( 8888016 )
+NH_TARGET_BODIES += ( 8888016 )
+BODY8888016_POLE_RA = ( 0. 0. 0. )
+BODY8888016_POLE_DEC = ( 90. 0. 0. )
+BODY8888016_PM = ( 270. 0. 0. )
+BODY8888016_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star Cas A:
+\begindata
+SITES += ( 'SITE8888016' )
+SITE8888016_FRAME = 'J2000'
+SITE8888016_IDCODE = 8888016
+SITE8888016_XYZ = ( 0.511214 -0.082341 0.855500 )
+SITE8888016_CENTER = -98
+\begintext
+
+Vir-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Vir-A' )
+NAIF_BODY_CODE += ( 8888017 )
+\begintext
+
+Vir A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Vir A' )
+NAIF_BODY_CODE += ( 8888017 )
+\begintext
+
+Virgo-A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Virgo-A' )
+NAIF_BODY_CODE += ( 8888017 )
+\begintext
+
+Virgo A (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'Virgo A' )
+NAIF_BODY_CODE += ( 8888017 )
+\begintext
+
+M87 (alternate name)
+
+\begindata
+NAIF_BODY_NAME += ( 'M87' )
+NAIF_BODY_CODE += ( 8888017 )
+\begintext
+
+M 87
+['SIMBAD:', 'M 87', '187.70593075', '+12.39112331', 'LINER-type Active Galaxy Nucleus']
+
+\begindata
+NAIF_BODY_NAME += ( 'M 87' )
+NAIF_BODY_CODE += ( 8888017 )
+NH_TARGET_BODIES += ( 8888017 )
+BODY8888017_POLE_RA = ( 0. 0. 0. )
+BODY8888017_POLE_DEC = ( 90. 0. 0. )
+BODY8888017_PM = ( 270. 0. 0. )
+BODY8888017_RADII = ( 100. 100. 100. )
+\begintext
+
+PINPOINT parameters for star M 87:
+\begindata
+SITES += ( 'SITE8888017' )
+SITE8888017_FRAME = 'J2000'
+SITE8888017_IDCODE = 8888017
+SITE8888017_XYZ = ( -0.967885 -0.130965 0.214584 )
+SITE8888017_CENTER = -98
+\begintext
+
+1994JR1; 2015810
+
+\begindata
+NAIF_BODY_NAME += ( '1994JR1' )
+NAIF_BODY_CODE += ( 2015810 )
+\begintext
+
+1994_JR1; 2015810
+
+\begindata
+NAIF_BODY_NAME += ( '1994_JR1' )
+NAIF_BODY_CODE += ( 2015810 )
+\begintext
+
+1994 JR1; 2015810
+
+\begindata
+NAIF_BODY_NAME += ( '1994 JR1' )
+NAIF_BODY_CODE += ( 2015810 )
+\begintext
+
+JR1; 2015810
+
+\begindata
+NAIF_BODY_NAME += ( 'JR1' )
+NAIF_BODY_CODE += ( 2015810 )
+\begintext
+
+ARAWN; 2015810
+
+\begindata
+NAIF_BODY_NAME += ( 'ARAWN' )
+NAIF_BODY_CODE += ( 2015810 )
+\begintext
+
+15810 ARAWN; 2015810
+
+\begindata
+NAIF_BODY_NAME += ( '15810 ARAWN' )
+NAIF_BODY_CODE += ( 2015810 )
+\begintext
+
+15810 ARAWN (1994 JR1); 2015810
+
+\begindata
+NAIF_BODY_NAME += ( '15810 ARAWN (1994 JR1)' )
+NAIF_BODY_CODE += ( 2015810 )
+NH_TARGET_BODIES += ( 2015810 )
+BODY2015810_POLE_RA = ( 0. 0. 0. )
+BODY2015810_POLE_DEC = ( 90. 0. 0. )
+BODY2015810_PM = ( 270. 0. 0. )
+BODY2015810_RADII = ( 100. 100. 100. )
+\begintext
+
+2010JJ124; 3523335
+
+\begindata
+NAIF_BODY_NAME += ( '2010JJ124' )
+NAIF_BODY_CODE += ( 3523335 )
+\begintext
+
+2010_JJ124; 3523335
+
+\begindata
+NAIF_BODY_NAME += ( '2010_JJ124' )
+NAIF_BODY_CODE += ( 3523335 )
+\begintext
+
+2010 JJ124; 3523335
+
+\begindata
+NAIF_BODY_NAME += ( '2010 JJ124' )
+NAIF_BODY_CODE += ( 3523335 )
+\begintext
+
+JJ124; 3523335
+
+\begindata
+NAIF_BODY_NAME += ( 'JJ124' )
+NAIF_BODY_CODE += ( 3523335 )
+\begintext
+
+523335 (2010 JJ124); 3523335
+
+\begindata
+NAIF_BODY_NAME += ( '523335 (2010 JJ124)' )
+NAIF_BODY_CODE += ( 3523335 )
+\begintext
+
+2010 JJ124; 3523335
+
+\begindata
+NAIF_BODY_NAME += ( '2010 JJ124' )
+NAIF_BODY_CODE += ( 3523335 )
+NH_TARGET_BODIES += ( 3523335 )
+BODY3523335_POLE_RA = ( 0. 0. 0. )
+BODY3523335_POLE_DEC = ( 90. 0. 0. )
+BODY3523335_PM = ( 270. 0. 0. )
+BODY3523335_RADII = ( 100. 100. 100. )
+\begintext
+
+1977UB; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( '1977UB' )
+NAIF_BODY_CODE += ( 2002060 )
+\begintext
+
+1977_UB; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( '1977_UB' )
+NAIF_BODY_CODE += ( 2002060 )
+\begintext
+
+1977 UB; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( '1977 UB' )
+NAIF_BODY_CODE += ( 2002060 )
+\begintext
+
+2060CHIRON; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( '2060CHIRON' )
+NAIF_BODY_CODE += ( 2002060 )
+\begintext
+
+2060_CHIRON; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( '2060_CHIRON' )
+NAIF_BODY_CODE += ( 2002060 )
+\begintext
+
+CHIRON; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( 'CHIRON' )
+NAIF_BODY_CODE += ( 2002060 )
+\begintext
+
+2060 CHIRON; 2002060
+
+\begindata
+NAIF_BODY_NAME += ( '2060 CHIRON' )
+NAIF_BODY_CODE += ( 2002060 )
+NH_TARGET_BODIES += ( 2002060 )
+BODY2002060_POLE_RA = ( 0. 0. 0. )
+BODY2002060_POLE_DEC = ( 90. 0. 0. )
+BODY2002060_PM = ( 270. 0. 0. )
+BODY2002060_RADII = ( 100. 100. 100. )
+\begintext
+
+2001KX76; 2028978
+
+\begindata
+NAIF_BODY_NAME += ( '2001KX76' )
+NAIF_BODY_CODE += ( 2028978 )
+\begintext
+
+2001_KX76; 2028978
+
+\begindata
+NAIF_BODY_NAME += ( '2001_KX76' )
+NAIF_BODY_CODE += ( 2028978 )
+\begintext
+
+2001 KX76; 2028978
+
+\begindata
+NAIF_BODY_NAME += ( '2001 KX76' )
+NAIF_BODY_CODE += ( 2028978 )
+\begintext
+
+KX76; 2028978
+
+\begindata
+NAIF_BODY_NAME += ( 'KX76' )
+NAIF_BODY_CODE += ( 2028978 )
+\begintext
+
+IXION; 2028978
+
+\begindata
+NAIF_BODY_NAME += ( 'IXION' )
+NAIF_BODY_CODE += ( 2028978 )
+\begintext
+
+28978 IXION; 2028978
+
+\begindata
+NAIF_BODY_NAME += ( '28978 IXION' )
+NAIF_BODY_CODE += ( 2028978 )
+\begintext
+
+28978 IXION (2001 KX76); 2028978
+
+\begindata
+NAIF_BODY_NAME += ( '28978 IXION (2001 KX76)' )
+NAIF_BODY_CODE += ( 2028978 )
+NH_TARGET_BODIES += ( 2028978 )
+BODY2028978_POLE_RA = ( 0. 0. 0. )
+BODY2028978_POLE_DEC = ( 90. 0. 0. )
+BODY2028978_PM = ( 270. 0. 0. )
+BODY2028978_RADII = ( 100. 100. 100. )
+\begintext
+
+2002MS4; 2307261
+
+\begindata
+NAIF_BODY_NAME += ( '2002MS4' )
+NAIF_BODY_CODE += ( 2307261 )
+\begintext
+
+2002_MS4; 2307261
+
+\begindata
+NAIF_BODY_NAME += ( '2002_MS4' )
+NAIF_BODY_CODE += ( 2307261 )
+\begintext
+
+2002 MS4; 2307261
+
+\begindata
+NAIF_BODY_NAME += ( '2002 MS4' )
+NAIF_BODY_CODE += ( 2307261 )
+\begintext
+
+MS4; 2307261
+
+\begindata
+NAIF_BODY_NAME += ( 'MS4' )
+NAIF_BODY_CODE += ( 2307261 )
+\begintext
+
+307261 (2002 MS4); 2307261
+
+\begindata
+NAIF_BODY_NAME += ( '307261 (2002 MS4)' )
+NAIF_BODY_CODE += ( 2307261 )
+\begintext
+
+ASTEROID 307261 (2002 MS4); 2307261
+
+\begindata
+NAIF_BODY_NAME += ( 'ASTEROID 307261 (2002 MS4)' )
+NAIF_BODY_CODE += ( 2307261 )
+NH_TARGET_BODIES += ( 2307261 )
+BODY2307261_POLE_RA = ( 0. 0. 0. )
+BODY2307261_POLE_DEC = ( 90. 0. 0. )
+BODY2307261_PM = ( 270. 0. 0. )
+BODY2307261_RADII = ( 100. 100. 100. )
+\begintext
+
+2002LM60; 2050000
+
+\begindata
+NAIF_BODY_NAME += ( '2002LM60' )
+NAIF_BODY_CODE += ( 2050000 )
+\begintext
+
+2002_LM60; 2050000
+
+\begindata
+NAIF_BODY_NAME += ( '2002_LM60' )
+NAIF_BODY_CODE += ( 2050000 )
+\begintext
+
+2002 LM60; 2050000
+
+\begindata
+NAIF_BODY_NAME += ( '2002 LM60' )
+NAIF_BODY_CODE += ( 2050000 )
+\begintext
+
+LM60; 2050000
+
+\begindata
+NAIF_BODY_NAME += ( 'LM60' )
+NAIF_BODY_CODE += ( 2050000 )
+\begintext
+
+QUAOAR; 2050000
+
+\begindata
+NAIF_BODY_NAME += ( 'QUAOAR' )
+NAIF_BODY_CODE += ( 2050000 )
+\begintext
+
+50000 QUAOAR; 2050000
+
+\begindata
+NAIF_BODY_NAME += ( '50000 QUAOAR' )
+NAIF_BODY_CODE += ( 2050000 )
+\begintext
+
+50000 QUAOAR (2002 LM60); 2050000
+
+\begindata
+NAIF_BODY_NAME += ( '50000 QUAOAR (2002 LM60)' )
+NAIF_BODY_CODE += ( 2050000 )
+NH_TARGET_BODIES += ( 2050000 )
+BODY2050000_POLE_RA = ( 0. 0. 0. )
+BODY2050000_POLE_DEC = ( 90. 0. 0. )
+BODY2050000_PM = ( 270. 0. 0. )
+BODY2050000_RADII = ( 100. 100. 100. )
+\begintext
+
+2014MU69; 3713011
+
+\begindata
+NAIF_BODY_NAME += ( '2014MU69' )
+NAIF_BODY_CODE += ( 3713011 )
+\begintext
+
+2014_MU69; 3713011
+
+\begindata
+NAIF_BODY_NAME += ( '2014_MU69' )
+NAIF_BODY_CODE += ( 3713011 )
+\begintext
+
+2014 MU69; 3713011
+
+\begindata
+NAIF_BODY_NAME += ( '2014 MU69' )
+NAIF_BODY_CODE += ( 3713011 )
+\begintext
+
+MU69; 3713011
+
+\begindata
+NAIF_BODY_NAME += ( 'MU69' )
+NAIF_BODY_CODE += ( 3713011 )
+\begintext
+
+486958 (2014 MU69); 3713011
+
+\begindata
+NAIF_BODY_NAME += ( '486958 (2014 MU69)' )
+NAIF_BODY_CODE += ( 3713011 )
+\begintext
+
+ASTEROID 486958 (2014 MU69); 3713011
+
+\begindata
+NAIF_BODY_NAME += ( 'ASTEROID 486958 (2014 MU69)' )
+NAIF_BODY_CODE += ( 3713011 )
+NH_TARGET_BODIES += ( 3713011 )
+BODY3713011_POLE_RA = ( 0. 0. 0. )
+BODY3713011_POLE_DEC = ( 90. 0. 0. )
+BODY3713011_PM = ( 270. 0. 0. )
+BODY3713011_RADII = ( 100. 100. 100. )
+\begintext
+
+::GUARD::; 390; last element is guard
+
+\begindata
+NAIF_BODY_NAME += ( '::GUARD::' )
+NAIF_BODY_CODE += ( 390 )
+NH_TARGET_BODIES += ( 390 )
+BODY390_POLE_RA = ( 0. 0. 0. )
+BODY390_POLE_DEC = ( 90. 0. 0. )
+BODY390_PM = ( 270. 0. 0. )
+BODY390_RADII = ( 100. 100. 100. )
+\begintext
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_v220.tf b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_v220.tf
new file mode 100644
index 0000000000000000000000000000000000000000..30d8a699b68bfe189fb683986f6e9a554c865262
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/nh_v220.tf
@@ -0,0 +1,2841 @@
+KPL/FK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "nh_v220.tf"
+MISSION_NAME = "NEW HORIZONS"
+SPACECRAFT_NAME = "NEW HORIZONS"
+DATA_SET_ID = "NH-J/P/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = FK
+PRODUCT_ID = "nh_v220.tf"
+PRODUCT_CREATION_TIME = 2014-07-01T00:00:00
+PRODUCER_ID = "APL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = {
+ JUPITER,
+ PLUTO,
+ "SOLAR SYSTEM"
+ }
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = FRAMES
+ DESCRIPTION = "NH frames kernel"
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+KPL/FK
+
+New Horizons Spacecraft Frames Kernel
+===============================================================================
+
+ This frame kernel contains the New Horizons spacecraft and science
+ instruments.
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ The TEXT_KERNEL_ID stores version information of loaded project text
+ kernels. Each entry associated with the keyword is a string that consists
+ of four parts: the kernel name, version, entry date, and type. For example,
+ the frames kernel might have an entry as follows:
+
+ TEXT_KERNEL_ID += 'NEWHORIZONS V1.0.0 22-FEBRUARY-2007 IK'
+ | | | |
+ | | | |
+ KERNEL NAME <-------+ | | |
+ | | V
+ VERSION <-------+ | KERNEL TYPE
+ |
+ V
+ ENTRY DATE
+
+ New Horizons Frame Kernel Version:
+
+ \begindata
+
+ TEXT_KERNEL_ID += 'NEWHORIZONS_FRAMES V2.2.0 16-OCT-2012 FK'
+
+ NAIF_BODY_NAME += ( 'NEW_HORIZONS' )
+ NAIF_BODY_CODE += ( -98 )
+
+ NAIF_BODY_NAME += ( 'NH' )
+ NAIF_BODY_CODE += ( -98 )
+
+ NAIF_BODY_NAME += ( 'NH_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -98 )
+
+ \begintext
+
+ Version 2.2.0 -- October 16, 2012 -- Lillian Nguyen, JHU/APL
+
+ -- Updated the Alice airglow frame with in-flight alignment values.
+
+ Version 2.1.1 -- January 15, 2009 -- Lillian Nguyen, JHU/APL
+
+ -- Corrected typos in the text.
+
+ Version 2.1.0 -- January 7, 2009 -- Lillian Nguyen, JHU/APL
+
+ -- Updated the Alice SOC frame with in-flight alignment values.
+
+ Version 2.0.0 -- August 4, 2008 -- Lillian Nguyen, JHU/APL
+
+ -- Added frames for the two Autonomous Star Trackers and the
+ Fine Sun Sensor.
+
+ -- Updated the frames heirarchy and spacecraft diagram.
+
+ Version 1.1.3 -- May 21, 2008 -- Lillian Nguyen, JHU/APL
+
+ -- Added diagrams for Alice and Ralph describing the layout of
+ the detectors.
+
+ Version 1.1.2 -- April 15, 2008 -- Lillian Nguyen, JHU/APL
+
+ -- Updated the LORRI boresight based on in-flight data.
+
+ Version 1.1.1 -- March 18, 2008 -- Lillian Nguyen, JHU/APL
+
+ -- Rotated the SOC frame such that the instrument +Y axis is
+ at the center of the 2x2 degree portion of the slit rather
+ than at the optical center of the slit.
+
+ Version 1.1.0 -- July 12, 2007 -- Lillian Nguyen, JHU/APL
+
+ -- PEPSSI frame renamed and a new PEPSSI frame defining a
+ coordinate system axis relabelling created.
+ -- Individual frame created for each PEPSSI sector and detector.
+
+ Version 1.0.1 -- April 11, 2007 -- Lillian Nguyen, JHU/APL
+
+ -- Alice airglow frame was updated with higher precision values
+ and an additional rotation to shift the boresight.
+
+ Version 1.0.0 -- February 22, 2007 -- Lillian Nguyen, JHU/APL
+
+ -- Corrected spelling errors.
+ -- Modified the frames hierarchy diagram.
+ -- Clarified that the entire Alice slit is visible through
+ both Alice apertures and updated the field of view
+ definitions and diagrams appropriately.
+ -- Noted that the standard acronym for the Alice Solar
+ Occultation Channel is SOCC.
+ -- Removed NH_ASTR frame from NAIF body name to ID mapping.
+ -- Promoting to version 1.0.0 denoting approval of kernel set
+ by instrument teams.
+
+ Version 0.0.5 -- January 15, 2007 -- Lillian Nguyen, JHU/APL
+
+ -- Draft Version. NOT YET APPROVED BY ALL INSTRUMENT TEAMS.
+ -- Star tracker frame inserted between spacecraft frame and
+ nominal instrument frames to reflect a spacecraft frame
+ change due to a star tracker calibration.
+ -- LORRI frame definition changed according to instrument team.
+ -- Ralph frames defined for LEISA and for each MVIC focal plane
+ array.
+ -- Alice Airglow frame updated with in-flight values.
+
+ Version 0.0.4 -- October 4, 2006 -- Lillian Nguyen, JHU/APL
+
+ -- Draft Version. NOT YET APPROVED BY INSTRUMENT TEAMS.
+ -- Removed 3-letter frame names, updated frame tree.
+ -- Corrected the PEPSSI frame definition.
+
+ Version 0.0.3 -- April 4, 2006 -- Lillian Nguyen, JHU/APL
+
+ -- Draft Version. NOT YET APPROVED BY INSTRUMENT TEAMS.
+ -- Alice airglow and SOC frames redefined according to
+ orientation diagrams received from instrument team.
+ -- SWAP and PEPSSI frames added.
+ -- Ralph frames modified according to focal plane definitions
+ received from instrument team.
+
+ Version 0.0.2 -- January 25, 2006 -- Lillian Nguyen, JHU/APL
+
+ -- Draft Version. NOT YET APPROVED BY INSTRUMENT TEAMS.
+ -- Includes the addition of frames for REX and SDC.
+ -- LORRI frame redefined according to orientation diagram
+ received from instrument team.
+
+ Version 0.0.1 -- November 16, 2005 -- Lillian Nguyen, JHU/APL
+
+ -- Draft Version. NOT YET APPROVED BY INSTRUMENT TEAMS.
+
+ Version 0.0.0 -- August 13, 2005 -- Brian Carcich
+
+ -- Testing Kernel.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``C-kernel Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``Frames Required Reading''
+
+ 4. nh_v000.tf (placeholder New Horizon SPICE frames kernel),
+ provided by Brian Carcich and dated 2005-08-13.
+
+ 5. New Horizons Spacecraft Requirements Document, 7399-9004
+
+ 6. New Horizons Spacecraft Configuration Drawings,
+ 7399-0002_-_10-28-03.pdf (\\Aplfsfrontier\project\pluto)
+
+ 7. New Horizons Spacecraft to PERSI/RALPH Interface
+ Control Document, Rev B, 7399-9201.
+
+ 8. New Horizons System Alignment Report, 7399-9189, dated
+ 12 December, 2005.
+
+ 9. Instrument Vectors v2.xls (containing an update to
+ Table 12 of [8]), received in an e-mail from John Troll
+ dated 1/16/2006; and PEPSSI baffle vector, received in an
+ e-mail from John Troll on 2/8/2006.
+
+ 10. ``Rotation Required Reading''
+
+ 11. Alice Instrument Specification, 05310.02-ISPEC-01.
+
+ 12. Spacecraft to Alice Interface Control Document (ICD),
+ 7399-9046.
+
+ 13. Ralph Instrument Specification, Rev. A ECR SWRI 5310-001.
+
+ 14. LOng-Range Reconnaissance Imager (LORRI) User's Manual,
+ 7400-9601, dated Jan. 10, 2006.
+
+ 15. LORRI_orientation_1-9-06, received on 1/23/2006 by e-mail
+ from Hal Weaver along with a description of the LORRI frame
+ relative to the spacecraft frame. Also a phone conversation
+ with Hal clarifying the diagrams in the document.
+
+ 16. E-mail exchange with David James (Laboratory for Atmospheric
+ and Space Physics at the University of Colorado (LASP)),
+ Jan. 26, 2006 - Feb. 1, 2006.
+
+ 17. P-ALICE_Orientation_on_SC, received from Joel Parker in an
+ e-mail dated Jan. 25, 2006; discussions with Dave Slater on
+ Mar. 16 and 23, 2006, and e-mail exchange with Dave Slater on
+ Mar. 28-29, 2006 regarding the diagram.
+
+ 18. Pluto Energetic Particle Spectrometer Science Investigation
+ (PEPSSI) Interface Control Document, 7399-9049, Rev. C.
+
+ 19. E-mail dated Feb. 8, 2006 from John Troll containing measured
+ PEPSSI baffle vector.
+
+ 20. New Horizons Spacecraft to SWAP Interface Control Document,
+ 7399-9047 Rev. A.
+
+ 21. New Horizons Critical Design Review Science Payload slides.
+
+ 22. Document titled "RalphArrayPositions.doc", received from
+ Cathy Olkin by e-mail, Mar. 23, 2006, and e-mail exchange
+ concerning the document, Apr. 3-4, 2006.
+
+ 23. Ralph Instrument Specification, Rev. A ECR SWRI 5310-001.
+
+ 24. Discussions with Scott Turner regarding his analysis of
+ PEPSSI data containing evidence of sunlight.
+
+ 25. PEPSSI mounting bracket mechanical drawing, JHU/APL
+ document 7399-0151.
+
+ 26. E-mail from Scott Turner describing the PEPSSI mounting
+ specification.
+
+ 27. E-mail discussions among Gabe Rogers, Scott Turner, Hal
+ Weaver, and Howard Taylor concerning instrument boresight
+ changes caused by a star tracker calibration.
+
+ 28. "AST1_SPIN_CAL.dat", received from Gabe Rogers on 12/4/2006.
+
+ 29. Discussions with Howard Taylor regarding LORRI instrument
+ frame definition and LORRI keywords, 12/21/2006.
+
+ 30. E-mail exchange with Cathy Olkin on MVIC coordinate system
+ and LEISA size.
+
+ 31. "RalphBoresights03.doc", received from Allen Lunsford
+ 2/2/2007.
+
+ 32. E-mail from Andrew Steffl regarding Alice pointing offsets,
+ received on 2/13/2007 and 3/22/2007.
+
+ 33. E-mail from Cathy Olkin regarding the removal of the
+ NH_RALPH_MVIC frame and the introduction of the NH_RALPH
+ frame, received 2/22/2007.
+
+ 34. E-mail from Maarten Versteeg clarifying that the entire
+ Alice slit is visible through both Alice apertures, received
+ 2/22/2007, and from Joel Parker confirming that we should
+ change the Alice fields of view to the entire lollipop-shaped
+ slit, received 2/28/2007.
+
+ 35. Telephone conversation with Hal Weaver about the Alice
+ instrument.
+
+ 36. Discussion with Jon Vandegriff and Larry Brown about the
+ PEPSSI frames and fields of view, 6/21/2007.
+
+ 37. E-mails from Henry Throop received on 2/6/2008 and 2/20/2008.
+
+ 38. E-mails from Hal Weaver received on 4/9/2008 and 4/15/2008.
+
+ 39. E-mails from Andrew Steffl containing optical and detector
+ parameters and detector layout information for Ralph,
+ received between 3/12/2008 and 5/21/2008.
+
+ 40. E-mail from Gabe Rogers received on 6/30/2008 containing
+ spacecraft to body matrices and fields of view for the star
+ trackers and sun sensor.
+
+ 41. 'Autonomous Star Tracker Performance for the New Horizons
+ Mission', AIAA/AAS Astrodynamics Specialist Conference,
+ Keystone, CO, August 21-24 2006.
+
+ 42. E-mail regarding Alice SOC alignment, received from
+ Andrew Steffl on 11/18/2008.
