From a7d8a148f54d5141c63ed45a24a71c890ca11de7 Mon Sep 17 00:00:00 2001
From: Amy Stamile <74275278+amystamile-usgs@users.noreply.github.com>
Date: Thu, 14 Dec 2023 14:14:15 -0700
Subject: [PATCH] DawnVIR Driver (#566)
* Draft DawnVIR driver
* Adds interpolate and framechain updates
* fixes line scan rate
* Fixed FrameChain
* updated gitignore
* Fixed Body Rotation
* fixed rebase deletion
* added tests
* failing tests - no alespiceroot
* fix tests
* Initial fixes for dawn virs
* Fixed tests
* addressed PR feedback
* Fixed dawn vir isd
---------
Co-authored-by: acpaquette <acp263@nau.edu>
---
.gitignore | 2 +
CHANGELOG.md | 1 +
ale/drivers/dawn_drivers.py | 318 +-
ale/formatters/formatter.py | 3 +
...rite_DawnVirIsisLabelNaifSpiceDriver.ipynb | 120 +
.../DAWN_203_SCLKSCET.00091.tsc | 673 +
.../VIR_IR_1A_1_362681634_1_isis3.lbl | 271 +
.../VIR_IR_1A_1_362681634_1_isis3_0.xsp | 1013 ++
.../dawn_fc_v3_0_sliced_-203120.xc | 31 +
.../dawn_sc_110627_110703_0_sliced_-203000.xc | 14536 ++++++++++++++++
.../data/VIR_IR_1A_1_362681634_1/dawn_v15.tf | 2285 +++
.../VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf | 93 +
.../dawn_vesta_v06.tpc | 306 +
.../VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti | 574 +
.../dawn_vir_zero_0_sliced_-203201.xc | 31 +
.../dawnvirAddendum001.ti | 22 +
.../data/VIR_IR_1A_1_362681634_1/naif0012.tls | 152 +
.../data/VIR_IR_1A_1_362681634_1/pck00009.tpc | 3639 ++++
tests/pytests/data/isds/dawnvir_isd.json | 1972 +++
tests/pytests/test_dawn_drivers.py | 152 +-
20 files changed, 26182 insertions(+), 12 deletions(-)
create mode 100644 notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc
create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl
create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp
create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc
create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti
create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls
create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc
create mode 100644 tests/pytests/data/isds/dawnvir_isd.json
diff --git a/.gitignore b/.gitignore
index a4e6eef..07b225e 100644
--- a/.gitignore
+++ b/.gitignore
@@ -13,6 +13,7 @@ __pycache__/
# Distribution / packaging
.Python
build/
+docs/
develop-eggs/
dist/
downloads/
@@ -222,3 +223,4 @@ dmypy.json
*.CUB
*.img
*.IMG
+print.prt
diff --git a/CHANGELOG.md b/CHANGELOG.md
index 8e012f7..791e85e 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -40,6 +40,7 @@ release.
### Added
- Mariner10 IsisLabelNaifSpice driver, tests, and test data [#547](https://github.com/DOI-USGS/ale/pull/547)
- DawnFC IsisLabelNaifSpice driver, tests, and test data [#567](https://github.com/DOI-USGS/ale/pull/567)
+- DawnVIR IsisLabelNaifSpice driver, tests, and test data [#566](https://github.com/DOI-USGS/ale/pull/566)
- Updated the spiceypy version used in environment.yml [#552]
### Fixed
diff --git a/ale/drivers/dawn_drivers.py b/ale/drivers/dawn_drivers.py
index ee9b043..0766700 100644
--- a/ale/drivers/dawn_drivers.py
+++ b/ale/drivers/dawn_drivers.py
@@ -1,22 +1,31 @@
-import pvl
+import re
import spiceypy as spice
import os
+import math
+import numpy as np
-from glob import glob
+from scipy.interpolate import CubicSpline
import ale
from ale.base import Driver
from ale.base.label_isis import IsisLabel
from ale.base.data_naif import NaifSpice
+from ale.base.data_isis import IsisSpice
from ale.base.label_pds3 import Pds3Label
from ale.base.type_distortion import NoDistortion
-from ale.base.type_sensor import Framer
+from ale.base.type_sensor import Framer, LineScanner
+from ale.base.data_isis import read_table_data
+from ale.base.data_isis import parse_table
+from ale.transformation import TimeDependentRotation
+from ale.transformation import ConstantRotation
ID_LOOKUP = {
"FC1" : "DAWN_FC1",
"FC2" : "DAWN_FC2"
}
+degs_per_rad = 57.2957795
+
class DawnFcPds3NaifSpiceDriver(Framer, Pds3Label, NaifSpice, Driver):
"""
Dawn driver for generating an ISD from a Dawn PDS3 image.
@@ -393,3 +402,306 @@ class DawnFcIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion,
center ephemeris time
"""
return self.ephemeris_start_time + (self.exposure_duration_ms / 2.0)
+
+
+class DawnVirIsisLabelNaifSpiceDriver(LineScanner, IsisLabel, NaifSpice, NoDistortion, Driver):
+ @property
+ def instrument_id(self):
+ """
+ Returns the ID of the instrument
+
+ Returns
+ -------
+ : str
+ Name of the instrument
+ """
+ lookup_table = {'VIR': 'Visual and Infrared Spectrometer'}
+ return lookup_table[super().instrument_id]
+
+ @property
+ def sensor_name(self):
+ """
+ Returns the name of the instrument
+
+ Returns
+ -------
+ : str
+ Name of the sensor
+ """
+ return self.label["IsisCube"]["Instrument"]["InstrumentId"]
+
+ @property
+ def line_exposure_duration(self):
+ """
+ The exposure duration of the image, in seconds
+
+ Returns
+ -------
+ : float
+ Exposure duration in seconds
+ """
+ return self.label["IsisCube"]["Instrument"]["FrameParameter"][0]
+
+ @property
+ def focal_length(self):
+ return float(spice.gdpool('INS{}_FOCAL_LENGTH'.format(self.ikid), 0, 1)[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 super().detector_center_sample - 0.5
+
+ @property
+ def ikid(self):
+ """
+ Returns the Naif ID code for the instrument
+ Expects the instrument_id to be defined. This must be a string containing
+ the short name of the instrument.
+
+ Returns
+ -------
+ : int
+ Naif ID used to for identifying the instrument in Spice kernels
+ """
+ lookup_table = {
+ 'VIS': -203211,
+ "IR": -203213
+ }
+ return lookup_table[self.label["IsisCube"]["Instrument"]["ChannelId"]]
+
+ @property
+ def sensor_frame_id(self):
+ """
+ Returns the FRAME_DAWN_VIR_{VIS/IR}_ZERO Naif ID code if there are no associated articulation kernels.
+ Otherwise the original Naif ID code is returned.
+ Returns
+ -------
+ : int
+ Naif ID code for the sensor frame
+ """
+ if self.has_articulation_kernel:
+ lookup_table = {
+ 'VIS': -203211,
+ "IR": -203213
+ }
+ else:
+ lookup_table = {
+ 'VIS': -203221,
+ "IR": -203223
+ }
+ return lookup_table[self.label["IsisCube"]["Instrument"]["ChannelId"]]
+
+ @property
+ def housekeeping_table(self):
+ """
+ This table named, "VIRHouseKeeping", contains four fields: ScetTimeClock, ShutterStatus,
+ MirrorSin, and MirrorCos. These fields contain the scan line time in SCLK, status of
+ shutter - open, closed (dark), sine and cosine of the scan mirror, respectively.
+
+ Returns
+ -------
+ : dict
+ Dictionary with ScetTimeClock, ShutterStatus, MirrorSin, and MirrorCos
+ """
+ isis_bytes = read_table_data(self.label['Table'], self._file)
+ return parse_table(self.label['Table'], isis_bytes)
+
+ @property
+ def line_scan_rate(self):
+ """
+ Returns
+ -------
+ : list
+ Start lines
+ : list
+ Line times
+ : list
+ Exposure durations
+ """
+ line_times = []
+ start_lines = []
+ exposure_durations = []
+
+ line_no = 0.5
+
+ for line_midtime in self.hk_ephemeris_time:
+ if not self.is_calibrated:
+ line_times.append(line_midtime - (self.line_exposure_duration / 2.0) - self.center_ephemeris_time)
+ start_lines.append(line_no)
+ exposure_durations.append(self.label["IsisCube"]["Instrument"]["FrameParameter"][2])
+ line_no += 1
+
+ line_times.append(line_times[-1] + self.label["IsisCube"]["Instrument"]["FrameParameter"][2])
+ start_lines.append(line_no)
+ exposure_durations.append(self.label["IsisCube"]["Instrument"]["FrameParameter"][2])
+
+ return start_lines, line_times, exposure_durations
+
+ @property
+ def sensor_model_version(self):
+ """
+ Returns
+ -------
+ : int
+ ISIS sensor model version
+ """
+ return 1
+
+ @property
+ def optical_angles(self):
+ hk_dict = self.housekeeping_table
+
+ opt_angles = []
+ x = np.array([])
+ y = np.array([])
+ for index, mirror_sin in enumerate(hk_dict["MirrorSin"]):
+ shutter_status = hk_dict["ShutterStatus"][index].lower().replace(" ", "")
+ is_dark = (shutter_status == "closed")
+
+ mirror_cos = hk_dict["MirrorCos"][index]
+
+ scan_elec_deg = math.atan(mirror_sin/mirror_cos) * degs_per_rad
+ opt_ang = ((scan_elec_deg - 3.7996979) * 0.25/0.257812) / 1000
+
+ if not is_dark:
+ x = np.append(x, index + 1)
+ y = np.append(y, opt_ang)
+
+ if not self.is_calibrated:
+ opt_angles.append(opt_ang)
+
+ cs = CubicSpline(x, y, extrapolate="periodic")
+
+ for i, opt_ang in enumerate(opt_angles):
+ shutter_status = hk_dict["ShutterStatus"][i].lower().replace(" ", "")
+ is_dark = (shutter_status == "closed")
+
+ if (is_dark):
+ if (i == 0):
+ opt_angles[i] = opt_angles[i+1]
+ elif (i == len(opt_angles) - 1):
+ opt_angles[i] = opt_angles[i-1]
+ else:
+ opt_angles[i] = cs(i+1)
+
+ return opt_angles
+
+ @property
+ def hk_ephemeris_time(self):
+
+ line_times = []
+ scet_times = self.housekeeping_table["ScetTimeClock"]
+ for scet in scet_times:
+ line_midtime = spice.scs2e(self.spacecraft_id, scet)
+ line_times.append(line_midtime)
+
+ return line_times
+
+ @property
+ def ephemeris_start_time(self):
+ """
+ Returns the starting ephemeris time of the image using the first et time from
+ the housekeeping table minus the line exposure duration / 2.
+
+ Returns
+ -------
+ : double
+ Starting ephemeris time of the image
+ """
+ return self.hk_ephemeris_time[0] - (self.line_exposure_duration / 2)
+
+
+ @property
+ def ephemeris_stop_time(self):
+ """
+ Returns the ephemeris stop time of the image using the last et time from
+ the housekeeping table plus the line exposure duration / 2.
+
+ Returns
+ -------
+ : double
+ Ephemeris stop time of the image
+ """
+ return self.hk_ephemeris_time[-1] + (self.line_exposure_duration / 2)
+
+ @property
+ def center_ephemeris_time(self):
+ return self.hk_ephemeris_time[int(len(self.hk_ephemeris_time)/2)]
+
+ @property
+ def is_calibrated(self):
+ """
+ Checks if image is calibrated.
+
+ Returns
+ -------
+ : bool
+ """
+ return self.label['IsisCube']['Archive']['ProcessingLevelId'] > 2
+
+ @property
+ def has_articulation_kernel(self):
+ """
+ Checks if articulation kernel exists in pool of kernels.
+
+ Returns
+ -------
+ : bool
+ """
+ try:
+ regex = re.compile('.*dawn_vir_[0-9]{9}_[0-9]{1}.BC')
+ return any([re.match(regex, i) for i in self.kernels])
+ except ValueError:
+ return False
+
+ @property
+ def frame_chain(self):
+ frame_chain = super().frame_chain
+ frame_chain.add_edge(rotation=self.inst_pointing_rotation)
+ return frame_chain
+
+ @property
+ def inst_pointing_rotation(self):
+ """
+ Returns a time dependent instrument pointing rotation for -203221 and -203223 sensor frame ids.
+
+ Returns
+ -------
+ : TimeDependentRotation
+ Instrument pointing rotation
+ """
+ time_dep_quats = np.zeros((len(self.hk_ephemeris_time), 4))
+ avs = []
+
+ for i, time in enumerate(self.hk_ephemeris_time):
+ try:
+ state_matrix = spice.sxform("J2000", spice.frmnam(self.sensor_frame_id), time)
+ except:
+ rotation_matrix = spice.pxform("J2000", spice.frmnam(self.sensor_frame_id), time)
+ state_matrix = spice.rav2xf(rotation_matrix, [0, 0, 0])
+
+ opt_angle = self.optical_angles[i]
+
+ xform = spice.eul2xf([0, -opt_angle, 0, 0, 0, 0], 1, 2, 3)
+ xform2 = spice.mxmg(xform, state_matrix)
+
+ rot_mat, av = spice.xf2rav(xform2)
+ avs.append(av)
+
+ quat_from_rotation = spice.m2q(rot_mat)
+ time_dep_quats[i,:3] = quat_from_rotation[1:]
+ time_dep_quats[i, 3] = quat_from_rotation[0]
+
+ time_dep_rot = TimeDependentRotation(time_dep_quats, self.hk_ephemeris_time, 1, self.sensor_frame_id, av=avs)
+
+ return time_dep_rot
+
+
\ No newline at end of file
diff --git a/ale/formatters/formatter.py b/ale/formatters/formatter.py
index afeb2f9..751afc6 100644
--- a/ale/formatters/formatter.py
+++ b/ale/formatters/formatter.py
@@ -2,6 +2,8 @@ import json
import numpy as np
from scipy.interpolate import interp1d, BPoly
+import spiceypy as spice
+
from networkx.algorithms.shortest_paths.generic import shortest_path
from ale.transformation import FrameChain
@@ -140,6 +142,7 @@ def to_isd(driver):
instrument_pointing['constant_frames'] = shortest_path(frame_chain, sensor_frame, destination_frame)
constant_rotation = frame_chain.compute_rotation(destination_frame, sensor_frame)
instrument_pointing['constant_rotation'] = constant_rotation.rotation_matrix().flatten()
+
meta_data['instrument_pointing'] = instrument_pointing
# interior orientation
diff --git a/notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb b/notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb
new file mode 100644
index 0000000..9f0e500
--- /dev/null
+++ b/notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb
@@ -0,0 +1,120 @@
+{
+ "cells": [
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": [
+ "fileName = 'VIR_IR_1A_1_362681634_1_isis3.cub'\n",
+ "\n",
+ "import os\n",
+ "os.environ[\"ISISDATA\"] = \"isisdata/isis_data\"\"\n",
+ "os.environ[\"ISISTESTDATA\"] = \"/isisdata/isis_testData\"\n",
+ "os.environ[\"ISISROOT\"] = \"/ISIS3/build\"\n",
+ "\n",
+ "import ale \n",
+ "from ale.drivers.dawn_drivers import DawnVirIsisNaifSpiceDriver\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')\n"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": [
+ "kernels"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {
+ "scrolled": false
+ },
+ "outputs": [],
+ "source": [
+ "with DawnVirIsisNaifSpiceDriver(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()"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": []
+ },
+ {
+ "cell_type": "code",
+ "execution_count": null,
+ "metadata": {},
+ "outputs": [],
+ "source": []
+ }
+ ],
+ "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/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc
new file mode 100755
index 0000000..b0afa1e
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc
@@ -0,0 +1,673 @@
+KPL/SCLK
+
+
+DAWN SCLK File
+===========================================================================
+
+ This file is a SPICE spacecraft clock (SCLK) kernel containing
+ information required for DAWN spacecraft on-board clock to UTC
+ conversion.
+
+
+Production/History of this SCLK file
+--------------------------------------------------------
+
+ This file was generated by the NAIF utility program MAKCLK, version
+ 3.5.2, from the most recent DAWN spacecraft SCLKvSCET file (see
+ corresponding sections of these comments for a copy of the source
+ SCLKvSCET file and MAKCLK setup file).
+
+
+Usage
+--------------------------------------------------------
+
+ This file must be loaded into the user's program by a call to the
+ FURNSH subroutine
+
+ CALL FURNSH( 'this_file_name' )
+
+ in order to use the SPICELIB SCLK family of subroutines to convert
+ DAWN spacecraft on-board clock to ET and vice versa.
+
+
+SCLK Format
+--------------------------------------------------------
+
+ The on-board clock, the conversion for which is provided by this SCLK
+ file, consists of two fields:
+
+ SSSSSSSSSS:FFF
+
+ where:
+
+ SSSSSSSSSS -- count of on-board seconds
+
+ FFF -- count of fractions of a second with one fraction
+ being 1/256 of a second; normally this field value
+ is within 0..255 range.
