diff --git a/ale/drivers/hayabusa_drivers.py b/ale/drivers/hayabusa_drivers.py new file mode 100644 index 0000000000000000000000000000000000000000..c4a261420d03d3002d97faee46ed2149e11627c6 --- /dev/null +++ b/ale/drivers/hayabusa_drivers.py @@ -0,0 +1,44 @@ +from ale.base.data_naif import NaifSpice +from ale.base.label_isis import IsisLabel +from ale.base.type_sensor import Framer +from ale.base.type_distortion import RadialDistortion, NoDistortion +from ale.base.base import Driver + +class HayabusaAmicaIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, RadialDistortion, Driver): + + @property + def instrument_id(self): + """ + Returns the ID of the instrument + + Returns + ------- + : str + Name of the instrument + """ + lookup_table = {'AMICA': 'HAYABUSA_AMICA'} + return lookup_table[super().instrument_id] + + @property + def sensor_model_version(self): + """ + The ISIS Sensor model number for HiRise in ISIS. This is likely just 1 + + Returns + ------- + : int + ISIS sensor model version + """ + return 1 + + @property + def sensor_name(self): + """ + Returns the name of the instrument + + Returns + ------- + : str + Name of the sensor + """ + return self.instrument_id \ No newline at end of file diff --git a/ale/transformation.py b/ale/transformation.py index aee0784069ef9037078208882d9b43022fe04d86..84ef0c415212f9a2dfc5d6f884a2b1e41b96d147 100644 --- a/ale/transformation.py +++ b/ale/transformation.py @@ -104,7 +104,7 @@ class FrameChain(nx.DiGraph): if len(target_times) > 1: target_times = np.asarray([ephemeris_times[0], ephemeris_times[-1]]) - if exact_ck_times and not nadir: + if exact_ck_times and len(ephemeris_times) > 1 and not nadir: try: sensor_times = cls.extract_exact_ck_times(ephemeris_times[0], ephemeris_times[-1], sensor_frame) except Exception as e: diff --git a/ale/util.py b/ale/util.py index c3458034848fee1e495b6f721cde9735651fbdb8..35ce235caed5a9a9d1dc3f667b31fcf453eb05d5 100644 --- a/ale/util.py +++ b/ale/util.py @@ -284,7 +284,9 @@ def get_kernels_from_isis_pvl(kernel_group, expand=True, format_as="list"): kernels = [expandvars(expandvars(k, isisprefs['DataDirectory'], case_sensitive=False)) for k in kernels] # Ensure that the ISIS Addendum kernel is last in case it overrides # some values from the default Instrument kernel + # Sorts planetary constants kernel first so it can be overridden by more specific kernels kernels = sorted(kernels, key=lambda x: "Addendum" in x) + kernels = sorted(kernels, key=lambda x: "pck00" in x, reverse=True) return kernels elif (format_as == 'dict'): # return created dict diff --git a/tests/pytests/conftest.py b/tests/pytests/conftest.py index 0430a83fad95c7360c0d64d5a914d60826b5d860..b68997925566a8d67614523acf3fadc0bfc92175 100644 --- a/tests/pytests/conftest.py +++ b/tests/pytests/conftest.py @@ -213,4 +213,12 @@ def convert_kernels(kernels): except: warnings.warn(f"Unable to convert {path} to binary kernel") updated_kernels.append(kernel) + + # Sort Kernels + # Ensure that the ISIS Addendum kernel is last in case it overrides + # some values from the default Instrument kernel + # Sorts planetary constants kernel first so it can be