+
+ 43. E-mail regarding Alice airglow alignment, received from
+ Andrew Steffl on 9/28/2012.
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Lillian Nguyen, JHU/APL, (443)-778-5477, Lillian.Nguyen@jhuapl.edu
+
+
+Implementation Notes
+-------------------------------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make use of
+ this instrument kernel must ``load'' the kernel, normally during program
+ initialization. Loading the kernel associates data items with their names
+ in a data structure called the ``kernel pool''. The SPICELIB routine FURNSH,
+ CSPICE routine furnsh_c, and IDL routine cspice_furnsh load SPICE kernels
+ as shown below:
+
+ FORTRAN (SPICELIB)
+
+ CALL FURNSH ( 'kernel_name' )
+
+ C (CSPICE)
+
+ furnsh_c ( "kernel_name" )
+
+ ICY (IDL)
+
+ cspice_furnsh, 'kernel_name'
+
+ In order for a program or subroutine to extract data from the pool, the
+ SPICELIB routines GDPOOL, GCPOOL, and GIPOOL are used. See [2] for details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+New Horizons Frames
+-------------------------------------------------------------------------------
+
+ The following New Horizons frames are defined in this kernel file:
+
+ Frame Name Relative To Type NAIF ID
+ ======================= =================== ======= =======
+
+ Spacecraft frames:
+ -----------------------------------
+ NH_SPACECRAFT J2000 CK -98000
+ NH_ASTR NH_SPACECRAFT FIXED -98001
+ NH_STAR_TRACKER_1 NH_SPACECRAFT FIXED -98010
+ NH_STAR_TRACKER_2 NH_SPACECRAFT FIXED -98011
+ NH_FINE_SUN_SENSOR NH_SPACECRAFT FIXED -98012
+
+ Alice Frames (-981xx):
+ -----------------------------------
+ NH_ALICE_SOC NH_ASTR FIXED -98100
+ NH_ALICE_AIRGLOW NH_SPACECRAFT FIXED -98101
+
+ RALPH Frames (-982xx):
+ -----------------------------------
+ NH_RALPH NH_RALPH_MVIC_FT FIXED -98200
+ NH_RALPH_LEISA NH_SPACECRAFT FIXED -98201
+ NH_RALPH_SIA NH_ASTR FIXED -98202
+ NH_RALPH_MVIC_FT NH_SPACECRAFT FIXED -98203
+ NH_RALPH_MVIC_PAN2 NH_SPACECRAFT FIXED -98204
+ NH_RALPH_MVIC_PAN1 NH_SPACECRAFT FIXED -98205
+ NH_RALPH_MVIC_RED NH_SPACECRAFT FIXED -98206
+ NH_RALPH_MVIC_BLUE NH_SPACECRAFT FIXED -98207
+ NH_RALPH_MVIC_METHANE NH_SPACECRAFT FIXED -98208
+ NH_RALPH_MVIC_NIR NH_SPACECRAFT FIXED -98209
+
+ LORRI Frames (-983xx):
+ -----------------------------------
+ NH_LORRI NH_SPACECRAFT FIXED -98300
+ NH_LORRI_1X1 NH_LORRI FIXED -98301
+ NH_LORRI_4X4 NH_LORRI FIXED -98302
+
+ PEPSSI Frames (-984xx):
+ -----------------------------------
+ NH_PEPSSI_ENG NH_ASTR FIXED -98400
+ NH_PEPSSI NH_PEPSSI_ENG FIXED -98401
+ NH_PEPSSI_S0 NH_PEPSSI FIXED -98402
+ NH_PEPSSI_S1 NH_PEPSSI FIXED -98403
+ NH_PEPSSI_S2 NH_PEPSSI FIXED -98404
+ NH_PEPSSI_S3 NH_PEPSSI FIXED -98405
+ NH_PEPSSI_S4 NH_PEPSSI FIXED -98406
+ NH_PEPSSI_S5 NH_PEPSSI FIXED -98407
+ NH_PEPSSI_D0 NH_PEPSSI FIXED -98408
+ NH_PEPSSI_D1 NH_PEPSSI FIXED -98409
+ NH_PEPSSI_D2 NH_PEPSSI FIXED -98410
+ NH_PEPSSI_D3 NH_PEPSSI FIXED -98411
+ NH_PEPSSI_D4 NH_PEPSSI FIXED -98412
+ NH_PEPSSI_D5 NH_PEPSSI FIXED -98413
+ NH_PEPSSI_D6 NH_PEPSSI FIXED -98414
+ NH_PEPSSI_D7 NH_PEPSSI FIXED -98415
+ NH_PEPSSI_D8 NH_PEPSSI FIXED -98416
+ NH_PEPSSI_D9 NH_PEPSSI FIXED -98417
+ NH_PEPSSI_D10 NH_PEPSSI FIXED -98418
+ NH_PEPSSI_D11 NH_PEPSSI FIXED -98419
+
+ REX Frames (-985xx):
+ -----------------------------------
+ NH_REX NH_ASTR FIXED -98500
+
+ SWAP Frames (-986xx):
+ -----------------------------------
+ NH_SWAP NH_ASTR FIXED -98600
+
+ SDC Frames (-987xx):
+ -----------------------------------
+ NH_SDC NH_ASTR FIXED -98700
+
+
+New Horizons Frames Hierarchy
+-------------------------------------------------------------------------------
+
+ The diagram below shows the New Horizons frames hierarchy:
+
+ 'J2000' INERTIAL
+ |
+ |<--- ck
+ |
+ 'NH_SPACECRAFT'
+ |
+ 'NH_STAR_TRACKER_1'
+ |
+ 'NH_STAR_TRACKER_2'
+ |
+ 'NH_FINE_SUN_SENSOR'
+ |
+ 'NH_RALPH_MVIC_FT'
+ | |
+ | 'NH_RALPH'
+ |
+ 'NH_RALPH_MVIC_PAN2'
+ |
+ 'NH_RALPH_MVIC_PAN1'
+ |
+ 'NH_RALPH_MVIC_RED'
+ |
+ 'NH_RALPH_MVIC_BLUE'
+ |
+ 'NH_RALPH_MVIC_METHANE'
+ |
+ 'NH_RALPH_MVIC_NIR'
+ |
+ 'NH_RALPH_LEISA'
+ |
+ 'NH_LORRI'
+ | |
+ | 'NH_LORRI_1X1'
+ | |
+ | 'NH_LORRI_4X4'
+ |
+ 'NH_ALICE_AIRGLOW'
+ |
+ 'NH_ASTR'
+ |
+ 'NH_ALICE_SOC'
+ |
+ 'NH_RALPH_SIA'
+ |
+ 'NH_PEPSSI_ENG'
+ | |
+ | 'NH_PEPSSI'
+ | |
+ | 'NH_PEPSSI_S0'
+ | |
+ | 'NH_PEPSSI_S1'
+ | |
+ | 'NH_PEPSSI_S2'
+ | |
+ | 'NH_PEPSSI_S3'
+ | |
+ | 'NH_PEPSSI_S4'
+ | |
+ | 'NH_PEPSSI_S5'
+ | |
+ | 'NH_PEPSSI_D0'
+ | |
+ | 'NH_PEPSSI_D1'
+ | |
+ | 'NH_PEPSSI_D2'
+ | |
+ | 'NH_PEPSSI_D3'
+ | |
+ | 'NH_PEPSSI_D4'
+ | |
+ | 'NH_PEPSSI_D5'
+ | |
+ | 'NH_PEPSSI_D6'
+ | |
+ | 'NH_PEPSSI_D7'
+ | |
+ | 'NH_PEPSSI_D8'
+ | |
+ | 'NH_PEPSSI_D9'
+ | |
+ | 'NH_PEPSSI_D10'
+ | |
+ | 'NH_PEPSSI_D11'
+ |
+ 'NH_REX'
+ |
+ 'NH_SWAP'
+ |
+ 'NH_SDC'
+
+
+
+Spacecraft Frame
+-------------------------------------------------------------------------------
+
+ From [5]: (Note: The figures referenced below can not be reproduced here.
+ There is a diagram below that basically illustrates what is contained
+ there.)
+
+ ``Figure 3.1.1-1 shows the New Horizons observatory and its coordinate
+ system. This coordinate system shall be the only coordinate system
+ used for all observatory-level hardware and software development.
+ Nominal thrust direction for an Atlas V or Delta IV launch is in the
+ +Y direction. Positive observatory roll is defined as a right handed
+ rotation about the +X axis, positive pitch is defined a right handed
+ rotation about the +Z axis and positive yaw is defined as a right
+ handed rotation about the +Y axis. The origin of the coordinate
+ system is located at the center of the bottom of the observatory
+ adapter ring.''
+
+
+ +X view:
+ --------
+ o
+ /|\
+ / | \
+ / | \
+ / | \
+ / | \
+ / | \
+ ___________________/______|______\__________________
+ `-. HGA(REX) ,-'
+ `-. ,-'
+ `-. ,-' __
+ `-.____________________________,-' / / PEPSSI
+ __________/_\________________________/_\_____|___|
+ PERSI .-| | | |______
+ Alice | | | RTG | | ||
+ '-| | .-*-. | |_____|| SWAP
+ | | / \ | | ||
+ |----| | \ / | | ||
+ PERSI | | | "-.-" | |
+ Ralph |___ | | | |
+ | |________________|_______________|________________|
+ | +X (out of page)
+ /__<------o_________\
+ +Zsc | adapter ring
+ |
+ |
+ V
+ -Ysc
+
+
+
+
+ +Y view:
+ --------
+
+ ______
+ ------
+ || SWAP
+ ----
+ _|__|______ __..---..__
+ | | \ _`-' ``-. HGA(REX)
+ PEPSSI | ---- _' `-_ `-.
+ | .' `-_ `.
+ .-| , `-_ `.
+ LORRI : | . `-_ `.
+ : | / `-_ \
+ '-|. `-_ . _______ _______
+ |' .-*-. `-_ ||+|+|+|+| |+|+|+|+|
+ | / \ `|--`-------------------|
+ | ! o-----> +X | | |
+ | \ | / _,|--.-------------------|
+ ASTR 1 \ |. "-|-" _,- ||+|+|+|+| |+|+|+|+|
+ \\|' | _,- ' ------- -------
+ Star \| ' V _,- / RTG (Radioisotope
+ Trackers | ` +Z _,- . Thermoelectric
+ /| ` _,- - Generator)
+ //| `. _,- .'
+ ASTR 2 / | '. _,- _.-'
+ |__________',-__ __,,,''
+ | | '' --- ''
+ | |
+ `-----' PERSI (Alice above, Ralph below)
+
+
+
+ Since the S/C bus attitude with respect to an inertial frame is provided
+ by a C-kernel (see [1] for more information), this frame is defined as
+ a CK-based frame.
+
+ \begindata
+
+ FRAME_NH_SPACECRAFT = -98000
+ FRAME_-98000_NAME = 'NH_SPACECRAFT'
+ FRAME_-98000_CLASS = 3
+ FRAME_-98000_CLASS_ID = -98000
+ FRAME_-98000_CENTER = -98
+ CK_-98000_SCLK = -98
+ CK_-98000_SPK = -98
+
+ \begintext
+
+
+ASTR (autonomous star trackers) Frame
+-------------------------------------------------------------------------------
+
+ From [27], the definition of the spacecraft body frame changed after
+ launch due to a calibration in the ASTR (star tracker) alignments to the
+ principal axes. The star tracker boresight needed to be rotated relative
+ to the original orientation in the pre-flight calibration report [8]
+ in order to match the thruster firing directions with the spin axis of the
+ spacecraft (i.e., to the principal moment of inertia).
+
+ In order to rotate all of the instrument boresights by the same amount,
+ we introduce a frame taking vectors from the ASTR frame to the spacecraft
+ body frame. The nominal instrument frames will be linked to the ASTR frame
+ rather than to the spacecraft frame.
+
+ The ASTR to spacecraft body matrix is given [28] by:
+
+ [ 0.99998698852861 0.00510125214304 0.00000025156926 ]
+ DCM = [-0.00510125214304 0.99998698366466 0.00009862975258 ]
+ [ 0.00000025156926 -0.00009862975258 0.99999999513605 ]
+
+
+ \begindata
+
+ FRAME_NH_ASTR = -98001
+ FRAME_-98001_NAME = 'NH_ASTR'
+ FRAME_-98001_CLASS = 4
+ FRAME_-98001_CLASS_ID = -98001
+ FRAME_-98001_CENTER = -98
+ TKFRAME_-98001_SPEC = 'MATRIX'
+ TKFRAME_-98001_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98001_MATRIX = ( 0.99998698852861,
+ -0.00510125214304,
+ 0.00000025156926,
+ 0.00510125214304,
+ 0.99998698366466,
+ -0.00009862975258,
+ 0.00000025156926,
+ 0.00009862975258,
+ 0.99999999513605)
+
+ \begintext
+
+
+ New Horizons has two autonomous star trackers (ASTRs) on the spacecraft -X
+ panel. Their boresights are separated by 90 degrees [41]. The star tracker
+ to spacecraft body matrices are given in [40] as:
+
+ Star Tracker 1 =
+
+ [ 0.00509822454128 0.70789996418568 -0.70629430750392 ]
+ [ 0.99998695603811 -0.00339039616065 0.00382007428188 ]
+ [ 0.00030961293888 -0.70630457022434 -0.70790801536644 ]
+
+ Star Tracker 2 =
+
+ [ 0.00578813992901173 -0.705383466342775 -0.708802273448943 ]
+ [ 0.999982550630013 0.00492038051247466 0.00326929519670704 ]
+ [ 0.00118147011512493 -0.708808828433902 0.705399637696606 ],
+
+ which translates to the following frame definitions:
+
+ \begindata
+
+ FRAME_NH_STAR_TRACKER_1 = -98010
+ FRAME_-98010_NAME = 'NH_STAR_TRACKER_1'
+ FRAME_-98010_CLASS = 4
+ FRAME_-98010_CLASS_ID = -98010
+ FRAME_-98010_CENTER = -98
+ TKFRAME_-98010_SPEC = 'MATRIX'
+ TKFRAME_-98010_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98010_MATRIX = ( 0.00509822454128,
+ 0.99998695603811,
+ 0.00030961293888,
+ 0.70789996418568,
+ -0.00339039616065,
+ -0.70630457022434,
+ -0.70629430750392,
+ 0.00382007428188,
+ -0.70790801536644)
+
+ FRAME_NH_STAR_TRACKER_2 = -98011
+ FRAME_-98011_NAME = 'NH_STAR_TRACKER_2'
+ FRAME_-98011_CLASS = 4
+ FRAME_-98011_CLASS_ID = -98011
+ FRAME_-98011_CENTER = -98
+ TKFRAME_-98011_SPEC = 'MATRIX'
+ TKFRAME_-98011_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98011_MATRIX = ( 0.00578813992901173,
+ 0.999982550630013,
+ 0.00118147011512493,
+ -0.705383466342775,
+ 0.00492038051247466,
+ -0.708808828433902,
+ -0.708802273448943,
+ 0.00326929519670704,
+ 0.705399637696606)
+
+ \begintext
+
+
+Sun Sensor Frame
+-------------------------------------------------------------------------------
+
+ The Fine Sun Sensor to spacecraft body matrix is given in [40] as:
+
+ Fine Sun Sensor =
+
+ [ 0.702792970261541 0.711384357815347 0.0037863447564826 ]
+ [ -0.00276516946126598 -0.00259068940063707 0.999992821057371 ]
+ [ 0.711389060071083 -0.702798394836006 0.000146380002554562 ],
+
+ which translates to the following frame definition:
+
+ \begindata
+
+ FRAME_NH_FINE_SUN_SENSOR = -98012
+ FRAME_-98012_NAME = 'NH_FINE_SUN_SENSOR'
+ FRAME_-98012_CLASS = 4
+ FRAME_-98012_CLASS_ID = -98012
+ FRAME_-98012_CENTER = -98
+ TKFRAME_-98012_SPEC = 'MATRIX'
+ TKFRAME_-98012_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98012_MATRIX = ( 0.702792970261541,
+ -0.00276516946126598,
+ 0.711389060071083,
+ 0.711384357815347,
+ -0.00259068940063707,
+ -0.702798394836006,
+ 0.0037863447564826,
+ 0.999992821057371,
+ 0.000146380002554562)
+
+ \begintext
+
+
+Alice Frames
+-------------------------------------------------------------------------------
+
+ The Alice instrument has two apertures, the Solar Occulation Channel, and
+ the Airglow opening. Light travels through a lollipop-shaped slit
+ described below for both apertures. Although [12], Rev A, defines the
+ Solar Occulation Channel field of view as only the 2.0 x 2.0 degree "box"
+ at the top of the lollipop-shaped slit and the Airglow field of view as the
+ 0.1 x 4.0 degree "stem" of the lollipop-shaped slit, the complete lollipop
+ shape is visible through both apertures [34].
+
+ The spectral resolution of airglow is degraded in the 2.0 x 2.0 degree
+ "box" portion of the slit, but data is nevertheless still available in that
+ portion of the slit. The 2.0 x 2.0 degree "box" portion of the slit is
+ wider than the narrow "stem" portion to observe the sun during Solar
+ Occulation Channel operations, but it is also possible for the sun to
+ appear in the narrower "stem" portion [10]. Hence, the fields of view for
+ both apertures have been defined here to be the entire lollipop-shaped
+ slit even though they are defined differently in [3], Rev A.
+
+Solar Occultation Channel (SOC) Frame Definition
+
+ The SOC is also referred to as the SOCC (Solar OCcultation Channel) to
+ distinguish it from the Science Operations Center. Since the documents
+ to which this kernel refers still use the SOC acronym for the Solar
+ Occultation Channel, we continue to use it here as well, although SOCC has
+ become the standard term [34].
+
+ The SOC frame is defined by the instrument team ([17] and [37]) such that
+ the +Y axis in the instrument frame is the center of the 2.0 x 2.0 degree
+ portion of the slit, and the X and Z axes are close to the spacecraft X and
+ Z axes, respectively.
+
+ From [12], the nominal SOC boresight is a line in the spacecraft YZ plane
+ right-hand rotated by 2 degrees around the spacecraft X axis from the REX
+ boresight (nominally the Y axis). We are given the alignment for the SOC
+ boresight in [9] and will use that measured vector to determine the frame.
+
+ Z ^
+ sc |
+ | SOC boresight
+ | _.- (optical boresight)
+ | _.-'
+ | _.-' o
+ |_.-' 2.0
+ o-------------->
+ X Y
+ sc sc
+
+ The diagram below shows the projection onto the sky of the Alice entrance
+ slit through the Alice optics for the SOC aperture. The SOC field of view
+ is the entire lollipop-shaped slit illustrated below [34].
+
+ Projection of Alice slit on the
+ sky through the SOC aperture
+ Spacecraft Axes
+ _
+ | | ^ +Z
+ | | | sc
+ | | |
+ | | |
+ | | |
+ | | x--------->
+ | | +Y (in) +X
+ | | sc sc
+ | |
+ --- |x| <---Alice optical
+ ^ o | | path center
+ | 2.0 | |
+ | ____| |____
+ | | |
+ | | |
+ _v_ | _ | /____ SOC
+ | | \ boresight
+ | |
+ |___________|
+
+ <------------------- wavelength
+
+
+ The following diagram [39] illustrates the projections of the spacecraft
+ axes through the SOCC aperture onto the Alice detector. The origin in
+ the detector view is at the bottom left.
+
+ ________________________________________________
+ increasing ^ | |
+ rows | | |
+ | | +Y (in) |
+ | | +X <---------x sc |
+ | | sc | |
+ | | | |
+ | | | |
+ | | V +Z |
+ | | sc |
+ O________________________________________________|
+ ------------------------>
+ [0,0]=[column, row] increasing columns
+ increasing wavelength
+
+ The following frame definition uses nominal pre-launch calibration
+ values. It remains here for reference but has been replaced with
+ in-flight values, described below.
+
+ From [9], the measured Alice optical path center in NH_ASTR coordinates
+ is:
+
+ [ -0.0011506 ]
+ Alice optical path center = [ 0.9993305 ]
+ [ 0.0365690 ]
+
+ The SOC frame is defined such that the boresight (the center of the
+ 2.0 x 2.0 degree portion of the slit) is the instrument +Y axis [37]. To
+ transform the optical center to the SOC boresight, the optical center is
+ rotated -2.0 degrees about the NH_ASTR +X axis to obtain the instrument
+ +Y axis:
+
+ [ -0.00115060000000000 ]
+ Alice SOC +Y Vector = [ 0.99999797455532025 ]
+ [ 0.00167059166380266 ]
+
+ The instrument +X vector is defined to be the NH_ASTR +X axis, so
+
+ [ 1.0 ]
+ Alice SOC +X Vector = [ 0.0 ]
+ [ 0.0 ]
+
+ The instrument +Z vector is determined by taking the cross product X x Y:
+
+ [ 0.0 ]
+ Alice SOC +Z Vector = [ -0.00167059271628372 ]
+ [ 0.99999860455901446 ]
+
+ And we use that to adjust the +X vector to form an orthogonal frame:
+
+ [ 0.99999933805964336 ]
+ Alice SOC +X Vector = Y x Z = [ 0.00115059835766032 ]
+ [ 0.00000192218391797 ]
+
+ Using these three vectors, we define the rotation that takes vectors from
+ the instrument frame to the NH_ASTR frame as
+
+ [ ] [ 0.99999933805964336 -0.00115060000000000 0.0 ]
+ [ ROT ] = [ 0.00115059835766032 0.99999797455532025 -0.00167059271628372 ]
+ [ ] [ 0.00000192218391797 0.00167059166380266 0.99999860455901446 ]
+
+ FRAME_NH_ALICE_SOC = -98100
+ FRAME_-98100_NAME = 'NH_ALICE_SOC'
+ FRAME_-98100_CLASS = 4
+ FRAME_-98100_CLASS_ID = -98100
+ FRAME_-98100_CENTER = -98
+ TKFRAME_-98100_SPEC = 'MATRIX'
+ TKFRAME_-98100_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98100_MATRIX = ( 0.99999933805964336,
+ 0.00115059835766032,
+ 0.00000192218391797,
+ -0.00115060000000000,
+ 0.99999797455532025,
+ 0.00167059166380266,
+ 0.0,
+ -0.00167059271628372,
+ 0.99999860455901446 )
+
+ An in-flight alignment gives the following redefinition of the SOC frame
+ [42]. Starting from the rotation matrix R1 taking vectors from the nominal
+ NH_ALICE_SOC frame to the NH_SPACECRAFT frame, an additional rotation of
+ 0.42205843 degrees about the spacecraft Y axis followed by a rotation of
+ 0.013987654 degrees about the spacecraft Z axis are required to fit the
+ alignment data. This results in the following rotation matrix, R2, taking
+ vectors from the instrument frame to the NH_SPACECRAFT frame:
+
+ [ ] [ ] [ ] [ ]
+ [ R2 ] = [ (0.013987654 deg) ] * [ (0.42205843 deg) ] * [ R1 ]
+ [ ] [ ]Z [ ]Y [ ]
+
+ [ 0.99996405571443 0.00418309873041 -0.00737488739974 ]
+ = [ -0.00419478716187 0.99998996915870 -0.00157014096732 ]
+ [ 0.00736824536873 0.00160102061271 0.99997157244253 ]
+
+ \begindata
+
+ FRAME_NH_ALICE_SOC = -98100
+ FRAME_-98100_NAME = 'NH_ALICE_SOC'
+ FRAME_-98100_CLASS = 4
+ FRAME_-98100_CLASS_ID = -98100
+ FRAME_-98100_CENTER = -98
+ TKFRAME_-98100_SPEC = 'MATRIX'
+ TKFRAME_-98100_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98100_MATRIX = ( 0.99996405571443,
+ -0.00419478716187,
+ 0.00736824536873,
+ 0.00418309873041,
+ 0.99998996915870,
+ 0.00160102061271,
+ -0.00737488739974,
+ -0.00157014096732,
+ 0.99997157244253 )
+
+ \begintext
+
+
+Airglow Channel Frame Definition
+
+ The airglow frame is defined [17] such that -X axis in the instrument frame
+ is the boresight, and +Y and +Z axes in the instrument frame are close to
+ the spacecraft +Y and +Z axes, respectively.
+
+ The diagram below shows the projection of the Alice slit onto the sky
+ through the Alice optics for the airglow aperture. The spacecraft axes are
+ shown to the right of the slit diagram. The airglow boresight is centered
+ in the 6.0 degree long slit. Its field of view is rotated +2.0 degrees with
+ respect to the spacecraft +X axis due to the 2.0 degree instrument tip to
+ center the +Y axis (the REX antenna boresight) in the center of the SOC
+ field of view [12, 17]. The airglow field of view is the entire lollipop-
+ shaped slit illustrated below [34].
+
+ Projection of Alice slit on the Spacecraft Axes
+ sky through the Airglow aperture
+ | o/ +Z
+ _ |2.0/ sc
+ | | | /
+ | | | /
+ | | |/
+ | | o - - - - -
+ | | +X (out) `-._ 2.0 deg
+ | | sc `-._
+ | | ` +Y
+ | | sc
+ | |
+ |+| <---Airglow Airglow instrument axes
+ | | boresight are rotated +2.0 degrees
+ | | about the spacecraft +X
+ ____| |____ axis.