+
+
+References
+--------------------------------------------------------
+
+ 1. SCLK Required Reading Document
+
+ 2. MAKCLK User's Guide Document
+
+ 3. SFOC SCLKvSCET SIS Document
+
+
+Inquiries
+--------------------------------------------------------
+
+ If you have any questions regarding this file contact NAIF at JPL
+
+ Charles H. Acton, Jr
+ (818) 354-3869
+ Chuck.Acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818) 354-8136
+ Boris.Semenov@jpl.nasa.gov
+
+
+Source SCLKvSCET File
+--------------------------------------------------------
+
+ CCSD3ZS00001$$sclk$$NJPL3KS0L015$$scet$$
+ MISSION_NAME=DAWN;
+ SPACECRAFT_NAME=DAWN;
+ DATA_SET_ID=SCLK_SCET;
+ FILE_NAME=DAWN_203_SCLKSCET.00091;
+ PRODUCT_CREATION_TIME=2018-270T19:25:38.266;
+ PRODUCT_VERSION_ID=00091;
+ PRODUCER_ID=DSMS_TIME_SERVICES;
+ APPLICABLE_START_TIME=2000-001T11:58:55.816;
+ APPLICABLE_STOP_TIME=2019-038T23:42:07.704;
+ MISSION_ENVIRONMENT=ops;
+ MISSION_ID=30;
+ SPACECRAFT_ID=203;
+ CCSD3RE00000$$scet$$NJPL3IS00613$$data$$
+ *____SCLK0_____ ________SCET0________ _DUT__ __SCLKRATE__
+ 0.000 2000-001T11:58:55.816 64.184 1.000000000
+ 189345665.000 2006-001T00:00:00.816 64.184 0.000010000
+ 189345666.000 2006-001T00:00:00.817 65.184 1.000000000
+ 244538000.000 2007-274T19:12:14.817 65.184 1.006101025
+ 244539000.000 2007-274T19:29:00.918 65.184 1.000007143
+ 244710000.000 2007-276T18:59:02.139 65.184 1.000010166
+ 244711000.000 2007-276T19:15:42.150 65.184 1.000007152
+ 245501801.000 2007-285T22:55:48.806 65.184 1.000033235
+ 245502801.000 2007-285T23:12:28.839 65.184 0.998999041
+ 245513651.000 2007-286T02:13:07.979 65.184 0.999015999
+ 245514651.000 2007-286T02:29:46.995 65.184 1.000000001
+ 249480000.000 2007-331T23:58:55.999 65.184 0.999158298
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+ CCSD3RE00000$$data$$CCSD3RE00000$$sclk$$
+
+
+
+MAKCLK Setup file
+--------------------------------------------------------
+
+ SCLKSCET_FILE = DAWN_203_SCLKSCET.00091.clean
+ OLD_SCLK_KERNEL = /sdma/naif/ops/projects/DAWN/scet/bin/dawn_template.tsc
+ FILE_NAME = DAWN_203_SCLKSCET.00091.tsc
+ NAIF_SPACECRAFT_ID = -203
+ LEAPSECONDS_FILE = /sdma/naif/ops/projects/DAWN/lsk/dawn.tls
+ PARTITION_TOLERANCE = 10
+ LOG_FILE = DAWN_203_SCLKSCET.00091.log
+
+
+
+Kernel DATA
+--------------------------------------------------------
+
+\begindata
+
+
+SCLK_KERNEL_ID = ( @2018-09-28/01:15:03.00 )
+
+SCLK_DATA_TYPE_203 = ( 1 )
+SCLK01_TIME_SYSTEM_203 = ( 2 )
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+
+SCLK_PARTITION_START_203 = ( 0.0000000000000E+00 )
+
+SCLK_PARTITION_END_203 = ( 1.0995116277750E+12 )
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+ 1.4887666483200E+11 5.8154947266800E+08 1.0000000390700E+00
+ 1.5030507417600E+11 5.8712919688600E+08 1.0000019999743E+00
+ 1.5030533017600E+11 5.8713019688800E+08 1.0000000370000E+00 )
+
+\begintext
+
+
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl
new file mode 100644
index 0000000..b1abddd
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl
@@ -0,0 +1,271 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 256
+ TileLines = 60
+
+ Group = Dimensions
+ Samples = 256
+ Lines = 60
+ Bands = 432
+ End_Group
+
+ Group = Pixels
+ Type = SignedWord
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = DAWN
+ MissionPhaseName = "VESTA SCIENCE APPROACH (VSA)"
+ InstrumentId = VIR
+ SpacecraftClockStartCount = 1/362681634.2933
+ SpacecraftClockStopCount = 1/362682578.0394
+ StartTime = 2011-06-30T05:53:54.29
+ StopTime = 2011-06-30T06:09:38.04
+ TargetName = VESTA
+ OriginalTargetName = "4 VESTA"
+ OrbitNumber = N/A
+ DataQualityId = 1
+ ChannelId = IR
+ InstrumentModeId = S_H_SPE_H_SPA_F
+ ScanModeId = 4
+ FrameParameter = (0.5, 1, 16, 58)
+ VirIrStartXPosition = 1
+ VirIrStartYPosition = 7
+ MaximumInstrumentTemperature = (81.5, 139.6, 140.6, 74.4)
+ End_Group
+
+ Group = Archive
+ SoftwareVersionId = "EGSE V1.14,AMDLSpace"
+ DataSetName = "DAWN VIR RAW (EDR) VESTA INFRARED SPECTRA
+ V1.0"
+ DataSetId = DAWN-A-VIR-2-EDR-IR-VESTA-SPECTRA-V1.0
+ ProductId = VIR_IR_1A_1_362681634_1
+ ProductType = EDR
+ ProducerFullName = "A. CORADINI"
+ ProducerInstitutionName = "ISTITUTO NAZIONALE DI ASTROFISICA"
+ ProductCreationTime = 2011-07-01T11:21:40.95
+ ProductVersionId = 01
+ InstrumentName = "VISIBLE AND INFRARED SPECTROMETER"
+ InstrumentType = "IMAGING SPECTROMETER"
+ ImageMidTime = NULL
+ ProcessingLevelId = 2
+ EncodingType = N/A
+ PhotometricCorrectionType = NONE
+ End_Group
+
+ Group = BandBin
+ Unit = MICROMETER
+ Center = (1.021, 1.030, 1.040, 1.049, 1.059, 1.068, 1.078, 1.087,
+ 1.096, 1.106, 1.115, 1.125, 1.134, 1.144, 1.153, 1.163,
+ 1.172, 1.182, 1.191, 1.200, 1.210, 1.219, 1.229, 1.238,
+ 1.248, 1.257, 1.267, 1.276, 1.286, 1.295, 1.305, 1.314,
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+ 1.399, 1.409, 1.418, 1.428, 1.437, 1.446, 1.456, 1.465,
+ 1.475, 1.484, 1.494, 1.503, 1.513, 1.522, 1.532, 1.541,
+ 1.550, 1.560, 1.569, 1.579, 1.588, 1.598, 1.607, 1.617,
+ 1.626, 1.636, 1.645, 1.655, 1.664, 1.673, 1.683, 1.692,
+ 1.702, 1.711, 1.721, 1.730, 1.740, 1.749, 1.759, 1.768,
+ 1.777, 1.787, 1.796, 1.806, 1.815, 1.825, 1.834, 1.844,
+ 1.853, 1.863, 1.872, 1.882, 1.891, 1.900, 1.910, 1.919,
+ 1.929, 1.938, 1.948, 1.957, 1.967, 1.976, 1.986, 1.995,
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+ 2.232, 2.241, 2.250, 2.260, 2.269, 2.279, 2.288, 2.298,
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+ 2.383, 2.392, 2.402, 2.411, 2.421, 2.430, 2.440, 2.449,
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+ 2.534, 2.544, 2.553, 2.563, 2.572, 2.582, 2.591, 2.600,
+ 2.610, 2.619, 2.629, 2.638, 2.648, 2.657, 2.667, 2.676,
+ 2.686, 2.695, 2.705, 2.714, 2.723, 2.733, 2.742, 2.752,
+ 2.761, 2.771, 2.780, 2.790, 2.799, 2.809, 2.818, 2.827,
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+ 3.140, 3.149, 3.159, 3.168, 3.177, 3.187, 3.196, 3.206,
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+ 3.291, 3.300, 3.310, 3.319, 3.329, 3.338, 3.348, 3.357,
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+ 4.350, 4.360, 4.369, 4.379, 4.388, 4.398, 4.407, 4.417,
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+ 5.032, 5.041, 5.050, 5.060, 5.069, 5.079, 5.088, 5.098)
+ Width = (0.0140, 0.0140, 0.0140, 0.0140, 0.0140, 0.0140, 0.0140,
+ 0.0140, 0.0140, 0.0139, 0.0139, 0.0139, 0.0139, 0.0139,
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+ 0.0127, 0.0127, 0.0127, 0.0127, 0.0126, 0.0126, 0.0126,
+ 0.0126, 0.0126, 0.0126, 0.0125, 0.0125, 0.0125, 0.0125,
+ 0.0125, 0.0125, 0.0124, 0.0124, 0.0124, 0.0124, 0.0124,
+ 0.0124, 0.0123, 0.0123, 0.0123, 0.0123, 0.0123, 0.0123,
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+ 0.0171, 0.0171, 0.0172, 0.0172, 0.0173, 0.0173, 0.0174,
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+ 0.0179, 0.0180, 0.0180, 0.0181, 0.0181, 0.0182, 0.0183,
+ 0.0183, 0.0184, 0.0185, 0.0185, 0.0186)
+ 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,
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+ 238, 239, 240, 241, 242, 243, 244, 245, 246, 247, 248, 249,
+ 250, 251, 252, 253, 254, 255, 256, 257, 258, 259, 260, 261,
+ 262, 263, 264, 265, 266, 267, 268, 269, 270, 271, 272, 273,
+ 274, 275, 276, 277, 278, 279, 280, 281, 282, 283, 284, 285,
+ 286, 287, 288, 289, 290, 291, 292, 293, 294, 295, 296, 297,
+ 298, 299, 300, 301, 302, 303, 304, 305, 306, 307, 308, 309,
+ 310, 311, 312, 313, 314, 315, 316, 317, 318, 319, 320, 321,
+ 322, 323, 324, 325, 326, 327, 328, 329, 330, 331, 332, 333,
+ 334, 335, 336, 337, 338, 339, 340, 341, 342, 343, 344, 345,
+ 346, 347, 348, 349, 350, 351, 352, 353, 354, 355, 356, 357,
+ 358, 359, 360, 361, 362, 363, 364, 365, 366, 367, 368, 369,
+ 370, 371, 372, 373, 374, 375, 376, 377, 378, 379, 380, 381,
+ 382, 383, 384, 385, 386, 387, 388, 389, 390, 391, 392, 393,
+ 394, 395, 396, 397, 398, 399, 400, 401, 402, 403, 404, 405,
+ 406, 407, 408, 409, 410, 411, 412, 413, 414, 415, 416, 417,
+ 418, 419, 420, 421, 422, 423, 424, 425, 426, 427, 428, 429,
+ 430, 431, 432)
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -203213
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = Table
+ Name = VIRHouseKeeping
+ StartByte = 13337176
+ Bytes = 2160
+ Records = 60
+ ByteOrder = Lsb
+ SourceFile = /work/users/slambright/prog/isis3/clean_trunk/isis/src/dawn/ap-
+ ps/dawnvir2isis/tsts/IR/input/VIR_IR_1A_1_362681634_1_HK.LBL
+
+ Group = Field
+ Name = ScetTimeClock
+ Type = Text
+ Size = 12
+ End_Group
+
+ Group = Field
+ Name = ShutterStatus
+ Type = Text
+ Size = 8
+ End_Group
+
+ Group = Field
+ Name = MirrorSin
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = MirrorCos
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 13336577
+ Bytes = 599
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 13339336
+ Bytes = 23983
+End_Object
+End
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp
new file mode 100644
index 0000000..80d0cdb
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp
@@ -0,0 +1,1013 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 45
+'VESTA '
+'159E106596D27^8'
+'159E194B5DFD66^8'
+'1E8484'
+'A'
+'1'
+'2'
+45
+'159C7EC^8'
+'2A3^6'
+'A2033858D210C^7'
+'2FA5A8E74EC04C^7'
+'-12395AFDA4D93^6'
+'-CB8ED7C6F5FF^4'
+'4E293527E88^3'
+'FC97C43B28^1'
+'-D8BBB84C^0'
+'-16DEBBF58^0'
+'1F2E564^-1'
+'3EE1F28C^-1'
+'-245D25^-1'
+'3341DC8^-3'
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+'-F115EF241BD4^7'
+'19B2BC7C78DAE3^7'
+'1B2C9820175DE^6'
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+'-39E478AD73^3'
+'221D085DD34^2'
+'2E6BB14C^0'
+'-A61B584^-2'
+'-A2D973C^-1'
+'342AB6D^-1'
+'F9E048^-2'
+'-1160FC4A8^-1'
+'31222^-2'
+'-7532F00F38B83^7'
+'401A3CFCD56164^6'
+'D34869F959BB8^5'
+'-25050E3A8019C^4'
+'-214524573A8^3'
+'B7706DB458^1'
+'34FE7446^0'
+'2D3F1C1F^-1'
+'-5A8571E^-1'
+'1557786DC^-1'
+'C1E5EC^-2'
+'-94E257858^-2'
+'BB928^-3'
+'15724EC^8'
+'546^6'
+'29^2'
+'1^1'
+END_ARRAY 1 45
+BEGIN_ARRAY 2 865
+'MONTE Difference Line Table '
+'159E106596D27^8'
+'159E194B5DFD66^8'
+'-CB'
+'1E8484'
+'1'
+'1'
+865
+'159E106E140B59^8'
+'A8C8901F5D56^2'
+'15191203EBAAC^3'
+'1FA59B05E1802^3'
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+'0^0'
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+'-18C7718877A607^0'
+'400EAD96155034^4'
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+'-33CBE843045E7^-A'
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+'72599ECB699998^-B'
+'0^0'
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+'159E1C33B1B7A3^8'
+'C^1'
+END_ARRAY 2 865
+BEGIN_ARRAY 3 39
+'DE-0421LE-0421 '
+'159E106596D27^8'
+'159E194B5DFD66^8'
+'A'
+'0'
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+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+TOTAL_ARRAYS 3
+ ~NAIF/SPC BEGIN COMMENTS~
+; /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3_0.bsp LOG FILE
+
+; Created 2023-12-10/09:42:34.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Users/astamile/isisdata/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3_0.bsp
+SOURCE_SPK_KERNEL = /Users/astamile/isisdata/isis_data/dawn/kernels/tspk/sb_vesta_110211.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 2000004
+ BEGIN_TIME = 2011 JUN 30 04:32:35.405
+ END_TIME = 2011 JUN 30 05:10:33.183
+SOURCE_SPK_KERNEL = /Users/astamile/isisdata/isis_data/dawn/kernels/spk/dawn_rec_110416-110802_110913_v1.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -203
+ BEGIN_TIME = 2011 JUN 30 04:32:35.405
+ END_TIME = 2011 JUN 30 05:10:33.183
+SOURCE_SPK_KERNEL = /Users/astamile/isisdata/isis_data/dawn/kernels/tspk/de421.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 10
+ BEGIN_TIME = 2011 JUN 30 04:32:35.405
+ END_TIME = 2011 JUN 30 05:10:33.183
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc
new file mode 100644
index 0000000..919a7a7
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'DAWN FC ALIGNMENT '
+BEGIN_ARRAY 1 10
+'DAWN FC2 ALIGNMENT, 10/22/15 '
+'159E1065C3^A'
+'159E194B8A^A'
+'-31970'
+'-318F8'
+'2'
+'1'
+10
+'FFFFE61784D86^0'
+'-1CE1654009A4C1^-2'
+'681F4D63A264F8^-2'
+'27DE1942838A74^-2'
+'0^0'
+'0^0'
+'0^0'
+'FFFFFFFF1C422^-2'
+'159E1065C3^A'
+'159E194B8A^A'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc
new file mode 100644
index 0000000..6243766
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc
@@ -0,0 +1,14536 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
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+'DAWN TLM-Based SC Bus CK File by NAIF/JPL '
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+'159E1895D7^A'
+'159E1896D7^A'
+'159E1897D7^A'
+'159E1898D7^A'
+'159E1899D7^A'
+'159E189AD7^A'
+'159E189BD7^A'
+'159E189CD7^A'
+'159E189DD7^A'
+'159E189ED7^A'
+'159E189FD7^A'
+'159E18A0D7^A'
+'159E18A1D7^A'
+'159E18A2D7^A'
+'159E18A3D7^A'
+'159E18A4D7^A'
+'159E18A5D7^A'
+'159E18A6D7^A'
+'159E18A7D7^A'
+'159E18A8D7^A'
+'159E18A9D7^A'
+'159E18AAD7^A'
+'159E18ABD7^A'
+'159E18ACD7^A'
+'159E18ADD7^A'
+'159E18AED7^A'
+'159E18AFD7^A'
+'159E18B0D7^A'
+'159E18B1D7^A'
+'159E18B2D7^A'
+'159E18B3D7^A'
+'159E18B4D7^A'
+'159E18B5D7^A'
+'159E18B6D7^A'
+'159E18B7D7^A'
+'159E18B8D7^A'
+'159E18B9D7^A'
+'159E18BAD7^A'
+'159E18BBD7^A'
+165
+'159E18BCD7^A'
+'159E18BDD7^A'
+'159E18BED7^A'
+'159E18BFD7^A'
+'159E18C0D7^A'
+'159E18C1D7^A'
+'159E18C2D7^A'
+'159E18C3D7^A'
+'159E18C4D7^A'
+'159E18C5D7^A'
+'159E18C6D7^A'
+'159E18C7D7^A'
+'159E18C8D7^A'
+'159E18C9D7^A'
+'159E18CAD7^A'
+'159E18CBD7^A'
+'159E18CCD7^A'
+'159E18CDD7^A'
+'159E18CED7^A'
+'159E18CFD7^A'
+'159E18D0D7^A'
+'159E18D1D7^A'
+'159E18D2D7^A'
+'159E18D3D7^A'
+'159E18D4D7^A'
+'159E18D5D7^A'
+'159E18D6D7^A'
+'159E18D7D7^A'
+'159E18D8D7^A'
+'159E18D9D7^A'
+'159E18DAD7^A'
+'159E18DBD7^A'
+'159E18DCD7^A'
+'159E18DDD7^A'
+'159E18DED7^A'
+'159E18DFD7^A'
+'159E18E0D7^A'
+'159E18E1D7^A'
+'159E18E2D7^A'
+'159E18E3D7^A'
+'159E18E4D7^A'
+'159E18E5D7^A'
+'159E18E6D7^A'
+'159E18E7D7^A'
+'159E18E8D7^A'
+'159E18E9D7^A'
+'159E18EAD7^A'
+'159E18EBD7^A'
+'159E18ECD7^A'
+'159E18EDD7^A'
+'159E18EED7^A'
+'159E18EFD7^A'
+'159E18F0D7^A'
+'159E18F1D7^A'
+'159E18F2D7^A'
+'159E18F3D7^A'
+'159E18F4D7^A'
+'159E18F5D7^A'
+'159E18F6D7^A'
+'159E18F7D7^A'
+'159E18F8D7^A'
+'159E18F9D7^A'
+'159E18FAD7^A'
+'159E18FBD7^A'
+'159E18FCD7^A'
+'159E18FDD7^A'
+'159E18FED7^A'
+'159E18FFD7^A'
+'159E1900D7^A'
+'159E1901D7^A'
+'159E1902D7^A'
+'159E1903D7^A'
+'159E1904D7^A'
+'159E1905D7^A'
+'159E1906D7^A'
+'159E1907D7^A'
+'159E1908D7^A'
+'159E1909D7^A'
+'159E190AD7^A'
+'159E190BD7^A'
+'159E190CD7^A'
+'159E190DD7^A'
+'159E190ED7^A'
+'159E190FD7^A'
+'159E1910D7^A'
+'159E1911D7^A'
+'159E1912D7^A'
+'159E1913D7^A'
+'159E1914D7^A'
+'159E1915D7^A'
+'159E1916D7^A'
+'159E1917D7^A'
+'159E1918D7^A'
+'159E1919D7^A'
+'159E191AD7^A'
+'159E191BD7^A'
+'159E191CD7^A'
+'159E191DD7^A'
+'159E191ED7^A'
+'159E191FD7^A'
+'159E1920D7^A'
+'159E1921D7^A'
+'159E1922D7^A'
+'159E1923D7^A'
+'159E1924D7^A'
+'159E1925D7^A'
+'159E1926D7^A'
+'159E1927D7^A'
+'159E1928D7^A'
+'159E1929D7^A'
+'159E192AD7^A'
+'159E192BD7^A'
+'159E192CD7^A'
+'159E192DD7^A'
+'159E192ED7^A'
+'159E192FD7^A'
+'159E1930D7^A'
+'159E1931D7^A'
+'159E1932D7^A'
+'159E1933D7^A'
+'159E1934D6FFFF^A'
+'159E1935D7^A'
+'159E1936D7^A'
+'159E1937D7^A'
+'159E1938D7^A'
+'159E1939D7^A'
+'159E193AD7^A'
+'159E193BD7^A'
+'159E193CD7^A'
+'159E193DD7^A'
+'159E193ED7^A'
+'159E193FD7^A'
+'159E1940D7^A'
+'159E1941D7^A'
+'159E1942D7^A'
+'159E1943D7^A'
+'159E1944D7^A'
+'159E1945D7^A'
+'159E1946D7^A'
+'159E1947D7^A'
+'159E1948D7^A'
+'159E1949D7^A'
+'159E194AD7^A'
+'159E194B8A^A'
+'159E112B0A^A'
+'159E11F30A^A'
+'159E12B9D7^A'
+'159E1381D7^A'
+'159E142DD7^A'
+'159E1491D7^A'
+'159E14F5D7^A'
+'159E1559D7^A'
+'159E15BDD7^A'
+'159E1621D7^A'
+'159E1685D7^A'
+'159E16E9D7^A'
+'159E174DD7^A'
+'159E17B1D7^A'
+'159E1815D7^A'
+'159E1879D7^A'
+'159E18DDD7^A'
+'159E1941D7^A'
+'159E1065C3^A'
+'1^1'
+'712^3'
+END_ARRAY 1 14501
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf
new file mode 100755
index 0000000..73f2a79
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf
@@ -0,0 +1,2285 @@
+KPL/FK
+
+Dawn Frames Kernel
+========================================================================
+
+ This frame kernel contains complete set of frame definitions for the
+ Dawn Spacecraft (DAWN) including definitions for the Dawn spacecraft
+ and Dawn science instrument and engineering structure frames. This
+ kernel also contains NAIF ID/name mapping for the Dawn instruments.
+
+
+Version and Date
+========================================================================
+
+
+ Version 1.5 -- October 19, 2018 -- Boris Semenov, NAIF
+
+ Added more DSK surface name-IDs.
+
+ Version 1.4 -- March 29, 2018 -- Boris Semenov, NAIF
+
+ Added DSK surface name-ID mapping section.
+
+ Version 1.3 -- April 6, 2016 -- Boris Semenov, NAIF
+
+ Redefined the DAWN_FC2 frame as a CK-based frame to facilitate
+ providing different FC2 alignments relative to the s/c frame for
+ Vesta and Ceres missions.
+
+ Version 1.2 -- October 29, 2012 -- Boris Semenov, NAIF
+
+ Added Euler dynamic frames for Vesta coordinate systems
+ ``IAU-2000'' and ``DAWN-Claudia''.
+
+ Version 1.1 -- July 5, 2011 -- Boris Semenov, NAIF
+
+ Corrected description of the FC1 and FC2 frames. All frame
+ definitions are identical to Version 1.0.
+
+ Version 1.0 -- March 21, 2011 -- Boris Semenov, NAIF
+
+ Incorporated updated definitions of the DAWN_VIR_VIS, DAWN_VIR_IR,
+ DAWN_VIR_VIS_ZERO, and DAWN_VIR_IR_ZERO frames provided by
+ by Dr. Federico Tosi, INAF in "dawn_v10_draft3.tf"
+
+ Changed IDs of DAWN_VIR_VIS_ZERO and DAWN_VIR_IR_ZERO frames from
+ -203212 and -203214 to -203221 and -203223 to eliminate confusion
+ that may result from the IDs -203212 and -203214 mapping to
+ different names in the frames and physical objects domains. Since
+ these frames are fixed-offset, class 4 frames that are referred to
+ only by name in SPICE API calls and other kernels (e.g. IKs) this
+ change should be transparent to the users of this FK.
+
+ Updated star tracker alignments (frames DAWN_ST1 and DAWN_ST2)
+ and FC alignments (frames DAWN_FC1 and DAWN_FC2) per MCR-111570.
+
+ Version 0.9 -- July 1, 2010 -- Boris Semenov, NAIF
+
+ Incorporated updated definitions of the DAWN_VIR_VIS, DAWN_VIR_IR,
+ DAWN_VIR_VIS_ZERO, and DAWN_VIR_IR_ZERO frames provided by
+ Eleonora Ammannito, INAF in "VIR_kernel_update_r2.doc".
+
+ Version 0.8 -- October 8, 2009 -- Dr. Federico Tosi, INAF - IFSI
+ Boris Semenov, NAIF
+
+ Redefined VIR frames to better encapsulate the instrument scan
+ mirror motion and optical path misalignments, specifically:
+
+ - added DAWN_VIR frame (-203200), fixed to the spacecraft, to
+ capture the instrument base alignment relative to the spacecraft
+
+ - added DAWN_VIR_SCAN frame (-203201), CK-based, to capture
+ the motion of the mirror
+
+ - changed the reference frame for DAWN_VIR_VIS and
+ DAWN_VIR_IR to DAWN_VIR_SCAN
+
+ - renamed DAWN_VIR_VIS_SCAN and DAWN_VIR_IR_SCAN to
+ DAWN_VIR_VIS_ZERO and DAWN_VIR_IR_ZERO while keeping the
+ same IDs (-203212 and -203214) and redefined them to be
+ fixed offset frames relative to DAWN_VIR
+
+ - added DAWN_VIR/-203200 and DAWN_VIR_SCAN/-203201 name/ID
+ mappings
+
+ Version 0.7 -- July 3, 2009 -- Boris Semenov, NAIF
+
+ Incorporated Thomas Roatsch's name/ID mappings and individual
+ frames for FC filters. Included FC alignments used by DLR to
+ process MGA data in the comments.
+
+ Corrected and completed comments in the "Dawn Mission
+ NAIF ID Codes -- Summary Section" section.
+
+ Re-worded some of the version section entries for clarity.
+
+ Version 0.6t2 -- June 23, 2009 -- Steven Joy, DSC
+
+ Propagated test version of the DAWN_VIR_VIS_96/-203218 and
+ DAWN_VIR_VIS_32/-203219 name/ID mapping. Neither this nor the
+ previous updates have still been reviewed by the VIR team.
+
+ Version 0.6t -- April 09, 2009 -- Steven Joy, DSC
+
+ Propagated test version of the DAWN_VIR_VIS_16/-203217 name/ID
+ mapping. Neither this nor the previous updates have still been
+ reviewed by the VIR team.
+
+ Version 0.6t -- Jan 12, 2009 -- Steven Joy, DSC
+
+ Propagated test version of the DAWN_VIR_VIS_124/-203215 and
+ DAWN_VIR_VIS_64/-203216 name/ID mappings from version 0.5t into
+ the version 0.6 released by Boris. These updates have still not
+ been reviewed by the VIR team.
+
+ Version 0.6 -- January 5, 2009 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Incorporated FC alignments provided by Nick Mastrodemos.
+
+ Version 0.5t -- June 23, 2008 -- Steven Joy, DSC with Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Added definitions for name/ID mappings DAWN_VIR_VIS_124/-203215
+ and DAWN_VIR_VIS_64/-203216. These IDs are needed to define
+ special FOV for the VIR scan mirror of 128 (64) positions, half
+ on either side of the mirror center position.
+
+ Updated HGA frame orientation based on [7].
+
+
+ Version 0.5 -- January 10, 2008 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Updated HGA frame orientation based on [7].
+
+ Version 0.4 -- May 8, 2007 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Added ID/name mappings for the solar array corners.
+
+ Version 0.3 -- August 7, 2006 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Added star tracker (ST1 and ST2) and flight thruster (FT1, FT2,
+ and FT3) frames and name/ID mappings. In this version all STn and
+ FTn frames provide on nominal alignment.
+
+ Version 0.2 -- July 27, 2006 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Renamed DAWN_LGA frame and structure name to be DAWN_LGA+Z. Added
+ DAWN_LGA+X and DAWN_LGA-Z frames and structure name/IDs.
+
+ Version 0.1 -- May 9, 2005 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+ Added FC and VIR radiator name-ID mapping keywords. Removed
+ definitions of VESTA_FIXED and CERES_FIXED frames; these frames
+ are now defined in separate FKs (per request from SOA).
+
+ Version 0.0 -- October 11, 2004 -- Boris Semenov, NAIF
+
+ Preliminary Version. Pending review and approval by Dawn
+ instrument teams.
+
+
+References
+========================================================================
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``C-Kernel Required Reading''
+
+ 4. Dawn CDR Presentations.
+
+ 5. Dawn Instrument ICD/MICD documents.
+
+ 6. DAWN FSDD, CDRL TD-006, 9/27/04
+
+ 7. HGA Boresight Direction, e-mail from Ed Swenka, 01/10/08
+
+ 8. "Post-Processing Of Framing Camera Alignments"
+ (FCalignment_110118.docx), Ian Roundhill, January 18, 2011
+
+ 9. "Star Tracker and IRU In-Flight Calibration Test Report.
+ DN-DAWN-ACS-026" (DN-DAWN-ACS-026_01.pdf), A. Cross, 01/15/08
+
+
+Contact Information
+========================================================================
+
+ Boris V. Semenov, NAIF/JPL, (818)-354-8136, boris.semenov@jpl.nasa.gov
+
+
+Implementation Notes
+========================================================================
+
+ This file is used by the SPICE system as follows: programs that make
+ use of this frame kernel must ``load'' the kernel, normally during
+ program initialization. The SPICE routine FURNSH loads a kernel file
+ into the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name; ) -- FORTRAN
+ furnsh_c ( "frame_kernel_name" ); -- C
+ cspice_furnsh, frame_kernel_name -- IDL
+ cspice_furnsh( 'frame_kernel_name' ) -- MATLAB
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Dawn Mission NAIF ID Codes -- Summary Section
+========================================================================
+
+ The following names and NAIF ID codes are assigned to the Dawn
+ spacecraft, its structures and science instruments (the keywords
+ implementing these definitions are located in the section "Dawn
+ Mission NAIF ID Codes -- Definition Section" at the end of this
+ file):
+
+ Dawn Targets:
+
+ VESTA 2000004 (synonyms: '4 VESTA')
+ CERES 2000001 (synonyms: '1 CERES')
+
+ Dawn Spacecraft and Spacecraft Structures names/IDs:
+
+ DAWN -203
+ DAWN_SPACECRAFT -203000
+ DAWN_SA+Y -203010
+ DAWN_SA+Y_GIMBAL -203011
+ DAWN_SA+Y_C1 -203012
+ DAWN_SA+Y_C2 -203013
+ DAWN_SA+Y_C3 -203014
+ DAWN_SA+Y_C4 -203015
+ DAWN_SA-Y -203020
+ DAWN_SA-Y_GIMBAL -203021
+ DAWN_SA-Y_C1 -203022
+ DAWN_SA-Y_C2 -203023
+ DAWN_SA-Y_C3 -203024
+ DAWN_SA-Y_C4 -203025
+ DAWN_HGA -203040
+ DAWN_LGA+Z -203030
+ DAWN_LGA+X -203050
+ DAWN_LGA-Z -203060
+ DAWN_ST1 -203071
+ DAWN_ST2 -203072
+ DAWN_FT1 -203081
+ DAWN_FT2 -203082
+ DAWN_FT3 -203083
+
+ FC1 and FC2 names/IDs:
+
+ DAWN_FC1 -203110
+ DAWN_FC1_FILTER_1 -203111
+ DAWN_FC1_FILTER_2 -203112
+ DAWN_FC1_FILTER_3 -203113
+ DAWN_FC1_FILTER_4 -203114
+ DAWN_FC1_FILTER_5 -203115
+ DAWN_FC1_FILTER_6 -203116
+ DAWN_FC1_FILTER_7 -203117
+ DAWN_FC1_FILTER_8 -203118
+ DAWN_FC1_RAD -203119
+
+ DAWN_FC2 -203120
+ DAWN_FC2_FILTER_1 -203121
+ DAWN_FC2_FILTER_2 -203122
+ DAWN_FC2_FILTER_3 -203123
+ DAWN_FC2_FILTER_4 -203124
+ DAWN_FC2_FILTER_5 -203125
+ DAWN_FC2_FILTER_6 -203126
+ DAWN_FC2_FILTER_7 -203127
+ DAWN_FC2_FILTER_8 -203128
+ DAWN_FC2_RAD -203129
+
+ VIR names/IDs:
+
+ DAWN_VIR -203200
+ DAWN_VIR_SCAN -203201
+ DAWN_VIR_VIS -203211
+ DAWN_VIR_IR -203213
+ DAWN_VIR_VIS_SCAN -203212
+ DAWN_VIR_IR_SCAN -203214
+ DAWN_VIR_VIS_128 -203215
+ DAWN_VIR_VIS_64 -203216
+ DAWN_VIR_VIS_16 -203217
+ DAWN_VIR_VIS_96 -203218
+ DAWN_VIR_VIS_32 -203219
+ DAWN_VIR_RAD -203209
+
+ GRAND names/IDs:
+
+ DAWN_GRAND -203300
+
+
+ Vesta and Ceres DSK Surface names/IDs:
+
+ See "Dawn DSK Surface NAIF Names/ID Codes -- Definition Section"
+ section at the end the file.
+
+
+Dawn Frames
+========================================================================
+
+ The following Dawn frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ Dawn Target frames:
+ ----------------------------------------------------
+ IAU_VESTA J2000 PCK 10099 (1)
+ VESTA_FIXED J2000 PCK 2000004 (2)
+ VESTA_IAU_2000 J2000 DYNAMIC -203911
+ DAWN_CLAUDIA J2000 DYNAMIC -203912
+
+ CERES_FIXED J2000 PCK 2000001
+
+ Dawn Spacecraft and Spacecraft Structures frames:
+ ----------------------------------------------------
+ DAWN_SPACECRAFT J2000 CK -203000
+ DAWN_SA+Y DAWN_SPACECRAFT CK -203010
+ DAWN_SA-Y DAWN_SPACECRAFT CK -203020
+ DAWN_HGA DAWN_SPACECRAFT FIXED -203040
+ DAWN_LGA+Z DAWN_SPACECRAFT FIXED -203030
+ DAWN_LGA+X DAWN_SPACECRAFT FIXED -203050
+ DAWN_LGA-Z DAWN_SPACECRAFT FIXED -203060
+ DAWN_ST1 DAWN_SPACECRAFT FIXED -203071
+ DAWN_ST2 DAWN_SPACECRAFT FIXED -203072
+ DAWN_FT1 DAWN_SPACECRAFT FIXED (3) -203081
+ DAWN_FT2 DAWN_SPACECRAFT FIXED (3) -203082
+ DAWN_FT3 DAWN_SPACECRAFT FIXED (3) -203083
+
+ FC1 and FC2 frames:
+ -------------------
+ DAWN_FC1 DAWN_SPACECRAFT FIXED -203110
+ DAWN_FC1_FILTER_1 DAWN_FC1 FIXED -203111
+ DAWN_FC1_FILTER_2 DAWN_FC1 FIXED -203112
+ DAWN_FC1_FILTER_3 DAWN_FC1 FIXED -203113
+ DAWN_FC1_FILTER_4 DAWN_FC1 FIXED -203114
+ DAWN_FC1_FILTER_5 DAWN_FC1 FIXED -203115
+ DAWN_FC1_FILTER_6 DAWN_FC1 FIXED -203116
+ DAWN_FC1_FILTER_7 DAWN_FC1 FIXED -203117
+ DAWN_FC1_FILTER_8 DAWN_FC1 FIXED -203118
+
+ DAWN_FC2 DAWN_SPACECRAFT CK -203120
+ DAWN_FC2_FILTER_1 DAWN_FC2 FIXED -203121
+ DAWN_FC2_FILTER_2 DAWN_FC2 FIXED -203122
+ DAWN_FC2_FILTER_3 DAWN_FC2 FIXED -203123
+ DAWN_FC2_FILTER_4 DAWN_FC2 FIXED -203124
+ DAWN_FC2_FILTER_5 DAWN_FC2 FIXED -203125
+ DAWN_FC2_FILTER_6 DAWN_FC2 FIXED -203126
+ DAWN_FC2_FILTER_7 DAWN_FC2 FIXED -203127
+ DAWN_FC2_FILTER_8 DAWN_FC2 FIXED -203128
+
+ VIR frames:
+ -----------
+ DAWN_VIR DAWN_SPACECRAFT FIXED -203200
+ DAWN_VIR_SCAN DAWN_VIR CK -203201
+ DAWN_VIR_VIS DAWN_VIR_SCAN FIXED -203211
+ DAWN_VIR_IR DAWN_VIR_SCAN FIXED -203213
+
+ DAWN_VIR_VIS_ZERO DAWN_VIR FIXED -203221
+ DAWN_VIR_IR_ZERO DAWN_VIR FIXED -203223
+
+ GRAND frames:
+ -------------
+ DAWN_GRAND DAWN_SPACECRAFT FIXED -203300
+
+ (1) The IAU_VESTA frame is built into the Toolkit starting with the
+ Toolkit version N0054 (June 2010).
+
+ (2) The VESTA_FIXED frame is defined in a separate FK. It is essentially
+ a synonym of the IAU_VESTA frame.
+
+ (3) Although all flight thrusters are mounted on gimbals and can be
+ articulated within a small angular range (+/- 5 degrees during
+ flight), in this version of the FK their frames are defined as
+ fixed offset frames with respect to the spacecraft frame.
+
+
+Spacecraft and Spacecraft Structures Frame Tree
+========================================================================
+
+ The diagram below shows the frame hierarchy for the Dawn spacecraft
+ and its structure frame (not including science instrument frames.)
+
+ "VESTA_IAU_2000"
+ ----------------
+ ^
+ |<-dynamic
+ |
+ | "DAWN_CLAUDIA"
+ | --------------
+ | ^
+ | |<-dynamic
+ | |
+ | |
+ | | "J2000" INERTIAL
+ +-----------------------------------------------------+
+ | | | |
+ |<-pck |<-pck | |<-pck
+ | | | |
+ V V | V
+ "VESTA_FIXED" "IAU_VESTA" | "CERES_FIXED"
+ ------------- ------------- | -------------
+ |
+ |
+ |
+ "DAWN_ST1" "DAWN_ST2" | "DAWN_LGA+X" "DAWN_LGA-Z"
+ --------- ---------- | ------------ ------------
+ ^ ^ | ^ ^
+ | | | | |
+ |<-fixed |<-fixed |<-ck |<-fixed |<-fixed
+ | | | | |
+ | | V | |
+ | | "DAWN_SPACECRAFT" | |
+ +-----------------------------------------------------+
+ | | . | | | | |
+ |<-ck |<-ck . | | | |<-fixed |<-fixed
+ | | . | | | | |
+ V V . | | | V V
+ "DAWN_SA+Y" "DAWN_SA-Y" . | | | "DAWN_LGA+Z" "DAWN_HGA"
+ ----------- ----------- . | | | ------------ ----------
+ . | | |
+ . | | |<-fixed
+ . | | |
+ . | | V
+ . | | "DAWN_FT1"
+ . | | ----------
+ . | |
+ . | |<-fixed
+ . | |
+ . | V
+ . | "DAWN_FT2"
+ . | ----------
+ . |
+ . |<-fixed
+ . |
+ . V
+ . "DAWN_FT3"
+ . ----------
+ .
+ .
+ V
+ Individual instrument frame trees are provided
+ in the other sections of this file
+
+
+Dawn Target Frames
+========================================================================
+
+ This section of the file contains the body-fixed frame definitions
+ for the Dawn mission targets -- asteroids 4 Vesta and 1 Ceres.
+
+ All target body-fixed frames are defined according to the standard
+ body-fixed frame formation rules:
+
+ - +Z axis is toward the North pole;
+
+ - +X axis is toward the prime meridian;
+
+ - +Y axis completes the right handed frame;
+
+ - the origin of this frame is at the center of the body.
+
+ Some of these frames are defined as PCK-based frames with the
+ orientation computed by evaluating corresponding rotation constants
+ provided in the PCK file(s).
+
+ Other frames are defined as Euler frames with the constants
+ equivalent to the PCK constants included directly into the frame
+ definition.
+
+
+Vesta Frames
+--------------------------------------
+
+``IAU_VESTA'' Frame
+
+ The IAU_VESTA frame is a PCK-based Vesta body-fixed frame built into
+ the SPICE Toolkit starting with the Toolkit version N0064 (June
+ 2010). Its orientation is computed using Vesta rotation constants
+ from the last loaded PCK file containing such constants.
+
+
+``VESTA_FIXED'' Frame
+
+ The VESTA_FIXED frame is a PCK-based Vesta body-fixed frame defined
+ in a separate FK (per request from SOA team on May 9, 2005). This
+ frame is a synonym of the IAU_VESTA frame. Its orientation is
+ computed using Vesta rotation constants from the last loaded PCK
+ file containing such constants.
+
+
+``IAU-2000'' Frame
+
+ The VESTA_IAU_2000 frame represents the ``IAU-2000'' coordinate
+ system used by the project prior to its arrival to Vesta as well as
+ in numerous pre-DAWN ground observations of Vesta. It is defined as
+ an Euler frame mathematically identical to the PCK frame IAU_VESTA
+ when the IAU_VESTA frame is used with the rotation constants from
+ the DAWN PCK file ``pck00008.tpc''.
+
+ The ``pck00008.tpc'' PCK data defining the ``IAU-2000'' coordinate
+ system orientation are:
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+
+ According to the section ``Example of an Euler Frame'' of [1] the
+ angles for the Euler frame relative to the J2000 frame with the
+ reference epoch of J2000 TDB are derived from the standard set of
+ text PCK body orientation terms as follows:
+
+ ANGLE_1 = -pi/2 - RA
+ ANGLE_2 = -pi/2 + Dec
+ ANGLE_3 = - PM
+
+ The definition below incorporates the angles derived in this way
+ from the ``IAU-2000'' coordinate system orientation constants
+ above, in degrees with with the PM rate term converted to
+ degrees/sec.
+
+ \begindata
+
+ FRAME_VESTA_IAU_2000 = -203911
+ FRAME_-203911_NAME = 'VESTA_IAU_2000'
+ FRAME_-203911_CLASS = 5
+ FRAME_-203911_CLASS_ID = -203911
+ FRAME_-203911_CENTER = 2000004
+ FRAME_-203911_RELATIVE = 'J2000'
+ FRAME_-203911_DEF_STYLE = 'PARAMETERIZED'
+ FRAME_-203911_FAMILY = 'EULER'
+ FRAME_-203911_EPOCH = @2000-JAN-01/12:00:00
+ FRAME_-203911_AXES = ( 3 1 3 )
+ FRAME_-203911_UNITS = 'DEGREES'
+ FRAME_-203911_ANGLE_1_COEFFS = ( -31.00 )
+ FRAME_-203911_ANGLE_2_COEFFS = ( -49.00 )
+ FRAME_-203911_ANGLE_3_COEFFS = ( -292.00, -0.18719129351851851E-01 )
+
+ \begintext
+
+
+``DAWN-Claudia'' Frame
+
+ The DAWN_CLAUDIA frame represents the ``DAWN-Claudia'' coordinate
+ system used by the project during operations at Vesta. It is defined
+ as an Euler frame mathematically identical to the PCK frame
+ IAU_VESTA when the IAU_VESTA frame is used with the rotation
+ constants from the DAWN PCK file ``dawn_vesta_v04.tpc''.
+
+ The ``dawn_vesta_v04.tpc'' PCK data defining the ``DAWN-Claudia''
+ coordinate system orientation are:
+
+ BODY2000004_POLE_RA = ( 309.031 0.0 0.0 )
+ BODY2000004_POLE_DEC = ( 42.235 0.0 0.0 )
+ BODY2000004_PM = ( 75.39 1617.3329428 0.0 )
+
+ According to the section ``Example of an Euler Frame'' of [1] the
+ angles for the Euler frame relative to the J2000 frame with the
+ reference epoch of J2000 TDB are derived from the standard set of
+ text PCK body orientation terms as follows:
+
+ ANGLE_1 = -pi/2 - RA
+ ANGLE_2 = -pi/2 + Dec
+ ANGLE_3 = - PM
+
+ The definition below incorporates the angles derived in this way
+ from the ``DAWN-Claudia'' coordinate system orientation constants
+ above, in degrees with with the PM rate term converted to
+ degrees/sec.
+
+ \begindata
+
+ FRAME_DAWN_CLAUDIA = -203912
+ FRAME_-203912_NAME = 'DAWN_CLAUDIA'
+ FRAME_-203912_CLASS = 5
+ FRAME_-203912_CLASS_ID = -203912
+ FRAME_-203912_CENTER = 2000004
+ FRAME_-203912_RELATIVE = 'J2000'
+ FRAME_-203912_DEF_STYLE = 'PARAMETERIZED'
+ FRAME_-203912_FAMILY = 'EULER'
+ FRAME_-203912_EPOCH = @2000-JAN-01/12:00:00
+ FRAME_-203912_AXES = ( 3 1 3 )
+ FRAME_-203912_UNITS = 'DEGREES'
+ FRAME_-203912_ANGLE_1_COEFFS = ( -39.031 )
+ FRAME_-203912_ANGLE_2_COEFFS = ( -47.765 )
+ FRAME_-203912_ANGLE_3_COEFFS = ( -75.39, -0.18719131282407406E-01 )
+
+ \begintext
+
+
+Dawn Spacecraft and Spacecraft Structures Frames
+========================================================================
+
+ This section of the file contains the definitions of the spacecraft
+ and spacecraft structures frames.
+
+
+Dawn Spacecraft Frame
+--------------------------------------
+
+ The Dawn spacecraft frame is defined as follows:
+
+ - +Z axis is along the nominal boresight direction of the framing
+ cameras;
+
+ - +X axis is along the nominal boresight direction of the HGA;
+
+ - +Y axis completes the right-hand frame;
+
+ - the origin of this frame is the launch vehicle interface point.
+
+ These diagrams illustrate the DAWN_SPACECRAFT frame:
+
+
+ +X s/c side (HGA side) view:
+ ----------------------------
+ ^
+ | toward asteroid
+ |
+
+ Science Deck
+ ._____________.
+ .__ _______________. | ._____. | .______________ ___.
+ | \ \ \ | .' `. | / \ \ |
+ | / / \ |/ | \| / / / |
+ | \ \ `. . | . .' \ \ |
+ | / / | o| o |o | / / |
+ | \ \ .' . .' `. . `. \ \ |
+ | / / / |\ +Zsc^ ` /| \ / / |
+ .__\ \_______________/ | `. | .' | \_______________\ \__.
+ -Y Solar Array .___` -|- '___. +Y Solar Array
+ / | \
+ `-o-----> +Ysc
+ +Xsc
+ +Xsc is out of
+ the page
+
+ +Z s/c side (science deck side) view:
+ -------------------------------------
+
+ ._____________.
+ | |
+ | |
+ | +Zsc +Ysc
+ o==/ /==================o | o----->|o==================/ /==o
+ -Y Solar Array | | | +Y Solar Array
+ | | |
+ .______|______.
+ .--V +Xsc
+ HGA .' `.