+ | |
+ | | Instrument Axes
+ | |
+ | | ^ +Z
+ | | | inst
+ |___________| |
+ |
+ -------------------> wavelength o-------> +Y
+ +X (out) inst
+ inst
+
+ The following diagram [39] illustrates the projections of the spacecraft
+ axes through the Airglow aperture onto the Alice detector. The origin in
+ the detector view is at the bottom left.
+
+ Note that the instrument tip about the spacecraft X axis is not depicted.
+ The actual projected spacecraft axes are rotated by a nominal -2.0
+ degrees about the spacecraft +X axis from the positions shown below.
+
+ ________________________________________________
+ increasing ^ | |
+ rows | | |
+ | | +X (out) |
+ | | +Y <---------o sc |
+ | | sc | |
+ | | | |
+ | | | |
+ | | V +Z |
+ | | sc |
+ O________________________________________________|
+ ------------------------>
+ [0,0]=[column, row] increasing columns
+ increasing wavelength
+
+
+ Note that the following calculations use nominal pre-launch calibration
+ values. These calculations remain here for reference, but have been
+ replaced with in-flight calibration values, which are described below the
+ nominal frame definition. The boresight has also changed from the center
+ of the Alice slit to slightly off-center.
+
+ The nominal frame is described here:
+
+ We are given in [9] the measured boresight vector in spacecraft
+ coordinates:
+
+ Airglow boresight = -X = [-0.9999836 0.0011311 0.0056122]
+ inst
+
+ We must calculate the instrument Y and Z axes in spacecraft coordinates in
+ order to define a rotation matrix, R, which takes vectors from the airglow
+ instrument frame to vectors in the spacecraft frame.
+
+ To calculate the instrument Y axis, we will rotate the spacecraft Y axis
+ by +2.0 degrees about the spacecraft +X axis and use the projection of the
+ rotated Y axis onto the plane perpendicular to the measured boresight as
+ the instrument Y axis. The instrument Z axis is then determined using the
+ cross product. Note that this calculation assumes there is no misalignment
+ in the plane perpendicular to the boresight (that there is no twist in the
+ misalignment). The rotation of the spacecraft Y axis is shown here:
+
+
+ +Z
+ | SC
+ |
+ | _. +Y
+ | _.-' o rotated
+ | _.-' 2
+ o'------------
+ +X (out) +Y
+ SC SC
+
+
+ The rotated Y axis in spacecraft coordinates is
+
+ +Y = [ 0.0 cos( 2.0 deg ) sin( 2.0 deg ) ]
+ rotated
+
+ We now calculate the projection of the rotated Y axis onto the plane
+ perpendicular to the measured boresight to get the instrument Y axis:
+
+
+ -X (Boresight)
+ ^ inst
+ |
+ | / +Y
+ | / rotated
+ | /
+ | /
+ |/
+ o--------->
+ +Z (out) +Y
+ inst inst
+
+
+ Since the boresight vector is unit length, using the dot product and vector
+ addition, we have
+
+ +Y = +Y - Boresight * dot(+Y , Boresight)
+ inst rotated rotated
+
+ The SPICE routine VPERP does this calculation for us, yielding
+
+ +Y = [ 0.001326253357475 0.999390205835991 0.034892084075427 ]
+ inst
+
+ The instrument Z axis is determined using the cross product:
+
+ +Z = +X x +Y
+ inst inst inst
+
+ = [ 0.005569311419949 -0.034898955455451 0.999375327731491 ]
+
+ The rotation matrix R taking vectors in the instrument frame to vectors
+ in the spacecraft frame is then
+
+ [ ] [ 0.9999836 0.001326253357475 0.005569311419949 ]
+ [ R ] = [ -0.0011311 0.999390205835991 -0.034898955455451 ]
+ [ ] [ -0.0056122 0.034892084075427 0.999375327731491 ]
+
+ This nominal frame definition is shown below. It remains here for
+ reference only and will not be loaded into the SPICE kernel pool.
+
+ FRAME_NH_ALICE_AIRGLOW = -98101
+ FRAME_-98101_NAME = 'NH_ALICE_AIRGLOW'
+ FRAME_-98101_CLASS = 4
+ FRAME_-98101_CLASS_ID = -98101
+ FRAME_-98101_CENTER = -98
+ TKFRAME_-98101_SPEC = 'MATRIX'
+ TKFRAME_-98101_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98101_MATRIX = ( 0.9999836,
+ -0.0011311,
+ -0.0056122,
+ 0.001326253357475,
+ 0.999390205835991,
+ 0.034892084075427,
+ 0.005569311419949,
+ -0.034898955455451,
+ 0.999375327731491)
+
+ The following definition updates the nominal frame, but has since been
+ replaced with more current values. These older values remain here for
+ reference only.
+
+ In-flight values for pointing offsets are described in [32] as:
+
+ "The error bars are the standard deviation of the residuals. To convert
+ from the s/c coordinate system to the Alice instrument coordinate system
+ (the boresight is defined to be [-1,0,0] in both coordinate systems),
+ perform the following rotations (in degrees):
+
+ Rotation about s/c X -1.717403537893697 +/- 0.14135753
+ Rotation about new Z 0.368710896944916 +/- 0.013300878
+ Rotation about new Y -0.313630482588893 +/- 0.013886115
+
+ Applying the inverse rotations, we arrive at the Alice boresight in
+ spacecraft coordinates:
+
+ [ -0.999964312690322 0.006435174723831 0.005473743878372 ]
+
+ The 6 degree entrance slit is imaged onto rows 6-25 (inclusive). Therefore
+ the center of the slit should fall exactly on the boundary between rows 15
+ and 16. However, I believe it is preferable that when the Alice boresight
+ aims toward a point source, the spectrum fall onto a single row (or as
+ close to this as possible). Therefore, I have added an additional rotation
+ of +0.10 degrees (1/3 of one 0.3 degree detector row) about the Y axis to
+ put all the flux into row 16. In this case the Alice boresight in s/c
+ coordinates is:
+
+ [ -0.999972343138423 0.006435174723831 0.003728469461561 ]
+
+ Rotation about new Y -0.213630482588893 +/- 0.002959385400478"
+
+ Note that the airglow boresight is no longer at the Alice slit center. The
+ slit center is located at
+
+ [ -0.999964312690322 0.006435174723831 0.005473743878372 ]
+
+ Using the SPICE subroutine ROTMAT, the three rotations described above are
+ calculated, leading to the following transformation, which takes vectors
+ in the instrument frame to vectors in the spacecraft frame:
+
+ [ ] [ 0.999972343138423 0.006543983365249 0.003534011879914 ]
+ [ R ] = [ -0.006435174723831 0.999530106264816 -0.029969237503143 ]
+ [ ] [ -0.003728469461561 0.029945666664166 0.999544574075370 ]
+
+ FRAME_NH_ALICE_AIRGLOW = -98101
+ FRAME_-98101_NAME = 'NH_ALICE_AIRGLOW'
+ FRAME_-98101_CLASS = 4
+ FRAME_-98101_CLASS_ID = -98101
+ FRAME_-98101_CENTER = -98
+ TKFRAME_-98101_SPEC = 'MATRIX'
+ TKFRAME_-98101_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98101_MATRIX = ( 0.999972343138423,
+ -0.006435174723831,
+ -0.003728469461561,
+ 0.006543983365249,
+ 0.999530106264816,
+ 0.029945666664166,
+ 0.003534011879914,
+ -0.029969237503143,
+ 0.999544574075370)
+
+ The frame defined above has been superceded by [43]. The above frame will
+ not be loaded into the kernel pool and remains here for reference only.
+ Updated values for the rotation matrix taking vectors from the instrument
+ frame to the spacecraft frame are described in [43] as:
+
+ "This new rotation matrix is the result of a re-analysis of data from the
+ Alice boresight alignment scans made during the post-launch commissioning.
+ Although the Alice slit is physically rectilinear, optical distortions
+ (mostly coma) introduced by the primary mirror result in a slit that appears
+ somewhat curved, when projected onto the sky. The initial analysis of the
+ alignment data failed to take this into account, resulting in the calculated
+ boresight being approximately 0.02 (20% of the 0.1 degree slit width)
+ degrees from the centerline of the slit. The new rotation matrix to
+ transform from the NH_SPACECRAFT coordinate system to the NH_ALICE_AIRGLOW
+ coordinate system is obtained by making the following rotations (in order):
+
+ Rotation about X: -1.59926267084552 degrees
+ Rotation about Z: 0.35521825089567 degrees
+ Rotation about Y: -0.23245579623587 degrees
+
+ The Alice airglow boresight ([-1, 0, 0] in the instrument frame) is located
+ at the following coordinates in the NH_SPACECRAFT frame:
+
+ [ -0.99997255180979 0.00608399347241 0.00422855181362]
+
+ Using the SPICE subroutine ROTMAT, the three rotations described above are
+ calculated, leading to the following transformation, which takes vectors
+ in the instrument frame to vectors in the spacecraft frame:
+
+ [ ] [ 0.99997255180979 0.00619968832527 0.00405702990897]
+ [ R ] = [ -0.00608399347241 0.99959126350983 -0.02793368823199]
+ [ ] [ -0.00422855181362 0.02790823855932 0.99960154540200]"
+
+ \begindata
+
+ FRAME_NH_ALICE_AIRGLOW = -98101
+ FRAME_-98101_NAME = 'NH_ALICE_AIRGLOW'
+ FRAME_-98101_CLASS = 4
+ FRAME_-98101_CLASS_ID = -98101
+ FRAME_-98101_CENTER = -98
+ TKFRAME_-98101_SPEC = 'MATRIX'
+ TKFRAME_-98101_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98101_MATRIX = ( 0.99997255180979,
+ -0.00608399347241,
+ -0.00422855181362,
+ 0.00619968832527,
+ 0.99959126350983,
+ 0.02790823855932,
+ 0.00405702990897,
+ -0.02793368823199,
+ 0.99960154540200)
+
+ \begintext
+
+
+RALPH Frames
+-------------------------------------------------------------------------------
+
+ The RALPH instrument consists of Linear Etalon Imaging Spectral Array
+ (LEISA) and Multispectral Visible Imaging Camera (MVIC). RALPH also has a
+ Solar Illumination Aperture (SIA). RALPH is mounted on the +Z side of the
+ New Horizons spacecraft.
+
+ MVIC obtains science imaging data using frame transfer data acquisition and
+ uses optical filters to provide spectral band discrimination in the blue,
+ red, near infrared (NIR), methane, and two panchromatic bands [23].
+
+ From [22], the instrument boresight is aligned with the center of the frame
+ transfer array. A summary of the relative positions of the individual
+ arrays is presented below, with detailed calculations following. To
+ convert the numbers in Table 1 from microns to microradians use the
+ conversion factor of 1.5208 microradian/micron.
+
+ From [22] Table 1:
+
+ The offset in microns of the individual focal plane arrays in Ralph
+ -------------------------------------------------------------------
+ Offset of the array Offset of the array
+ from the instrument from the instrument
+ boresight in the MVIC boresight in the MVIC
+ Array row direction (microns) column direction (microns)
+ ----- --------------------- ---------------------
+ Frame Transfer 0.0 0.0
+ Pan 2 2041.0 0.0
+ Pan 1 3354.0 0.0
+ Red 4693.0 0.0
+ Blue 5941.0 0.0
+ Methane 7280.0 0.0
+ NIR 8632.0 0.0
+ LEISA -218.0 3334.0
+
+
+ From [22] Table 2 (LEISA from [30]):
+
+ Size in pixels of the MVIC and LEISA arrays
+ -------------------------------------------------------------------
+ Array Rows Columns
+ ----- ---- -------
+ Frame Transfer 128 5024
+ Pan 2 32 5024
+ Pan 1 32 5024
+ Red 32 5024
+ Blue 32 5024
+ Methane 32 5024
+ NIR 32 5024
+ LEISA 256 256
+
+
+ The detail of the calculations used in Table 1 for the MVIC arrays [22]:
+
+ Pan 2: (221 - 64) * 13 microns/pixel = 2041 microns
+ Pan 1: (322 - 64) * 13 microns/pixel = 3354 microns
+ Red: (425 - 64) * 13 microns/pixel = 4693 microns
+ Blue: (521 - 64) * 13 microns/pixel = 5941 microns
+ Methane: (624 - 64) * 13 microns/pixel = 7280 microns
+ NIR: (728 - 64) * 13 microns/pixel = 8632 microns
+
+ The first number in the calculations above is the MVIC row at which the
+ filter is centered. Subtracted from that number is 64 in all cases, which
+ is the MVIC row of the center of the frame transfer array. The MVIC pixels
+ are 13 microns wide with a single pixel FOV of 19.8 microradians [22].
+
+ The detail of the calculation used in Table 1 for LEISA [22]:
+
+ The center of the MVIC frame transfer (FT) array corresponds to column
+ 44.65 and row 133.45 of LEISA. The distance from the instrument
+ boresight (center of the FT array) to the center of the LEISA array is
+ calculated here:
+
+ In MVIC row direction (128 - 133.45)* 40 microns/pixel = -218 microns
+ In MVIC col direction (128 - 44.65)* 40 microns/pixel = 3334 microns
+
+ The LEISA scale is used here because this is the difference between two
+ different LEISA pixel coordinates. The MVIC directions are used so that all
+ offsets are presented in the same coordinate system. The LEISA pixels are
+ 40 microns wide with a single pixel FOV of 61 microradians.
+
+
+Multispectral Visible Imaging Camera (MVIC) Frames Definition
+
+ From [39]:
+
+ MVIC Frame Transfer is a staring instrument. Each stare/read cycle
+ produces 1 readout image that is translated into an image plane in
+ the corresponding image file created by the SOC (Science Operations
+ Center). Each image plane has roughly the same viewing geometry.
+ All of Ralph's FOVs share a single telescope, nominally aligned to
+ the spacecraft -X axis.
+
+ When viewed by an observer looking out MVIC's Frame Transfer boresight,
+ the spacecraft axes on the sky will look like:
+
+ Diagram 1
+ ---------
+ Sky View Looking out from MVIC Frame Transfer
+ _______________________________________________________
+ | |
+ | ^ +Y |
+ | | |
+ | | |
+ | | |
+ | <------- o |
+ | +Z +X (out) |
+ | |
+ 0_______________________________________________________|
+
+
+ Displaying one MVIC Frame Transfer image plane using IDL after SOC
+ processing will look like the following:
+
+ Diagram 2
+ ---------
+ MVIC Frame Transfer IDL Display
+ _______________________________________________________
+ | |
+ | ^ +Y |
+ ^ | | |
+ | | | |
+ | | | |
+ | | <-------o |
+ Increasing | | +Z |
+ rows (128) | | |
+ 0_______________________________________________________|
+ -------------------------->
+ Increasing columns (5024)
+
+
+ NOTE: the following calculations use nominal alignment values and have been
+ preceded by in-flight values. The following two frames remain in this
+ kernel for reference only. Only the frames enclosed within the
+ "\begindata \begintext" block are used by SPICE.
+
+ The base instrument frame, NH_RALPH_MVIC, describes the nominal instrument
+ misalignment (note that the definition of this frame has changed after
+ in-flight calibration - see below).
+
+ Because the RALPH coordinate system is the same as the spacecraft coordinate
+ system [7], the rotation matrix that takes vectors represented in the
+ nominal MVIC frame into the spacecraft frame is the identity. We will
+ adjust the rotation to take into account the measured alignment provided
+ in [9].
+
+ From [9], the measured MVIC boresight vector in spacecraft coordinates is:
+
+ [ -0.9999688 ]
+ MVIC Boresight Vector = -X = [ 0.0078090 ]
+ [ -0.0011691 ]
+
+ and the detector direction (+Z axis in the instrument frame) is measured
+ to be:
+
+ [ -0.0011761 ]
+ MVIC Detector Direction = [ 0.0036511 ]
+ [ 0.9999926 ]
+
+ Taking the cross product of these two vectors gives us:
+
+ [ 0.007813211258259 ]
+ MVIC +Y Vector = Z x X = [ 0.999962844813125 ]
+ [ -0.003641802174272 ]
+
+ And we use that to adjust the Z vector to form an orthogonal frame:
+
+ [ -0.001140617758206 ]
+ MVIC +Z Vector = X x Y = [ 0.003650823069793 ]
+ [ 0.999992685214268 ]
+
+ Using these three vectors, we define the rotation that takes vectors from
+ the instrument frame to the spacecraft frame as
+
+ [ ] [ 0.9999688 0.007813211258259 -0.001140617758206 ]
+ [ ROT ] = [ -0.0078090 0.999962844813125 0.003650823069793 ]
+ [ ] [ 0.0011691 -0.003641802174272 0.999992685214268 ]
+
+ FRAME_NH_RALPH_MVIC = -98200
+ FRAME_-98200_NAME = 'NH_RALPH_MVIC'
+ FRAME_-98200_CLASS = 4
+ FRAME_-98200_CLASS_ID = -98200
+ FRAME_-98200_CENTER = -98
+ TKFRAME_-98200_SPEC = 'MATRIX'
+ TKFRAME_-98200_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98200_MATRIX = ( 0.9999688,
+ -0.0078090,
+ 0.0011691,
+ 0.007813211258259,
+ 0.999962844813125,
+ -0.003641802174272,
+ -0.001140617758206,
+ 0.003650823069793,
+ 0.999992685214268 )
+
+ Since the instrument boresight is aligned with the center of the frame
+ transfer array [22], the rotation matrix taking vectors in the frame
+ transfer array frame to the base instrument frame is the identity:
+
+ FRAME_NH_RALPH_MVIC_FT = -98203
+ FRAME_-98203_NAME = 'NH_RALPH_MVIC_FT'
+ FRAME_-98203_CLASS = 4
+ FRAME_-98203_CLASS_ID = -98203
+ FRAME_-98203_CENTER = -98
+ TKFRAME_-98203_SPEC = 'MATRIX'
+ TKFRAME_-98203_RELATIVE = 'NH_RALPH_MVIC'
+ TKFRAME_-98203_MATRIX = ( 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0 )
+
+ The above nominal NH_RALPH_MVIC frame has been updated in version 0.0.5 of
+ this kernel. The calculations above had erroneously been done in single
+ precision in earlier versions. Version 0.0.5 also connects NH_RALPH_MVIC to
+ the NH_ASTR frame rather than the NH_SPACECRAFT frame to take into account
+ the in-flight change to the star tracker alignment. Note that the
+ NH_RALPH_MVIC and NH_RALPH_MVIC_FT frames defined above are in the text
+ section of the kernel and will not be loaded into SPICE. They have been
+ replaced by the frames defined below using in-flight measured values and
+ remain in this kernel for reference only.
+
+ The definitions below have been provided in [31]. [31] notes that the
+ matrix values below contain an adjustment to correct a shift in values
+ returned by SPICE. The MVIC and LEISA matrices may be updated in a future
+ release once the cause of the shift is known. Note that the instrument
+ reference frames are all defined with respect to the NH_SPACECRAFT frame.
+
+ MVIC Pan Frame Transfer Array
+
+ \begindata
+
+ FRAME_NH_RALPH_MVIC_FT = -98203
+ FRAME_-98203_NAME = 'NH_RALPH_MVIC_FT'
+ FRAME_-98203_CLASS = 4
+ FRAME_-98203_CLASS_ID = -98203
+ FRAME_-98203_CENTER = -98
+ TKFRAME_-98203_SPEC = 'MATRIX'
+ TKFRAME_-98203_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98203_MATRIX = ( 0.999915461106432,
+ -0.012957863475922,
+ 0.001301425571368,
+ 0.012962551750366,
+ 0.999908274152575,
+ -0.003840453099600,
+ -0.001188689962478,
+ 0.003857294149614,
+ 0.999990855106924 )
+
+ \begintext
+
+ The NH_RALPH_MVIC frame has been removed [33]. A new frame, NH_RALPH,
+ describes the Ralph instrument boresight, which is by definition the
+ center of the frame transfer array, and is such set to the identity matrix
+ with respect to the NH_RALPH_MVIC_FT frame.
+
+ Basic boresight for the instrument
+
+ \begindata
+
+ FRAME_NH_RALPH = -98200
+ FRAME_-98200_NAME = 'NH_RALPH'
+ FRAME_-98200_CLASS = 4
+ FRAME_-98200_CLASS_ID = -98200
+ FRAME_-98200_CENTER = -98
+ TKFRAME_-98200_SPEC = 'MATRIX'
+ TKFRAME_-98200_RELATIVE = 'NH_RALPH_MVIC_FT'
+ TKFRAME_-98200_MATRIX = ( 1.0, 0.0, 0.0,
+ 0.0, 1.0, 0.0,
+ 0.0, 0.0, 1.0 )
+
+ \begintext
+
+
+MVIC Time Delay Integration (TDI) Frames Frame Definitions
+(includes PAN1, PAN2, RED, BLUE, METHANE, and NIR)
+
+ From [39]:
+
+ MVIC TDI is a scanning instrument. Each scan/read cycle produces 1 readout
+ line that is translated into a single image row in the corresponding image
+ file created by the SOC (Science Operations Center). All of Ralph's FOVs
+ share a single telescope, nominally aligned to the spacecraft -X axis. The
+ FOVs for the TDI frames are each slightly offset from each other, but the
+ following diagrams are a valid approximation for all.
+
+ When viewed by an observer looking out MVIC's TDI boresight, the spacecraft
+ axes on the sky will look like:
+
+ Diagram 1
+ ---------
+ Sky View Looking out from MVIC TDI Frames
+
+ ^ +Y
+ | scan ^
+ | direction |
+ | |
+ ___________________________|___________________________ |
+ | +Z <-------o +X (out) | |
+ |_______________________________________________________| |
+
+
+ Displaying the MVIC TDI image using IDL after SOC processing will look
+ like the following:
+
+ Diagram 2
+ ---------
+ MVIC TDI IDL Display
+ _______________________________________________________
+ | |
+ | |
+ | |
+ | |
+ ^ | |
+ | | ^ +Y |
+ | | | |
+ | | | |
+ | | | |
+ | | <-------o |
+ Increasing | | +Z |
+ image row, | | |
+ scan time | | |
+ 0_______________________________________________________|
+ -------------------------->
+ Increasing columns (5024)
+
+
+ When viewed by an observer looking out MVIC's TDI boresights, each FOV
+ is aligned slightly offset from each other, along the +Y direction:
+
+ Diagram 3
+ ---------
+ Sky View Looking out from MVIC TDI Frames
+
+ NIR |========================================================|
+
+ METHANE |========================================================|
+
+ RED |========================================================|
+
+ BLUE |========================================================|
+
+ PAN1 |========================================================|
+
+ PAN2 |========================================================|
+
+ ^ +Y
+ | scan ^
+ | direction |
+ | |
+ +Z <-------o +X (out)
+
+ TDI Arrays
+
+ \begindata
+
+ FRAME_NH_RALPH_MVIC_NIR = -98209
+ FRAME_-98209_NAME = 'NH_RALPH_MVIC_NIR'
+ FRAME_-98209_CLASS = 4
+ FRAME_-98209_CLASS_ID = -98209
+ FRAME_-98209_CENTER = -98
+ TKFRAME_-98209_SPEC = 'MATRIX'
+ TKFRAME_-98209_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98209_MATRIX = ( 0.999655573953295,
+ -0.026218528636659,
+ 0.001363247322305,
+ 0.026223117930647,
+ 0.999649201897941,
+ -0.003626292333940,
+ -0.001204840860741,
+ 0.003661087780433,
+ 0.999991572287813 )
+
+ FRAME_NH_RALPH_MVIC_METHANE = -98208
+ FRAME_-98208_NAME = 'NH_RALPH_MVIC_METHANE'
+ FRAME_-98208_CLASS = 4
+ FRAME_-98208_CLASS_ID = -98208
+ FRAME_-98208_CENTER = -98
+ TKFRAME_-98208_SPEC = 'MATRIX'
+ TKFRAME_-98208_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98208_MATRIX = ( 0.999706214601813,
+ -0.024211181536640,
+ 0.001355962837282,
+ 0.024215758201663,
+ 0.999699832809316,
+ -0.003629168417489,
+ -0.001204837178782,
+ 0.003661233729783,
+ 0.999991571758176 )
+
+ FRAME_NH_RALPH_MVIC_BLUE = -98207
+ FRAME_-98207_NAME = 'NH_RALPH_MVIC_BLUE'
+ FRAME_-98207_CLASS = 4
+ FRAME_-98207_CLASS_ID = -98207
+ FRAME_-98207_CENTER = -98
+ TKFRAME_-98207_SPEC = 'MATRIX'
+ TKFRAME_-98207_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98207_MATRIX = ( 0.999795403077788,
+ -0.020196202570963,
+ 0.001341376615173,
+ 0.020200753919525,
+ 0.999789001887114,
+ -0.003634876673948,
+ -0.001204830694104,
+ 0.003661525649188,
+ 0.999991570697647 )
+
+ FRAME_NH_RALPH_MVIC_RED = -98206
+ FRAME_-98206_NAME = 'NH_RALPH_MVIC_RED'
+ FRAME_-98206_CLASS = 4
+ FRAME_-98206_CLASS_ID = -98206
+ FRAME_-98206_CENTER = -98
+ TKFRAME_-98206_SPEC = 'MATRIX'
+ TKFRAME_-98206_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98206_MATRIX = ( 0.999752824372622,
+ -0.022203736816693,
+ 0.001348672591773,
+ 0.022208300833224,
+ 0.999746432868338,
+ -0.003632029868004,
+ -0.001204833789898,
+ 0.003661379686231,
+ 0.999991571228120 )
+
+ FRAME_NH_RALPH_MVIC_PAN1 = -98205
+ FRAME_-98205_NAME = 'NH_RALPH_MVIC_PAN1'
+ FRAME_-98205_CLASS = 4
+ FRAME_-98205_CLASS_ID = -98205
+ FRAME_-98205_CENTER = -98
+ TKFRAME_-98205_SPEC = 'MATRIX'
+ TKFRAME_-98205_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98205_MATRIX = ( 0.999833950545631,
+ -0.018188586893952,
+ 0.001334074936899,
+ 0.018193125555121,
+ 0.999827539694002,
+ -0.003637708823840,
+ -0.001204827891411,
+ 0.003661671618066,
+ 0.999991570166760 )
+
+ FRAME_NH_RALPH_MVIC_PAN2 = -98204
+ FRAME_-98204_NAME = 'NH_RALPH_MVIC_PAN2'
+ FRAME_-98204_CLASS = 4
+ FRAME_-98204_CLASS_ID = -98204
+ FRAME_-98204_CENTER = -98
+ TKFRAME_-98204_SPEC = 'MATRIX'
+ TKFRAME_-98204_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98204_MATRIX = ( 0.999868466620725,
+ -0.016180897880494,
+ 0.001326767586392,
+ 0.016185423834895,
+ 0.999862046133615,
+ -0.003640526306263,
+ -0.001204825381830,
+ 0.003661817592276,
+ 0.999991569635460 )
+
+ \begintext
+
+
+Linear Etalon Imaging Spectral Array (LEISA) Frames Definition
+
+ From [39]:
+
+ LEISA is a scanning instrument. Each scan/read cycle produces 1 readout
+ image that is translated into an image plane in the corresponding image
+ file created by the SOC (Science Operations Center). All of Ralph's FOVs
+ share a single telescope, nominally aligned to the spacecraft -X axis.