+ /___________\
+ `.|.' +Zsc is out
+ of the page
+
+
+ Since the orientation of the DAWN_SPACECRAFT frame is computed
+ on-board, sent down in telemetry, and stored in the s/c CK files, it
+ is defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_DAWN_SPACECRAFT = -203000
+ FRAME_-203000_NAME = 'DAWN_SPACECRAFT'
+ FRAME_-203000_CLASS = 3
+ FRAME_-203000_CLASS_ID = -203000
+ FRAME_-203000_CENTER = -203
+ CK_-203000_SCLK = -203
+ CK_-203000_SPK = -203
+
+ \begintext
+
+
+Dawn Solar Array Frames
+--------------------------------------
+
+ Since the Dawn solar arrays can be articulated (each having one
+ degree of freedom), the solar Array frames, DAWN_SA+Y and DAWN_SA-Y,
+ are defined as CK frames with their orientation given relative to
+ the DAWN_SPACECRAFT frame.
+
+ Both array frames are defined as follows (from [5]):
+
+ - +Y axis is parallel to the longest side of the array,
+ positively oriented from the yoke to the end of the wing;
+
+ - +Z axis is normal to the solar array plane, the solar cells
+ facing +Z;
+
+ - +X axis is defined such that (X,Y,Z) is right handed;
+
+ - the origin of the frame is located at the yoke geometric
+ center.
+
+ The axis of rotation is parallel to the Y axis of the spacecraft and
+ solar array frames.
+
+ This diagram illustrates the DAWN_SA+Y and DAWN_SA-Y frames:
+
+
+ +X s/c side (HGA side) view:
+ ----------------------------
+ ^
+ | toward asteroid
+ |
+
+ Science Deck
+ ._____________. +Xsa+y
+ .__ _______________. | ._____. |^ .______________ ___.
+ | \ \ \ | .' `. || / \ \ |
+ | / / \ |/ | \|| / / / |
+ | \ \ `. . | .|.' \ \ |
+ | / / +Ysa-y <-----x| o |x-----> +Ysa+y / / |
+ | \ \ .'|. .' `. . `. \ \ |
+ | / / / ||\ +Zsc^ ` /| \ / / |
+ .__\ \_______________/ || `. | .' | \_______________\ \__.
+ -Y Solar Array V.___` -|- '___. +Y Solar Array
+ +Xsa-y / | \
+ `-o-----> +Ysc
+ +Xsc
+ +Xsc is out of the page
+
+ +Zsa+y and +Zsa-y
+ are into the page
+
+ Active solar cell is
+ facing away from the viewer
+
+
+ These sets of keywords define the solar array frames as CK frames:
+
+ \begindata
+
+ FRAME_DAWN_SA+Y = -203010
+ FRAME_-203010_NAME = 'DAWN_SA+Y'
+ FRAME_-203010_CLASS = 3
+ FRAME_-203010_CLASS_ID = -203010
+ FRAME_-203010_CENTER = -203
+ CK_-203010_SCLK = -203
+ CK_-203010_SPK = -203
+
+ FRAME_DAWN_SA-Y = -203020
+ FRAME_-203020_NAME = 'DAWN_SA-Y'
+ FRAME_-203020_CLASS = 3
+ FRAME_-203020_CLASS_ID = -203020
+ FRAME_-203020_CENTER = -203
+ CK_-203020_SCLK = -203
+ CK_-203020_SPK = -203
+
+ \begintext
+
+
+Dawn Low Gain Antenna Frames
+--------------------------------------
+
+ DAWN has three Low Gain Antennas (LGAs) [see 6]: LGA+Z pointing along
+ the s/c +Z axis, LGA+X pointing along the s/c +X axis, and LGA-Z
+ pointing along the s/c -Z axis. All three LGAs are rigidly attached
+ to the s/c bus. Therefore, their frames -- DAWN_LGA+Z, DAWN_LGA+X,
+ and DAWN_LGA-Z -- are defined as a fixed offset frames with
+ orientation given relative to the DAWN_SPACECRAFT frame.
+
+ Each of the DAWN LGA frames - DAWN_LGA+Z, DAWN_LGA+X, and DAWN_LGA-Z
+ -- is defined as follows:
+
+ - +Z axis is in the antenna boresight direction;
+
+ - +Y axis is nominally parallel to the s/c +Y axis;
+
+ - +X axis completes the right handed frame;
+
+ - the origin of the frame is located at the geometric center of
+ the LGA outer patch.
+
+ Neither +X nor +Y axis of in each frame is lined up with the antenna
+ clock angle reference direction, which was not known at the time
+ when this version of the FK was created.
+
+ This diagram illustrates the DAWN LGA frames:
+
+ +Z s/c side view:
+ -----------------
+
+ ._____________.
+ | |
+ | |
+ | +Zsc +Ysc
+ o==/ /==================o | o----> o==================/ /==o
+ -Y Solar Array +Zlga+z | ^+Xlga-z +Y Solar Array
+ | o-----> |
+ ._|____|______|
+ | .--V--. x-----> +Ylga-z
+ | +Xsc `. x-----> +Ylga+x
+ V _________\|
+ +Xlga+z `.|.' |
+ |
+ HGA V
+ +Zlga+x
+
+ +Zsc and +Zlga+z are out
+ of the page
+
+ +Xlga+x and +Zlga-z are
+ into the page
+
+ As seen on the diagram the DAWN_LGA+Z frame and the s/c frame are
+ nominally co-aligned, the DAWN_LGA+X frame is rotated from the s/c
+ frame by +90 degrees about Y, and the DAWN_LGA-Z frame is rotated
+ from the s/c frame by 180 degree about Y.
+
+ These sets of keywords define the LGA frames:
+
+ \begindata
+
+ FRAME_DAWN_LGA+Z = -203030
+ FRAME_-203030_NAME = 'DAWN_LGA+Z'
+ FRAME_-203030_CLASS = 4
+ FRAME_-203030_CLASS_ID = -203030
+ FRAME_-203030_CENTER = -203
+ TKFRAME_-203030_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203030_SPEC = 'ANGLES'
+ TKFRAME_-203030_UNITS = 'DEGREES'
+ TKFRAME_-203030_ANGLES = ( 0.000, 0.000, 0.000 )
+ TKFRAME_-203030_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_LGA+X = -203050
+ FRAME_-203050_NAME = 'DAWN_LGA+X'
+ FRAME_-203050_CLASS = 4
+ FRAME_-203050_CLASS_ID = -203050
+ FRAME_-203050_CENTER = -203
+ TKFRAME_-203050_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203050_SPEC = 'ANGLES'
+ TKFRAME_-203050_UNITS = 'DEGREES'
+ TKFRAME_-203050_ANGLES = ( 0.000, -90.00, 0.000 )
+ TKFRAME_-203050_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_LGA-Z = -203060
+ FRAME_-203060_NAME = 'DAWN_LGA-Z'
+ FRAME_-203060_CLASS = 4
+ FRAME_-203060_CLASS_ID = -203060
+ FRAME_-203060_CENTER = -203
+ TKFRAME_-203060_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203060_SPEC = 'ANGLES'
+ TKFRAME_-203060_UNITS = 'DEGREES'
+ TKFRAME_-203060_ANGLES = ( 0.000, 180.00, 0.000 )
+ TKFRAME_-203060_AXES = ( 1, 2, 3 )
+
+ \begintext
+
+
+Dawn High Gain Antenna Frame
+--------------------------------------
+
+ The Dawn High Gain Antenna is rigidly attached to the +X side of the
+ s/c bus. Therefore, the Dawn HGA frame, DAWN_HGA, is defined as a
+ fixed offset frame with its orientation given relative to the
+ DAWN_SPACECRAFT frame.
+
+ The DAWN_HGA frame is defined as follows:
+
+ - +Z axis is in the antenna boresight direction;
+
+ - +Y axis is nominally parallel to the s/c +Y axis;
+
+ - +X axis completes the right handed frame;
+
+ - the origin of the frame is located at the geometric center of
+ the HGA dish outer rim circle.
+
+ This diagram illustrates the DAWN_HGA frame:
+
+ +Z s/c side (science deck side) view:
+ -------------------------------------
+
+ ._____________.
+ | |
+ | |
+ | +Zsc +Ysc
+ o==/ /==================o | o----->|o==================/ /==o
+ -Y Solar Array | | | +Y Solar Array
+ | | |
+ .______|______.
+ .--V +Xsc
+ HGA .' `.
+ /_____x----->
+ `.|.' +Yhga +Zsc is out
+ | of the page
+ |
+ V +Zhga +Xhga is into
+ the page
+
+
+
+ As seen on the diagram a single rotation by +90 degrees about +Y is
+ needed to align the s/c frame with the HGA frame.
+
+ According to [7] the actual HGA boresight direction in the spacecraft
+ frame used in the on-board FSW code and ACS ground tools is:
+
+ AcTable.Boresight.HighGainAntenna.v =
+ {0.999999899738598, -0.000219079458599998, -0.000390547031294996}
+
+ The following two rotations are needed to align the spacecraft frame
+ with the HGA frame having +Z along this direction: first by
+ +90.02237670 degrees about Y, then by +0.01255233 degrees about X.
+
+ This set of keywords defines the HGA frame as a fixed offset frame:
+
+ \begindata
+
+ FRAME_DAWN_HGA = -203040
+ FRAME_-203040_NAME = 'DAWN_HGA'
+ FRAME_-203040_CLASS = 4
+ FRAME_-203040_CLASS_ID = -203040
+ FRAME_-203040_CENTER = -203
+ TKFRAME_-203040_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203040_SPEC = 'ANGLES'
+ TKFRAME_-203040_UNITS = 'DEGREES'
+ TKFRAME_-203040_ANGLES = ( -90.02237670, -0.01255233, 0.0 )
+ TKFRAME_-203040_AXES = ( 2, 1, 3 )
+
+ \begintext
+
+
+Dawn Star Tracker Frames
+--------------------------------------
+
+ The star trackers (ST1 and ST2) are rigidly attached to the +Z side
+ of the s/c bus. Therefore, the star tracker frames, DAWN_ST1 and
+ DAWN_ST2, are defined as fixed offset frames with their orientation
+ given relative to the DAWN_SPACECRAFT frame.
+
+ The star tracker frames are defined as follows:
+
+ - +Z axis is in the star tracker boresight direction;
+
+ - +X axis nominally points along the s/c +Z axis;
+
+ - +Y axis completes the right handed frame;
+
+ - the origin of the frame is located at the star tracker focal
+ point.
+
+ This diagram illustrates the star tracker frames:
+
+ +Z s/c side (science deck side) view:
+ -------------------------------------
+
+
+ \ 30 deg | 30 deg /
+ \<--------->|<--------->/
+ \ | /
+
+ +Zst2 +Zst1
+ ^ +Yst1 ^
+ \ ^ /
+ \ .' /
+ ._\__.'_____/_.
+ +Xst2 o' o +Xst1
+ | `.|
+ | +Zsc `. +Yst2
+ o==/ /==================o | o----->|o`>================/ /==o
+ -Y Solar Array | | +Ysc +Y Solar Array
+ | | |
+ .______|______.
+ .--V +Xsc
+ HGA .' `.
+ /___________\
+ `.|.' +Zsc, +Xst1 and +Xst2 are
+ out of the page
+
+
+ As seen on the diagram two rotations -- first by -90 degrees about Y
+ and second by -30 degree (for ST1) or +30 degrees (for ST2) about X
+ -- are needed to align the s/c frame with the star tracker frames.
+
+ This nominal alignment was provided in the officially released
+ FK versions 0.1 to 0.8.
+
+ Per MCR-111570, 03/18/11, the nominal alignments were replaced with
+ the following actual alignments provided in [8] and [9].
+
+ Star Tracker 1 wrt Spacecraft Frame: R_ST1_2,SF in the "Inputs"
+ section of [8]:
+
+ -0.00167591111459615 -0.00865834105070781 -0.999961111469934
+ 0.497384915940654 0.867489831468208 -0.00834492024941222
+ 0.867528349229375 -0.497379558716992 0.00285269238533509
+
+ Star Tracker 2 wrt Spacecraft Frame: QBdyToSta[1] and
+ DcmBdyToSta[1] on page 24 in the "Appendix A" of [9]:
+
+ 0.003428012232148947 -0.002975996167250916 -0.9999896960363887
+ -0.5035582110269716 0.8639506124714249 -0.004297361698267110
+ 0.8639544992876952 0.5035677537899567 0.001463045961520582
+
+ Because these alignments are for the ACS star tracker frames with
+ the boresight along -Z they had to be rotated by 180 degrees about Y
+ to agree with the frame definition described above (boresight along
+ +Z). Such rotation is equivalent to flipping the sign for each
+ component in the top and bottom rows of the matrices. These
+ alignments were incorporated into the FK starting with version 1.0
+ (March 2011).
+
+ The sets of keywords below defines the star tracker frames.
+
+ \begindata
+
+ FRAME_DAWN_ST1 = -203071
+ FRAME_-203071_NAME = 'DAWN_ST1'
+ FRAME_-203071_CLASS = 4
+ FRAME_-203071_CLASS_ID = -203071
+ FRAME_-203071_CENTER = -203
+ TKFRAME_-203071_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203071_SPEC = 'MATRIX'
+ TKFRAME_-203071_MATRIX = (
+
+ 0.00167591111459615 0.00865834105070781 0.999961111469934
+ 0.497384915940654 0.867489831468208 -0.00834492024941222
+ -0.867528349229375 0.497379558716992 -0.00285269238533509
+
+ )
+
+
+ FRAME_DAWN_ST2 = -203072
+ FRAME_-203072_NAME = 'DAWN_ST2'
+ FRAME_-203072_CLASS = 4
+ FRAME_-203072_CLASS_ID = -203072
+ FRAME_-203072_CENTER = -203
+ TKFRAME_-203072_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203072_SPEC = 'MATRIX'
+ TKFRAME_-203072_MATRIX = (
+
+ -0.003428012232148947 0.002975996167250916 0.9999896960363887
+ -0.5035582110269716 0.8639506124714249 -0.004297361698267110
+ -0.8639544992876952 -0.5035677537899567 -0.001463045961520582
+
+ )
+
+ \begintext
+
+
+Dawn Flight Thruster Frames
+--------------------------------------
+
+ Although the flight thrusters (FT1, FT2, and FT3) are mounted on
+ gimbals and can be articulated within a small angular range (+/- 5
+ degrees during flight), in this version of the FK their frames --
+ DAWN_FT1, DAWN_FT2, and DAWN_FT3 -- are defined as fixed offset
+ frames with respect to the spacecraft frame.
+
+ Each of the flight thruster frames is defined in the same way as
+ follows:
+
+ - +Z axis is in the thrust direction;
+
+ - +Y axis nominally points along the s/c +Y axis;
+
+ - +X axis completes the right handed frame;
+
+ - the origin of the frame is located at the geometric center of
+ the thruster nozzle outer rim circle.
+
+ This diagram illustrates the flight thruster frames:
+
+ +Y s/c side view:
+ -----------------
+ Science Deck
+ ._____________.
+ . | . |
+ |`. | |+Y solar array
+ | \ | | |
+ .'| .| | |
+ --| | o |
+ `.| '| | | .> +Xft1
+ | / | +Zsc^ | .'
+ |.' | | | .'
+ o______|______o'
+ / `. / | \ \
+ / <-----o-----> \
+ / +Xsc `>| +Xft3 \
+ V +Xft1| V +Zft1
+ +Zft2 |
+ V +Zft3
+
+ / 48 deg | 48 deg \ +Ysc, +Yft1, +Yft2,
+ /<------------>|<------------>\ and +Yft3 are out of
+ / | \ the page
+
+
+ As seen on the diagram one rotation -- about +Y by -132 degrees for
+ FT1, +132 degrees for FT2, or 180 degrees for FT3 -- is needed to
+ align the s/c frame with the individual thruster frame.
+
+ The sets of keywords below defines the flight thruster frames:
+
+ \begindata
+
+ FRAME_DAWN_FT1 = -203081
+ FRAME_-203081_NAME = 'DAWN_FT1'
+ FRAME_-203081_CLASS = 4
+ FRAME_-203081_CLASS_ID = -203081
+ FRAME_-203081_CENTER = -203
+ TKFRAME_-203081_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203081_SPEC = 'ANGLES'
+ TKFRAME_-203081_UNITS = 'DEGREES'
+ TKFRAME_-203081_ANGLES = ( 0.000, 132.000, 0.000 )
+ TKFRAME_-203081_AXES = ( 3, 2, 1 )
+
+ FRAME_DAWN_FT2 = -203082
+ FRAME_-203082_NAME = 'DAWN_FT2'
+ FRAME_-203082_CLASS = 4
+ FRAME_-203082_CLASS_ID = -203082
+ FRAME_-203082_CENTER = -203
+ TKFRAME_-203082_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203082_SPEC = 'ANGLES'
+ TKFRAME_-203082_UNITS = 'DEGREES'
+ TKFRAME_-203082_ANGLES = ( 0.000, -132.000, 0.000 )
+ TKFRAME_-203082_AXES = ( 3, 2, 1 )
+
+ FRAME_DAWN_FT3 = -203083
+ FRAME_-203083_NAME = 'DAWN_FT3'
+ FRAME_-203083_CLASS = 4
+ FRAME_-203083_CLASS_ID = -203083
+ FRAME_-203083_CENTER = -203
+ TKFRAME_-203083_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203083_SPEC = 'ANGLES'
+ TKFRAME_-203083_UNITS = 'DEGREES'
+ TKFRAME_-203083_ANGLES = ( 0.000, 180.000, 0.000 )
+ TKFRAME_-203083_AXES = ( 3, 2, 1 )
+
+ \begintext
+
+
+FC1 and FC2 Frames
+========================================================================
+
+ This section of the file contains the definitions of the Framing
+ Camera 1 (FC1) and Framing Camera 2 (FC2) frames.
+
+
+FC1 and FC2 Frame Tree
+--------------------------------------
+
+ The diagram below shows the FC1 and FC2 frame hierarchy.
+
+ "VESTA_IAU_2000"
+ ----------------
+ ^
+ |<-dynamic
+ |
+ | "DAWN_CLAUDIA"
+ | --------------
+ | ^
+ | |<-dynamic
+ | |
+ | |
+ | | "J2000" INERTIAL
+ +-----------------------------------------------------+
+ | | | |
+ |<-pck |<-pck | |<-pck
+ | | | |
+ V V | V
+ "VESTA_FIXED" "IAU_VESTA" | "CERES_FIXED"
+ ------------- ------------- | -------------
+ |
+ |<-ck
+ |
+ V
+ "DAWN_SPACECRAFT"
+ +-----------------------------------------------------+
+ | |
+ |<-fixed |<-ck
+ | |
+ V V
+ "DAWN_FC1" "DAWN_FC2"
+ ---------- ----------
+ | |
+ |<-fixed |<-fixed
+ | |
+ V V
+ "DAWN_FC1_FILTER_[1..8]" "DAWN_FC2_FILTER_[1..8]"
+ ------------------------ ------------------------
+
+
+FC1 and FC2 Frames
+--------------------------------------
+
+ The Framing Cameras 1 and 2 camera frames -- DAWN_FC1 and DAWN_FC2
+ -- are defined as follows:
+
+ - +Z axis points along the camera boresight;
+
+ - +X axis is parallel to the apparent image lines; it is
+ nominally co-aligned with the s/c +X axis;
+
+ - +Y axis completes the right handed frame; it is nominally
+ parallel the to the apparent image columns and co-aligned with
+ the s/c +Y axis;
+
+ - the origin of the frame is located at the camera focal point.
+
+ The Framing Cameras 1 and 2 filter frames -- DAWN_FC1_FILTER_[1..8]
+ and DAWN_FC2_FILTER_[1..8] -- are defined to be nominally co-aligned
+ with the corresponding camera frames.
+
+ This diagram illustrates the FC1 and FC2 camera frames:
+
+
+ +Z s/c side (science deck side) view:
+ -------------------------------------
+
+ +Yfc1
+ ._____________.
+ | o---o->---> +Yfc2
+ | | | |
+ | | | |+Ysc
+ o==/ /==================o | | o-|--->|o==================/ /==o
+ -Y Solar Array | V | V | +Y Solar Array
+ |+Xfc1 | +Xfc2
+ .______|______.
+ .--V +Xsc
+ HGA .' `. +Zsc, +Zfc1, and
+ /___________\ +Zfc2 are out
+ `.|.' of the page
+
+
+ Nominally, the FC1 and FC2 frames are co-aligned with the s/c frame.
+ The following nominal FC1 and FC2 frame definitions were provided in
+ the FK from October 11, 2004 to January 5, 2009 (ver. 0.0 to 0.5):
+
+ FRAME_DAWN_FC1 = -203110
+ FRAME_-203110_NAME = 'DAWN_FC1'
+ FRAME_-203110_CLASS = 4
+ FRAME_-203110_CLASS_ID = -203110
+ FRAME_-203110_CENTER = -203
+ TKFRAME_-203110_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203110_SPEC = 'ANGLES'
+ TKFRAME_-203110_UNITS = 'DEGREES'
+ TKFRAME_-203110_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203110_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2 = -203120
+ FRAME_-203120_NAME = 'DAWN_FC2'
+ FRAME_-203120_CLASS = 4
+ FRAME_-203120_CLASS_ID = -203120
+ FRAME_-203120_CENTER = -203
+ TKFRAME_-203120_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203120_SPEC = 'ANGLES'
+ TKFRAME_-203120_UNITS = 'DEGREES'
+ TKFRAME_-203120_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203120_AXES = ( 1, 2, 3 )
+
+ These frame alignments were used by FC team at DLR, Germany to
+ process February 2009 Mars Gravity Assist data;
+
+ FRAME_DAWN_FC1 = -203110
+ FRAME_-203110_NAME = 'DAWN_FC1'
+ FRAME_-203110_CLASS = 4
+ FRAME_-203110_CLASS_ID = -203110
+ FRAME_-203110_CENTER = -203
+ TKFRAME_-203110_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203110_SPEC = 'ANGLES'
+ TKFRAME_-203110_UNITS = 'DEGREES'
+ TKFRAME_-203110_ANGLES = ( -0.00302298, 0.07040644, 0.06472022 )
+ TKFRAME_-203110_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2 = -203120
+ FRAME_-203120_NAME = 'DAWN_FC2'
+ FRAME_-203120_CLASS = 4
+ FRAME_-203120_CLASS_ID = -203120
+ FRAME_-203120_CENTER = -203
+ TKFRAME_-203120_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203120_SPEC = 'ANGLES'
+ TKFRAME_-203120_UNITS = 'DEGREES'
+ TKFRAME_-203120_ANGLES = ( -0.07360254, 0.19136667, 0.08369507 )
+ TKFRAME_-203120_AXES = ( 1, 2, 3 )
+
+ The two matrices below represent the actual orientation of the FC1
+ and FC2 frames. These matrices rotate vectors from the s/c frame to
+ the corresponding camera frames. These matrices were determined by
+ Nick Mastrodemos, DAWN Optical Navigation Team, using the Functional,
+ Performance and Calibration test images taken in 2007-2008. They
+ were provided to NAIF on January 5, 2009 and were incorporated into
+ the FK starting with version 0.6 (January 2009):
+
+ FC1:
+
+ 0.999998669076022 -0.001146506533836 0.001160762229150
+ 0.001146467511555 0.999999342218256 0.000034282638084
+ -0.001160800770890 -0.000032951816272 0.999999325727647
+
+
+ FC2:
+
+ 0.999993562497650 -0.001478972971767 0.003269189839768
+ 0.001475079784942 0.999998200488307 0.001192962604301
+ -0.003270948316271 -0.001188132608755 0.999993944600674
+
+ Per MCR-111570, 03/18/11, the actual alignments above were replaced
+ with the following updated values provided in [8] and incorporated
+ in the FK with version 1.0 (March 2011):
+
+ FC1:
+
+ 0.99999903640145 -0.00088624511873564 0.001068487703551
+ 0.000886539816130183 0.999999569071098 -0.000275356733179061
+ -0.0010682432039777 0.000276303753185878 0.999999391254863
+
+ FC2:
+
+ 0.999994211374513 -0.00121806017718856 0.00317701858659441
+ 0.00121525960845842 0.999998871426382 0.000883293086781172
+ -0.00317809089965586 -0.000879427042947794 0.999994563157032
+
+ The FC1 matrix is provided in the frame definition below.
+
+ Per MCR-117124, 04/01/15, the FC2 alignment was adjusted based on an
+ analysis of 196 pictures from Ceres Opnavs 1-5, taken 01/13/15 to
+ 03/02/15. The new alignment is:
+
+ FC2:
+
+ 0.999994729254062 -0.00121791297955331 0.00300965983081698
+ 0.00121554146625864 0.999998949394655 0.000789674082497601
+ -0.00301061841759422 -0.000786011525583021 0.999995159168256
+
+ Since two different FC2 alignments -- one applicable to the Vesta
+ mission time period and the other to the Ceres mission time period
+ -- cannot be incorporated into a single fixed-offset frame, in the
+ FK version 1.3 (April 2015) the DAWN_FC2 frame class was changed
+ from a fixed-offset (class 4) to CK based (class 3) and two
+ different FC2 alignments were stored in a CK file for ID -203120.
+
+ \begindata
+
+ FRAME_DAWN_FC1 = -203110
+ FRAME_-203110_NAME = 'DAWN_FC1'
+ FRAME_-203110_CLASS = 4
+ FRAME_-203110_CLASS_ID = -203110
+ FRAME_-203110_CENTER = -203
+ TKFRAME_-203110_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203110_SPEC = 'MATRIX'
+ TKFRAME_-203110_MATRIX = (
+
+ 0.99999903640145 -0.00088624511873564 0.001068487703551
+ 0.000886539816130183 0.999999569071098 -0.000275356733179061
+ -0.0010682432039777 0.000276303753185878 0.999999391254863
+
+ )
+
+ FRAME_DAWN_FC2 = -203120
+ FRAME_-203120_NAME = 'DAWN_FC2'
+ FRAME_-203120_CLASS = 3
+ FRAME_-203120_CLASS_ID = -203120
+ FRAME_-203120_CENTER = -203
+ CK_-203120_SCLK = -203
+ CK_-203120_SPK = -203
+
+ \begintext
+
+ The keywords below define the FC filter frames to be co-aligned with
+ the corresponding camera frames.
+
+ \begindata
+
+ FRAME_DAWN_FC1_FILTER_1 = -203111
+ FRAME_-203111_NAME = 'DAWN_FC1_FILTER_1'
+ FRAME_-203111_CLASS = 4
+ FRAME_-203111_CLASS_ID = -203111
+ FRAME_-203111_CENTER = -203
+ TKFRAME_-203111_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203111_SPEC = 'ANGLES'
+ TKFRAME_-203111_UNITS = 'DEGREES'
+ TKFRAME_-203111_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203111_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_2 = -203112
+ FRAME_-203112_NAME = 'DAWN_FC1_FILTER_2'
+ FRAME_-203112_CLASS = 4
+ FRAME_-203112_CLASS_ID = -203112
+ FRAME_-203112_CENTER = -203
+ TKFRAME_-203112_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203112_SPEC = 'ANGLES'
+ TKFRAME_-203112_UNITS = 'DEGREES'
+ TKFRAME_-203112_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203112_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_3 = -203113
+ FRAME_-203113_NAME = 'DAWN_FC1_FILTER_3'
+ FRAME_-203113_CLASS = 4
+ FRAME_-203113_CLASS_ID = -203113
+ FRAME_-203113_CENTER = -203
+ TKFRAME_-203113_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203113_SPEC = 'ANGLES'
+ TKFRAME_-203113_UNITS = 'DEGREES'
+ TKFRAME_-203113_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203113_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_4 = -203114
+ FRAME_-203114_NAME = 'DAWN_FC1_FILTER_4'
+ FRAME_-203114_CLASS = 4
+ FRAME_-203114_CLASS_ID = -203114
+ FRAME_-203114_CENTER = -203
+ TKFRAME_-203114_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203114_SPEC = 'ANGLES'
+ TKFRAME_-203114_UNITS = 'DEGREES'
+ TKFRAME_-203114_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203114_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_5 = -203115
+ FRAME_-203115_NAME = 'DAWN_FC1_FILTER_5'
+ FRAME_-203115_CLASS = 4
+ FRAME_-203115_CLASS_ID = -203115
+ FRAME_-203115_CENTER = -203
+ TKFRAME_-203115_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203115_SPEC = 'ANGLES'
+ TKFRAME_-203115_UNITS = 'DEGREES'
+ TKFRAME_-203115_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203115_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_6 = -203116
+ FRAME_-203116_NAME = 'DAWN_FC1_FILTER_6'
+ FRAME_-203116_CLASS = 4
+ FRAME_-203116_CLASS_ID = -203116
+ FRAME_-203116_CENTER = -203
+ TKFRAME_-203116_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203116_SPEC = 'ANGLES'
+ TKFRAME_-203116_UNITS = 'DEGREES'
+ TKFRAME_-203116_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203116_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_7 = -203117
+ FRAME_-203117_NAME = 'DAWN_FC1_FILTER_7'
+ FRAME_-203117_CLASS = 4
+ FRAME_-203117_CLASS_ID = -203117
+ FRAME_-203117_CENTER = -203
+ TKFRAME_-203117_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203117_SPEC = 'ANGLES'
+ TKFRAME_-203117_UNITS = 'DEGREES'
+ TKFRAME_-203117_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203117_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC1_FILTER_8 = -203118
+ FRAME_-203118_NAME = 'DAWN_FC1_FILTER_8'
+ FRAME_-203118_CLASS = 4
+ FRAME_-203118_CLASS_ID = -203118
+ FRAME_-203118_CENTER = -203
+ TKFRAME_-203118_RELATIVE = 'DAWN_FC1'
+ TKFRAME_-203118_SPEC = 'ANGLES'
+ TKFRAME_-203118_UNITS = 'DEGREES'
+ TKFRAME_-203118_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203118_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_1 = -203121
+ FRAME_-203121_NAME = 'DAWN_FC2_FILTER_1'
+ FRAME_-203121_CLASS = 4
+ FRAME_-203121_CLASS_ID = -203121
+ FRAME_-203121_CENTER = -203
+ TKFRAME_-203121_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203121_SPEC = 'ANGLES'
+ TKFRAME_-203121_UNITS = 'DEGREES'
+ TKFRAME_-203121_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203121_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_2 = -203122
+ FRAME_-203122_NAME = 'DAWN_FC2_FILTER_2'
+ FRAME_-203122_CLASS = 4
+ FRAME_-203122_CLASS_ID = -203122
+ FRAME_-203122_CENTER = -203
+ TKFRAME_-203122_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203122_SPEC = 'ANGLES'
+ TKFRAME_-203122_UNITS = 'DEGREES'
+ TKFRAME_-203122_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203122_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_3 = -203123
+ FRAME_-203123_NAME = 'DAWN_FC2_FILTER_3'
+ FRAME_-203123_CLASS = 4
+ FRAME_-203123_CLASS_ID = -203123
+ FRAME_-203123_CENTER = -203
+ TKFRAME_-203123_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203123_SPEC = 'ANGLES'
+ TKFRAME_-203123_UNITS = 'DEGREES'
+ TKFRAME_-203123_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203123_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_4 = -203124
+ FRAME_-203124_NAME = 'DAWN_FC2_FILTER_4'
+ FRAME_-203124_CLASS = 4
+ FRAME_-203124_CLASS_ID = -203124
+ FRAME_-203124_CENTER = -203
+ TKFRAME_-203124_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203124_SPEC = 'ANGLES'
+ TKFRAME_-203124_UNITS = 'DEGREES'
+ TKFRAME_-203124_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203124_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_5 = -203125
+ FRAME_-203125_NAME = 'DAWN_FC2_FILTER_5'
+ FRAME_-203125_CLASS = 4
+ FRAME_-203125_CLASS_ID = -203125
+ FRAME_-203125_CENTER = -203
+ TKFRAME_-203125_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203125_SPEC = 'ANGLES'
+ TKFRAME_-203125_UNITS = 'DEGREES'
+ TKFRAME_-203125_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203125_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_6 = -203126
+ FRAME_-203126_NAME = 'DAWN_FC2_FILTER_6'
+ FRAME_-203126_CLASS = 4
+ FRAME_-203126_CLASS_ID = -203126
+ FRAME_-203126_CENTER = -203
+ TKFRAME_-203126_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203126_SPEC = 'ANGLES'
+ TKFRAME_-203126_UNITS = 'DEGREES'
+ TKFRAME_-203126_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203126_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_7 = -203127
+ FRAME_-203127_NAME = 'DAWN_FC2_FILTER_7'
+ FRAME_-203127_CLASS = 4
+ FRAME_-203127_CLASS_ID = -203127
+ FRAME_-203127_CENTER = -203
+ TKFRAME_-203127_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203127_SPEC = 'ANGLES'
+ TKFRAME_-203127_UNITS = 'DEGREES'
+ TKFRAME_-203127_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203127_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_FC2_FILTER_8 = -203128
+ FRAME_-203128_NAME = 'DAWN_FC2_FILTER_8'
+ FRAME_-203128_CLASS = 4
+ FRAME_-203128_CLASS_ID = -203128
+ FRAME_-203128_CENTER = -203
+ TKFRAME_-203128_RELATIVE = 'DAWN_FC2'
+ TKFRAME_-203128_SPEC = 'ANGLES'
+ TKFRAME_-203128_UNITS = 'DEGREES'
+ TKFRAME_-203128_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203128_AXES = ( 1, 2, 3 )
+
+ \begintext
+
+
+VIR frames:
+========================================================================
+
+ This section of the file contains the definitions of the VIR frames.
+
+
+VIR Frame Tree
+--------------------------------------
+
+ The diagram below shows the VIR frame hierarchy.
+
+ "VESTA_IAU_2000"
+ ----------------
+ ^
+ |<-dynamic
+ |
+ | "DAWN_CLAUDIA"
+ | --------------
+ | ^
+ | |<-dynamic
+ | |
+ | |
+ | | "J2000" INERTIAL
+ +-----------------------------------------------------+
+ | | | |
+ |<-pck |<-pck | |<-pck
+ | | | |
+ V V | V
+ "VESTA_FIXED" "IAU_VESTA" | "CERES_FIXED"
+ ------------- ------------- | -------------
+ |
+ |<-ck
+ |
+ V
+ "DAWN_SPACECRAFT"
+ -----------------
+ |
+ |<-fixed
+ |
+ V
+ DAWN_VIR
+ +-----------------------------------------------------+
+ | | |
+ |<-fixed |<-ck |<-fixed
+ | | |
+ V V V
+ "DAWN_VIR_VIS_ZERO" DAWN_VIR_SCAN "DAWN_VIR_IR_ZERO"
+ ------------------- +-----------------+ ------------------
+ | |
+ |<-fixed |<-fixed
+ | |
+ V V
+ "DAWN_VIR_VIS" "DAWN_VIR_IR"
+ -------------- -------------
+
+
+VIR Frames
+--------------------------------------
+
+ The following frames are defined for VIR instrument:
+
+ - the instrument base frame -- DAWN_VIR (ID -203200) -- is
+ defined as a fixed offset frame relative to the
+ DAWN_SPACECRAFT frame. It is intended to capture the
+ instrument base and scan mirror rotation axis alignment
+ relative to the spacecraft.
+
+ - the reflected scan mirror view direction frame --
+ DAWN_VIR_SCAN (ID -203201) -- is defined as a CK-based frame
+ with its orientation provided in CK files relative to the
+ DAWN_VIR frame. It is intended to capture change in the
+ instrument view direction due to the scan mirror motion.
+
+ - the reflected instrument detector view frames -- DAWN_VIR_VIS
+ (ID -203211) and DAWN_VIR_IR (ID -203213) -- are defined as
+ fixed offset frames relative to the DAWN_VIR_SCAN frame. They
+ are intended to capture reflected instrument boresights and
+ detector misalignments at any scan mirror position.
+
+ - the non-moving instrument detector view frames -- DAWN_VIR_VIS_ZERO
+ (ID -203221) and DAWN_VIR_IR_ZERO (ID -203223) -- are defined as
+ fixed offset frames relative to the DAWN_VIR frame. They are
+ intended to capture instrument boresights and detector
+ misalignments at the "0" scan mirror position and are used for
+ defining FOVs corresponding the full (256-step) and partial
+ (128-, 64-, 16-, 96-, and 32-step) scan mirror sweeps.
+
+ The +Y axes of the base and scan mirror frames (DAWN_VIR and
+ DAWN_VIR_SCAN) are co-aligned with the scan mirror rotation axis.
+
+ The +Z axes of the reflected and non-moving instrument detector view
+ frames are in the direction of the instrument boresight at any (for
+ DAWN_VIR_VIS and DAWN_VIR_IR) or the "0" (for DAWN_VIR_VIS_ZERO and
+ DAWN_VIR_IR_ZERO) scan mirror position. The +Y axes of these frames
+ are in the direction of spatial resolution and the +X axes complete
+ the right-handed frames.
+
+ Nominally, at the "0" scan mirror position all VIR frames are co-aligned
+ with each other and with the s/c frame as shown on this diagram:
+
+
+ +Z s/c side (science deck side) view:
+ -------------------------------------
+
+ o-----> +Yvir*
+ ._____|_______.
+ | | |
+ +Xvir*| |
+ | V +Ysc
+ o==/ /==================o | o----->|o==================/ /==o
+ -Y Solar Array | | | +Y Solar Array
+ | | |
+ .______|______.
+ .--V +Xsc
+ HGA .' `.
+ /___________\
+ `.|.' +Zsc and +Zvir*
+ are out of the page
+
+ The keywords below define the VIR frames. In this version of the FK
+ all misalignments are set be zero.
+
+ Preliminary alignment data for VIR-VIS indicate that the instrument
+ boresight (center pixel view direction) is tilted with respect to the
+ spacecraft +Z axis by 1.50 milliradians toward -Y axis and 1.25
+ milliradians toward +X. This misalignment is incorporated as a two
+ rotations, first by +1.50 milliradians about +X axis and then by
+ +1.25 milliradians about +Y axis, into the definitions of the
+ DAWN_VIR_VIS and DAWN_VIR_VIS_ZERO frames.
+
+ Preliminary alignment data for VIR-IR indicate that the instrument
+ boresight (center pixel view direction) is tilted with respect to the
+ spacecraft +Z axis by 0.75 milliradians toward -Y axis and 1.50
+ milliradians toward +X. This misalignment is incorporated as a two
+ rotations, first by +0.75 milliradians about +X axis and then by
+ +1.50 milliradians about +Y axis, into the definitions of the
+ DAWN_VIR_IR and DAWN_VIR_IR_ZERO frames.
+
+ \begindata
+
+ FRAME_DAWN_VIR = -203200
+ FRAME_-203200_NAME = 'DAWN_VIR'
+ FRAME_-203200_CLASS = 4
+ FRAME_-203200_CLASS_ID = -203200
+ FRAME_-203200_CENTER = -203
+ TKFRAME_-203200_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203200_SPEC = 'ANGLES'
+ TKFRAME_-203200_UNITS = 'DEGREES'
+ TKFRAME_-203200_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203200_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_VIR_SCAN = -203201
+ FRAME_-203201_NAME = 'DAWN_VIR_SCAN'
+ FRAME_-203201_CLASS = 3
+ FRAME_-203201_CLASS_ID = -203201
+ FRAME_-203201_CENTER = -203
+ CK_-203201_SCLK = -203
+ CK_-203201_SPK = -203
+
+ FRAME_DAWN_VIR_VIS = -203211
+ FRAME_-203211_NAME = 'DAWN_VIR_VIS'
+ FRAME_-203211_CLASS = 4
+ FRAME_-203211_CLASS_ID = -203211
+ FRAME_-203211_CENTER = -203
+ TKFRAME_-203211_RELATIVE = 'DAWN_VIR_SCAN'
+ TKFRAME_-203211_SPEC = 'ANGLES'
+ TKFRAME_-203211_UNITS = 'DEGREES'
+ TKFRAME_-203211_ANGLES = (-0.085943669, -0.071619724, 0.0)
+ TKFRAME_-203211_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_VIR_IR = -203213
+ FRAME_-203213_NAME = 'DAWN_VIR_IR'
+ FRAME_-203213_CLASS = 4
+ FRAME_-203213_CLASS_ID = -203213
+ FRAME_-203213_CENTER = -203
+ TKFRAME_-203213_RELATIVE = 'DAWN_VIR_SCAN'
+ TKFRAME_-203213_SPEC = 'ANGLES'
+ TKFRAME_-203213_UNITS = 'DEGREES'
+ TKFRAME_-203213_ANGLES = (-0.042971835, -0.085943669, 0.0)
+ TKFRAME_-203213_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_VIR_VIS_ZERO = -203221
+ FRAME_-203221_NAME = 'DAWN_VIR_VIS_ZERO'
+ FRAME_-203221_CLASS = 4
+ FRAME_-203221_CLASS_ID = -203221
+ FRAME_-203221_CENTER = -203
+ TKFRAME_-203221_RELATIVE = 'DAWN_VIR'
+ TKFRAME_-203221_SPEC = 'ANGLES'
+ TKFRAME_-203221_UNITS = 'DEGREES'
+ TKFRAME_-203221_ANGLES = (-0.085943669, -0.071619724, 0.0)
+ TKFRAME_-203221_AXES = ( 1, 2, 3 )
+
+ FRAME_DAWN_VIR_IR_ZERO = -203223
+ FRAME_-203223_NAME = 'DAWN_VIR_IR_ZERO'
+ FRAME_-203223_CLASS = 4
+ FRAME_-203223_CLASS_ID = -203223
+ FRAME_-203223_CENTER = -203
+ TKFRAME_-203223_RELATIVE = 'DAWN_VIR'
+ TKFRAME_-203223_SPEC = 'ANGLES'
+ TKFRAME_-203223_UNITS = 'DEGREES'
+ TKFRAME_-203223_ANGLES = (-0.042971835, -0.085943669, 0.0)
+ TKFRAME_-203223_AXES = ( 1, 2, 3 )
+
+ \begintext
+
+
+GRAND frames
+========================================================================
+
+ This section of the file contains the definitions of the GRAND
+ frames.
+
+
+GRAND Frame Tree
+--------------------------------------
+
+ The diagram below shows the GRAND frame hierarchy.
+
+ "VESTA_IAU_2000"
+ ----------------
+ ^
+ |<-dynamic
+ |
+ | "DAWN_CLAUDIA"
+ | --------------
+ | ^
+ | |<-dynamic
+ | |
+ | |
+ | | "J2000" INERTIAL
+ +-----------------------------------------------------+
+ | | | |
+ |<-pck |<-pck | |<-pck
+ | | | |
+ V V | V
+ "VESTA_FIXED" "IAU_VESTA" | "CERES_FIXED"
+ ------------- ------------- | -------------
+ |
+ |<-ck
+ |
+ V
+ "DAWN_SPACECRAFT"
+ +-----------------------------------------------------+
+ |
+ |<-fixed
+ |
+ V
+ "DAWN_GRAND"
+ ------------
+
+
+GRAND Frame
+--------------------------------------
+
+ The GRAND frame is defined as follows:
+
+ - +Z axis is nominally co-aligned with the s/c +Z axis;
+
+ - +Y axis is nominally co-aligned with the s/c +Y axis;
+
+ - +X axis completes the right handed frame; it is nominally
+ co-aligned with the s/c +X axis;
+
+ - the origin of the frame is located at the instrument "FOV"
+ vertex.