+
+ When viewed by an observer looking out LEISA's boresight, the spacecraft
+ axes on the sky will look like:
+
+ Diagram 1
+ ---------
+ Sky View Looking out from LEISA
+ _______________________________
+ | |
+ | |
+ | ^ +Y | ^
+ | | | |
+ | | | |
+ | | | | Scan
+ | | | | direction(s)
+ | <-------o | |
+ | +Z +X (out) | |
+ | | |
+ | | |
+ | | |
+ | | v
+ | |
+ |_______________________________|
+
+
+ Displaying one LEISA image plane using IDL after SOC processing will
+ look like the following:
+
+ Diagram 2
+ ---------
+ LEISA IDL Display (1 image)
+ _______________________________
+ | |
+ | +Y |
+ |High Res ^ | ^
+ |--------------|----------------| |
+ ^ |Low Res | | |
+ | | | | |S
+ | | | | |c
+ | | x---------> | |a
+ | | +Z | |n
+ | | | |
+ | | | |
+ Increasing | | | |
+ rows (256), | | | v
+ wavelengths | | |
+ 0_______________________________|
+ --------------------->
+ Increasing columns (256)
+ Fixed wavelength
+
+
+ Displaying one LEISA image row (constant wavelength) over all image
+ planes using IDL after SOC processing will look like the following (note
+ that the vertical dimension of the image is determined by the length of
+ the scan; the horizontal dimension is the number of spatial pixels):
+
+ Diagram 3
+ ---------
+ LEISA IDL Display (1 wavelength)
+ _______________________________
+ | |
+ | |
+ | |
+ | |
+ | |
+ | +Y or -Y |
+ | ^ (depends on |
+ | | scan direction)|
+ | | |
+ | | |
+ | | |
+ ^ | | |
+ | | x---------> |
+ | | +Z |
+ | | |
+ | | |
+ Increasing | | |
+ image plane, | | |
+ scan time | | |
+ 0_______________________________|
+ --------------------->
+ Increasing columns (256)
+
+
+ The LEISA frame is defined in [31] as
+
+ \begindata
+
+ FRAME_NH_RALPH_LEISA = -98201
+ FRAME_-98201_NAME = 'NH_RALPH_LEISA'
+ FRAME_-98201_CLASS = 4
+ FRAME_-98201_CLASS_ID = -98201
+ FRAME_-98201_CENTER = -98
+ TKFRAME_-98201_SPEC = 'MATRIX'
+ TKFRAME_-98201_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98201_MATRIX = ( 0.999833725668520,
+ -0.018154907521815,
+ 0.001873657185926,
+ 0.018161563736818,
+ 0.999817822153710,
+ -0.003715956943165,
+ -0.001743042311673,
+ 0.003750674847578,
+ 0.999990409103958 )
+
+ \begintext
+
+
+Solar Illumination Aperture (SIA) Frame Definition
+
+ We define the SIA frame such that +Z axis in the instrument frame is the
+ boresight and +X in the instrument frame is aligned to the spacecraft +X
+ axis. Looking down the spacecraft X axis, we have
+
+
+ Z ^
+ sc |
+ |
+ |
+ | _.- SIA boresight vector (+Z )
+ | _.-' inst
+ | _.-' o
+ |_.-' 2.0
+ o-------------->
+ X = X Y
+ inst sc sc
+
+
+ Plane X = 0
+
+ The rotation matrix that transforms vectors in the instrument frame to the
+ spacecraft frame can be defined by the single rotation
+
+ [ ] [ ]
+ [ ROT ] = [ (90.0 - 2.0) ]
+ [ ] [ ]
+ X
+
+ where [x] represents the rotation matrix of a given angle x about axis i.
+ i
+
+ \begindata
+
+ FRAME_NH_RALPH_SIA = -98202
+ FRAME_-98202_NAME = 'NH_RALPH_SIA'
+ FRAME_-98202_CLASS = 4
+ FRAME_-98202_CLASS_ID = -98202
+ FRAME_-98202_CENTER = -98
+ TKFRAME_-98202_SPEC = 'ANGLES'
+ TKFRAME_-98202_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98202_ANGLES = ( 0.0, 88.0, 0.0 )
+ TKFRAME_-98202_AXES = ( 3 1 3 )
+ TKFRAME_-98202_UNITS = 'DEGREES'
+
+ \begintext
+
+
+LOng Range Reconnaissance Imager (LORRI) Frames
+-------------------------------------------------------------------------------
+
+ The following diagrams are reproduced from [15] and [29].
+
+ When viewed by an observer looking out LORRI's boresight, the spacecraft
+ axes on the sky will look like:
+
+ Diagram 1
+ ---------
+ Sky View Looking out from LORRI
+ _________________________________
+ | |
+ | |
+ | ^ +Y |
+ | | sc |
+ | | |
+ | | |
+ | | |
+ | <--------o |
+ | +Z +X (out) |
+ | sc sc |
+ | |
+ | |
+ | |
+ | |
+ |_________________________________|
+
+
+ The LORRI optics inverts images in both the Y and Z directions, so that the
+ projection of these spacecraft axes onto the LORRI CCD will look like the
+ following: (Note that we are looking INTO the LORRI telescope in the
+ diagram below, whereas above we were looking outwards, hence the position
+ of the +Z axis does not appear to have changed when in fact it has flipped).
+
+ Diagram 2
+ ---------
+ Looking in at the LORRI CCD
+ _________________________________
+ | | Spacecraft Axes
+ | |
+ | | ^ +Y
+ | | | sc
+ increasing ^ | | |
+ columns | | p | x-----> +Z
+ | | p +X (in) | +X (in) sc
+ | | +Z <---------x sc | sc
+ | | sc | |
+ | | | |
+ | | | |
+ | | | p |
+ | | V +Y |
+ | | sc |
+ O_________________________________|
+ ------------------------>
+ [0,0]=[column, row] increasing rows
+
+ p p
+ Note that in Diagram 2, the axes are labeled Z and Y to clarify
+ sc sc
+ that although these are still spacecraft coordinates, they are the
+ projections of the spacecraft axes from Diagram 1 onto the LORRI CCD, not
+ the actual spacecraft axes. The actual spacecraft axes are depicted to the
+ right of Diagram 2. The origin in the CCD view is at the bottom left, and
+ the CCD storage area and serial register are to the left.
+
+ The LORRI IDL display further inverts the image in Diagram 2 about the
+ diagonal originating at [0,0]:
+
+ Diagram 3
+ ---------
+ LORRI IDL Display
+ _________________________________
+ | | Spacecraft Axes
+ | |
+ | | ^ +Z
+ | | | sc
+ increasing ^ | | |
+ rows | | p | o-----> +Y
+ | | p +X (out) | +X (out) sc
+ | | +Y <---------x sc | sc
+ | | sc | |
+ | | | |
+ | | | |
+ | | | p |
+ | | V +Z |
+ | | sc |
+ O_________________________________|
+ ------------------------>
+ [0,0]=[column, row] increasing columns
+
+
+
+ Also provided here are the same set of three diagrams using the LORRI
+ instrument axes, X , Y , Z , rather than the spacecraft axes.
+ L L L
+
+ Diagram 1a
+ ----------
+ Sky View Looking out from LORRI
+ _________________________________
+ | |
+ | | Spacecraft Axes
+ | |
+ | | ^ +Y
+ | | | sc
+ | | |
+ | | <-----o
+ | o---------> | +Z +X (out)
+ | | Y | sc sc
+ | | L |
+ | | |
+ | | |
+ | V X |
+ | L |
+ |_________________________________|
+
+
+ Diagram 2a
+ ----------
+ Looking in at the LORRI CCD
+ _________________________________
+ | |
+ | p |
+ | ^ X |
+ | | L |
+ increasing ^ | | |
+ columns | | | |
+ | | | |
+ | | x---------> p |
+ | | Y |
+ | | L |
+ | | |
+ | | |
+ | | |
+ | | |
+ O_________________________________|
+ ------------------------>
+ [0,0]=[column, row] increasing rows
+
+ As in Diagram 2, the axes in Diagram 2a are the projections of the LORRI
+ instrument axes through the optics onto the LORRI CCD.
+
+ Diagram 3a
+ ---------
+ LORRI IDL Display
+ _________________________________
+ | |
+ | p |
+ | ^ Y |
+ | | L |
+ increasing ^ | | |
+ rows | | | |
+ | | | |
+ | | p o---------> p |
+ | | Z (out) X |
+ | | L L |
+ | | |
+ | | |
+ | | |
+ | | |
+ O_________________________________|
+ ------------------------>
+ [0,0]=[column, row] increasing columns
+
+
+
+ Taken from [29], we have the following coordinate system definition for the
+ LORRI frame:
+
+ The -Z axis in instrument coordinates is defined to be the boresight and
+ is approximately aligned with the spacecraft -X axis. The Y axis in
+ instrument coordinates is approximately aligned with the spacecraft -Z axis
+ and is in the direction of increasing rows. The X axis in instrument
+ coordinates is approximately aligned with the spacecraft -Y axis and is in
+ the direction of increasing columns.
+
+ The following nominal frame definition remains here for reference only and
+ will not be loaded into the SPICE kernel pool. See below for the updated
+ frame.
+
+ Using the measured vectors from [9], we have:
+
+ [ -0.9999955 ]
+ LORRI Boresight Vector (-Z ) = [ 0.0005485 ]
+ inst [ -0.0029601 ]
+
+ and the detector direction (-Y axis in the instrument frame) in spacecraft
+ coordinates is measured to be:
+
+ [ -0.0029702 ]
+ LORRI -Y Vector = [ 0.0069403 ]
+ [ 0.9999715 ]
+
+ Taking the cross product of these two vectors gives us:
+
+ [ -0.000569028334549 ]
+ LORRI +X Vector = Y x Z = [ -0.999975765451163 ]
+ [ 0.006938639428225 ]
+
+ And we use that to adjust the Y vector to form an orthogonal frame:
+
+ [ 0.002956222326369 ]
+ LORRI +Y Vector = Z x X = [ -0.006940292366278 ]
+ [ -0.999971546140903 ]
+
+ Using these three vectors, we define the rotation that takes vectors from
+ the instrument frame to the spacecraft frame as
+
+ [ ] [ -0.000569028334549 0.002956222326369 0.9999955 ]
+ [ ROT ] = [ -0.999975765451163 -0.006940292366278 -0.0005485 ]
+ [ ] [ 0.006938639428225 -0.999971546140903 0.0029601 ]
+
+ FRAME_NH_LORRI = -98300
+ FRAME_-98300_NAME = 'NH_LORRI'
+ FRAME_-98300_CLASS = 4
+ FRAME_-98300_CLASS_ID = -98300
+ FRAME_-98300_CENTER = -98
+ TKFRAME_-98300_SPEC = 'MATRIX'
+ TKFRAME_-98300_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98300_MATRIX = ( -0.000569028334549,
+ -0.999975765451163,
+ 0.006938639428225,
+ 0.002956222326369,
+ -0.006940292366278,
+ -0.999971546140903,
+ 0.9999955,
+ -0.0005485,
+ 0.0029601 )
+
+
+ The updated, in-flight value for the LORRI boresight is given in [38] as:
+
+ [ -0.99998064 ]
+ LORRI Boresight Vector (-Z ) = [ 0.00543141 ]
+ inst [ -0.00303788 ]
+
+ The new LORRI +Y vector is the component of the nominal LORRI +Y vector
+ in the NH_SPACECRAFT frame perpendicular to the updated boresight vector.
+ The LORRI X axis completes the right-handed orthogonal frame:
+
+ [ ] [ -0.005452680629036 0.002999533810427 0.99998064 ]
+ [ ROT ] = [ -0.999960367261253 -0.007054338553346 -0.00543141 ]
+ [ ] [ 0.007037910250677 -0.999970619120629 0.00303788 ]
+
+ \begindata
+
+ FRAME_NH_LORRI = -98300
+ FRAME_-98300_NAME = 'NH_LORRI'
+ FRAME_-98300_CLASS = 4
+ FRAME_-98300_CLASS_ID = -98300
+ FRAME_-98300_CENTER = -98
+ TKFRAME_-98300_SPEC = 'MATRIX'
+ TKFRAME_-98300_RELATIVE = 'NH_SPACECRAFT'
+ TKFRAME_-98300_MATRIX = ( -0.005452680629036,
+ -0.999960367261253,
+ 0.007037910250677,
+ 0.002999533810427,
+ -0.007054338553346,
+ -0.999970619120629,
+ 0.99998064,
+ -0.00543141,
+ 0.00303788 )
+ \begintext
+
+ LORRI has two binning modes - 1x1 and 4x4. Separate frames are defined
+ below for each of those modes. The frames are identical to the NH_LORRI
+ frame, hence the identity rotation.
+
+ \begindata
+
+ FRAME_NH_LORRI_1X1 = -98301
+ FRAME_-98301_NAME = 'NH_LORRI_1X1'
+ FRAME_-98301_CLASS = 4
+ FRAME_-98301_CLASS_ID = -98301
+ FRAME_-98301_CENTER = -98
+ TKFRAME_-98301_SPEC = 'MATRIX'
+ TKFRAME_-98301_RELATIVE = 'NH_LORRI'
+ TKFRAME_-98301_MATRIX = ( 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0 )
+
+ FRAME_NH_LORRI_4X4 = -98302
+ FRAME_-98302_NAME = 'NH_LORRI_4X4'
+ FRAME_-98302_CLASS = 4
+ FRAME_-98302_CLASS_ID = -98302
+ FRAME_-98302_CENTER = -98
+ TKFRAME_-98302_SPEC = 'MATRIX'
+ TKFRAME_-98302_RELATIVE = 'NH_LORRI'
+ TKFRAME_-98302_MATRIX = ( 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0 )
+ \begintext
+
+
+Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Frames
+-------------------------------------------------------------------------------
+
+ From [18], PEPSSI is mounted on the spacecraft +Y panel in the -X/-Z corner
+ of the spacecraft's top panel. It has been mounted on a bracket to provide
+ a clear field of view.
+
+ The PEPSSI coordinate system is defined in Figure A-4 of [18] such that
+ the instrument Z axis is the normal vector to the baffle shielding the
+ the instrument from the high gain antenna, the instrument Y axis is the
+ instrument look direction, and the instrument X axis completes the right-
+ handed frame. Three coarse reproductions of Figure A-4 are shown below.
+ The coordinate system is displayed above each diagram. Figure A-5 of [18]
+ shows the instrument mounted to its bracket. The mounting bracket is
+ represented by the column of "B"s in the diagrams below):
+
+ +Z -X +Z
+ ^ inst ^ inst ^ inst
+ | | |
+ | | |
+ x----> +X o----> +Y o----> +Y
+ +Y (in) inst +Z (out) inst +X (out) inst
+ inst inst __ inst
+ | ``-.
+ | `.
+ ____________________ B _________|_ ' ____________
+ |____________________| B| `. \ B ______|____________|
+ | | B| \ . B| |____|
+ ^ | | B| | | B| | ^
+ | | | B| / ' B| | ^ |
+ | | | B|_________ _,' / B| | | |
+ baffle | | B | , B| | | baffle
+ points |________| | ,' B|_________| |
+ into baffle --> |__..-` B sensor
+ page
+
+ The PEPSSI alignment is given in [9] as a single vector - the measured
+ normal to the instrument baffle. This vector defines the instrument +Z
+ axis:
+
+ [ 0.4574230384 ]
+ PEPSSI baffle normal (+Z ) = [ 0.2112844736 ]
+ inst [ 0.8637841369 ]
+
+ The nominal instrument look direction is determined by analyzing the
+ mechanical drawings of the instrument mounting bracket [25]. Figure A-5
+ of [18] shows PEPSSI mounted on the sloped face of the bracket, with its
+ look direction (instrument +Y axis) normal to the sloped face. Two views
+ of the mounting bracket in the spacecraft coordinate frame are [25]:
+
+ ^ Y ^ Y
+ | sc | sc
+ | |
+ X <------x Z (in) X (in) x------> Z
+ sc sc sc sc
+
+ _ _ _ _ _ _ _____ _ _ _ _ _ _ ______
+ o _.-' | o _.-' |
+ 28.343 _.-' _| 27.832 _.-' |
+ .-' _.-' | .-' |
+ | _.-' | | |
+ | _.-' | | |
+ .-'_____________| |________________|
+ //////////////////////// ////////////////////////
+ spacecraft spacecraft
+
+ The face of the bracket on which PEPSSI is mounted is the outward-facing
+ sloped surface in the above left diagram. The normal to the face is the
+ instrument +Y axis. To calculate the normal, we first use the given angles
+ to find two vectors in the plane of the bracket face:
+
+ V1 = [ cos(28.343 deg), -sin(28.343 deg), 0 ]
+
+ V2 = [ 0, -sin(27.832 deg), -cos(27.832 deg) ]
+
+ The normal to the bracket face (instrument +Y) is given in spacecraft
+ coordinates by the cross product:
+
+ [ 0.430539299735951 ]
+ Y = V1 x V2 = [ 0.798162645175740 ]
+ inst [ -0.421393288068217 ]
+
+ The instrument X axis is orthogonal to the plane containing the
+ instrument Y and Z axes:
+
+ [ 0.778475068630558 ]
+ X = Y x Z = [ -0.564648724992781 ]
+ inst inst inst [ -0.274132057382342 ]
+
+ The Y axis is adjusted to form an orthogonal frame:
+
+ [ 0.429814764127889 ]
+ Y = Z x X = [ 0.797828733864454 ]
+ inst inst inst [ -0.422763030500455 ]
+
+ Using these three vectors, we define the rotation that takes vectors from
+ the instrument frame to the spacecraft frame as
+
+ [ ] [ 0.778475068630558 0.429814764127889 0.4574230384 ]
+ [ ROT ] = [ -0.564648724992781 0.797828733864454 0.2112844736 ]
+ [ ] [ -0.274132057382342 -0.422763030500455 0.8637841369 ]
+
+ \begindata
+
+ FRAME_NH_PEPSSI_ENG = -98400
+ FRAME_-98400_NAME = 'NH_PEPSSI_ENG'
+ FRAME_-98400_CLASS = 4
+ FRAME_-98400_CLASS_ID = -98400
+ FRAME_-98400_CENTER = -98
+ TKFRAME_-98400_SPEC = 'MATRIX'
+ TKFRAME_-98400_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98400_MATRIX = ( 0.778475068630558
+ -0.564648724992781
+ -0.274132057382342
+ 0.429814764127889
+ 0.797828733864454
+ -0.422763030500455
+ 0.4574230384
+ 0.2112844736
+ 0.8637841369 )
+
+ \begintext
+
+ Note that it was determined ([24], [26]) that PEPSSI was incorrectly
+ mounted on the spacecraft. The above frame definition describes the
+ actual mounting on the spacecraft, which is different from the intended
+ mounting specification, described in [26]. [24] also suggests that the
+ Euler rotations in Figure A-5 of [18] describe neither the mounting
+ specification nor the actual mounting, but rather a permutation of the
+ mounting specification.
+
+ The PEPSSI frame defined above has been named NH_PEPSSI_ENG to denote that
+ its coordinate system is defined in the engineering diagrams found in [18].
+ The NH_PEPSSI frame below is a rotation of the NH_PEPSSI_ENG frame that is
+ more suitable for data analysis [36]. In the NH_PEPSSI frame, the +Z axis
+ is the boresight, and the -Y axis is the normal vector to the baffle. The
+ NH_PEPSSI frame defined in this way is also referred to in the instrument
+ kernel as the frame for defining the boresight vectors and boundary corner
+ vectors of the PEPSSI sectors.
+
+ \begindata
+
+ FRAME_NH_PEPSSI = -98401
+ FRAME_-98401_NAME = 'NH_PEPSSI'
+ FRAME_-98401_CLASS = 4
+ FRAME_-98401_CLASS_ID = -98401
+ FRAME_-98401_CENTER = -98
+ TKFRAME_-98401_SPEC = 'MATRIX'
+ TKFRAME_-98401_RELATIVE = 'NH_PEPSSI_ENG'
+ TKFRAME_-98401_MATRIX = ( 1.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0
+ -1.0
+ 0.0
+ 1.0
+ 0.0 )
+
+ \begintext
+
+ As a convenience, an individual frame is defined below for each of the six
+ PEPSSI sectors and twelve detectors. The boresight is defined to be the
+ +Z axis in each frame.
+
+ The following sector frames were determined by rotating the NH_PEPSSI frame
+ about the NH_PEPSSI Y axis by the number of degrees required to move the
+ NH_PEPSSI boresight (NH_PEPSSI +Z axis) into the center of the sector's
+ field of view. Refer to the PEPSSI instrument kernel, nh_pepssi.ti, for
+ more details on the rotation angles and physical locations of sectors S0
+ through S5.
+
+ \begindata
+
+ FRAME_NH_PEPSSI_S0 = -98402
+ FRAME_-98402_NAME = 'NH_PEPSSI_S0'
+ FRAME_-98402_CLASS = 4
+ FRAME_-98402_CLASS_ID = -98402
+ FRAME_-98402_CENTER = -98
+ TKFRAME_-98402_SPEC = 'MATRIX'
+ TKFRAME_-98402_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98402_MATRIX = (0.382683432365090
+ 0.000000000000000
+ 0.923879532511287
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.923879532511287
+ 0.000000000000000
+ 0.382683432365090 )
+
+ FRAME_NH_PEPSSI_S1 = -98403
+ FRAME_-98403_NAME = 'NH_PEPSSI_S1'
+ FRAME_-98403_CLASS = 4
+ FRAME_-98403_CLASS_ID = -98403
+ FRAME_-98403_CENTER = -98
+ TKFRAME_-98403_SPEC = 'MATRIX'
+ TKFRAME_-98403_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98403_MATRIX = (0.760405965600031
+ 0.000000000000000
+ 0.649448048330184
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.649448048330184
+ 0.000000000000000
+ 0.760405965600031 )
+
+ FRAME_NH_PEPSSI_S2 = -98404
+ FRAME_-98404_NAME = 'NH_PEPSSI_S2'
+ FRAME_-98404_CLASS = 4
+ FRAME_-98404_CLASS_ID = -98404
+ FRAME_-98404_CENTER = -98
+ TKFRAME_-98404_SPEC = 'MATRIX'
+ TKFRAME_-98404_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98404_MATRIX = (0.972369920397677
+ 0.000000000000000
+ 0.233445363855905
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.233445363855905
+ 0.000000000000000
+ 0.972369920397677 )
+
+ FRAME_NH_PEPSSI_S3 = -98405
+ FRAME_-98405_NAME = 'NH_PEPSSI_S3'
+ FRAME_-98405_CLASS = 4
+ FRAME_-98405_CLASS_ID = -98405
+ FRAME_-98405_CENTER = -98
+ TKFRAME_-98405_SPEC = 'MATRIX'
+ TKFRAME_-98405_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98405_MATRIX = (0.972369920397677
+ 0.000000000000000
+ -0.233445363855905
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.233445363855905
+ 0.000000000000000
+ 0.972369920397677 )
+
+ FRAME_NH_PEPSSI_S4 = -98406
+ FRAME_-98406_NAME = 'NH_PEPSSI_S4'
+ FRAME_-98406_CLASS = 4
+ FRAME_-98406_CLASS_ID = -98406
+ FRAME_-98406_CENTER = -98
+ TKFRAME_-98406_SPEC = 'MATRIX'
+ TKFRAME_-98406_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98406_MATRIX = (0.760405965600031
+ 0.000000000000000
+ -0.649448048330184
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.649448048330184
+ 0.000000000000000
+ 0.760405965600031 )
+
+ FRAME_NH_PEPSSI_S5 = -98407
+ FRAME_-98407_NAME = 'NH_PEPSSI_S5'
+ FRAME_-98407_CLASS = 4
+ FRAME_-98407_CLASS_ID = -98407
+ FRAME_-98407_CENTER = -98
+ TKFRAME_-98407_SPEC = 'MATRIX'
+ TKFRAME_-98407_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98407_MATRIX = (0.382683432365090
+ 0.000000000000000
+ -0.923879532511287
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.923879532511287
+ 0.000000000000000
+ 0.382683432365090 )
+
+ \begintext
+
+
+ The following detector frames were determined by rotating the NH_PEPSSI
+ frame about the NH_PEPSSI Y axis by the number of degrees required to move
+ the NH_PEPSSI boresight (NH_PEPSSI +Z axis) into the center of the
+ detector's field of view. Refer to the PEPSSI instrument kernel,
+ nh_pepssi.ti, for more details on the rotation angles and physical
+ locations of detectors D0 through D11.