+
+ This diagram illustrates the GRAND frame:
+
+
+ +Z s/c side (science deck side) view:
+ -------------------------------------
+
+ ._____________.
+ | |
+ | |
+ | +Zsc +Ysc
+ o==/ /==================o | o----->|o==================/ /==o
+ -Y Solar Array +Xgrand | | +Y Solar Array
+ |o-----> +Ygrand
+ .|_____|______.
+ | .--V +Xsc
+ | ' `.
+ V __________\
+ +Xgrand `.|.' +Zsc and +Zgrand
+ HGA are out
+ of the page
+
+ Nominally, the GRAND frame is co-aligned with the s/c frame.
+
+ \begindata
+
+ FRAME_DAWN_GRAND = -203300
+ FRAME_-203300_NAME = 'DAWN_GRAND'
+ FRAME_-203300_CLASS = 4
+ FRAME_-203300_CLASS_ID = -203300
+ FRAME_-203300_CENTER = -203
+ TKFRAME_-203300_RELATIVE = 'DAWN_SPACECRAFT'
+ TKFRAME_-203300_SPEC = 'ANGLES'
+ TKFRAME_-203300_UNITS = 'DEGREES'
+ TKFRAME_-203300_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-203300_AXES = ( 1, 2, 3 )
+
+ \begintext
+
+
+Dawn Mission NAIF ID Codes -- Definition Section
+========================================================================
+
+ This section contains name to NAIF ID mappings for the Dawn mission.
+
+
+Dawn Target IDs:
+-------------------------------------------------------------
+
+ This table summarizes Dawn Target IDs:
+
+ Name ID Synonyms
+ --------------------- ------- ---------------------------
+ VESTA 2000004 '4 VESTA'
+ CERES 2000001 '1 CERES'
+
+ Name-ID Mapping keywords:
+
+ \begindata
+
+ NAIF_BODY_NAME += ( '4 VESTA' )
+ NAIF_BODY_CODE += ( 2000004 )
+
+ NAIF_BODY_NAME += ( 'VESTA' )
+ NAIF_BODY_CODE += ( 2000004 )
+
+ NAIF_BODY_NAME += ( '1 CERES' )
+ NAIF_BODY_CODE += ( 2000001 )
+
+ NAIF_BODY_NAME += ( 'CERES' )
+ NAIF_BODY_CODE += ( 2000001 )
+
+ \begintext
+
+
+Dawn Spacecraft ID
+-------------------------------------------------------------
+
+ This table summarizes Dawn Spacecraft IDs:
+
+ Name ID
+ --------------------- -------
+ DAWN -203
+
+ Name-ID Mapping keywords:
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'DAWN' )
+ NAIF_BODY_CODE += ( -203 )
+
+ \begintext
+
+
+Dawn Spacecraft Structures IDs
+--------------------------------------
+
+ This table summarizes Dawn Spacecraft Structure IDs:
+
+ Name ID
+ --------------------- -------
+ DAWN -203
+ DAWN_SPACECRAFT -203000
+ DAWN_SA+Y -203010
+ DAWN_SA+Y_GIMBAL -203011
+ DAWN_SA+Y_C1 -203012
+ DAWN_SA+Y_C2 -203013
+ DAWN_SA+Y_C3 -203014
+ DAWN_SA+Y_C4 -203015
+ DAWN_SA-Y -203020
+ DAWN_SA-Y_GIMBAL -203021
+ DAWN_SA-Y_C1 -203022
+ DAWN_SA-Y_C2 -203023
+ DAWN_SA-Y_C3 -203024
+ DAWN_SA-Y_C4 -203025
+ DAWN_HGA -203040
+ DAWN_LGA+Z -203030
+ DAWN_LGA+X -203050
+ DAWN_LGA-Z -203060
+ DAWN_ST1 -203071
+ DAWN_ST2 -203072
+ DAWN_FT1 -203081
+ DAWN_FT2 -203082
+ DAWN_FT3 -203083
+
+ Name-ID Mapping keywords:
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'DAWN_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -203000 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA+Y' )
+ NAIF_BODY_CODE += ( -203010 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA+Y_GIMBAL' )
+ NAIF_BODY_CODE += ( -203011 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA+Y_C1' )
+ NAIF_BODY_CODE += ( -203012 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA+Y_C2' )
+ NAIF_BODY_CODE += ( -203013 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA+Y_C3' )
+ NAIF_BODY_CODE += ( -203014 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA+Y_C4' )
+ NAIF_BODY_CODE += ( -203015 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA-Y' )
+ NAIF_BODY_CODE += ( -203020 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA-Y_GIMBAL' )
+ NAIF_BODY_CODE += ( -203021 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA-Y_C1' )
+ NAIF_BODY_CODE += ( -203022 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA-Y_C2' )
+ NAIF_BODY_CODE += ( -203023 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA-Y_C3' )
+ NAIF_BODY_CODE += ( -203024 )
+
+ NAIF_BODY_NAME += ( 'DAWN_SA-Y_C4' )
+ NAIF_BODY_CODE += ( -203025 )
+
+ NAIF_BODY_NAME += ( 'DAWN_HGA' )
+ NAIF_BODY_CODE += ( -203040 )
+
+ NAIF_BODY_NAME += ( 'DAWN_LGA+Z' )
+ NAIF_BODY_CODE += ( -203030 )
+
+ NAIF_BODY_NAME += ( 'DAWN_LGA+X' )
+ NAIF_BODY_CODE += ( -203050 )
+
+ NAIF_BODY_NAME += ( 'DAWN_LGA-Z' )
+ NAIF_BODY_CODE += ( -203060 )
+
+ NAIF_BODY_NAME += ( 'DAWN_ST1' )
+ NAIF_BODY_CODE += ( -203071 )
+
+ NAIF_BODY_NAME += ( 'DAWN_ST2' )
+ NAIF_BODY_CODE += ( -203072 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FT1' )
+ NAIF_BODY_CODE += ( -203081 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FT2' )
+ NAIF_BODY_CODE += ( -203082 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FT3' )
+ NAIF_BODY_CODE += ( -203083 )
+
+ \begintext
+
+
+FC1 and FC2 IDs
+--------------------------------------
+
+ This table summarizes FC1 and FC2 IDs:
+
+ Name ID
+ --------------------- -------
+ DAWN_FC1 -203110
+ DAWN_FC1_FILTER_1 -203111
+ DAWN_FC1_FILTER_2 -203112
+ DAWN_FC1_FILTER_3 -203113
+ DAWN_FC1_FILTER_4 -203114
+ DAWN_FC1_FILTER_5 -203115
+ DAWN_FC1_FILTER_6 -203116
+ DAWN_FC1_FILTER_7 -203117
+ DAWN_FC1_FILTER_8 -203118
+ DAWN_FC1_RAD -203119
+
+ DAWN_FC2 -203120
+ DAWN_FC2_FILTER_1 -203121
+ DAWN_FC2_FILTER_2 -203122
+ DAWN_FC2_FILTER_3 -203123
+ DAWN_FC2_FILTER_4 -203124
+ DAWN_FC2_FILTER_5 -203125
+ DAWN_FC2_FILTER_6 -203126
+ DAWN_FC2_FILTER_7 -203127
+ DAWN_FC2_FILTER_8 -203128
+ DAWN_FC2_RAD -203129
+
+ Name-ID Mapping keywords:
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1' )
+ NAIF_BODY_CODE += ( -203110 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_1' )
+ NAIF_BODY_CODE += ( -203111 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_2' )
+ NAIF_BODY_CODE += ( -203112 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_3' )
+ NAIF_BODY_CODE += ( -203113 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_4' )
+ NAIF_BODY_CODE += ( -203114 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_5' )
+ NAIF_BODY_CODE += ( -203115 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_6' )
+ NAIF_BODY_CODE += ( -203116 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_7' )
+ NAIF_BODY_CODE += ( -203117 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_8' )
+ NAIF_BODY_CODE += ( -203118 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC1_RAD' )
+ NAIF_BODY_CODE += ( -203119 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2' )
+ NAIF_BODY_CODE += ( -203120 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_1' )
+ NAIF_BODY_CODE += ( -203121 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_2' )
+ NAIF_BODY_CODE += ( -203122 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_3' )
+ NAIF_BODY_CODE += ( -203123 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_4' )
+ NAIF_BODY_CODE += ( -203124 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_5' )
+ NAIF_BODY_CODE += ( -203125 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_6' )
+ NAIF_BODY_CODE += ( -203126 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_7' )
+ NAIF_BODY_CODE += ( -203127 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_8' )
+ NAIF_BODY_CODE += ( -203128 )
+
+ NAIF_BODY_NAME += ( 'DAWN_FC2_RAD' )
+ NAIF_BODY_CODE += ( -203129 )
+
+ \begintext
+
+
+VIR IDs
+--------------------------------------
+
+ This table summarizes VIR IDs:
+
+ Name ID
+ --------------------- -------
+ DAWN_VIR -203200
+ DAWN_VIR_SCAN -203201
+ DAWN_VIR_VIS -203211
+ DAWN_VIR_IR -203213
+ DAWN_VIR_VIS_SCAN -203212
+ DAWN_VIR_IR_SCAN -203214
+ DAWN_VIR_VIS_128 -203215
+ DAWN_VIR_VIS_64 -203216
+ DAWN_VIR_VIS_16 -203217
+ DAWN_VIR_VIS_96 -203218
+ DAWN_VIR_VIS_32 -203219
+ DAWN_VIR_RAD -203209
+
+ Name-ID Mapping keywords:
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR' )
+ NAIF_BODY_CODE += ( -203200 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_SCAN' )
+ NAIF_BODY_CODE += ( -203201 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS' )
+ NAIF_BODY_CODE += ( -203211 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_IR' )
+ NAIF_BODY_CODE += ( -203213 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_SCAN' )
+ NAIF_BODY_CODE += ( -203212 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_IR_SCAN' )
+ NAIF_BODY_CODE += ( -203214 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_128' )
+ NAIF_BODY_CODE += ( -203215 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_64' )
+ NAIF_BODY_CODE += ( -203216 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_16' )
+ NAIF_BODY_CODE += ( -203217 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_96' )
+ NAIF_BODY_CODE += ( -203218 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_32' )
+ NAIF_BODY_CODE += ( -203219 )
+
+ NAIF_BODY_NAME += ( 'DAWN_VIR_RAD' )
+ NAIF_BODY_CODE += ( -203209 )
+
+ \begintext
+
+
+GRAND IDs
+--------------------------------------
+
+ This table summarizes GRAND IDs:
+
+ Name ID
+ --------------------- -------
+ DAWN_GRAND -203300
+
+ Name-ID Mapping keywords:
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'DAWN_GRAND' )
+ NAIF_BODY_CODE += ( -203300 )
+
+ \begintext
+
+
+Dawn DSK Surface NAIF Names/ID Codes -- Definition Section
+========================================================================
+
+ This section contains name to NAIF ID mappings for the Vesta and
+ Ceres DSK surfaces.
+
+ The following surface name-ID mappings are defined for Ceres:
+
+ Surface Name Surface ID Body ID
+ --------------------------- ---------- -------------
+ DAWN_DLR_SPG_135METER_V1 10101 2000001
+
+ DAWN_GRAV_SPC_0128ICQ_V1 20101 2000001
+ DAWN_GRAV_SPC_0256ICQ_V1 20102 2000001
+ DAWN_GRAV_SPC_0512ICQ_V1 20103 2000001
+ DAWN_GRAV_SPC_1024ICQ_V1 20104 2000001
+ DAWN_GRAV_SPC_300METER_V1 20105 2000001
+ DAWN_GRAV_SPC_100METER_V1 20106 2000001
+ DAWN_GRAV_SPC_035METER_V1 20107 2000001
+ DAWN_GRAV_SPC_0128ICQ_V2 20108 2000001
+ DAWN_GRAV_SPC_0256ICQ_V2 20109 2000001
+ DAWN_GRAV_SPC_0512ICQ_V2 20110 2000001
+ DAWN_GRAV_SPC_1024ICQ_V2 20111 2000001
+
+
+ \begindata
+
+ NAIF_SURFACE_NAME += 'DAWN_DLR_SPG_135METER_V1'
+ NAIF_SURFACE_CODE += 10101
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0128ICQ_V1'
+ NAIF_SURFACE_CODE += 20101
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0256ICQ_V1'
+ NAIF_SURFACE_CODE += 20102
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0512ICQ_V1'
+ NAIF_SURFACE_CODE += 20103
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_1024ICQ_V1'
+ NAIF_SURFACE_CODE += 20104
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_300METER_V1'
+ NAIF_SURFACE_CODE += 20105
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_100METER_V1'
+ NAIF_SURFACE_CODE += 20106
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_035METER_V1'
+ NAIF_SURFACE_CODE += 20107
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0128ICQ_V2'
+ NAIF_SURFACE_CODE += 20108
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0256ICQ_V2'
+ NAIF_SURFACE_CODE += 20109
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0512ICQ_V2'
+ NAIF_SURFACE_CODE += 20110
+ NAIF_SURFACE_BODY += 2000001
+
+ NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_1024ICQ_V2'
+ NAIF_SURFACE_CODE += 20111
+ NAIF_SURFACE_BODY += 2000001
+
+ \begintext
+
+
+End of FK.
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf
new file mode 100755
index 0000000..4160703
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf
@@ -0,0 +1,93 @@
+KPL/FK
+
+Dawn Frames Kernel for Asteroid Vesta
+========================================================================
+
+ This frame kernel contains definition of the body-fixed frame for
+ asteroid Vesta.
+
+
+Version and Date
+========================================================================
+
+ Version 0.0 -- May 9, 2005 -- Boris Semenov, NAIF
+
+ Preliminary Version.
+
+
+References
+========================================================================
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``PC-Kernel Required Reading''
+
+
+Contact Information
+========================================================================
+
+ Boris V. Semenov, NAIF/JPL, (818)-354-8136, boris.semenov@jpl.nasa.gov
+
+
+Implementation Notes
+========================================================================
+
+ This file is used by the SPICE system as follows: programs that make
+ use of this frame kernel must `load' the kernel, normally during
+ program initialization. The SPICELIB routine FURNSH and CSPICE
+ function furnsh_c load a kernel file into the kernel pool as shown
+ below.
+
+ CALL FURNSH ( 'frame_kernel_name' )
+ furnsh_c ( "frame_kernel_name" );
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Dawn Frames
+========================================================================
+
+ The following Dawn frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ Dawn Target frames:
+ -------------------
+ VESTA_FIXED J2000 PCK 2000004
+
+
+Dawn Target Frames
+========================================================================
+
+ This section of the file contains the body-fixed frame definition
+ for one of the Dawn mission targets -- asteroids 4 Vesta.
+
+ A body-fixed frame is defined for Vesta using standard body-fixed,
+ PCK-based frame formation rules:
+
+ - +Z axis is toward the North pole;
+
+ - +X axis is toward the prime meridian;
+
+ - +Y axis completes the right hand frame;
+
+ - the origin of this frame is at the center of the body.
+
+ The orientation of this frame is computed by evaluating
+ corresponding rotation constants provided in the PCK file(s).
+
+ \begindata
+
+ FRAME_VESTA_FIXED = 2000004
+ FRAME_2000004_NAME = 'VESTA_FIXED'
+ FRAME_2000004_CLASS = 2
+ FRAME_2000004_CLASS_ID = 2000004
+ FRAME_2000004_CENTER = 2000004
+ OBJECT_2000004_FRAME = 'VESTA_FIXED'
+
+ \begintext
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc
new file mode 100755
index 0000000..d9bc466
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc
@@ -0,0 +1,306 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "dawn_vesta_v06.tpc"
+MISSION_NAME = "DAWN MISSION TO VESTA AND CERES"
+SPACECRAFT_NAME = DAWN
+DATA_SET_ID = "DAWN-M/A-SPICE-6-V1.0"
+KERNEL_TYPE_ID = PCK
+PRODUCT_ID = "dawn_vesta_v06.tpc"
+PRODUCT_CREATION_TIME = 2012-09-27T14:04:32
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ "INITIAL CHECKOUT (ICO)",
+ "EARTH-MARS CRUISE (EMC)",
+ "MARS GRAVITY ASSIST (MGA)",
+ "MARS-VESTA CRUISE (MVC)",
+ "VESTA ENCOUNTER",
+ "VESTA-CERES CRUISE (VCC)",
+ "CERES ENCOUNTER",
+ "END OF MISSION"
+ }
+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 = {
+ "4 VESTA",
+ "1 CERES"
+ }
+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 = "SPICE PCK file containing constants for
+Vesta, created by NAIF, JPL. Vesta rotation constants provided in this PCK
+are for the ``Claudia Double-Prime'' coordinate system used in science
+products included in the DAWN Vesta mission PDS archives. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Asteroid Vesta P_constants (PcK) SPICE kernel file
+===========================================================================
+
+
+Organization
+--------------------------------------------------------
+
+ The sections of this file are as follows.
+
+ Introductory Information:
+
+ -- Version description
+
+ -- Disclaimer
+
+ -- Sources
+
+ Pck Data:
+
+ -- Orientation constants for asteroid Vesta
+
+ -- Radii for asteroid Vesta
+
+
+Version description
+--------------------------------------------------------
+
+ Version 0.6 -- October 20, 2012 -- Dr. Carol Raymond, DAWN Deputy PI,
+ Boris Semenov, NAIF
+
+ Corrected the Claudia center longitudes provided in the comment
+ sections ``Values in the Version 0.5'' (136.7 -> 136.0) and
+ ``Values in the Version 0.6'' (146.7 -> 146.0) *WITHOUT*
+ changing the file version or file name.
+
+ September 5, 2012 -- Dr. Carol Raymond, DAWN Deputy PI,
+ Dr. Steven Joy, Dawn Science Center Manager,
+ Boris Semenov, NAIF
+
+ Corrected W0 (295.39 -> 285.39).
+
+ Version 0.5 -- May 2, 2012 -- Dr. Carol Raymond, DAWN Deputy PI,
+ Dr. Steven Joy, Dawn Science Center Manager,
+ Boris Semenov, NAIF
+
+ Corrected W0 (75.39 -> 295.39).
+
+ Version 0.4 -- November 2, 2011 -- Dr. Carol Raymond, DAWN Deputy PI,
+ Boris Semenov, NAIF
+
+ Corrected W0 (76.06 -> 75.39).
+
+ Version 0.3 -- September 29, 2011 -- Dr. Carol Raymond, DAWN Deputy PI,
+ Boris Semenov, NAIF
+
+ Per MCR-112436 Vesta pole orientation and prime meridian
+ (Ra, Dec, W0) were changed to (309.031, 42.235, 76.06) degrees
+
+ Version 0.2 -- February 25, 2011 -- Boris Semenov, NAIF
+
+ Vesta pole orientation (Ra, Dec) was changed to (305.8, 41.4)
+ degrees per MCR-111475 and "Dawn Planetary Constants and Models
+ Document" Revision 2.0, Feb 16, 2011
+
+ Version 0.1 -- October 12, 2004 -- Boris Semenov, NAIF
+
+ VESTA_FIXED frame definition was removed. It is now in the DAWN
+ Frames Kernel file.
+
+ Version 0.0 -- October 6, 2003 -- Boris Semenov, NAIF
+
+ This is a preliminary PCK containing draft values for the pole
+ direction, prime meridian location, rotation period and shape
+ (from [1].)
+
+
+Disclaimer
+--------------------------------------------------------
+
+ This constants file may not contain the parameter values that you
+ prefer. Note that this file may be readily modified by you or
+ anyone else. NAIF suggests that you inspect this file visually
+ before proceeding with any critical or extended data processing.
+
+ NAIF requests that you update the ``by line'' and date if you
+ modify the file.
+
+
+Sources
+--------------------------------------------------------
+
+ The sources for the constants listed in this and the earlier
+ versions of this file are:
+
+ 1) Thomas, Peter C. et al. ``Vesta: Spin Pole, Size, and Shape
+ from HST Images.'' ICARUS 128, 1997. Article NO. IS975736.
+ pp. 93-94.
+
+ 2) "Dawn Planetary Constants and Models Document" Revision 2.0,
+ Feb 16, 2011
+
+ 3) Analysis of Data from Dawn's Survey Orbit, Sep 23, 2011.
+ (IOM attached to MCR-112436).
+
+
+Orientation constants for asteroid Vesta
+--------------------------------------------------------
+
+ The inertial reference frame for these constants is J2000; this is
+ the default reference frame for PCK orientation data.
+
+ The epoch of the constants is J2000; this is Julian ephemeris date
+ (JED) 2451545.0.
+
+ The NAIF integer code for Vesta is 2000004. See the NAIF_IDs
+ required reading for further information on NAIF integer codes.
+
+
+Values in the Versions 0.0 and 0.1
+
+ The pole direction, prime meridian location, and rotation period
+ in the versions 0.0 and 0.1 were set to the following values from
+ [1]:
+
+ "New data from the 1996 Hubble HST observations of Vesta allow a
+ refinement of the pole solution to: RA = 301 deg, Dec = 41 deg,
+ +/- 5 deg. The prime meridian is now given by W = 292 deg +
+ 1617.332776 deg * d; see Section 3a and Eq. 1. The new data,
+ and a scaling correction, change the fit radii to 289, 280,
+ 229, +/- 5 km."
+
+
+Values in the Version 0.2
+
+ The pole direction, prime meridian location, and rotation period
+ in the version 0.2 were set to the following values from [2]:
+
+ "5.3 Vesta Pole and Prime Meridian
+
+ The Vesta pole and prime meridian values are shown below.