+
+ \begindata
+
+ FRAME_NH_PEPSSI_D0 = -98408
+ FRAME_-98408_NAME = 'NH_PEPSSI_D0'
+ FRAME_-98408_CLASS = 4
+ FRAME_-98408_CLASS_ID = -98408
+ FRAME_-98408_CENTER = -98
+ TKFRAME_-98408_SPEC = 'MATRIX'
+ TKFRAME_-98408_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98408_MATRIX = (0.279829014030992
+ 0.000000000000000
+ 0.960049854385929
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.960049854385929
+ 0.000000000000000
+ 0.279829014030992 )
+
+ FRAME_NH_PEPSSI_D1 = -98409
+ FRAME_-98409_NAME = 'NH_PEPSSI_D1'
+ FRAME_-98409_CLASS = 4
+ FRAME_-98409_CLASS_ID = -98409
+ FRAME_-98409_CENTER = -98
+ TKFRAME_-98409_SPEC = 'MATRIX'
+ TKFRAME_-98409_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98409_MATRIX = (0.480988768919388
+ 0.000000000000000
+ 0.876726755707508
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.876726755707508
+ 0.000000000000000
+ 0.480988768919388 )
+
+ FRAME_NH_PEPSSI_D2 = -98410
+ FRAME_-98410_NAME = 'NH_PEPSSI_D2'
+ FRAME_-98410_CLASS = 4
+ FRAME_-98410_CLASS_ID = -98410
+ FRAME_-98410_CENTER = -98
+ TKFRAME_-98410_SPEC = 'MATRIX'
+ TKFRAME_-98410_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98410_MATRIX = (0.685182990326359
+ 0.000000000000000
+ 0.728370969882400
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.728370969882400
+ 0.000000000000000
+ 0.685182990326359 )
+
+ FRAME_NH_PEPSSI_D3 = -98411
+ FRAME_-98411_NAME = 'NH_PEPSSI_D3'
+ FRAME_-98411_CLASS = 4
+ FRAME_-98411_CLASS_ID = -98411
+ FRAME_-98411_CENTER = -98
+ TKFRAME_-98411_SPEC = 'MATRIX'
+ TKFRAME_-98411_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98411_MATRIX = (0.826589749127189
+ 0.000000000000000
+ 0.562804927695069
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.562804927695069
+ 0.000000000000000
+ 0.826589749127189 )
+
+ FRAME_NH_PEPSSI_D4 = -98412
+ FRAME_-98412_NAME = 'NH_PEPSSI_D4'
+ FRAME_-98412_CLASS = 4
+ FRAME_-98412_CLASS_ID = -98412
+ FRAME_-98412_CENTER = -98
+ TKFRAME_-98412_SPEC = 'MATRIX'
+ TKFRAME_-98412_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98412_MATRIX = (0.941176015256371
+ 0.000000000000000
+ 0.337916718003327
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.337916718003327
+ 0.000000000000000
+ 0.941176015256371 )
+
+ FRAME_NH_PEPSSI_D5 = -98413
+ FRAME_-98413_NAME = 'NH_PEPSSI_D5'
+ FRAME_-98413_CLASS = 4
+ FRAME_-98413_CLASS_ID = -98413
+ FRAME_-98413_CENTER = -98
+ TKFRAME_-98413_SPEC = 'MATRIX'
+ TKFRAME_-98413_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98413_MATRIX = (0.992004949679715
+ 0.000000000000000
+ 0.126198969135830
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ -0.126198969135830
+ 0.000000000000000
+ 0.992004949679715 )
+
+ FRAME_NH_PEPSSI_D6 = -98414
+ FRAME_-98414_NAME = 'NH_PEPSSI_D6'
+ FRAME_-98414_CLASS = 4
+ FRAME_-98414_CLASS_ID = -98414
+ FRAME_-98414_CENTER = -98
+ TKFRAME_-98414_SPEC = 'MATRIX'
+ TKFRAME_-98414_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98414_MATRIX = (0.992004949679715
+ 0.000000000000000
+ -0.126198969135830
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.126198969135830
+ 0.000000000000000
+ 0.992004949679715 )
+
+ FRAME_NH_PEPSSI_D7 = -98415
+ FRAME_-98415_NAME = 'NH_PEPSSI_D7'
+ FRAME_-98415_CLASS = 4
+ FRAME_-98415_CLASS_ID = -98415
+ FRAME_-98415_CENTER = -98
+ TKFRAME_-98415_SPEC = 'MATRIX'
+ TKFRAME_-98415_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98415_MATRIX = (0.941176015256371
+ 0.000000000000000
+ -0.337916718003327
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.337916718003327
+ 0.000000000000000
+ 0.941176015256371 )
+
+ FRAME_NH_PEPSSI_D8 = -98416
+ FRAME_-98416_NAME = 'NH_PEPSSI_D8'
+ FRAME_-98416_CLASS = 4
+ FRAME_-98416_CLASS_ID = -98416
+ FRAME_-98416_CENTER = -98
+ TKFRAME_-98416_SPEC = 'MATRIX'
+ TKFRAME_-98416_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98416_MATRIX = (0.826589749127189
+ 0.000000000000000
+ -0.562804927695069
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.562804927695069
+ 0.000000000000000
+ 0.826589749127189 )
+
+ FRAME_NH_PEPSSI_D9 = -98417
+ FRAME_-98417_NAME = 'NH_PEPSSI_D9'
+ FRAME_-98417_CLASS = 4
+ FRAME_-98417_CLASS_ID = -98417
+ FRAME_-98417_CENTER = -98
+ TKFRAME_-98417_SPEC = 'MATRIX'
+ TKFRAME_-98417_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98417_MATRIX = (0.685182990326359
+ 0.000000000000000
+ -0.728370969882400
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.728370969882400
+ 0.000000000000000
+ 0.685182990326359 )
+
+ FRAME_NH_PEPSSI_D10 = -98418
+ FRAME_-98418_NAME = 'NH_PEPSSI_D10'
+ FRAME_-98418_CLASS = 4
+ FRAME_-98418_CLASS_ID = -98418
+ FRAME_-98418_CENTER = -98
+ TKFRAME_-98418_SPEC = 'MATRIX'
+ TKFRAME_-98418_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98418_MATRIX = (0.480988768919388
+ 0.000000000000000
+ -0.876726755707508
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.876726755707508
+ 0.000000000000000
+ 0.480988768919388 )
+
+ FRAME_NH_PEPSSI_D11 = -98419
+ FRAME_-98419_NAME = 'NH_PEPSSI_D11'
+ FRAME_-98419_CLASS = 4
+ FRAME_-98419_CLASS_ID = -98419
+ FRAME_-98419_CENTER = -98
+ TKFRAME_-98419_SPEC = 'MATRIX'
+ TKFRAME_-98419_RELATIVE = 'NH_PEPSSI'
+ TKFRAME_-98419_MATRIX = (0.279829014030992
+ 0.000000000000000
+ -0.960049854385929
+ 0.000000000000000
+ 1.000000000000000
+ 0.000000000000000
+ 0.960049854385929
+ 0.000000000000000
+ 0.279829014030992 )
+
+ \begintext
+
+
+Radio Science Experiment (REX) Frames
+-------------------------------------------------------------------------------
+
+ We are defining the REX coordinate system such that the +Z axis in
+ instrument coordinates is the boresight, the +X axis in instrument
+ coordinates is aligned with the spacecraft +X axis, and the +Y axis in
+ instrument coordinates is aligned with the spacecraft -Z axis. The
+ measured boresight vector is given in [9] as
+
+ [ 0.0000823 ]
+ REX Boresight Vector (+Z ) = [ 1.0 ]
+ inst [ -0.0001249 ]
+
+ Since we defined the instrument +X axis to be the spacecraft +X axis, we
+ have:
+
+ [ 1.0 ]
+ REX +X Vector = [ 0.0 ]
+ [ 0.0 ]
+
+ The instrument +Y vector is determined by taking the cross product Z x X:
+
+ [ 0.0 ]
+ REX +Y Vector = [ -0.000124900004202 ]
+ [ -0.999999992199995 ]
+
+ And we use that to adjust the +X vector to form an orthogonal frame:
+
+ [ 0.999999996613355 ]
+ REX +X Vector = Y x Z = [ -0.000082299999378 ]
+ [ 0.000000010279270 ]
+
+ Using these three vectors, we define the rotation matrix that takes vectors
+ from the instrument frame to the spacecraft frame as
+
+ [ ] [ 0.999999996613355 0.0 0.0000823 ]
+ [ ROT ] = [ -0.000082299999378 -0.000124900004202 1.0 ]
+ [ ] [ 0.000000010279270 -0.999999992199995 -0.0001249 ]
+
+ \begindata
+
+ FRAME_NH_REX = -98500
+ FRAME_-98500_NAME = 'NH_REX'
+ FRAME_-98500_CLASS = 4
+ FRAME_-98500_CLASS_ID = -98500
+ FRAME_-98500_CENTER = -98
+ TKFRAME_-98500_SPEC = 'MATRIX'
+ TKFRAME_-98500_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98500_MATRIX = ( 0.999999996613355,
+ -0.000082299999378,
+ 0.000000010279270,
+ 0.0,
+ -0.000124900004202,
+ -0.999999992199995,
+ 0.0000823,
+ 1.0,
+ -0.0001249 )
+
+ \begintext
+
+
+Solar Wind Around Pluto (SWAP) Frames
+-------------------------------------------------------------------------------
+
+ From [20], SWAP is mounted on the -Z panel of the New Horizons Spacecraft
+ and uses the same coordinate system as the spacecraft. The rotation matrix
+ that takes vectors represented in the nominal SWAP frame into the spacecraft
+ frame is the identity. We will adjust the rotation to take into account the
+ measured alignment provided in [9]:
+
+ [ 0.9999672 ]
+ SWAP Measured +X Vector = [ 0.0080965 ]
+ [ -0.0000296 ]
+
+ [ 0.0000469 ]
+ SWAP Measured +Z Vector = [ -0.0021315 ]
+ [ 0.9999977 ]
+
+ Taking the cross product of these two vectors gives us:
+
+ [ -0.0080964188 ]
+ SWAP +Y Vector (Boresight) = Z x X = [ 0.9999649500 ]
+ [ 0.0021318100 ]
+
+ And we use that to adjust the Z vector to form an orthogonal frame:
+
+ [ 0.000046859163 ]
+ SWAP +Z Vector = X x Y = [ -0.002131500500 ]
+ [ 0.999997730000 ]
+
+ [ ] [ 0.9999672 -0.0080964188 0.000046859163 ]
+ [ ROT ] = [ 0.0080965 0.9999649500 -0.002131500500 ]
+ [ ] [ -0.0000296 0.0021318100 0.999997730000 ]
+
+ \begindata
+
+ FRAME_NH_SWAP = -98600
+ FRAME_-98600_NAME = 'NH_SWAP'
+ FRAME_-98600_CLASS = 4
+ FRAME_-98600_CLASS_ID = -98600
+ FRAME_-98600_CENTER = -98
+ TKFRAME_-98600_SPEC = 'MATRIX'
+ TKFRAME_-98600_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98600_MATRIX = ( 0.9999672,
+ 0.0080965,
+ -0.0000296,
+ -0.0080964188,
+ 0.9999649500,
+ 0.0021318100,
+ 0.000046859163,
+ -0.002131500500,
+ 0.999997730000 )
+
+ \begintext
+
+
+Student Dust Counter (SDC) Frames
+-------------------------------------------------------------------------------
+
+ The SDC coordinate system is defined [16] such that the boresight is the
+ instrument +Z axis. This corresponds to the spacecraft -Y axis. The
+ instrument X axis is defined such that it is along the detector's long
+ dimension, with instrument +X corresponding to spacecraft +Z. The
+ instrument Y axis is defined such that it is along the detector's short
+ dimension, with instrument +Y corresponding to the spacecraft -X axis. The
+ rotation matrix that takes vectors from the instrument frame to the
+ spacecraft frame is then:
+
+ [ ] [ 0 -1 0 ]
+ [ ROT ] = [ 0 0 -1 ]
+ [ ] [ 1 0 0 ]
+
+ \begindata
+
+ FRAME_NH_SDC = -98700
+ FRAME_-98700_NAME = 'NH_SDC'
+ FRAME_-98700_CLASS = 4
+ FRAME_-98700_CLASS_ID = -98700
+ FRAME_-98700_CENTER = -98
+ TKFRAME_-98700_SPEC = 'MATRIX'
+ TKFRAME_-98700_RELATIVE = 'NH_ASTR'
+ TKFRAME_-98700_MATRIX = ( 0.0,
+ 0.0,
+ 1.0,
+ -1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ -1.0,
+ 0.0 )
+
+ \begintext
+
+
diff --git a/tests/pytests/data/lsb_0296962438_0x53c_eng/pck00010.tpc b/tests/pytests/data/lsb_0296962438_0x53c_eng/pck00010.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..1bc2d759b231fe8682b7b2e4693c87be7ed7770a
--- /dev/null
+++ b/tests/pytests/data/lsb_0296962438_0x53c_eng/pck00010.tpc
@@ -0,0 +1,4096 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "pck00010.tpc"
+MISSION_NAME = "NEW HORIZONS"
+SPACECRAFT_NAME = "NEW HORIZONS"
+DATA_SET_ID = "NH-J/P/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = PCK
+PRODUCT_ID = "pck00010.tpc"
+PRODUCT_CREATION_TIME = 2011-10-21T00:00:00
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = {
+ JUPITER,
+ PLUTO,
+ "SOLAR SYSTEM"
+ }
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = TARGET_CONSTANTS
+ DESCRIPTION = "NAIF planetary constants kernel "
+END_OBJECT = SPICE_KERNEL
+END
+\endlabel
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2011 October 21
+
+
+Purpose
+--------------------------------------------------------
+
+ This file makes available for use in SPICE-based application
+ software orientation and size/shape data for natural bodies. The
+ principal source of the data is a published report by the IAU
+ Working Group on Cartographic Coordinates and Rotational Elements
+ [1].
+
+ Orientation and size/shape data not provided by this file may be
+ available in mission-specific PCK files. Such PCKs may be the
+ preferred data source for mission-related applications.
+ Mission-specific PCKs can be found in PDS archives or on the NAIF
+ web site at URL:
+
+ http://naif.jpl.nasa.gov/naif/data
+
+
+File Organization
+--------------------------------------------------------
+
+ The contents of this file are as follows.
+
+ Introductory Information:
+
+ -- Purpose
+
+ -- File Organization
+
+ -- Version description
+
+ -- Disclaimer
+
+ -- Sources
+
+ -- Explanatory notes
+
+ -- Body numbers and names
+
+
+ PcK Data:
+
+
+ Orientation Data
+ ----------------
+
+ -- Orientation constants for the Sun, planets, and
+ Pluto. Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole value
+ for the epochs 2012
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids
+
+ Davida
+ Eros
+ Gaspra
+ Ida
+ Itokawa
+ Lutetia
+ Pallas
+ Steins
+ Vesta
+
+ -- Orientation constants for comets
+
+ 19P/Borrelly
+ 9P/Tempel 1
+
+
+ Orientation data provided in this file are used
+ by the SPICE Toolkit to evaluate the orientation
+ of body-fixed, body-centered reference frames
+ with respect to the ICRF frame ("J2000" in
+ SPICE documentation). These body-fixed frames
+ have names of the form
+
+ IAU_<body name>
+
+ for example
+
+ IAU_JUPITER
+
+ See the PCK Required Reading file pck.req for details.
+
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun, planets, and Pluto
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids
+
+ Ceres
+ Davida
+ Eros
+ Gaspra
+ Ida
+ Itokawa
+ Lutetia
+ Mathilde
+ Steins
+ Toutatis
+ Vesta
+
+ -- Radii of comets
+
+ 19P/Borrelly
+ 81P/Wild 2
+ 9P/Tempel 1
+ Halley
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on October 21, 2011 at NASA's Navigation and
+ Ancillary Information Facility (NAIF), located at the Jet
+ Propulsion Laboratory, Pasadena, CA.
+
+ The previous version of the file was
+
+ pck00009.tpc
+
+ That file was published March 3 2010.
+
+ This version incorporates data from reference [1]. This file
+ contains size, shape, and orientation data for all objects covered
+ by the previous version of the file.
+
+ New objects covered by this file but not the previous
+ version are:
+
+ Anthe
+ Daphnis
+ Davida
+ Lutetia
+ Methone
+ Pallas
+ Pallene
+ Polydeuces
+ Steins
+
+
+
+Disclaimer
+--------------------------------------------------------
+
+Applicability of Data
+
+ This P_constants file may not contain the parameter values that
+ you prefer. NAIF suggests that you inspect this file visually
+ before proceeding with any critical or extended data processing.
+
+File Modifications by Users
+
+ Note that this file may be readily modified by you to change
+ values or add/delete parameters. NAIF requests that you update the
+ "by line," date, version description section, and file name
+ if you modify this file.
+
+ A user-modified file should be thoroughly tested before
+ being published or otherwise distributed.
+
+ P_constants files must conform to the standards described
+ in the two SPICE technical reference documents:
+
+ PCK Required Reading
+ Kernel Required Reading
+
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU Working Group Report [1] to be accurate to 0.1 degree
+ ([1], p.158). However, NAIF notes that orientation models for
+ natural satellites and asteroids have in some cases changed
+ substantially with the availability of new observational data, so
+ users are urged to investigate the suitability for their
+ applications of the models presented here.
+
+ Earth orientation
+ -----------------
+
+ NAIF strongly cautions against using the earth rotation model
+ (from [1]), corresponding to the SPICE reference frame name
+ IAU_EARTH, for work demanding high accuracy. This model has been
+ determined by NAIF to have an error in the prime meridian location
+ of magnitude at least 150 arcseconds, with a local minimum
+ occurring during the year 1999. Regarding availability of better
+ earth orientation data for use with the SPICE system:
+
+ Earth orientation data are available from NAIF in the form of
+ binary earth PCK files. These files provide orientation data
+ for the ITRF93 (terrestrial) reference frame relative to the
+ ICRF.
+
+ NAIF employs an automated process to create these files; each
+ time JPL's Tracking Systems and Applications Section produces a
+ new earth orientation parameter (EOP) file, a new PCK is
+ produced. These PCKs cover a roughly 10 year time span starting
+ at Jan. 1, 2000. In these PCK files, the following effects are
+ accounted for in modeling the earth's rotation:
+
+ - Precession: 1976 IAU model
+
+ - Nutation: 1980 IAU model, plus interpolated
+ EOP nutation corrections
+
+ - Polar motion: interpolated from EOP file
+
+ - True sidereal time:
+
+ UT1 - UT1R (if needed): given by analytic formula
+ + TAI - UT1 (or UT1R): interpolated from EOP file
+ + UT1 - GMST: given by analytic formula
+ + equation of equinoxes: given by analytic formula
+
+ where
+
+ TAI = International Atomic Time
+ UT1 = Greenwich hour angle of computed mean sun - 12h
+ UT1R = Regularized UT1
+ GMST = Greenwich mean sidereal time
+
+ These kernels are available from the NAIF web site
+
+ http://naif.jpl.nasa.gov
+
+ (follow the links to Data, generic_kernels, and PCK data) or
+
+ ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck
+
+ or via anonymous ftp from the server
+
+ naif.jpl.nasa.gov
+
+ The kernels are in the path
+
+ pub/naif/generic_kernels/pck
+
+ At this time, these kernels have file names of the form
+
+ earth_000101_yymmdd_yymmdd.bpc
+
+ The first date in the file name, meaning 2000 January 1, is the
+ file's coverage begin time. The second and third dates are,
+ respectively, the file's coverage end time and the epoch of the
+ last datum.
+
+ These binary PCK files are very accurate (error < 0.1
+ microradian) for epochs preceding the epoch of the last datum.
+ For later epochs, the error rises to several microradians.
+
+ Binary PCK files giving accurate earth orientation from 1972 to
+ 2007 and *low accuracy* predicted earth orientation from
+ 2007 to 2037 are also available in the same location. See the
+ aareadme.txt file at the "pck" URL above for details.
+
+ Characteristics and names of the binary kernels described here
+ are subject to change. See the "pck" URL above for information
+ on current binary earth PCKs.
+
+
+ Lunar orientation
+ -----------------
+
+ The lunar orientation formula provided by this file is a
+ trigonometric polynomial approximation yielding the orientation of
+ the lunar "Mean Earth/Polar Axis" (ME) reference frame. The
+ SPICE reference frame name corresponding to this model is
+ IAU_MOON.
+
+ A more accurate approximation can be obtained by using both the
+ NAIF lunar frame kernel and the binary lunar orientation PCK file.
+ These files provide orientation data for the both the Mean
+ Earth/Polar Axis frame, which has the SPICE name MOON_ME, and the
+ Lunar Principal Axes frame, which has the SPICE name MOON_PA.
+
+ These files are available on the NAIF web site (see URLs above)
+ and in the NAIF server's ftp area. The lunar frame kernel is
+ located in the path
+
+ pub/naif/generic_kernels/fk/satellites
+
+ and has a name of the form
+
+ moon_yymmdd.tf
+
+ The binary lunar PCK is in the path
+
+ pub/naif/generic_kernels/pck
+
+ and has a name of the form
+
+ moon_pa_dennn_yyyy-yyyy.bpc
+
+ See the "aareadme.txt" files in the paths shown above for details
+ on file contents and versions. We also suggest you refer to the
+ SPICE tutorial named "lunar_earth_pck-fk," which is available from
+ the NAIF web site.
+
+
+ Earth geomagnetic dipole
+ ------------------------
+
+ The SPICE Toolkit doesn't currently contain software to model the
+ earth's north geomagnetic centered dipole as a function of time.
+ As a convenience for users, the north dipole location from the
+ epoch 2012.0 was selected as a representative datum, and the
+ planetocentric longitude and latitude of this location have been
+ associated with the keywords
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT
+
+ Values for the earth's north geomagnetic centered dipole are
+ presented in comments as a discrete time series for the time range
+ 1945-2000. For details concerning the geomagnetic field model from
+ which these values were derived, including a discussion of the
+ model's accuracy, see [9] and [11].
+
+
+ Prime meridian offsets
+ ----------------------
+
+ Prime meridian offset kernel variables, which have names
+ of the form
+
+ BODYnnn_LONG_AXIS
+
+ are not used by SPICE geometry software. These variables should be
+ considered deprecated; however, they will be retained for
+ backwards compatibility.
+
+ Users wishing to specify an offset reflecting the orientation of a
+ reference ellipsoid relative to a body-fixed reference frame
+ specified here should do so by creating a constant-offset frame
+ (also called a "TK" frame) specification. See the Frames Required
+ Reading frames.req for details.
+
+ The Mars prime meridian offset given by [5] is provided for
+ informational purposes only.
+
+
+ Software limitations
+ --------------------
+
+ SPICE Toolkits prior to version N0057 cannot make use of
+ trigonometric polynomial terms in the formulas for orientation of
+ the planets.
+
+ The second nutation precession angle (M2) for Mars is represented
+ by a quadratic polynomial in the 2006 IAU report. The SPICELIB
+ subroutine BODEUL can not handle this term (which is extremely
+ small), so we truncate the polynomial to a linear one. The
+ resulting orientation error has a maximum magnitude of less
+ than 0.0032 degrees over the time span 1996-2015 and less than
+ 0.0082 degrees over the time span 1986-2025.
+
+
+Sources and References
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] Archinal, B.A., A'Hearn, M.F., Bowell, E., Conrad, A.,
+ Consolmagno, G.J., Courtin, R., Fukushima, T.,
+ Hestroffer, D., Hilton, J.L., Krasinsky, G.A.,
+ Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P.,
+ Tholen, D.J., Thomas, P.C., and Williams, I.P.
+ "Report of the IAU Working Group on Cartographic Coordinates
+ and Rotational Elements: 2009."
+
+ [2] Archinal, B.A., A'Hearn, M.F., Conrad, A.,
+ Consolmagno, G.J., Courtin, R., Fukushima, T.,
+ Hestroffer, D., Hilton, J.L., Krasinsky, G.A.,
+ Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P.,
+ Tholen, D.J., Thomas, P.C., and Williams, I.P.