+
+ RA Vesta = 305.8 +/- 3.1 deg Right Ascension in EME2000 [25]
+ DEC Vesta = 41.4 +/- 1.5 deg Declination in EME2000 [25]
+ W Vesta = 292 + w * D deg Prime Meridian
+ w Vesta = 1617.332776 deg/day Rotation rate
+
+
+ 5.4 Vesta Shape Parameters
+
+ The Vesta shape is described as a triaxial ellipsoid with
+ values 289, 280, 229 km [15] or as a sphere with a radius
+ of 265 km [16]. ...
+
+
+ 9 References
+
+ ...
+ 15. "Vesta: Spin Pole, Size, and Shape from HST Images", P.
+ Thomas, et al., Icarus, v128, p88~94 (1997)."
+ 16. "Impact Excavation on Asteroid 4 Vesta: Hubble Space
+ Telescope Result", P. C. Thomas, et al, Science, 227,
+ 1492-1494, 1997.
+ ...
+ 25. "Improved Measurement of Asteroid (4) Vesta's Rotational
+ Axis Orientation", Jian-Yang Li, et al., Icarus, 211,
+ 528-534, 2010.."
+
+
+Values in the Version 0.3
+
+ The pole direction, prime meridian location, rotation period and
+ radii in this version are set to the following values from [3]:
+
+ "...
+ The recommended new pole is:
+ - RA: 309.031 Dec: 42.235
+ - Error is estimated as +/-0.03deg 3-sigma
+
+ Data considered:
+ - Konopoliv (Gravity) 309.029 42.225
+ - Preusker (DLR) Survey 309.031 42.235
+ - OpNav 309.025 42.245
+ - NAV OD radio 309.025 42.247
+
+ The rotation rate of Vesta was determined to be .222588677 +/-
+ .000000009 days/rev, which agrees very well with the weighted
+ average of all previous determinations.
+ ...
+ A new prime meridian was chosen as defined by the small crater
+ Claudia that is assigned a longitude of 356 deg East. This new system
+ was chosen because the old system was not well-defined and the
+ team wanted to make a clear distinction between the old and new
+ to avoid confusion. The offset between the old W0 (292) from
+ Thomas et al. (1997) and the new W0 (76.06) is about 144.06 deg."
+
+ These values are provided in the keywords below. The W1 was derived
+ from .222588677 days/rev as follows:
+
+ W1 = 1 / 0.222588677 * 360 = 1617.3329428
+
+Values in the Version 0.4
+
+ The pole direction, rotation period, and radii in the version 0.4
+ are the same as in the version 0.3.
+
+ The W0 value is 75.39 deg (changed from 76.06 deg to match the
+ correct rotation rate while preserving the longitude of Claudia).
+
+Values in the Version 0.5
+
+ The pole direction, rotation period, and radii in the version 0.5
+ are the same as in the previous version 0.4.
+
+ The W0 value is 295.39 deg (changed from 75.39 deg) so that the
+ prime meridian is roughly in the center of the feature originally
+ identified as Olbers and the Claudia crater is now defined to be at
+ 136.0 deg East.
+
+ body2000004_pole_ra = ( 309.031 0.0 0.0 )
+ body2000004_pole_dec = ( 42.235 0.0 0.0 )
+ body2000004_pm = ( 295.39 1617.3329428 0.0 )
+
+
+Values in the Current Version 0.6
+
+ The pole direction, rotation period, and radii in the version 0.6
+ are the same as in the previous versions 0.4 and 0.5.
+
+ The W0 value is 285.39 deg (changed from 295.39 deg) to improve the
+ alignment of the prime meridian with the center of the albedo feature
+ originally identified as Olbers in the Hubble data, based on the
+ analysis of P. Thomas and J.-Y. Li in July/August 2012. The center
+ of Claudia crater is now defined to be at 146.0 deg East.
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 309.031 0.0 0.0 )
+ BODY2000004_POLE_DEC = ( 42.235 0.0 0.0 )
+ BODY2000004_PM = ( 285.39 1617.3329428 0.0 )
+
+ \begintext
+
+
+
+Radii for asteroid Vesta
+--------------------------------------------------------
+
+ The Vesta radii from [2] are provided in the keyword below.
+
+ \begindata
+
+ BODY2000004_RADII = ( 289.0 280.0 229.0 )
+
+ \begintext
+
+End of PCK file.
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti
new file mode 100755
index 0000000..47e9755
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti
@@ -0,0 +1,574 @@
+KPL/IK
+
+VIR Instrument kernel
+===========================================================================
+
+ This instrument kernel (I-kernel) contains Dawn VIR optics,
+ detector, and field-of-view parameters.
+
+
+Version and Date
+---------------------------------------------------------------------------
+
+ Version 0.5 -- March 2, 2011 -- Boris Semenov, NAIF
+
+ Rearranged comments and data blocks in the "FOV Definitions"
+ section to have all FOVs defined for full and partial scan mirror
+ sweeps described in a single comment block and defined in a
+ single data block to more clearly separate them from actual,
+ non-sweep FOV definitions.
+
+ NO CHANGES WERE MADE TO ANY KEYWORD VALUES.
+
+ Version 0.4 -- October 7, 2009 -- Dr. Federico Tosi, INAF - IFSI
+ Boris Semenov, NAIF
+
+ Changed the reference frame for the full and partial VIS sweep
+ FOVs associated with IDs -203212, -203215 ... -203219 to
+ DAWN_VIR_VIS_ZERO.
+
+ Changed the reference frame for the full IR sweep FOV associated
+ with IDs -203214 to DAWN_VIR_IR_ZERO.
+
+ Replaced -226 with -203 in the keywords in the ``Platform ID''
+ section.
+
+ Replaced cross-track/along-track with along-slit/cross-slit
+ in all comments.
+
+ Filled in instrument description.
+
+ Version 0.3 -- July 3, 2009 -- Boris Semenov
+
+ Extended comments to cover partial VIS scan FOVs added by Steve
+ Joy.
+
+ Version 0.2T2 -- June 23, 2009 -- Steven Joy
+
+ Added FOVs for VIR_VIS_96 (-203218) and VIR_VIS_32 (-203219)
+
+ Version 0.2T -- April 09, 2009 -- Steven Joy
+
+ Added FOVs for VIR_VIS_16 (-203217)
+
+ Version 0.2 -- June 24, 2008 -- Steven Joy, DSC with Boris Semenov, NAIF/JPL
+
+ Added FOVs for VIR_VIS_128 (-203215) and VIR_VIS_64 (-203216).
+
+ Version 0.1 -- May 9, 2005 -- Boris Semenov, NAIF/JPL
+
+ Added radiator FOV.
+
+ Version 0.0 -- October 12, 2004 -- Boris Semenov, NAIF/JPL
+
+ Initial release.
+
+
+References
+---------------------------------------------------------------------------
+
+ 1. ``Kernel Pool Required Reading''
+
+ 2. ``C-kernel Required Reading''
+
+ 3. VIR ICD/MICD, latest version as of 10/12/04
+
+ 4. Dawn Frames Definition Kernel (FK), latest version.
+
+ 5. VIR CDR Presentations
+
+ 6. Rosetta VIRTIS Documentation (ROS-EST-RS-30015/EID B and RO-VIR-UM-001)
+
+ 7. VIR Home Page http://www.ifsi-roma.inaf.it/vir/; accessed 10/07/09
+
+
+Implementation Notes
+--------------------------------------------------------
+
+ Applications that need SPICE I-kernel data must ``load'' the I-kernel
+ file, normally during program initialization.
+
+ Loading the kernel using the SPICELIB routine FURNSH causes the data
+ items and their associated values present in the kernel to become
+ associated with a data structure called the ``kernel pool''. The
+ application program may then obtain the value(s) for any IK data
+ item using the SPICELIB routines GDPOOL, GIPOOL, GCPOOL. Routine
+ GETFOV may be used if the file contains instrument field-of-view
+ (FOV) specification. See [1] for details.
+
+ This file was created with, and can be updated with a text editor or
+ word processor.
+
+
+Conventions for Specifying Data
+--------------------------------------------------------
+
+ Data items are specified using ``keyword=value'' assignments [1].
+ All keywords referencing values in this I-kernel start with the
+ characters `INS' followed by the NAIF Dawn instrument ID code,
+ constructed using the spacecraft ID number (-226) followed by the
+ NAIF three digit ID number for VIR module. These IDs are defined in
+ [4] as follows:
+
+ Instrument name ID
+ -------------------- -------
+ DAWN_VIR -203200
+ DAWN_VIR_SCAN -203201
+ DAWN_VIR_VIS -203211
+ DAWN_VIR_IR -203213
+
+ DAWN_VIR_VIS_SCAN -203212 (*)
+ DAWN_VIR_IR_SCAN -203214 (*)
+ DAWN_VIR_VIS_128 -203215 (*)
+ DAWN_VIR_VIS_64 -203216 (*)
+ DAWN_VIR_VIS_16 -203217 (*)
+ DAWN_VIR_VIS_96 -203218 (*)
+ DAWN_VIR_VIS_32 -203219 (*)
+
+ DAWN_VIR_RAD -203209
+
+ (*) _SCAN, _128, _64, _16, _96 and _32 names/IDs are defined to
+ allow specifying FOVs circumscribing full or partial side scans
+ of the VIR scan mirror. These frames are used only for planning
+ purposes and have nothing to do with the real angular aperture
+ (FOV) of the VIR instrument.
+
+ The remainder of the keyword is an underscore character followed by
+ the unique name of the data item. For example, the focal length of
+ the VIR VIS optics is specified by
+
+ INS-203211_FOCAL_LENGTH
+
+ The upper bound on the length of all keywords is 32 characters.
+
+ If a keyword is included in more than one file, or if the same
+ keyword appears more than once within a single file, the last
+ assignment supersedes any earlier assignments.
+
+
+Overview
+--------------------------------------------------------
+
+ From [7]:
+
+ What is VIR?
+
+ The Dawn mapping spectrometer VIR is a Visual and Infrared
+ Imaging Spectrometer that produces spectral images in the 0.25-1
+ mkm and 1-5 mkm ranges. VIR is a rebuild of the VIRTIS mapping
+ spectrometer on board the ESA Rosetta mission and it also derives
+ much design heritage from the Cassini VIMS spectrometer. The
+ design of the instrument fully accomplishes the mission's
+ scientific and measurement objectives with a simple
+ space-qualified low risk approach and high performance,
+ reliability, heritage and cost effectiveness.
+
+ Some technical details
+
+ VIR is a Visual and Infrared Imaging Spectrometer in a single
+ optical head. A Shafer telescope is mated to an Offner slit
+ spectrometer. Spectral images are formed on two matrix detectors
+ to cover the 0.25-1 mkm and 1-5 mkm ranges. The design uses a
+ dual arm optical and focal design with mapping ability to 5
+ mkm.The Dawn mapping spectrometer (VIR) is a rebuild of the
+ VIRTIS mapping spectrometer on board the ESA Rosetta mission with
+ an operational durations of 2y and flight time of 13y. The MS
+ spectrometer will only use the - M channel of VIRTIS, thus
+ allowing a great mass reduction. VIR also derives much of its
+ design from the Cassini VIMS spectrometer with an operational
+ lifetime of >4y and a mission life>10y.
+
+ VIR modules
+
+ The spectrometer consists of only three modules: the optical
+ system, 5.0 kg mass; the proximity electronics, 3.0 kg and 5 W;
+ the cryocooler including driving electronics, 1.3 kg and 12.6 W.
+ A mechanical and thermal mounting of 5.0 kg mass accommodates the
+ spectrometer subsystems. The optical system, which includes
+ foreoptics, dispersive elements, filters, focal plane assemblies
+ as well as the cryocooler and proximity electronics is a complete
+ re-build of the VIRTIS M instrument The data processing unit box
+ (DPU) is shared with the framing camera to save mass. The DPU
+ handles the data for both camera and spectrometer, compresses and
+ buffers them, and controls both the FCs and MS. Flight software
+ is based on Rosetta VIRTIS and ROLIS developments. The camera is
+ operated only when the spectrometer is not operating. As
+ VIRTIS-M, VIR does not use beam-splitters. Two different groove
+ densities are ruled on a single grating. The central part of the
+ grating (about 30% of the pupil) is ruled with a higher groove
+ density, which generate the higher spectral resolution needed in
+ the visible channel. The infrared channel utilizes the outer 70%
+ of the grating, which is ruled with a lower groove density. The
+ larger collecting area in the IR compensates for the lower solar
+ irradiance in this region. The visible detector array is based on
+ the Thomson-CSF type TH 7896 CCD detector. The IR detector used
+ in the MS is based on a bidimensional array of IR-sensitive
+ photovoltaic Mercury Cadmium Telluride coupled to silicon CMOS
+ multiplexer. This detector can operate at temperatures of the
+ order of 75 K. For this reason cryocoolers have to be used. The
+ calibration unit will make use of the cover, which -inside is
+ coated. It will diffuse the light coming from two internal
+ calibration lamps (one for the VISFPA and one for the IR-FPA),
+ calibrated at IAS.
+
+
+Mounting Alignment
+--------------------------------------------------------
+
+ Refer to the latest version of the Dawn Frames Definition Kernel
+ (FK) [4] for the VIR reference frame definitions and mounting
+ alignment information.
+
+
+Apparent FOV Layout
+--------------------------------------------------------
+
+ WARNING --- the description/diagram below have not been verified
+
+ This diagram illustrates the VIR apparent FOV layout for "zero"
+ scan mirror position in the corresponding reference frame.
+
+
+ ^ +Xvis
+ | +Xir
+ | |
+ | ~0.014 degrees |
+ | |
+ v Pixel 1 | Pixel 256
+ --- +---------|---------+
+ | 1 line | x-------------> +Yvis
+ --- +-------------------+ +Yir
+ ^ 256 pixels/line
+ |
+ | ~3.67 degrees |
+ |<----------------->|
+ | | Boresight (+Z axis)
+ is into the page
+
+
+ This diagram illustrates the VIR apparent FOV layout resulting from
+ a full, 256 step, +/- 1.83 degree scan mirror sweep about Y axis.
+ For partial scans of 16, 32, 64, 96, or 128 lines the cross-slit
+ FOV extent is proportionally decreased to 0.23, 0.46, 0.92, 1.38,
+ and 1.84 degrees correspondingly.
+
+
+ ^ +Xvis
+ | +Xir
+ | Pixel 1,1 |
+ --- *---------|---------+
+ ^ | | |
+ | ~3.67 | | |
+ | degrees | | |
+ | | | |
+ | 256 lines | x-------------> +Yvis
+ | (each for | | +Yir
+ | a step in | |
+ | scan seq.)| |
+ V | |
+ --- +-------------------+
+ | 256 pixels/line
+
+
+ | ~3.67 degrees |
+ |<----------------->|
+ | | Boresight (+Z axis)
+ is into the page
+
+
+Optical Parameters
+--------------------------------------------------------
+
+ The following VIR VIS and IR nominal first order optical parameters
+ are included in the data section below, from [6]:
+
+ -----------------------------------------------------------------
+ parameter VIR/VIS VIR/IR
+ -----------------------------------------------------------------
+ Focal Length, mm 152.0 152.0
+ f/ratio f/5.6 f/3.2
+ IFOV, rad/pixel
+ along-slit 0.00025 0.00025
+ cross-slit 0.00025 0.00025
+ Field of view (deg)
+ along-slit 3.6669 3.6669
+ cross-slit 0.0143 0.0143
+ Field of view (deg) - scan
+ along-slit 3.6669 3.6669
+ cross-slit 3.6669 3.6669
+ -----------------------------------------------------------------
+
+ The keywords below provide nominal values from the table above.
+ Angular size values in the keywords are given radians, with the
+ along-slit size being the first value and the cross-slit size
+ being the second value in each pair.
+
+ \begindata
+
+ INS-203211_FOCAL_LENGTH = ( 152.0 )
+ INS-203211_F/RATIO = ( 5.6 )
+ INS-203211_FOV_ANGULAR_SIZE = ( 0.064000, 0.000250 )
+ INS-203211_IFOV = ( 0.000250, 0.000250 )
+
+ INS-203213_FOCAL_LENGTH = ( 152.0 )
+ INS-203213_F/RATIO = ( 3.2 )
+ INS-203213_FOV_ANGULAR_SIZE = ( 0.064000, 0.000250 )
+ INS-203213_IFOV = ( 0.000250, 0.000250 )
+
+ \begintext
+
+
+Detector Parameters
+--------------------------------------------------------
+
+ The nominal VIR detector parameters from [6] are:
+
+ -----------------------------------------------------------------
+ parameter VIR/VIS VIR/IR
+ -----------------------------------------------------------------
+ Detector Array Size/Physical
+ along-slit 508 270
+ cross-slit 1024 436
+ Detector Array Size/Spatial
+ along-slit 256 (1) 256 (2)
+ cross-slit 1 1
+ Detector Array Center/Spatial
+ along-slit 127.5 127.5
+ cross-slit 0.5 0.5
+ Pixel Size, microns/Spatial
+ along-slit 38 (3) 38
+ cross-slit 38 38
+ -----------------------------------------------------------------
+
+ (1) VIS CCD pixels are 2x2 binned at detector level
+
+ (2) assuming IR reads out the same number of pixels as VIS
+
+ (3) size of a 2x2 binned pixel
+
+ The values are given in microns for PIXEL_SIZE keywords and in counts
+ for PIXEL_SAMPLES, PIXEL_LINES, and CENTER keywords.
+
+ \begindata
+
+ INS-203211_PIXEL_SIZE = ( 38, 38 )
+ INS-203211_PIXEL_SAMPLES = ( 256 )
+ INS-203211_PIXEL_LINES = ( 1 )
+ INS-203211_CCD_CENTER = ( 127.5, 0.5 )
+
+ INS-203213_PIXEL_SIZE = ( 38, 38 )
+ INS-203213_PIXEL_SAMPLES = ( 256 )
+ INS-203213_PIXEL_LINES = ( 1 )
+ INS-203213_CCD_CENTER = ( 127.5, 0.5 )
+
+ \begintext
+
+
+FOV Definitions
+---------------------------------------------------------------------------
+
+ This section contains definitions for the VIR FOVs. These
+ definitions are provided in a format required by the SPICE (CSPICE)
+ function GETFOV (getfov_c).
+
+ The set of assignments in the data section below defines the VIR VIS
+ and IR actual slit FOVs with respect to the corresponding moving
+ frames to be a rectangles with the corners defined by the first and
+ last pixels of the spatial line along +Y and the boresight along the
+ +Z axis. These FOV definitions use angular extent style
+ specification with the cross and along track angular sizes taken
+ from the ``Optics Parameters'' section above.
+
+ \begindata
+
+ INS-203211_FOV_FRAME = 'DAWN_VIR_VIS'
+ INS-203211_FOV_SHAPE = 'RECTANGLE'
+ INS-203211_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203211_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203211_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203211_FOV_REF_ANGLE = ( 0.00716197 )
+ INS-203211_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203211_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203213_FOV_FRAME = 'DAWN_VIR_IR'
+ INS-203213_FOV_SHAPE = 'RECTANGLE'
+ INS-203213_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203213_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203213_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203213_FOV_REF_ANGLE = ( 0.00716197 )
+ INS-203213_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203213_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
+
+ The set of assignments in the data section below defines the VIR VIS
+ apparent FOVs resulting from a full, 256-step and partial 128-, 64-,
+ 16-, 96-, and 32- step scan mirror sweeps about Y axis with respect
+ to the non-moving frame 'DAWN_VIR_VIS_ZERO' to be a rectangles with the
+ corners defined by the first and last pixels of the spatial line in
+ the first and last scan positions and the boresight along the +Z
+ axis. These FOV definitions use angular extent style specification
+ with the angular sizes taken from the ``Optics Parameters'' section
+ above.
+
+ Note that FOVs defined below are used only for planning purposes and
+ have nothing to do with the real angular aperture (FOV) of the VIR
+ instrument; therefore they should not be used to reproduce the geometry
+ of real VIR acquisitions.
+
+ \begindata
+
+ INS-203212_FOV_FRAME = 'DAWN_VIR_VIS_ZERO'
+ INS-203212_FOV_SHAPE = 'RECTANGLE'
+ INS-203212_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203212_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203212_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203212_FOV_REF_ANGLE = ( 1.83346494 )
+ INS-203212_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203212_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203214_FOV_FRAME = 'DAWN_VIR_IR_ZERO'
+ INS-203214_FOV_SHAPE = 'RECTANGLE'
+ INS-203214_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203214_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203214_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203214_FOV_REF_ANGLE = ( 1.83346494 )
+ INS-203214_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203214_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203215_FOV_FRAME = 'DAWN_VIR_VIS_ZERO'
+ INS-203215_FOV_SHAPE = 'RECTANGLE'
+ INS-203215_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203215_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203215_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203215_FOV_REF_ANGLE = ( 0.91673247 )
+ INS-203215_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203215_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203216_FOV_FRAME = 'DAWN_VIR_VIS_ZERO'
+ INS-203216_FOV_SHAPE = 'RECTANGLE'
+ INS-203216_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203216_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203216_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203216_FOV_REF_ANGLE = ( 0.45836624 )
+ INS-203216_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203216_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203217_FOV_FRAME = 'DAWN_VIR_VIS_ZERO'
+ INS-203217_FOV_SHAPE = 'RECTANGLE'
+ INS-203217_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203217_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203217_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203217_FOV_REF_ANGLE = ( 0.11459156 )
+ INS-203217_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203217_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203218_FOV_FRAME = 'DAWN_VIR_VIS_ZERO'
+ INS-203218_FOV_SHAPE = 'RECTANGLE'
+ INS-203218_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203218_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203218_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203218_FOV_REF_ANGLE = ( 0.68754935 )
+ INS-203218_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203218_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ INS-203219_FOV_FRAME = 'DAWN_VIR_VIS_ZERO'
+ INS-203219_FOV_SHAPE = 'RECTANGLE'
+ INS-203219_BORESIGHT = (
+ 0.000000 0.000000 152.000000
+ )
+ INS-203219_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203219_FOV_REF_VECTOR = (
+ 1.000000 0.000000 0.000000
+ )
+ INS-203219_FOV_REF_ANGLE = ( 0.22918312 )
+ INS-203219_FOV_CROSS_ANGLE = ( 1.83346494 )
+ INS-203219_FOV_ANGLE_UNITS = 'DEGREES'
+
+
+ \begintext
+
+
+Radiator Sun Avoidance FOV Definition
+--------------------------------------------------------
+
+ Sun avoidance for VIR radiator is 175 degree cone centered on
+ spacecraft -X axis [3].