+ "Erratum to: Reports of the IAU Working Group on
+ Cartographic Coordinates and Rotational Elements: 2006 &
+ 2009."
+
+ [3] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Conrad, A., Consolmagno, G.J., Hestroffer, D.,
+ Hilton, J.L., Krasinsky, G.A., Neumann, G.,
+ Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J.,
+ and Thomas, P.C. "Report of the IAU/IAG Working Group
+ on cartographic coordinates and rotational elements: 2006."
+
+ [4] Nautical Almanac Office, United States Naval Observatory
+ and H.M. Nautical Almanac Office, Rutherford Appleton
+ Laboratory (2010). "The Astronomical Almanac for
+ the Year 2010," U.S. Government Printing Office,
+ Washington, D.C.: and The Stationary Office, London.
+
+ [5] Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+ Conventions," presentation to the Mars Express Data
+ Archive Working Group, Dec. 14, 2001.
+
+ [6] Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic
+ Field and Magnetosphere." <http://www-ssc.igpp.ucla.
+ edu/personnel/russell/papers/earth_mag>. Originally
+ published in "Encyclopedia of Planetary Sciences," J.H.
+ Shirley and R.W. Fainbridge, eds. Chapman and Hall,
+ New York, pp 208-211.
+
+ [7] Russell, C.T. (1971). "Geophysical Coordinate
+ Transformations," Cosmic Electrodynamics 2 184-186.
+ NAIF document 181.0.
+
+ [8] ESA/ESTEC Space Environment Information System (SPENVIS)
+ (2003). Web page: "Dipole approximations of the
+ geomagnetic field." <http://www.spenvis.oma.be/spenvis/
+ help/background/magfield/cd.html>.
+
+ [9] International Association of Geomagnetism and Aeronomy
+ and International Union of Geodesy and Geophysics (2004).
+ Web page: "The 9th Generation International Geomagnetic
+ Reference Field." <http://www.ngdc.noaa.gov/
+ IAGA/vmod/igrf.html>.
+
+ [10] Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
+ and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
+ Working Group on Cartographic Coordinates and Rotational
+ Elements of the Planets and Satellites: 1988," Celestial
+ Mechanics and Dynamical Astronomy, v.46, no.2, pp.
+ 187-204.
+
+ [11] International Association of Geomagnetism and Aeronomy
+ Web page: "International Geomagnetic Reference Field."
+ Discussion URL:
+
+ http://www.ngdc.noaa.gov/IAGA/vmod/igrf.html
+
+ Coefficients URL:
+
+ http://www.ngdc.noaa.gov/IAGA/vmod/igrf11coeffs.txt
+
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [4].
+
+ -- Prime meridian constant (W0) terms for Pluto, Charon,
+ and Ida are from [2].
+
+ -- The second nutation precession angle (M2) for Mars is
+ represented by a quadratic polynomial in the 2000
+ IAU report. The SPICELIB subroutine BODEUL can not
+ handle this term (which is extremely small), so we
+ truncate the polynomial to a linear one.
+
+ -- Earth north geomagnetic centered dipole values are from
+ [11]. The values were also computed from the 11th
+ generation IGRF by Nat Bachman.
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00009.tpc dated March 3, 2010. Most of these values came
+ from the 2006 IAU report [3].
+
+
+
+
+Explanatory Notes
+--------------------------------------------------------
+
+ This file, which is logically part of the SPICE P-kernel, contains
+ constants used to model the orientation, size and shape of the
+ Sun, planets, natural satellites, and selected comets and
+ asteroids. The orientation models express the direction of the
+ pole and location of the prime meridian of a body as a function of
+ time. The size/shape models ("shape models" for short) represent
+ all bodies as ellipsoids, using two equatorial radii and a polar
+ radius. Spheroids and spheres are obtained when two or all three
+ radii are equal.
+
+ The SPICE Toolkit routines that use this file are documented in
+ the SPICE "Required Reading" file pck.req. They are also
+ documented in the "PCK" SPICE tutorial, which is available on
+ the NAIF web site.
+
+File Format
+
+ A terse description of the PCK file format is given here. See the
+ SPICE "Required Reading" files pck.req and kernel.req for a
+ detailed explanation of the SPICE text kernel file format. The
+ files pck.req and kernel.req are included in the documentation
+ provided with the SPICE Toolkit.
+
+ The file starts out with the ``ID word'' string
+
+ KPL/PCK
+
+ This string identifies the file as a text kernel containing PCK
+ data.
+
+ This file consists of a series of comment blocks and data blocks.
+ Comment blocks, which contain free-form descriptive or explanatory
+ text, are preceded by a \begintext token. Data blocks follow a
+ \begindata token. In order to be recognized, each of these tokens
+ must be placed on a line by itself.
+
+ The portion of the file preceding the first data block is treated
+ as a comment block; it doesn't require an initial \begintext
+ token.
+
+ This file identifies data using a series of
+
+ KEYWORD = VALUE
+
+ assignments. The left hand side of each assignment is a
+ "kernel variable" name; the right hand side is an associated value
+ or list of values. The SPICE subroutine API allows SPICE routines
+ and user applications to retrieve the set of values associated
+ with each kernel variable name.
+
+ Kernel variable names are case-sensitive and are limited to
+ 32 characters in length.
+
+ Numeric values may be integer or floating point. String values
+ are normally limited to 80 characters in length; however, SPICE
+ provides a mechanism for identifying longer, "continued" strings.
+ See the SPICE routine STPOOL for details.
+
+ String values are single quoted.
+
+ When the right hand side of an assignment is a list of values,
+ the list items may be separated by commas or simply by blanks.
+ The list must be bracketed by parentheses. Example:
+
+ BODY399_RADII = ( 6378.1366 6378.1366 6356.7519 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.1366
+ 6378.1366
+ 6356.7519 )
+
+ This file may contain blank lines anywhere. Non-printing
+ characters including TAB should not be present in the file: the
+ presence of such characters may cause formatting errors when the
+ file is viewed.
+
+Time systems and reference frames
+
+ The 2009 IAU Working Group Report [1] states the time scale used
+ as the independent variable for the rotation formulas is
+ Barycentric Dynamical Time (TDB) and that the epoch of variable
+ quantities is J2000 TDB (2000 Jan 1 12:00:00 TDB, Julian ephemeris
+ date 2451545.0 TDB). Throughout SPICE documentation and in this
+ file, we use the names "J2000 TDB" and "J2000" for this epoch. The
+ name "J2000.0" is equivalent.
+
+ SPICE documentation refers to the time system used in this file
+ as either "ET" or "TDB." SPICE software makes no distinction
+ between TDB and the time system associated with the independent
+ variable of the JPL planetary ephemerides T_eph.
+
+ The inertial reference frame used for the rotational elements in
+ this file is identified by [1] as the ICRF (International
+ Celestial Reference Frame).
+
+ The SPICE PCK software that reads this file uses the label "J2000"
+ to refer to the ICRF; this is actually a mislabeling which has
+ been retained in the interest of backward compatibility. Using
+ data from this file, by means of calls to the SPICE frame
+ transformation routines, will actually compute orientation
+ relative to the ICRF.
+
+ The difference between the J2000 frame and the ICRF is
+ on the order of tens of milliarcseconds and is well below the
+ accuracy level of the formulas in this file.
+
+Orientation models
+
+ All of the orientation models use three Euler angles to describe
+ the orientation of the coordinate axes of the "Body Equator and
+ Prime Meridian" system with respect to an inertial system. By
+ default, the inertial system is the ICRF (labeled as "J2000"), but
+ other inertial frames can be specified in the file. See the PCK
+ Required Reading for details.
+
+ The first two angles, in order, are the ICRF right ascension and
+ declination (henceforth RA and DEC) of the north pole of a body as
+ a function of time. The third angle is the prime meridian location
+ (represented by "W"), which is expressed as a rotation about the
+ north pole, and is also a function of time.
+
+ For each body, the expressions for the north pole's right
+ ascension and declination, as well as prime meridian location, are
+ sums (as far as the models that appear in this file are concerned)
+ of quadratic polynomials and trigonometric polynomials, where the
+ independent variable is time.
+
+ In this file, the time arguments in expressions always refer to
+ Barycentric Dynamical Time (TDB), measured in centuries or days
+ past a reference epoch. By default, the reference epoch is the
+ J2000 epoch, which is Julian ephemeris date 2451545.0 (2000 Jan 1
+ 12:00:00 TDB), but other epochs can be specified in the file. See
+ the PCK Required Reading for details.
+
+ Orientation models for satellites and some planets (including
+ Jupiter) involve both polynomial terms and trigonometric terms.
+ The arguments of the trigonometric terms are linear polynomials.
+ In this file, we call the arguments of these trigonometric terms
+ "nutation precession angles."
+
+ Example: 2009 IAU Model for orientation of Jupiter. Note that
+ these values are used as an example only; see the data area below
+ for current values.
+
+ Right ascension
+ ---------------
+
+ alpha = 268.056595 - 0.006499 T + 0.000117 sin(Ja)
+ 0 + 0.000938 sin(Jb) + 0.001432 sin(Jc)
+ + 0.000030 sin(Jd) + 0.002150 sin(Je)
+
+ Declination
+ -----------
+
+ delta = 64.495303 + 0.002413 T + 0.000050 cos(Ja)
+ 0 + 0.000404 cos(Jb) + 0.000617 cos(Jc)
+ - 0.000013 cos(Jd) + 0.000926 cos(Je)
+
+ Prime meridian
+ --------------
+
+ W = 284.95 + 870.5366420 d
+
+
+ Here
+
+ T represents centuries past J2000 ( TDB ),
+
+ d represents days past J2000 ( TDB ).
+
+ Ja-Je are nutation precession angles.
+
+ In this file, the polynomials' coefficients above are assigned
+ to kernel variable names (left-hand-side symbols) as follows
+
+ BODY599_POLE_RA = ( 268.056595 -0.006499 0. )
+ BODY599_POLE_DEC = ( 64.495303 0.002413 0. )
+ BODY599_PM = ( 284.95 870.5360000 0. )
+
+ and the trigonometric polynomials' coefficients are assigned
+ as follows
+
+ BODY599_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117
+ 0.000938
+ 0.001432
+ 0.000030
+ 0.002150 )
+
+ BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050
+ 0.000404
+ 0.000617
+ -0.000013
+ 0.000926 )
+
+ BODY599_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0 )
+
+ Note the number "599"; this is the NAIF ID code for Jupiter.
+
+ In this file, the polynomial expressions for the nutation
+ precession angles are listed along with the planet's RA, DEC, and
+ prime meridian terms. Below are the 2006 IAU nutation precession
+ angles for the Jupiter system.
+
+ J1 = 73.32 + 91472.9 T
+ J2 = 24.62 + 45137.2 T
+ J3 = 283.90 + 4850.7 T
+ J4 = 355.80 + 1191.3 T
+ J5 = 119.90 + 262.1 T
+ J6 = 229.80 + 64.3 T
+ J7 = 352.25 + 2382.6 T
+ J8 = 113.35 + 6070.0 T
+
+ J9 = 146.64 + 182945.8 T
+ J10 = 49.24 + 90274.4 T
+
+ Ja = 99.360714 + 4850.4046 T
+ Jb = 175.895369 + 1191.9605 T
+ Jc = 300.323162 + 262.5475 T
+ Jd = 114.012305 + 6070.2476 T
+ Je = 49.511251 + 64.3000 T
+
+ Here
+
+ T represents centuries past J2000 ( TDB )
+
+ J1-J10 and Ja-Je are the nutation precession angles. The angles
+ J9 and J10 are equal to 2*J1 and 2*J2, respectively.
+
+ Angles J9 and J10 are not present in [1]; they have been added
+ to fit the terms 2*J1 and 2*J2, which appear in the orientation
+ models of several satellites, into a form that can be accepted
+ by the PCK system.
+
+ The assignment of the nutation precession angles for the
+ Jupiter system is as follows:
+
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.25 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4
+ 99.360714 4850.4046
+ 175.895369 1191.9605
+ 300.323162 262.5475
+ 114.012305 6070.2476
+ 49.511251 64.3000 )
+
+ You'll see an additional symbol grouped with the ones listed
+ above; it is
+
+ BODY599_LONG_AXIS
+
+ This is a deprecated feature; see the note on "Prime meridian
+ offsets" under "Known Limitations and Caveats" above.
+
+ The pattern of the formulas for satellite orientation is similar
+ to that for Jupiter. Example: 2006 IAU values for Io. Again, these
+ values are used as an example only; see the data area below for
+ current values.
+
+ Right ascension
+ ---------------
+
+ alpha = 268.05 - 0.009 T + 0.094 sin(J3) + 0.024 sin(J4)
+ 0
+
+ Declination
+ -----------
+
+ delta = 64.50 + 0.003 T + 0.040 cos(J3) + 0.011 cos(J4)
+ 0
+
+ Prime meridian
+ --------------
+
+ W = 200.39 + 203.4889538 d - 0.085 sin(J3) - 0.022 sin(J4)
+
+
+ d represents days past J2000.
+
+ J3 and J4 are nutation precession angles.
+
+ The polynomial terms are assigned to symbols by the statements
+
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( 64.50 0.003 0. )
+ BODY501_PM = ( 200.39 203.4889538 0. )
+
+ The coefficients of the trigonometric terms are assigned to symbols by
+ the statements
+
+ BODY501_NUT_PREC_RA = ( 0. 0. 0.094 0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. 0.040 0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+
+ 501 is the NAIF ID code for Io.
+
+ SPICE software expects the models for satellite orientation to
+ follow the form of the model shown here: the polynomial portions of the
+ RA, DEC, and W expressions are expected to be quadratic, the
+ trigonometric terms for RA and W (satellite prime meridian) are expected
+ to be linear combinations of sines of nutation precession angles, the
+ trigonometric terms for DEC are expected to be linear combinations of
+ cosines of nutation precession angles, and the polynomials for the
+ nutation precession angles themselves are expected to be linear.
+
+ Eventually, the software will handle more complex expressions, we
+ expect.
+
+
+Shape models
+
+ There is only one kind of shape model supported by the SPICE
+ Toolkit software at present: the triaxial ellipsoid. The 2009 IAU
+ report [1] does not use any other models, except in the case of
+ Mars, where separate values are given for the north and south
+ polar radii. In this file, we provide as a datum the mean Mars
+ polar radius provided by [1]. The North and South values are
+ included as comments.
+
+ For each body, three radii are listed: The first number is
+ the largest equatorial radius (the length of the semi-axis
+ containing the prime meridian), the second number is the smaller
+ equatorial radius, and the third is the polar radius.
+
+ Example: Radii of the Earth.
+
+ BODY399_RADII = ( 6378.1366 6378.1366 6356.7519 )
+
+
+
+Body Numbers and Names
+--------------------------------------------------------
+
+
+ The following NAIF body ID codes and body names appear in this
+ file. See the NAIF IDs Required Reading file naif_ids.req for
+ a detailed discussion and a complete list of ID codes and names.
+
+
+ 1 Mercury barycenter
+ 2 Venus barycenter
+ 3 Earth barycenter
+ 4 Mars barycenter
+ 5 Jupiter barycenter
+ 6 Saturn barycenter
+ 7 Uranus barycenter
+ 8 Neptune barycenter
+ 9 Pluto barycenter
+ 10 Sun
+
+
+ 199 Mercury
+
+
+ 299 Venus
+
+
+ 399 Earth
+
+ 301 Moon
+
+
+ 499 Mars
+
+ 401 Phobos 402 Deimos
+
+
+ 599 Jupiter
+
+ 501 Io 502 Europa 503 Ganymede 504 Callisto
+ 505 Amalthea 506 Himalia 507 Elara 508 Pasiphae
+ 509 Sinope 510 Lysithea 511 Carme 512 Ananke
+ 513 Leda 514 Thebe 515 Adrastea 516 Metis
+
+
+ 699 Saturn
+
+ 601 Mimas 602 Enceladus 603 Tethys 604 Dione
+ 605 Rhea 606 Titan 607 Hyperion 608 Iapetus
+ 609 Phoebe 610 Janus 611 Epimetheus 612 Helene
+ 613 Telesto 614 Calypso 615 Atlas 616 Prometheus
+ 617 Pandora 618 Pan 632 Methone 633 Pallene
+ 634 Polydeuces 635 Daphnis 649 Anthe
+
+
+ 799 Uranus
+
+ 701 Ariel 702 Umbriel 703 Titania 704 Oberon
+ 705 Miranda 706 Cordelia 707 Ophelia 708 Bianca
+ 709 Cressida 710 Desdemona 711 Juliet 712 Portia
+ 713 Rosalind 714 Belinda 715 Puck
+
+
+ 899 Neptune
+
+ 801 Triton 802 Nereid 803 Naiad 804 Thalassa
+ 805 Despina 806 Galatea 807 Larissa 808 Proteus
+
+
+ 999 Pluto
+
+ 901 Charon
+
+
+ 1000005 Comet 19P/Borrelly
+ 1000036 Comet Halley
+ 1000093 Comet 9P/Tempel 1
+ 1000107 Comet 81P/Wild 2
+
+ 2000001 Asteroid Ceres
+ 2000002 Asteroid Pallas
+ 2000004 Asteroid Vesta
+ 2000021 Asteroid Lutetia
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2000511 Asteroid Davida
+ 2002867 Asteroid Steins
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY10_POLE_RA = ( 286.13 0. 0. )
+ BODY10_POLE_DEC = ( 63.87 0. 0. )
+ BODY10_PM = ( 84.176 14.18440 0. )
+ BODY10_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Mercury
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body199_pole_ra = ( 281.01 -0.033 0. )
+ body199_pole_dec = ( 61.45 -0.005 0. )
+ body199_pm = ( 329.548 6.1385025 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.0097 -0.0328 0. )
+ BODY199_POLE_DEC = ( 61.4143 -0.0049 0. )
+ BODY199_PM = ( 329.5469 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ BODY199_NUT_PREC_RA = ( 0. 0. 0. 0. 0. )
+
+ BODY199_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. )
+
+ BODY199_NUT_PREC_PM = ( 0.00993822
+ -0.00104581
+ -0.00010280
+ -0.00002364
+ -0.00000532 )
+ \begintext
+
+ The linear coefficients have been scaled up from degrees/day
+ to degrees/century, because the SPICELIB PCK reader expects
+ these units. The original constants were:
+
+ 174.791086 4.092335
+ 349.582171 8.184670
+ 164.373257 12.277005
+ 339.164343 16.369340
+ 153.955429 20.461675
+
+
+ \begindata
+
+ BODY1_NUT_PREC_ANGLES = ( 174.791086 0.14947253587500003E+06
+ 349.582171 0.29894507175000006E+06
+ 164.373257 0.44841760762500006E+06
+ 339.164343 0.59789014350000012E+06
+ 153.955429 0.74736267937499995E+06 )
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_POLE_RA = ( 272.76 0. 0. )
+ BODY299_POLE_DEC = ( 67.16 0. 0. )
+ BODY299_PM = ( 160.20 -1.4813688 0. )
+
+ BODY299_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2009 report.
+
+ Current values:
+
+ \begindata
+
+ BODY399_POLE_RA = ( 0. -0.641 0. )
+ BODY399_POLE_DEC = ( 90. -0.557 0. )
+ BODY399_PM = ( 190.147 360.9856235 0. )
+ BODY399_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Nutation precession angles for the Earth-Moon system:
+
+ The linear coefficients have been scaled up from degrees/day
+ to degrees/century, because the SPICELIB PCK reader expects
+ these units. The original constants were:
+
+ 125.045D0 -0.0529921D0
+ 250.089D0 -0.1059842D0
+ 260.008D0 13.0120009D0
+ 176.625D0 13.3407154D0
+ 357.529D0 0.9856003D0
+ 311.589D0 26.4057084D0
+ 134.963D0 13.0649930D0
+ 276.617D0 0.3287146D0
+ 34.226D0 1.7484877D0
+ 15.134D0 -0.1589763D0
+ 119.743D0 0.0036096D0
+ 239.961D0 0.1643573D0
+ 25.053D0 12.9590088D0
+
+
+ \begindata
+
+
+ BODY3_NUT_PREC_ANGLES = ( 125.045 -1935.5364525000
+ 250.089 -3871.0729050000
+ 260.008 475263.3328725000
+ 176.625 487269.6299850000
+ 357.529 35999.0509575000
+ 311.589 964468.4993100000
+ 134.963 477198.8693250000
+ 276.617 12006.3007650000
+ 34.226 63863.5132425000
+ 15.134 -5806.6093575000
+ 119.743 131.8406400000
+ 239.961 6003.1503825000
+ 25.053 473327.7964200000 )
+
+
+ \begintext
+
+
+ Earth north geomagnetic centered dipole:
+
+ The north dipole location is time-varying. The values shown
+ below, taken from [8], represent a discrete sampling of the
+ north dipole location from 1945 to 2000. The terms DGRF and
+ IGRF refer to, respectively, "Definitive Geomagnetic
+ Reference Field" and "International Geomagnetic Reference
+ Field." See references [6], [8], and [9] for details.
+
+ Coordinates are planetocentric.
+
+ Data source Lat Lon
+ ----------- ----- ------
+ DGRF 1945 78.47 291.47
+ DGRF 1950 78.47 291.15
+ DGRF 1955 78.46 290.84
+ DGRF 1960 78.51 290.53
+ DGRF 1965 78.53 290.15
+ DGRF 1970 78.59 289.82
+ DGRF 1975 78.69 289.53
+ DGRF 1980 78.81 289.24
+ DGRF 1985 78.97 289.10
+ DGRF 1990 79.13 288.89
+ IGRF 1995 79.30 288.59
+ IGRF 2000 79.54 288.43
+
+ Original values:
+
+ Values are from [7]. Note the year of publication was 1971.
+
+ body399_mag_north_pole_lon = ( -69.761 )
+ body399_mag_north_pole_lat = ( 78.565 )
+
+ Previous values:
+
+ body399_n_geomag_ctr_dipole_lon = ( 288.43 )
+ body399_n_geomag_ctr_dipole_lat = ( 79.54 )
+
+
+ Current values:
+
+ Values are given for the epoch 2012.0 and were derived
+ by Nat Bachman from constants provided by [11].
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 287.62 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 80.13 )
+
+ \begintext
+
+
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY499_POLE_RA = ( 317.68143 -0.1061 0. )
+ BODY499_POLE_DEC = ( 52.88650 -0.0609 0. )
+ BODY499_PM = ( 176.630 350.89198226 0. )
+
+ \begintext
+
+ Source [5] specifies the following value for the lambda_a term
+ (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
+ LONGITUDE, measured from the prime meridian, of the meridian
+ containing the longest axis of the reference ellipsoid.
+ (CAUTION: previous values were POSITIVE WEST.)
+
+ body499_long_axis = ( 252. )
+
+ We list this lambda_a value for completeness. The IAU report
+ [1] gives equal values for both equatorial radii, so the
+ lambda_a offset does not apply to the IAU model.
+
+ The 2003 IAU report defines M2, the second nutation precession angle,
+ by:
+
+ 2
+ 192.93 + 1128.4096700 d + 8.864 T
+
+ We truncate the M2 series to a linear expression, because the PCK
+ software cannot handle the quadratic term.
+
+ Again, the linear terms are scaled by 36525.0:
+
+ -0.4357640000000000 --> -15916.28010000000
+ 1128.409670000000 --> 41215163.19675000
+ -1.8151000000000000E-02 --> -662.9652750000000
+
+ We also introduce a fourth nutation precession angle, which
+ is the pi/2-complement of the third angle. This angle is used
+ in computing the prime meridian location for Deimos. See the
+ discussion of this angle below in the section containing orientation
+ constants for Deimos.
+
+ \begindata
+
+ BODY4_NUT_PREC_ANGLES = ( 169.51 -15916.2801
+ 192.93 41215163.19675
+ 53.47 -662.965275
+ 36.53 662.965275 )
+
+ \begintext
+
+
+Jupiter
+
+ Old values:
+
+ The rotation rate is from the 2006 IAU report; all other
+ values are unchanged in the 2009 report.
+
+ body599_pm = ( 284.95 870.5366420 0. )
+
+
+ Current values:
+
+ The number of nutation precession angles is 15. The ninth and
+ tenth are twice the first and second, respectively. The
+ eleventh through fifteenth correspond to angles JA-JE in
+ the 2006 IAU report; angles JA-JE were not used prior to that
+ report.
+
+ \begindata
+
+
+ BODY599_POLE_RA = ( 268.056595 -0.006499 0. )
+ BODY599_POLE_DEC = ( 64.495303 0.002413 0. )
+ BODY599_PM = ( 284.95 870.5360000 0. )
+ BODY599_LONG_AXIS = ( 0. )
+
+ BODY599_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117
+ 0.000938
+ 0.001432
+ 0.000030
+ 0.002150 )
+
+ BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050
+ 0.000404
+ 0.000617
+ -0.000013
+ 0.000926 )
+
+ BODY599_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0 )
+
+
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.25 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4
+ 99.360714 4850.4046
+ 175.895369 1191.9605
+ 300.323162 262.5475
+ 114.012305 6070.2476
+ 49.511251 64.3000 )
+ \begintext
+
+
+Saturn
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+
+ body699_pole_ra = ( 40.589 -0.036 0. )
+ body699_pole_dec = ( 83.537 -0.004 0. )
+ body699_pm = ( 38.90 810.7939024 0. )
+ body699_long_axis = ( 0. )
+
+
+ The first seven angles given here are the angles S1
+ through S7 from the 2000 report; the eighth and
+ ninth angles are 2*S1 and 2*S2, respectively.
+
+
+ body6_nut_prec_angles = ( 353.32 75706.7
+ 28.72 75706.7
+ 177.40 -36505.5
+ 300.00 -7225.9
+ 316.45 506.2
+ 345.20 -1016.3
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+
+
+ Current values:
+
+
+ The change from the previous set of values is the
+ removal of S7. This causes BODY6_NUT_PREC_ANGLES
+ elements that formerly corresponded to 2*S1 and 2*S1
+ to be shifted toward the start of the array.
+
+ \begindata
+
+ BODY699_POLE_RA = ( 40.589 -0.036 0. )
+ BODY699_POLE_DEC = ( 83.537 -0.004 0. )
+ BODY699_PM = ( 38.90 810.7939024 0. )
+ BODY699_LONG_AXIS = ( 0. )
+
+ \begintext
+
+ The first six angles given here are the angles S1
+ through S6 from the 2009 report; the seventh and
+ eigth angles are 2*S1 and 2*S2, respectively.
+
+
+ \begindata
+
+ BODY6_NUT_PREC_ANGLES = ( 353.32 75706.7
+ 28.72 75706.7
+ 177.40 -36505.5
+ 300.00 -7225.9
+ 316.45 506.2
+ 345.20 -1016.3
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_POLE_RA = ( 257.311 0. 0. )
+ BODY799_POLE_DEC = ( -15.175 0. 0. )
+ BODY799_PM = ( 203.81 -501.1600928 0. )
+ BODY799_LONG_AXIS = ( 0. )
+
+ \begintext
+
+ The first 16 angles given here are the angles U1
+ through U16 from the 2000 report; the 17th and
+ 18th angles are 2*U11 and 2*U12, respectively.
+
+ \begindata
+
+ BODY7_NUT_PREC_ANGLES = ( 115.75 54991.87
+ 141.69 41887.66
+ 135.03 29927.35
+ 61.77 25733.59
+ 249.32 24471.46
+ 43.86 22278.41
+ 77.66 20289.42
+ 157.36 16652.76
+ 101.81 12872.63
+ 138.64 8061.81
+ 102.23 -2024.22
+ 316.41 2863.96
+ 304.01 -51.94
+ 308.71 -93.17
+ 340.82 -75.32
+ 259.14 -504.81
+ 204.46 -4048.44
+ 632.82 5727.92 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY899_POLE_RA = ( 299.36 0. 0. )
+ BODY899_POLE_DEC = ( 43.46 0. 0. )
+ BODY899_PM = ( 253.18 536.3128492 0. )
+ BODY899_LONG_AXIS = ( 0. )
+
+
+ BODY899_NUT_PREC_RA = ( 0.70 0. 0. 0. 0. 0. 0. 0. )
+ BODY899_NUT_PREC_DEC = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
+ BODY899_NUT_PREC_PM = ( -0.48 0. 0. 0. 0. 0. 0. 0. )
+
+ \begintext
+
+ The 2000 report defines the nutation precession angles
+
+ N, N1, N2, ... , N7
+
+ and also uses the multiples of N1 and N7
+
+ 2*N1
+
+ and
+
+ 2*N7, 3*N7, ..., 9*N7
+
+ In this file, we treat the angles and their multiples as
+ separate angles. In the kernel variable
+
+ BODY8_NUT_PREC_ANGLES
+
+ the order of the angles is
+
+ N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
+
+ Each angle is defined by a linear polynomial, so two
+ consecutive array elements are allocated for each
+ angle. The first term of each pair is the constant term,
+ the second is the linear term.
+
+ \begindata
+
+ BODY8_NUT_PREC_ANGLES = ( 357.85 52.316
+ 323.92 62606.6
+ 220.51 55064.2
+ 354.27 46564.5
+ 75.31 26109.4
+ 35.36 14325.4
+ 142.61 2824.6
+ 177.85 52.316
+ 647.840 125213.200
+ 355.700 104.632
+ 533.550 156.948
+ 711.400 209.264
+ 889.250 261.580
+ 1067.100 313.896
+ 1244.950 366.212
+ 1422.800 418.528
+ 1600.650 470.844 )
+
+ \begintext
+
+
+
+
+Orientation Constants for the Dwarf Planet Pluto
+--------------------------------------------------------
+
+Pluto
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body999_pole_ra = ( 312.993 0. 0. )
+ body999_pole_dec = ( 6.163 0. 0. )
+ body999_pm = ( 237.305 -56.3625225 0. )
+ body999_long_axis = ( 0. )
+
+
+ Current values:
+
+ Due to the new definition of planetocentric coordinates
+ for small bodies, and to the reclassification of Pluto
+ as a dwarf planet, Pluto's north pole direction has been
+ inverted.
+
+ The PM constant W0 is from [2].
+
+ \begindata
+
+ BODY999_POLE_RA = ( 132.993 0. 0. )
+ BODY999_POLE_DEC = ( -6.163 0. 0. )
+ BODY999_PM = ( 302.695 56.3625225 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ New values:
+
+ \begindata
+
+
+ BODY301_POLE_RA = ( 269.9949 0.0031 0. )
+ BODY301_POLE_DEC = ( 66.5392 0.0130 0. )
+ BODY301_PM = ( 38.3213 13.17635815 -1.4D-12 )
+ BODY301_LONG_AXIS = ( 0. )
+
+ BODY301_NUT_PREC_RA = ( -3.8787 -0.1204 0.0700 -0.0172
+ 0.0 0.0072 0.0 0.0
+ 0.0 -0.0052 0.0 0.0
+ 0.0043 )
+
+ BODY301_NUT_PREC_DEC = ( 1.5419 0.0239 -0.0278 0.0068
+ 0.0 -0.0029 0.0009 0.0
+ 0.0 0.0008 0.0 0.0
+ -0.0009 )
+
+ BODY301_NUT_PREC_PM = ( 3.5610 0.1208 -0.0642 0.0158
+ 0.0252 -0.0066 -0.0047 -0.0046
+ 0.0028 0.0052 0.0040 0.0019
+ -0.0044 )
+ \begintext
+
+
+
+Satellites of Mars
+
+
+ Phobos
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+
+ Current values:
+
+ The quadratic prime meridian term is scaled by 1/36525**2:
+
+ 8.864000000000000 ---> 6.6443009930565219E-09
+
+ \begindata
+
+ BODY401_POLE_RA = ( 317.68 -0.108 0. )
+ BODY401_POLE_DEC = ( 52.90 -0.061 0. )
+ BODY401_PM = ( 35.06 1128.8445850 6.6443009930565219E-09 )
+
+ BODY401_LONG_AXIS = ( 0. )
+
+ BODY401_NUT_PREC_RA = ( 1.79 0. 0. 0. )
+ BODY401_NUT_PREC_DEC = ( -1.08 0. 0. 0. )
+ BODY401_NUT_PREC_PM = ( -1.42 -0.78 0. 0. )
+
+
+ \begintext
+
+
+ Deimos
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ New values:
+
+ The Deimos prime meridian expression is:
+
+
+ 2
+ W = 79.41 + 285.1618970 d - 0.520 T - 2.58 sin M
+ 3
+
+ + 0.19 cos M .
+ 3
+
+
+ At the present time, the PCK kernel software (the routine
+ BODEUL in particular) cannot handle the cosine term directly,
+ but we can represent it as
+
+ 0.19 sin M
+ 4
+
+ where
+
+ M = 90.D0 - M
+ 4 3
+
+ Therefore, the nutation precession angle assignments for Phobos
+ and Deimos contain four coefficients rather than three.
+
+ The quadratic prime meridian term is scaled by 1/36525**2:
+
+ -0.5200000000000000 ---> -3.8978300049519307E-10
+
+ \begindata
+
+ BODY402_POLE_RA = ( 316.65 -0.108 0. )
+ BODY402_POLE_DEC = ( 53.52 -0.061 0. )
+ BODY402_PM = ( 79.41 285.1618970 -3.897830D-10 )
+ BODY402_LONG_AXIS = ( 0. )
+
+ BODY402_NUT_PREC_RA = ( 0. 0. 2.98 0. )
+ BODY402_NUT_PREC_DEC = ( 0. 0. -1.78 0. )
+ BODY402_NUT_PREC_PM = ( 0. 0. -2.58 0.19 )
+
+ \begintext
+
+
+
+
+Satellites of Jupiter
+
+
+ Io
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( 64.50 0.003 0. )
+ BODY501_PM = ( 200.39 203.4889538 0. )
+ BODY501_LONG_AXIS = ( 0. )
+
+ BODY501_NUT_PREC_RA = ( 0. 0. 0.094 0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. 0.040 0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+
+ \begintext
+
+
+
+ Europa
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY502_POLE_RA = ( 268.08 -0.009 0. )
+ BODY502_POLE_DEC = ( 64.51 0.003 0. )
+ BODY502_PM = ( 36.022 101.3747235 0. )
+ BODY502_LONG_AXIS = ( 0. )
+
+ BODY502_NUT_PREC_RA = ( 0. 0. 0. 1.086 0.060 0.015 0.009 )
+ BODY502_NUT_PREC_DEC = ( 0. 0. 0. 0.468 0.026 0.007 0.002 )
+ BODY502_NUT_PREC_PM = ( 0. 0. 0. -0.980 -0.054 -0.014 -0.008 )
+
+ \begintext
+
+
+ Ganymede
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY503_POLE_RA = ( 268.20 -0.009 0. )
+ BODY503_POLE_DEC = ( 64.57 0.003 0. )
+ BODY503_PM = ( 44.064 50.3176081 0. )
+ BODY503_LONG_AXIS = ( 0. )
+
+ BODY503_NUT_PREC_RA = ( 0. 0. 0. -0.037 0.431 0.091 )
+ BODY503_NUT_PREC_DEC = ( 0. 0. 0. -0.016 0.186 0.039 )
+ BODY503_NUT_PREC_PM = ( 0. 0. 0. 0.033 -0.389 -0.082 )
+
+ \begintext
+
+
+ Callisto
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY504_POLE_RA = ( 268.72 -0.009 0. )
+ BODY504_POLE_DEC = ( 64.83 0.003 0. )
+ BODY504_PM = ( 259.51 21.5710715 0. )
+ BODY504_LONG_AXIS = ( 0. )
+
+ BODY504_NUT_PREC_RA = ( 0. 0. 0. 0. -0.068 0.590 0. 0.010 )
+ BODY504_NUT_PREC_DEC = ( 0. 0. 0. 0. -0.029 0.254 0. -0.004 )
+ BODY504_NUT_PREC_PM = ( 0. 0. 0. 0. 0.061 -0.533 0. -0.009 )
+
+ \begintext
+
+
+ Amalthea
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY505_POLE_RA = ( 268.05 -0.009 0. )
+ BODY505_POLE_DEC = ( 64.49 0.003 0. )
+ BODY505_PM = ( 231.67 722.6314560 0. )
+ BODY505_LONG_AXIS = ( 0. )
+
+ BODY505_NUT_PREC_RA = ( -0.84 0. 0. 0. 0. 0. 0. 0. 0.01 0. )
+ BODY505_NUT_PREC_DEC = ( -0.36 0. 0. 0. 0. 0. 0. 0. 0. 0. )
+ BODY505_NUT_PREC_PM = ( 0.76 0. 0. 0. 0. 0. 0. 0. -0.01 0. )
+
+ \begintext
+
+
+ Thebe
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY514_POLE_RA = ( 268.05 -0.009 0. )
+ BODY514_POLE_DEC = ( 64.49 0.003 0. )
+ BODY514_PM = ( 8.56 533.7004100 0. )
+ BODY514_LONG_AXIS = ( 0. )
+
+ BODY514_NUT_PREC_RA = ( 0. -2.11 0. 0. 0. 0. 0. 0. 0. 0.04 )
+ BODY514_NUT_PREC_DEC = ( 0. -0.91 0. 0. 0. 0. 0. 0. 0. 0.01 )
+ BODY514_NUT_PREC_PM = ( 0. 1.91 0. 0. 0. 0. 0. 0. 0. -0.04 )
+
+ \begintext
+
+
+ Adrastea
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY515_POLE_RA = ( 268.05 -0.009 0. )
+ BODY515_POLE_DEC = ( 64.49 0.003 0. )
+ BODY515_PM = ( 33.29 1206.9986602 0. )
+ BODY515_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Metis
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY516_POLE_RA = ( 268.05 -0.009 0. )
+ BODY516_POLE_DEC = ( 64.49 0.003 0. )
+ BODY516_PM = ( 346.09 1221.2547301 0. )
+ BODY516_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Mimas
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body601_pole_ra = ( 40.66 -0.036 0. )
+ body601_pole_dec = ( 83.52 -0.004 0. )
+ body601_pm = ( 337.46 381.9945550 0. )
+ body601_long_axis = ( 0. )
+
+ body601_nut_prec_ra = ( 0. 0. 13.56 0. 0. 0. 0. 0. 0. )
+ body601_nut_prec_dec = ( 0. 0. -1.53 0. 0. 0. 0. 0. 0. )
+ body601_nut_prec_pm = ( 0. 0. -13.48 0. -44.85 0. 0. 0. 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY601_POLE_RA = ( 40.66 -0.036 0. )
+ BODY601_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY601_PM = ( 333.46 381.9945550 0. )
+ BODY601_LONG_AXIS = ( 0. )
+
+ BODY601_NUT_PREC_RA = ( 0. 0. 13.56 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_DEC = ( 0. 0. -1.53 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_PM = ( 0. 0. -13.48 0. -44.85 0. 0. 0. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body602_pole_ra = ( 40.66 -0.036 0. )
+ body602_pole_dec = ( 83.52 -0.004 0. )
+ body602_pm = ( 2.82 262.7318996 0. )
+ body602_long_axis = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY602_POLE_RA = ( 40.66 -0.036 0. )
+ BODY602_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY602_PM = ( 6.32 262.7318996 0. )
+ BODY602_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body603_pole_ra = ( 40.66 -0.036 0. )
+ body603_pole_dec = ( 83.52 -0.004 0. )
+ body603_pm = ( 10.45 190.6979085 0. )
+ body603_long_axis = ( 0. )
+
+ body603_nut_prec_ra = ( 0. 0. 0. 9.66 0. 0. 0. 0. 0. )
+ body603_nut_prec_dec = ( 0. 0. 0. -1.09 0. 0. 0. 0. 0. )
+ body603_nut_prec_pm = ( 0. 0. 0. -9.60 2.23 0. 0. 0. 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY603_POLE_RA = ( 40.66 -0.036 0. )
+ BODY603_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY603_PM = ( 8.95 190.6979085 0. )
+ BODY603_LONG_AXIS = ( 0. )
+
+ BODY603_NUT_PREC_RA = ( 0. 0. 0. 9.66 0. 0. 0. 0. )
+ BODY603_NUT_PREC_DEC = ( 0. 0. 0. -1.09 0. 0. 0. 0. )
+ BODY603_NUT_PREC_PM = ( 0. 0. 0. -9.60 2.23 0. 0. 0. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body604_pole_ra = ( 40.66 -0.036 0. )
+ body604_pole_dec = ( 83.52 -0.004 0. )
+ body604_pm = ( 357.00 131.5349316 0. )
+ body604_long_axis = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY604_POLE_RA = ( 40.66 -0.036 0. )
+ BODY604_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY604_PM = ( 357.6 131.5349316 0. )
+ BODY604_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are from the 2009 IAU report.
+
+ body605_pole_ra = ( 40.38 -0.036 0. )
+ body605_pole_dec = ( 83.55 -0.004 0. )
+ body605_pm = ( 235.16 79.6900478 0. )
+ body605_long_axis = ( 0. )
+
+ body605_nut_prec_ra = ( 0. 0. 0. 0. 0. 3.10 0. 0. 0. )
+ body605_nut_prec_dec = ( 0. 0. 0. 0. 0. -0.35 0. 0. 0. )
+ body605_nut_prec_pm = ( 0. 0. 0. 0. 0. -3.08 0. 0. 0. )
+
+
+ Current values:
+
+ Data values are unchanged in the 2009 IAU report. However
+ the kernel variable contents have changed due to removal of
+ the angle S7.
+
+ \begindata
+
+ BODY605_POLE_RA = ( 40.38 -0.036 0. )
+ BODY605_POLE_DEC = ( 83.55 -0.004 0. )
+ BODY605_PM = ( 235.16 79.6900478 0. )
+ BODY605_LONG_AXIS = ( 0. )
+
+ BODY605_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 3.10 0. 0. )
+ BODY605_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. -0.35 0. 0. )
+ BODY605_NUT_PREC_PM = ( 0. 0. 0. 0. 0. -3.08 0. 0. )
+
+ \begintext
+
+
+
+ Titan
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ BODY606_POLE_RA = ( 36.41 -0.036 0. )
+ BODY606_POLE_DEC = ( 83.94 -0.004 0. )
+ BODY606_PM = ( 189.64 22.5769768 0. )
+ BODY606_LONG_AXIS = ( 0. )
+
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 2.66 0. 0 )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. -0.30 0. 0 )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. -2.64 0. 0 )
+
+
+ Current values:
+
+ Note removal of dependence on the nutation precession
+ angles.
+
+ \begindata
+
+ BODY606_POLE_RA = ( 39.4827 0. 0. )
+ BODY606_POLE_DEC = ( 83.4279 0. 0. )
+ BODY606_PM = ( 186.5855 22.5769768 0. )
+ BODY606_LONG_AXIS = ( 0. )
+
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+
+ \begintext
+
+
+
+ Hyperion
+
+ The IAU report does not give an orientation model for Hyperion.
+ Hyperion's rotation is in chaotic and is not predictable for
+ long periods.
+
+
+ Iapetus
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body608_pole_ra = ( 318.16 -3.949 0. )
+ body608_pole_dec = ( 75.03 -1.143 0. )
+ body608_pm = ( 350.20 4.5379572 0. )
+ body608_long_axis = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY608_POLE_RA = ( 318.16 -3.949 0. )
+ BODY608_POLE_DEC = ( 75.03 -1.143 0. )
+ BODY608_PM = ( 355.2 4.5379572 0. )
+ BODY608_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY609_POLE_RA = ( 356.90 0. 0. )
+ BODY609_POLE_DEC = ( 77.80 0. 0. )
+ BODY609_PM = ( 178.58 931.639 0. )
+ BODY609_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Janus
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+
+ Current values:
+
+ Data values are unchanged in the 2009 IAU report. However
+ the kernel variable contents have changed due to removal of
+ the angle S7.
+
+ \begindata
+
+ BODY610_POLE_RA = ( 40.58 -0.036 0. )
+ BODY610_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY610_PM = ( 58.83 518.2359876 0. )
+ BODY610_LONG_AXIS = ( 0. )
+
+ BODY610_NUT_PREC_RA = ( 0. -1.623 0. 0. 0. 0. 0. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ Data values are unchanged in the 2009 IAU report. However
+ the kernel variable contents have changed due to removal of
+ the angle S7.
+
+ \begindata
+
+ BODY611_POLE_RA = ( 40.58 -0.036 0. )
+ BODY611_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY611_PM = ( 293.87 518.4907239 0. )
+ BODY611_LONG_AXIS = ( 0. )
+
+ BODY611_NUT_PREC_RA = ( -3.153 0. 0. 0. 0. 0. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY612_POLE_RA = ( 40.85 -0.036 0. )
+ BODY612_POLE_DEC = ( 83.34 -0.004 0. )
+ BODY612_PM = ( 245.12 131.6174056 0. )
+ BODY612_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Telesto
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY613_POLE_RA = ( 50.51 -0.036 0. )
+ BODY613_POLE_DEC = ( 84.06 -0.004 0. )
+ BODY613_PM = ( 56.88 190.6979332 0. )
+ BODY613_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Calypso
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY614_POLE_RA = ( 36.41 -0.036 0. )
+ BODY614_POLE_DEC = ( 85.04 -0.004 0. )
+ BODY614_PM = ( 153.51 190.6742373 0. )
+ BODY614_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Atlas
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY615_POLE_RA = ( 40.58 -0.036 0. )
+ BODY615_POLE_DEC = ( 83.53 -0.004 0. )
+ BODY615_PM = ( 137.88 598.3060000 0. )
+ BODY615_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Prometheus
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY616_POLE_RA = ( 40.58 -0.036 )
+ BODY616_POLE_DEC = ( 83.53 -0.004 )
+ BODY616_PM = ( 296.14 587.289000 )
+ BODY616_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Pandora
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY617_POLE_RA = ( 40.58 -0.036 0. )
+ BODY617_POLE_DEC = ( 83.53 -0.004 0. )
+ BODY617_PM = ( 162.92 572.7891000 0. )
+ BODY617_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Pan
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY618_POLE_RA = ( 40.6 -0.036 0. )
+ BODY618_POLE_DEC = ( 83.5 -0.004 0. )
+ BODY618_PM = ( 48.8 626.0440000 0. )
+ BODY618_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+
+Satellites of Uranus
+
+
+
+ Ariel
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY701_POLE_RA = ( 257.43 0. 0. )
+ BODY701_POLE_DEC = ( -15.10 0. 0. )
+ BODY701_PM = ( 156.22 -142.8356681 0. )
+ BODY701_LONG_AXIS = ( 0. )
+
+ BODY701_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0.29 )
+
+ BODY701_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0.28 )
+
+ BODY701_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0.05 0.08 )
+ \begintext
+
+
+
+ Umbriel
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY702_POLE_RA = ( 257.43 0. 0. )
+ BODY702_POLE_DEC = ( -15.10 0. 0. )
+ BODY702_PM = ( 108.05 -86.8688923 0. )
+ BODY702_LONG_AXIS = ( 0. )
+
+ BODY702_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0.21 )
+
+ BODY702_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0.20 )
+
+ BODY702_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. -0.09 0. 0.06 )
+
+ \begintext
+
+
+
+ Titania
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY703_POLE_RA = ( 257.43 0. 0. )
+ BODY703_POLE_DEC = ( -15.10 0. 0. )
+ BODY703_PM = ( 77.74 -41.3514316 0. )
+ BODY703_LONG_AXIS = ( 0. )
+
+ BODY703_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.29 )
+
+ BODY703_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.28 )
+
+ BODY703_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.08 )
+ \begintext
+
+
+
+ Oberon
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY704_POLE_RA = ( 257.43 0. 0. )
+ BODY704_POLE_DEC = ( -15.10 0. 0. )
+ BODY704_PM = ( 6.77 -26.7394932 0. )
+ BODY704_LONG_AXIS = ( 0. )
+
+
+ BODY704_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.16 )
+
+ BODY704_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.16 )
+
+ BODY704_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.04 )
+ \begintext
+
+
+
+ Miranda
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY705_POLE_RA = ( 257.43 0. 0. )
+ BODY705_POLE_DEC = ( -15.08 0. 0. )
+ BODY705_PM = ( 30.70 -254.6906892 0. )
+ BODY705_LONG_AXIS = ( 0. )
+
+ BODY705_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 4.41 0. 0. 0. 0.
+ 0. -0.04 0. )
+
+ BODY705_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 4.25 0. 0. 0. 0.
+ 0. -0.02 0. )
+
+ BODY705_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 1.15 -1.27 0. 0. 0.