+
+ \begindata
+
+ INS-203209_FOV_FRAME = 'DAWN_SPACECRAFT'
+ INS-203209_FOV_SHAPE = 'CIRCLE'
+ INS-203209_BORESIGHT = (
+ -1.000000 0.000000 0.000000
+ )
+ INS-203209_FOV_CLASS_SPEC = 'ANGLES'
+ INS-203209_FOV_REF_VECTOR = (
+ 0.000000 1.000000 0.000000
+ )
+ INS-203209_FOV_REF_ANGLE = ( 87.5 )
+ INS-203209_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Optical Distortion
+--------------------------------------------------------
+
+ [TBD]
+
+
+Platform ID
+---------------------------------------------------------------------------
+
+ This number is the NAIF instrument ID of the platform on which the
+ instrument mounted. All VIR components it is the spacecraft.
+
+ \begindata
+
+ INS-203200_PLATFORM_ID = ( -203000 )
+ INS-203211_PLATFORM_ID = ( -203000 )
+ INS-203213_PLATFORM_ID = ( -203000 )
+
+ \begintext
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc
new file mode 100644
index 0000000..ed21972
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'DAWN VIR ZERO OFFSET CK '
+BEGIN_ARRAY 1 10
+'DAWN VIR ZERO OFFSET CK '
+'159E1065C3^A'
+'159E194B8A^A'
+'-319C1'
+'-319C0'
+'2'
+'1'
+10
+'1^1'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'10000000001F14^-1'
+'159E1065C3^A'
+'159E194B8A^A'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti
new file mode 100755
index 0000000..e48d829
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti
@@ -0,0 +1,22 @@
+\begindata
+
+ INS-203211_PIXEL_PITCH = 0.038
+ INS-203211_BORESIGHT_SAMPLE = 127.5
+ INS-203211_BORESIGHT_LINE = 0.5
+
+ INS-203211_TRANSX = (0.0, 0.0, 0.038)
+ INS-203211_TRANSY = (0.0, 0.038, 0.0)
+ INS-203211_ITRANSS = (0.0, 0.0, 26.315789473684)
+ INS-203211_ITRANSL = (0.0, 26.315789473684, 0.0)
+
+ INS-203213_PIXEL_PITCH = 0.038
+ INS-203213_BORESIGHT_SAMPLE = 127.5
+ INS-203213_BORESIGHT_LINE = 0.5
+
+ INS-203213_TRANSX = (0.0, 0.0, 0.038)
+ INS-203213_TRANSY = (0.0, 0.038, 0.0)
+ INS-203213_ITRANSS = (0.0, 0.0, 26.315789473684)
+ INS-203213_ITRANSL = (0.0, 26.315789473684, 0.0)
+
+\begintext
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls b/tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls
new file mode 100755
index 0000000..e1afdee
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/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/VIR_IR_1A_1_362681634_1/pck00009.tpc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc
new file mode 100755
index 0000000..bfadaab
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+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/IAG
+ 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
+
+
+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 and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+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, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG 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]) 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. 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 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. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which 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
+ J2000 epoch 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].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value 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 only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ 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
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] 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."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] 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.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [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.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- 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
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+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 = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ 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 2006 IAU/IAG 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 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 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, 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: 2006 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 = ( 284.95 870.5366420 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 term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ 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 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ 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 = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers 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
+
+
+ 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
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body10_pole_ra = ( 286.13 0. 0. )
+ body10_pole_dec = ( 63.87 0. 0. )
+ body10_pm = ( 84.10 14.18440 0. )
+ body10_long_axis = ( 0. )
+
+ 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 unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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:
+
+ Old 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 )
+
+
+ Current values:
+
+ 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
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 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:
+
+ Values are from the 2003 IAU report.
+
+
+ body599_pole_ra = ( 268.05 -0.009 0. )
+ body599_pole_dec = ( 64.49 0.003 0. )
+ body599_pm = ( 284.95 870.5366420 0. )
+ body599_long_axis = ( 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
+ 352.35 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4 )
+
+
+
+ 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 = ( 284.95 870.5366420 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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 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.
+
+
+ \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
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 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 )
+
+
+ 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 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. )
+
+ \begintext
+
+
+
+ Titan
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ 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 2006 IAU report.
+
+ Current values:
+
+ \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. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+Itokawa
+
+
+ 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
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values 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 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ 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 )
+
+ \begintext
+
+ 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.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ 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) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ 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 )
+
+
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+ 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.
+
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 IAU report.
+
+ Current values:
+
+ The 2000 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 2000
+ 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 from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \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 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/isds/dawnvir_isd.json b/tests/pytests/data/isds/dawnvir_isd.json
new file mode 100644
index 0000000..90674bb
--- /dev/null
+++ b/tests/pytests/data/isds/dawnvir_isd.json
@@ -0,0 +1,1972 @@
+{
+ "isis_camera_version": 1,
+ "image_lines": 60,
+ "image_samples": 256,
+ "name_platform": "DAWN",
+ "name_sensor": "VIR",
+ "reference_height": {
+ "maxheight": 1000,
+ "minheight": -1000,
+ "unit": "m"
+ },
+ "name_model": "USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL",
+ "interpolation_method": "lagrange",
+ "line_scan_rate": [
+ [
+ 0.5,
+ -480.24997586011887,
+ 16
+ ],
+ [
+ 1.5,
+ -464.24997663497925,
+ 16
+ ],
+ [
+ 2.5,
+ -448.2499774694443,
+ 16
+ ],
+ [
+ 3.5,
+ -432.24997824430466,
+ 16
+ ],
+ [
+ 4.5,
+ -416.2499790787697,
+ 16
+ ],
+ [
+ 5.5,
+ -400.24997985363007,
+ 16
+ ],
+ [
+ 6.5,
+ -384.2499806880951,
+ 16
+ ],
+ [
+ 7.5,
+ -368.2499814629555,
+ 16
+ ],
+ [
+ 8.5,
+ -352.24998223781586,
+ 16
+ ],
+ [
+ 9.5,
+ -336.2499830722809,
+ 16
+ ],
+ [
+ 10.5,
+ -320.24998384714127,
+ 16
+ ],
+ [
+ 11.5,
+ -304.24998474121094,
+ 16
+ ],
+ [
+ 12.5,
+ -288.2499855160713,
+ 16
+ ],
+ [
+ 13.5,
+ -272.24998635053635,
+ 16
+ ],
+ [
+ 14.5,
+ -256.24998712539673,
+ 16
+ ],
+ [
+ 15.5,
+ -240.2499879002571,
+ 16
+ ],
+ [
+ 16.5,
+ -224.24998873472214,
+ 16
+ ],
+ [
+ 17.5,
+ -208.24998950958252,
+ 16
+ ],
+ [
+ 18.5,
+ -192.24999034404755,
+ 16
+ ],
+ [
+ 19.5,
+ -176.24999111890793,
+ 16
+ ],
+ [
+ 20.5,
+ -160.24999195337296,
+ 16
+ ],
+ [
+ 21.5,
+ -144.24999272823334,
+ 16
+ ],
+ [
+ 22.5,
+ -128.249993622303,
+ 16
+ ],
+ [
+ 23.5,
+ -112.24999439716339,
+ 16
+ ],
+ [
+ 24.5,
+ -96.24999517202377,
+ 16
+ ],
+ [
+ 25.5,
+ -80.2499960064888,
+ 16
+ ],
+ [
+ 26.5,
+ -64.24999678134918,
+ 16
+ ],
+ [
+ 27.5,
+ -48.24999761581421,
+ 16
+ ],
+ [
+ 28.5,
+ -32.24999839067459,
+ 16
+ ],
+ [
+ 29.5,
+ -16.249999225139618,
+ 16
+ ],
+ [
+ 30.5,
+ -0.25,
+ 16
+ ],
+ [
+ 31.5,
+ 15.749999225139618,
+ 16
+ ],
+ [
+ 32.5,
+ 31.74999839067459,
+ 16
+ ],
+ [
+ 33.5,
+ 47.74999761581421,
+ 16
+ ],
+ [
+ 34.5,
+ 63.74999672174454,
+ 16
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+ [
+ -0.015370155827196868,
+ -0.096791951925612,
+ -0.028460680579772087
+ ],
+ [
+ -0.015370157726607431,
+ -0.09679197294450023,
+ -0.02846068053045201
+ ],
+ [
+ -0.015370159626345413,
+ -0.09679199396435798,
+ -0.02846068048077359
+ ],
+ [
+ -0.01537016152336946,
+ -0.09679201498495695,
+ -0.028460680432774096
+ ],
+ [
+ -0.015370163420349855,
+ -0.09679203600650545,
+ -0.028460680384681837
+ ],
+ [
+ -0.015370165317730425,
+ -0.09679205702890976,
+ -0.028460680336174847
+ ],
+ [
+ -0.015370167215100082,
+ -0.09679207805227452,
+ -0.028460680287582363
+ ],
+ [
+ -0.015370169111691211,
+ -0.09679209907644963,
+ -0.028460680239357317
+ ],
+ [
+ -0.015370171007045429,
+ -0.09679212010152241,
+ -0.02846068019181439
+ ],
+ [
+ -0.01537017290283984,
+ -0.09679214112745922,
+ -0.028460680143871285
+ ],
+ [
+ -0.015370174798215884,
+ -0.09679216215427731,
+ -0.02846068009606279
+ ],
+ [
+ -0.01537017669357374,
+ -0.09679218318204402,
+ -0.028460680048152425
+ ],
+ [
+ -0.015370178588134878,
+ -0.09679220421062655,
+ -0.02846068000062769
+ ],
+ [
+ -0.015370180481502757,
+ -0.09679222524011494,
+ -0.028460679953785074
+ ],
+ [
+ -0.01537018237409211,
+ -0.09679224627042277,
+ -0.028460679907317172
+ ],
+ [
+ -0.01537018426902796,
+ -0.09679226730176742,
+ -0.028460679859177617
+ ],
+ [
+ -0.015370186159620061,
+ -0.09679228833379602,
+ -0.02846067981377564
+ ]
+ ],
+ "reference_frame": 1
+ },
+ "sun_position": {
+ "spk_table_start_time": 362681633.6134121,
+ "spk_table_end_time": 362682578.1133645,
+ "spk_table_original_size": 2,
+ "ephemeris_times": [
+ 362681633.6134121,
+ 362682578.1133645
+ ],
+ "positions": [
+ [
+ -172941319.79632777,
+ 253566864.2505451,
+ 123598648.3648744
+ ],
+ [
+ -172958379.36543128,
+ 253557526.00676197,
+ 123597159.24349931
+ ]
+ ],
+ "velocities": [
+ [
+ -18.06231086334586,
+ -9.886532426983118,
+ -1.5764102324061096
+ ],
+ [
+ -18.061712341666222,
+ -9.88740987084806,
+ -1.5768379395399243
+ ]
+ ],
+ "reference_frame": 1
+ }
+}
\ No newline at end of file
diff --git a/tests/pytests/test_dawn_drivers.py b/tests/pytests/test_dawn_drivers.py
index 62f2e8b..d311d6f 100644
--- a/tests/pytests/test_dawn_drivers.py
+++ b/tests/pytests/test_dawn_drivers.py
@@ -6,16 +6,44 @@ from importlib import reload
import json
import unittest
+from unittest import mock
from unittest.mock import patch
from ale.drivers import AleJsonEncoder
from conftest import get_image_label, get_image_kernels, get_isd, convert_kernels, compare_dicts
import ale
-from ale.drivers.dawn_drivers import DawnFcPds3NaifSpiceDriver, DawnFcIsisLabelNaifSpiceDriver
+from ale.drivers.dawn_drivers import DawnFcPds3NaifSpiceDriver, DawnFcIsisLabelNaifSpiceDriver, DawnVirIsisLabelNaifSpiceDriver
+housekeeping_dict = {'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09', '362681682.09', '362681698.09', '362681714.09',
+ '362681730.09', '362681746.09', '362681762.09', '362681778.09', '362681794.09', '362681810.09',
+ '362681826.09', '362681842.09', '362681858.09', '362681874.09', '362681890.09', '362681906.09',
+ '362681922.09', '362681938.09', '362681954.09', '362681970.09', '362681986.09', '362682002.09',
+ '362682018.09', '362682034.09', '362682050.09', '362682066.09', '362682082.09', '362682098.09',
+ '362682114.09', '362682130.09', '362682146.09', '362682162.09', '362682178.09', '362682194.09',
+ '362682210.09', '362682226.09', '362682242.09', '362682258.09', '362682274.09', '362682290.09',
+ '362682306.09', '362682322.09', '362682338.09', '362682354.09', '362682370.09', '362682386.09',
+ '362682402.09', '362682418.09', '362682434.09', '362682450.09', '362682466.09', '362682482.09',
+ '362682498.09', '362682514.09', '362682530.09', '362682546.09', '362682562.09', '362682578.09'],
+ 'ShutterStatus': ['closed', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open',
+ 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open',
+ 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open',
+ 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open',
+ 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'closed'],
+ 'MirrorSin': [0.066178, -0.037118, -0.037118, -0.032479, -0.028083, -0.023443, -0.019048, -0.014652, -0.010012, -0.005617,
+ -0.000977, 0.003175, 0.007814, 0.01221, 0.016606, 0.021245, 0.025641, 0.030281, 0.034676, 0.039072, 0.043712,
+ 0.048107, 0.052747, 0.057143, 0.061538, 0.066178, 0.070574, 0.075214, 0.079609, 0.084005, 0.088645, 0.09304,
+ 0.097436, 0.102076, 0.106471, 0.110867, 0.115507, 0.119902, 0.124298, 0.128938, 0.133333, 0.137729, 0.142124,
+ 0.146764, 0.15116, 0.155555, 0.159951, 0.164347, 0.168986, 0.173382, 0.177778, 0.182173, 0.186569, 0.190964,
+ 0.19536, 0.199756, 0.204151, 0.208547, 0.212942, 0.217338],
+ 'MirrorCos': [0.997557, 0.999266, 0.999266, 0.999266, 0.999511, 0.999511, 0.999755, 0.999755, 0.999755, 0.999755, 0.999755,
+ 0.999755, 0.999755, 0.999755, 0.999755, 0.999755, 0.999511, 0.999511, 0.999266, 0.999022, 0.999022, 0.998778,
+ 0.998534, 0.99829, 0.998045, 0.997557, 0.997313, 0.997069, 0.99658, 0.996336, 0.995848, 0.995603, 0.995115,
+ 0.994627, 0.994138, 0.99365, 0.993161, 0.992673, 0.992185, 0.991452, 0.990964, 0.990231, 0.989743, 0.98901,
+ 0.988277, 0.987789, 0.987056, 0.986324, 0.985591, 0.984614, 0.983882, 0.983149, 0.982172, 0.98144, 0.980463,
+ 0.97973, 0.978754, 0.977777, 0.9768, 0.975823]}
@pytest.fixture(scope="module", autouse=True)
-def test_kernels():
+def fc_kernels():
kernels = get_image_kernels('FC21A0038582_15170161546F6F')
updated_kernels, binary_kernels = convert_kernels(kernels)
yield updated_kernels
@@ -23,7 +51,7 @@ def test_kernels():
os.remove(kern)
@pytest.mark.parametrize("label_type", ['pds3', 'isis3'])
-def test_load(test_kernels, label_type):
+def test_fc_load(fc_kernels, label_type):
if label_type == 'isis3':
label_prefix_file = "FC21A0038582_15170161546F6G"
compare_dict = get_isd("dawnfc_isis")
@@ -33,13 +61,33 @@ def test_load(test_kernels, label_type):
label_file = get_image_label(label_prefix_file, label_type=label_type)
- isd_str = ale.loads(label_file, props={'kernels': test_kernels})
+ isd_str = ale.loads(label_file, props={'kernels': fc_kernels})
isd_obj = json.loads(isd_str)
# print(json.dumps(isd_obj, indent=2))
assert compare_dicts(isd_obj, compare_dict) == []
-# ========= Test pds3label and naifspice driver =========
-class test_pds3_naif(unittest.TestCase):
+@pytest.fixture(scope="module", autouse=True)
+def vir_kernels():
+ kernels = get_image_kernels('VIR_IR_1A_1_362681634_1')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+def test_vir_load(vir_kernels):
+ label_file = get_image_label("VIR_IR_1A_1_362681634_1", label_type="isis3")
+ with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+ patch('ale.drivers.dawn_drivers.parse_table', return_value=housekeeping_dict) as parse_table:
+
+ compare_dict = get_isd("dawnvir")
+
+ isd_str = ale.loads(label_file, props={"kernels": vir_kernels, "nadir": False}, verbose=False)
+ isd_obj = json.loads(isd_str)
+ x = compare_dicts(isd_obj, compare_dict)
+ assert x == []
+
+# ========= Test dawn fc pds3label and naifspice driver =========
+class test_dawn_fc_pds3_naif(unittest.TestCase):
def setUp(self):
label = get_image_label("FC21A0038582_15170161546F6F", "pds3")
@@ -101,12 +149,12 @@ class test_pds3_naif(unittest.TestCase):
bods2c.assert_called_with('DAWN_FC2_FILTER_6')
gdpool.assert_called_with('INS54321_CCD_CENTER', 0, 2)
-# ========= Test isis3label and naifspice driver =========
-class test_isis3_naif(unittest.TestCase):
+# ========= Test dawn fc isis3label and naifspice driver =========
+class test_dawn_fc_isis3_naif(unittest.TestCase):
def setUp(self):
label = get_image_label("FC21A0038582_15170161546F6G", "isis3");
- self.driver = DawnFcIsisLabelNaifSpiceDriver(label);
+ self.driver = DawnFcIsisLabelNaifSpiceDriver(label)
def test_short_mission_name(self):
assert self.driver.short_mission_name == 'dawn'
@@ -125,3 +173,89 @@ class test_isis3_naif(unittest.TestCase):
assert self.driver.ephemeris_start_time == 12345.193
scs2e.assert_called_with(-203, '488002612:246')
+
+# ========= Test dawn vir isis3label and naifspice driver =========
+class test_dawn_vir_isis3_naif(unittest.TestCase):
+ def setUp(self):
+ label = get_image_label("VIR_IR_1A_1_362681634_1", "isis3")
+ self.driver = DawnVirIsisLabelNaifSpiceDriver(label)
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "Visual and Infrared Spectrometer"
+
+ def test_sensor_name(self):
+ assert self.driver.sensor_name == "VIR"
+
+ def test_line_exposure_duration(self):
+ np.testing.assert_array_equal(self.driver.line_exposure_duration, [0.5])
+
+ def test_focal_length(self):
+ with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=[152.0]) as gdpool:
+ assert self.driver.focal_length == 152.0
+
+ def test_ikid(self):
+ assert self.driver.ikid == -203213
+
+ def test_sensor_frame_id(self):
+ ale.spice_root = "/foo/bar"
+ assert self.driver.sensor_frame_id == -203223
+
+ def test_line_scan_rate(self):
+ with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+ patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362681649.6134113) as scs2e, \
+ patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+ 'ShutterStatus': ['closed', 'open', 'open'], \
+ 'MirrorSin': [0.066178, -0.037118, -0.037118], \
+ 'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+ assert self.driver.line_scan_rate == ([0.5, 1.5, 2.5, 3.5], [-0.25, -0.25, -0.25, 15.75], [16, 16, 16, 16])
+
+ def test_sensor_model_version(self):
+ assert self.driver.sensor_model_version == 1
+
+ def test_optical_angles(self):
+ with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+ patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+ 'ShutterStatus': ['closed', 'open', 'open'], \
+ 'MirrorSin': [0.066178, -0.037118, -0.037118], \
+ 'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+ assert self.driver.optical_angles == [-0.005747392247876606, -0.005747392247876606, -0.005747392247876606]
+
+ def test_hk_ephemeris_time(self):
+ with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+ patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362681633.8634121) as scs2e, \
+ patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+ 'ShutterStatus': ['closed', 'open', 'open'], \
+ 'MirrorSin': [0.066178, -0.037118, -0.037118], \
+ 'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+ assert self.driver.hk_ephemeris_time == [362681633.8634121, 362681633.8634121, 362681633.8634121]
+
+ def test_ephemeris_start_time(self):
+ with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+ patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362681633.8634121) as scs2e, \
+ patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+ 'ShutterStatus': ['closed', 'open', 'open'], \
+ 'MirrorSin': [0.066178, -0.037118, -0.037118], \
+ 'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+ assert self.driver.ephemeris_start_time == 362681633.8634121 - (0.5 / 2)
+
+ def test_ephemeris_stop_time(self):
+ with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+ patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362682578.1133645) as scs2e, \
+ patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+ 'ShutterStatus': ['closed', 'open', 'open'], \
+ 'MirrorSin': [0.066178, -0.037118, -0.037118], \
+ 'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+ assert self.driver.ephemeris_stop_time == 362682578.1133645 + (0.5 / 2)
+
+ def test_is_calibrated(self):
+ assert self.driver.is_calibrated == False
+
+ def test_has_articulation_kernel(self):
+ ale.spice_root = "/foo/bar"
+ assert self.driver.has_articulation_kernel == False
+
--
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