+ 0. -0.09 0.15 )
+ \begintext
+
+
+
+ Cordelia
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY706_POLE_RA = ( 257.31 0. 0. )
+ BODY706_POLE_DEC = ( -15.18 0. 0. )
+ BODY706_PM = ( 127.69 -1074.5205730 0. )
+ BODY706_LONG_AXIS = ( 0. )
+
+ BODY706_NUT_PREC_RA = ( -0.15 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY706_NUT_PREC_DEC = ( 0.14 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY706_NUT_PREC_PM = ( -0.04 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Ophelia
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY707_POLE_RA = ( 257.31 0. 0. )
+ BODY707_POLE_DEC = ( -15.18 0. 0. )
+ BODY707_PM = ( 130.35 -956.4068150 0. )
+ BODY707_LONG_AXIS = ( 0. )
+
+ BODY707_NUT_PREC_RA = ( 0. -0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY707_NUT_PREC_DEC = ( 0. 0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY707_NUT_PREC_PM = ( 0. -0.03 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Bianca
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY708_POLE_RA = ( 257.31 0. 0. )
+ BODY708_POLE_DEC = ( -15.18 0. 0. )
+ BODY708_PM = ( 105.46 -828.3914760 0. )
+ BODY708_LONG_AXIS = ( 0. )
+
+ BODY708_NUT_PREC_RA = ( 0. 0. -0.16 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY708_NUT_PREC_DEC = ( 0. 0. 0.16 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY708_NUT_PREC_PM = ( 0. 0. -0.04 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Cressida
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+ BODY709_POLE_RA = ( 257.31 0. 0. )
+ BODY709_POLE_DEC = ( -15.18 0. 0. )
+ BODY709_PM = ( 59.16 -776.5816320 0. )
+ BODY709_LONG_AXIS = ( 0. )
+
+
+ BODY709_NUT_PREC_RA = ( 0. 0. 0. -0.04 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ BODY709_NUT_PREC_DEC = ( 0. 0. 0. 0.04 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ BODY709_NUT_PREC_PM = ( 0. 0. 0. -0.01 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ \begintext
+
+
+
+ Desdemona
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY710_POLE_RA = ( 257.31 0. 0. )
+ BODY710_POLE_DEC = ( -15.18 0. 0. )
+ BODY710_PM = ( 95.08 -760.0531690 0. )
+ BODY710_LONG_AXIS = ( 0. )
+
+ BODY710_NUT_PREC_RA = ( 0. 0. 0. 0. -0.17
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY710_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.16
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY710_NUT_PREC_PM = ( 0. 0. 0. 0. -0.04
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Juliet
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY711_POLE_RA = ( 257.31 0. 0. )
+ BODY711_POLE_DEC = ( -15.18 0. 0. )
+ BODY711_PM = ( 302.56 -730.1253660 0. )
+ BODY711_LONG_AXIS = ( 0. )
+
+ BODY711_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ -0.06 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY711_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0.06 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY711_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ -0.02 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Portia
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY712_POLE_RA = ( 257.31 0. 0. )
+ BODY712_POLE_DEC = ( -15.18 0. 0. )
+ BODY712_PM = ( 25.03 -701.4865870 0. )
+ BODY712_LONG_AXIS = ( 0. )
+
+ BODY712_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. -0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY712_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY712_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. -0.02 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Rosalind
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY713_POLE_RA = ( 257.31 0. 0. )
+ BODY713_POLE_DEC = ( -15.18 0. 0. )
+ BODY713_PM = ( 314.90 -644.6311260 0. )
+ BODY713_LONG_AXIS = ( 0. )
+
+ BODY713_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. -0.29 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY713_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0.28 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY713_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. -0.08 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Belinda
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY714_POLE_RA = ( 257.31 0. 0. )
+ BODY714_POLE_DEC = ( -15.18 0. 0. )
+ BODY714_PM = ( 297.46 -577.3628170 0. )
+ BODY714_LONG_AXIS = ( 0. )
+
+ BODY714_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. -0.03 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY714_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0.03 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY714_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. -0.01 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+ \begintext
+
+
+
+ Puck
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY715_POLE_RA = ( 257.31 0. 0. )
+ BODY715_POLE_DEC = ( -15.18 0. 0. )
+ BODY715_PM = ( 91.24 -472.5450690 0. )
+ BODY715_LONG_AXIS = ( 0. )
+
+ BODY715_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. -0.33
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY715_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.31
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY715_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. -0.09
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+
+Satellites of Neptune
+
+
+ Triton
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY801_POLE_RA = ( 299.36 0. 0. )
+ BODY801_POLE_DEC = ( 41.17 0. 0. )
+ BODY801_PM = ( 296.53 -61.2572637 0. )
+ BODY801_LONG_AXIS = ( 0. )
+
+
+ BODY801_NUT_PREC_RA = ( 0. 0. 0. 0.
+ 0. 0. 0. -32.35
+ 0. -6.28 -2.08 -0.74
+ -0.28 -0.11 -0.07 -0.02
+ -0.01 )
+
+
+ BODY801_NUT_PREC_DEC = ( 0. 0. 0. 0.
+ 0. 0. 0. 22.55
+ 0. 2.10 0.55 0.16
+ 0.05 0.02 0.01 0.
+ 0. )
+
+
+ BODY801_NUT_PREC_PM = ( 0. 0. 0. 0.
+ 0. 0. 0. 22.25
+ 0. 6.73 2.05 0.74
+ 0.28 0.11 0.05 0.02
+ 0.01 )
+
+ \begintext
+
+
+
+
+ Nereid
+
+ Old values:
+
+ Values are from the 1988 IAU report [10]. Note that this
+ rotation model pre-dated the 1989 Voyager 2 Neptune
+ encounter.
+
+
+ body802_pole_ra = ( 273.48 0. 0. )
+ body802_pole_dec = ( 67.22 0. 0. )
+ body802_pm = ( 237.22 0.9996465 0. )
+ body802_long_axis = ( 0. )
+
+
+ The report seems to have a typo: in the nut_prec_ra expression,
+ where the report gives -0.51 sin 3N3, we use -0.51 3N2.
+
+ body802_nut_prec_ra = ( 0. -17.81
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ 2.56 -0.51 0.11 -0.03 )
+
+ body802_nut_prec_dec = ( 0. -6.67
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ 0.47 -0.07 0.01 )
+
+ body802_nut_prec_pm = ( 0. 16.48
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ -2.57 0.51 -0.11 0.02 )
+
+
+
+ Current values:
+
+ The 2009 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (notes following table 2).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY803_POLE_RA = ( 299.36 0. 0. )
+ BODY803_POLE_DEC = ( 43.36 0. 0. )
+ BODY803_PM = ( 254.06 +1222.8441209 0. )
+ BODY803_LONG_AXIS = ( 0. )
+
+
+ BODY803_NUT_PREC_RA = ( 0.70 -6.49 0. 0.
+ 0. 0. 0. 0.
+ 0.25 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY803_NUT_PREC_DEC = ( -0.51 -4.75 0. 0.
+ 0. 0. 0. 0.
+ 0.09 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY803_NUT_PREC_PM = ( -0.48 4.40 0. 0.
+ 0. 0. 0. 0.
+ -0.27 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+
+ Thalassa
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY804_POLE_RA = ( 299.36 0. 0. )
+ BODY804_POLE_DEC = ( 43.45 0. 0. )
+ BODY804_PM = ( 102.06 1155.7555612 0. )
+ BODY804_LONG_AXIS = ( 0. )
+
+
+ BODY804_NUT_PREC_RA = ( 0.70 0. -0.28 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+
+ BODY804_NUT_PREC_DEC = ( -0.51 0. -0.21 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY804_NUT_PREC_PM = ( -0.48 0. 0.19 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+ Despina
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY805_POLE_RA = ( 299.36 0. 0. )
+ BODY805_POLE_DEC = ( 43.45 0. 0. )
+ BODY805_PM = ( 306.51 +1075.7341562 0. )
+ BODY805_LONG_AXIS = ( 0. )
+
+
+ BODY805_NUT_PREC_RA = ( 0.70 0. 0. -0.09
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY805_NUT_PREC_DEC = ( -0.51 0. 0. -0.07
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY805_NUT_PREC_PM = ( -0.49 0. 0. 0.06
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+
+ Galatea
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY806_POLE_RA = ( 299.36 0. 0. )
+ BODY806_POLE_DEC = ( 43.43 0. 0. )
+ BODY806_PM = ( 258.09 839.6597686 0. )
+ BODY806_LONG_AXIS = ( 0. )
+
+
+ BODY806_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ -0.07 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY806_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ -0.05 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY806_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0.05 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+ Larissa
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY807_POLE_RA = ( 299.36 0. 0. )
+ BODY807_POLE_DEC = ( 43.41 0. 0. )
+ BODY807_PM = ( 179.41 +649.0534470 0. )
+ BODY807_LONG_AXIS = ( 0. )
+
+
+ BODY807_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ 0. -0.27 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY807_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ 0. -0.20 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY807_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0. 0.19 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+
+ Proteus
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY808_POLE_RA = ( 299.27 0. 0. )
+ BODY808_POLE_DEC = ( 42.91 0. 0. )
+ BODY808_PM = ( 93.38 +320.7654228 0. )
+ BODY808_LONG_AXIS = ( 0. )
+
+
+ BODY808_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ 0. 0. -0.05 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY808_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ 0. 0. -0.04 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY808_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0. 0. 0.04 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+
+
+Satellites of Pluto
+
+ Charon
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body901_pole_ra = ( 312.993 0. 0. )
+ body901_pole_dec = ( 6.163 0. 0. )
+ body901_pm = ( 57.305 -56.3625225 0. )
+ body901_long_axis = ( 0. )
+
+
+ Current values:
+
+ Due to the new definition of planetocentric coordinates
+ for small bodies, and to the reclassification of Pluto
+ as a dwarf planet, Charon's north pole direction has been
+ inverted.
+
+ The PM constant W0 is from [2].
+
+ \begindata
+
+ BODY901_POLE_RA = ( 132.993 0. 0. )
+ BODY901_POLE_DEC = ( -6.163 0. 0. )
+ BODY901_PM = ( 122.695 56.3625225 0. )
+ BODY901_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+Ceres
+
+ Current values:
+
+ \begindata
+
+ BODY2000001_POLE_RA = ( 291. 0. 0. )
+ BODY2000001_POLE_DEC = ( 59. 0. 0. )
+ BODY2000001_PM = ( 170.90 952.1532 0. )
+ BODY2000001_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Pallas
+
+ Current values:
+
+ \begindata
+
+ BODY2000002_POLE_RA = ( 33. 0. 0. )
+ BODY2000002_POLE_DEC = ( -3. 0. 0. )
+ BODY2000002_PM = ( 38. 1105.8036 0. )
+ BODY2000002_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Vesta
+
+ Old values:
+
+ Values are from the 2009 IAU report.
+
+ body2000004_pole_ra = ( 301. 0. 0. )
+ body2000004_pole_dec = ( 41. 0. 0. )
+ body2000004_pm = ( 292. 1617.332776 0. )
+ body2000004_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 305.8 0. 0. )
+ BODY2000004_POLE_DEC = ( 41.4 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Lutetia
+
+ Current values:
+
+ \begindata
+
+ BODY2000021_POLE_RA = ( 52. 0. 0. )
+ BODY2000021_POLE_DEC = ( 12. 0. 0. )
+ BODY2000021_PM = ( 94. 1057.7515 0. )
+ BODY2000021_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Ida
+
+ Old values:
+
+ BODY2431010_POLE_RA = ( 168.76 0. 0. )
+ BODY2431010_POLE_DEC = ( -2.88 0. 0. )
+ BODY2431010_PM = ( 265.95 +1864.6280070 0. )
+ BODY2431010_LONG_AXIS = ( 0. )
+
+ Current values:
+
+ The PM constant W0 is from [2].
+
+ \begindata
+
+ BODY2431010_POLE_RA = ( 168.76 0. 0. )
+ BODY2431010_POLE_DEC = ( -2.88 0. 0. )
+ BODY2431010_PM = ( 274.05 +1864.6280070 0. )
+ BODY2431010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000433_POLE_RA = ( 11.35 0. 0. )
+ BODY2000433_POLE_DEC = ( 17.22 0. 0. )
+ BODY2000433_PM = ( 326.07 1639.38864745 0. )
+ BODY2000433_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Davida
+
+ Current values:
+
+ \begindata
+
+ BODY2000511_POLE_RA = ( 297. 0. 0. )
+ BODY2000511_POLE_DEC = ( 5. 0. 0. )
+ BODY2000511_PM = ( 268.1 1684.4193549 0. )
+ BODY2000511_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY9511010_POLE_RA = ( 9.47 0. 0. )
+ BODY9511010_POLE_DEC = ( 26.70 0. 0. )
+ BODY9511010_PM = ( 83.67 1226.9114850 0. )
+ BODY9511010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Steins
+
+ Current values:
+
+ \begindata
+
+ BODY2002867_POLE_RA = ( 90. 0. 0. )
+ BODY2002867_POLE_DEC = ( -62. 0. 0. )
+ BODY2002867_PM = ( 93.94 1428.852332 0. )
+ BODY2002867_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Itokawa
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2025143_POLE_RA = ( 90.53 0. 0. )
+ BODY2025143_POLE_DEC = ( -66.30 0. 0. )
+ BODY2025143_PM = ( 000.0 712.143 0. )
+ BODY2025143_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY1000093_POLE_RA = ( 294. 0. 0. )
+ BODY1000093_POLE_DEC = ( 73. 0. 0. )
+ BODY1000093_PM = ( 252.63 212.064 0. )
+ BODY1000093_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+19P/Borrelly
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY1000005_POLE_RA = ( 218.5 0. 0. )
+ BODY1000005_POLE_DEC = ( -12.5 0. 0. )
+ BODY1000005_PM = ( 000. 390.0 0. )
+ BODY1000005_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body399_radii = ( 6378.14 6378.14 6356.75 )
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.1366 6378.1366 6356.7519 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+
+ Current values:
+
+ The 2009 IAU report gives separate values for the north and
+ south polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ The report provides the average of these values as well,
+ which we use as the polar radius for the triaxial model.
+
+ \begindata
+
+ BODY499_RADII = ( 3396.19 3396.19 3376.20 )
+
+ \begintext
+
+
+
+Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Radii of the Dwarf Planet Pluto
+--------------------------------------------------------
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body401_radii = ( 13.4 11.2 9.2 )
+ body402_radii = ( 7.5 6.1 5.2 )
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.0 11.4 9.1 )
+ BODY402_RADII = ( 7.8 6.0 5.1 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report,
+ except for those of Europa, Ganymede, Callisto,
+ and Metis. For Metis, now all three radii are
+ provided.
+
+ body502_radii = ( 1564.13 1561.23 1560.93 )
+ body503_radii = ( 2632.4 2632.29 2632.35 )
+ body504_radii = ( 2409.4 2409.2 2409.3 )
+
+ The value for the second radius for body 516 is not given in
+ 2003 IAU report. The values given are:
+
+ body516_radii = ( 30 --- 20 )
+
+ For use within the SPICE system, we use only the mean radius.
+
+ body516_radii = ( 21.5 21.5 21.5 )
+
+
+
+
+ Current values:
+
+ Note that for Ganymede and Callisto only mean radii
+ are provided.
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.4 1815.7 )
+ BODY502_RADII = ( 1562.6 1560.3 1559.5 )
+ BODY503_RADII = ( 2631.2 2631.2 2631.2 )
+ BODY504_RADII = ( 2410.3 2410.3 2410.3 )
+ BODY505_RADII = ( 125 73 64 )
+
+ \begintext
+
+ Only mean radii are available in the 2003 IAU report for bodies
+ 506-513.
+
+ \begindata
+
+ BODY506_RADII = ( 85 85 85 )
+ BODY507_RADII = ( 40 40 40 )
+ BODY508_RADII = ( 18 18 18 )
+ BODY509_RADII = ( 14 14 14 )
+ BODY510_RADII = ( 12 12 12 )
+ BODY511_RADII = ( 15 15 15 )
+ BODY512_RADII = ( 10 10 10 )
+ BODY513_RADII = ( 5 5 5 )
+ BODY514_RADII = ( 58 49 42 )
+ BODY515_RADII = ( 10 8 7 )
+ BODY516_RADII = ( 30 20 17 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body601_radii = ( 207.4 196.8 190.6 )
+ body602_radii = ( 256.6 251.4 248.3 )
+ body603_radii = ( 540.4 531.1 527.5 )
+ body604_radii = ( 563.8 561.0 560.3 )
+ body605_radii = ( 767.2 762.5 763.1 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 747.4 747.4 712.4 )
+ body609_radii = ( 108.6 107.7 101.5 )
+ body610_radii = ( 97.0 95.0 77.0 )
+ body611_radii = ( 69.0 55.0 55.0 )
+
+
+ Only the first equatorial radius for Helene (body 612) is given in the
+ 2006 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius is 16km; we use this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+ body612_radii = ( 17.5 17.5 17.5 )
+ body613_radii = ( 15 12.5 7.5 )
+ body614_radii = ( 15.0 8.0 8.0 )
+ body615_radii = ( 18.5 17.2 13.5 )
+ body616_radii = ( 74.0 50.0 34.0 )
+ body617_radii = ( 55.0 44.0 31.0 )
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ body618_radii = ( 10 10 10 )
+
+
+
+ Current values:
+
+ \begindata
+
+ BODY601_RADII = ( 207.8 196.7 190.6 )
+ BODY602_RADII = ( 256.6 251.4 248.3 )
+ BODY603_RADII = ( 538.4 528.3 526.3 )
+ BODY604_RADII = ( 563.4 561.3 559.6 )
+ BODY605_RADII = ( 765.0 763.1 762.4 )
+ BODY606_RADII = ( 2575.15 2574.78 2574.47 )
+ BODY607_RADII = ( 180.1 133.0 102.7 )
+ BODY608_RADII = ( 745.7 745.7 712.1 )
+ BODY609_RADII = ( 109.4 108.5 101.8 )
+ BODY610_RADII = ( 101.5 92.5 76.3 )
+ BODY611_RADII = ( 64.9 57.0 53.1 )
+ BODY612_RADII = ( 21.7 19.1 13.0 )
+ BODY613_RADII = ( 16.3 11.8 10.0 )
+ BODY614_RADII = ( 15.1 11.5 7.0 )
+ BODY615_RADII = ( 20.4 17.7 9.4 )
+ BODY616_RADII = ( 67.8 39.7 29.7 )
+ BODY617_RADII = ( 52.0 40.5 32.0 )
+ BODY618_RADII = ( 17.2 15.7 10.4 )
+
+ BODY632_RADII = ( 1.6 1.6 1.6 )
+ BODY633_RADII = ( 2.9 2.8 2.0 )
+ BODY634_RADII = ( 1.5 1.2 1.0 )
+ BODY635_RADII = ( 4.3 4.1 3.2 )
+ BODY649_RADII = ( 1 1 1 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY701_RADII = ( 581.1 577.9 577.7 )
+ BODY702_RADII = ( 584.7 584.7 584.7 )
+ BODY703_RADII = ( 788.9 788.9 788.9 )
+ BODY704_RADII = ( 761.4 761.4 761.4 )
+ BODY705_RADII = ( 240.4 234.2 232.9 )
+
+ \begintext
+
+ The 2000 report gives only mean radii for satellites 706--715.
+
+ \begindata
+
+ BODY706_RADII = ( 13 13 13 )
+ BODY707_RADII = ( 15 15 15 )
+ BODY708_RADII = ( 21 21 21 )
+ BODY709_RADII = ( 31 31 31 )
+ BODY710_RADII = ( 27 27 27 )
+ BODY711_RADII = ( 42 42 42 )
+ BODY712_RADII = ( 54 54 54 )
+ BODY713_RADII = ( 27 27 27 )
+ BODY714_RADII = ( 33 33 33 )
+ BODY715_RADII = ( 77 77 77 )
+
+ \begintext
+
+
+
+
+Satellites of Neptune
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ The 2009 report gives mean radii only for bodies 801-806.
+
+ \begindata
+
+ BODY801_RADII = ( 1352.6 1352.6 1352.6 )
+ BODY802_RADII = ( 170 170 170 )
+ BODY803_RADII = ( 29 29 29 )
+ BODY804_RADII = ( 40 40 40 )
+ BODY805_RADII = ( 74 74 74 )
+ BODY806_RADII = ( 79 79 79 )
+
+ \begintext
+
+ The second equatorial radius for Larissa is not given in the 2009
+ report. The available values are:
+
+ BODY807_RADII = ( 104 --- 89 )
+
+ For use within the SPICE system, we use only the mean radius.
+
+ \begindata
+
+ BODY807_RADII = ( 96 96 96 )
+ BODY808_RADII = ( 218 208 201 )
+
+ \begintext
+
+
+
+
+Satellites of Pluto
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+
+
+Ceres
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+
+Vesta
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+
+Lutetia
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000021_RADII = ( 62.0 50.5 46.5 )
+
+ \begintext
+
+
+
+Ida
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+Mathilde
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+
+
+Eros
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+
+Davida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000511_RADII = ( 180. 147. 127. )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+Steins
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2002867_RADII = ( 3.24 2.73 2.04 )
+
+ \begintext
+
+
+
+Toutatis
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \begintext
+
+
+
+Itokawa
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+Kleopatra
+
+
+ Old values:
+
+ Values are from the 2003 report.
+
+
+ body2000216_radii = ( 108.5 47 40.5 )
+
+
+ Current values:
+
+
+ No values are provided in the 2009 report.
+
+
+
+
+
+Halley
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Old values:
+
+ The effective radius is unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ The value in the data assignment below is the
+ "effective radius."
+
+ According to [1]:
+
+ The maximum and minimum radii are not properly
+ the values of the principal semi-axes, they
+ are half the maximum and minimum values of the
+ diameter. Due to the large deviations from a
+ simple ellipsoid, they may not correspond with
+ measurements along the principal axes, or be
+ orthogonal to each other.
+
+ \begindata
+
+ BODY1000093_RADII = ( 3.0 3.0 3.0 )
+
+ \begintext
+
+
+19P/Borrelly
+
+
+ Old values:
+
+ Values are unchanged in the 2009 report.
+
+ Current values:
+
+
+ The value in the data assignment below is the
+ "effective radius."
+
+ The first principal axis length is
+
+ 3.5 km
+
+ The lengths of the other semi-axes are not provided
+ by [1].
+
+ \begindata
+
+ BODY1000005_RADII = ( 4.22 4.22 4.22 )
+
+ \begintext
+
+
+
+81P/Wild 2
+
+
+ Old values:
+
+ Values are unchanged in the 2009 report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00010.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/test_newhorizons_drivers.py b/tests/pytests/test_newhorizons_drivers.py
index fcb9c65277c15dea25ae350fb72df19609b4c677..f8f421882f8eee60cfc4c2a64d56b7aa969eedbd 100644
--- a/tests/pytests/test_newhorizons_drivers.py
+++ b/tests/pytests/test_newhorizons_drivers.py
@@ -14,21 +14,78 @@ from unittest.mock import patch
from conftest import get_image_label, get_image_kernels, convert_kernels, compare_dicts
-from ale.drivers.nh_drivers import NewHorizonsLorriIsisLabelNaifSpiceDriver
+from ale.drivers.nh_drivers import NewHorizonsLorriIsisLabelNaifSpiceDriver, NewHorizonsLeisaIsisLabelNaifSpiceDriver
from conftest import get_image_kernels, convert_kernels, get_image_label, get_isd
+image_dict = {
+ 'lor_0034974380_0x630_sci_1': get_isd("nhlorri"),
+ 'lsb_0296962438_0x53c_eng': get_isd("nhleisa")
+}
+
+
@pytest.fixture()
def test_kernels(scope="module"):
- kernels = get_image_kernels("lor_0034974380_0x630_sci_1")
- updated_kernels, binary_kernels = convert_kernels(kernels)
+ updated_kernels = {}
+ binary_kernels = {}
+ for image in image_dict.keys():
+ kernels = get_image_kernels(image)
+ updated_kernels[image], binary_kernels[image] = convert_kernels(kernels)
yield updated_kernels
- for kern in binary_kernels:
- os.remove(kern)
+ for kern_list in binary_kernels.values():
+ for kern in kern_list:
+ os.remove(kern)
+
+# Test load of nh lorri labels
+@pytest.mark.parametrize("image", ['lor_0034974380_0x630_sci_1'])
+def test_nhlorri_load(test_kernels, image):
+ label_file = get_image_label(image, 'isis')
+ isd_str = ale.loads(label_file, props={'kernels': test_kernels[image]})
+ compare_isd = image_dict[image]
+ isd_obj = json.loads(isd_str)
+ print(json.dumps(isd_obj, indent=2))
+ assert compare_dicts(isd_obj, compare_isd) == []
-def test_newhorizons_load(test_kernels):
- label_file = get_image_label("lor_0034974380_0x630_sci_1", "isis")
- isd_str = ale.loads(label_file, props={'kernels': test_kernels})
+# Test load of nh leisa labels
+@pytest.mark.parametrize("image", ['lsb_0296962438_0x53c_eng'])
+def test_nhleisa_load(test_kernels, image):
+ label_file = get_image_label(image, 'isis')
+ isd_str = ale.loads(label_file, props={'kernels': test_kernels[image]})
+ compare_isd = image_dict[image]
isd_obj = json.loads(isd_str)
- compare_dict = get_isd('newhorizons')
print(json.dumps(isd_obj, indent=2))
- assert compare_dicts(isd_obj, compare_dict) == []
+ assert compare_dicts(isd_obj, compare_isd) == []
+
+
+# ========= Test Leisa isislabel and naifspice driver =========
+class test_leisa_isis_naif(unittest.TestCase):
+ def setUp(self):
+ label = get_image_label("lsb_0296962438_0x53c_eng", "isis")
+ self.driver = NewHorizonsLeisaIsisLabelNaifSpiceDriver(label)
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "NH_RALPH_LEISA"
+
+ def test_ikid(self):
+ assert self.driver.ikid == -98901
+
+ def test_ephemeris_start_time(self):
+ with patch('ale.drivers.nh_drivers.spice.scs2e', return_value=12345) as scs2e:
+ assert self.driver.ephemeris_start_time == 12345
+ scs2e.assert_called_with(-98, '0296962438:00000')
+
+ def test_ephemeris_stop_time(self):
+ with patch('ale.drivers.nh_drivers.spice.scs2e', return_value=12345) as scs2e:
+ assert self.driver.ephemeris_stop_time == (12345 + self.driver.exposure_duration * self.driver.image_lines)
+ scs2e.assert_called_with(-98, '0296962438:00000')
+
+ def test_detector_center_sample(self):
+ assert self.driver.detector_center_sample == 0
+
+ def test_detector_center_line(self):
+ assert self.driver.detector_center_line == 0
+
+ def test_sensor_name(self):
+ assert self.driver.sensor_name == "NH_RALPH_LEISA"
+
+ def test_exposure_duration(self):
+ np.testing.assert_almost_equal(self.driver.exposure_duration, 0.856)