overridden by more specific kernels + updated_kernels = sorted(updated_kernels, key=lambda x: "Addendum" in x) + updated_kernels = sorted(updated_kernels, key=lambda x: "pck00" in x, reverse=True) + return updated_kernels, binary_kernels diff --git a/tests/pytests/data/isds/hayabusaamica_isd.json b/tests/pytests/data/isds/hayabusaamica_isd.json new file mode 100644 index 0000000000000000000000000000000000000000..4f4812aa78bbf30f5aeeee7c5ddf33036d92f6c9 --- /dev/null +++ b/tests/pytests/data/isds/hayabusaamica_isd.json @@ -0,0 +1,278 @@ +{ + "isis_camera_version": 1, + "image_lines": 1024, + "image_samples": 1024, + "name_platform": "HAYABUSA", + "name_sensor": "HAYABUSA_AMICA", + "reference_height": { + "maxheight": 1000, + "minheight": -1000, + "unit": "m" + }, + "name_model": "USGS_ASTRO_FRAME_SENSOR_MODEL", + "center_ephemeris_time": 182502855.87767982, + "radii": { + "semimajor": 0.274, + "semiminor": 0.138, + "unit": "km" + }, + "body_rotation": { + "time_dependent_frames": [ + 2025143, + 1 + ], + "ck_table_start_time": 182502855.87767982, + "ck_table_end_time": 182502855.87767982, + "ck_table_original_size": 1, + "ephemeris_times": [ + 182502855.87767982 + ], + "quaternions": [ + [ + -0.08077042629450831, + -0.3978802006010579, + 0.8955645826414776, + 0.1820207749792905 + ] + ], + "angular_velocities": [ + [ + -2.512589340256263e-08, + 5.61469404198439e-05, + -0.00013244767067246732 + ] + ], + "reference_frame": 1 + }, + "instrument_pointing": { + "time_dependent_frames": [ + -130000, + 1 + ], + "ck_table_start_time": 182502855.87767982, + "ck_table_end_time": 182502855.87767982, + "ck_table_original_size": 1, + "ephemeris_times": [ + 182502855.87767982 + ], + "quaternions": [ + [ + -0.35631878528559185, + 0.6008590807630156, + 0.37126158431750983, + 0.6116944697537136 + ] + ], + "angular_velocities": [ + [ + -3.8262173581753043e-07, + -7.423354754135573e-06, + -4.099140843147822e-05 + ] + ], + "reference_frame": 1, + "constant_frames": [ + -130102, + -130101, + -130000 + ], + "constant_rotation": [ + 0.006635481026673982, + 0.9999756648566065, + 0.002154085915888306, + 0.9999768321090574, + -0.006632187003876368, + -0.0015327559101681021, + -0.0015184323097166528, + 0.002164206583021168, + -0.9999965052804872 + ] + }, + "naif_keywords": { + "BODY2025143_RADII": [ + 0.274, + 0.156, + 0.138 + ], + "BODY_FRAME_CODE": 2025143, + "BODY_CODE": 2025143, + "TKFRAME_-130102_AXES": [ + 1.0, + 2.0, + 3.0 + ], + "TKFRAME_-130102_SPEC": "ANGLES", + "TKFRAME_-130102_RELATIVE": "HAYABUSA_AMICA_IDEAL", + "INS-130102_FOCAL_LENGTH": 0.1208, + "FRAME_-130102_NAME": "HAYABUSA_AMICA", + "FRAME_-130102_CLASS_ID": -130102.0, + "INS-130102_PIXEL_LINES": 1024.0, + "INS-130102_CENTER": [ + 511.5, + 511.5 + ], + "INS-130102_LT_SURFACE_CORRECT": "FALSE", + "INS-130102_F_NUMBER": 8.0, + "INS-130102_PIXEL_SIZE": 1.2e-05, + "INS-130102_SWAP_OBSERVER_TARGET": "TRUE", + "INS-130102_PIXEL_SAMPLES": 1024.0, + "FRAME_-130102_CLASS": 4.0, + "INS-130102_ITRANSL": [ + 0.0, + 0.0, + -83.33333333 + ], + "INS-130102_LIGHTTIME_CORRECTION": "NONE", + "INS-130102_FOV_BOUNDARY_CORNERS": [ + 0.006144, + 0.006144, + 0.1204711614, + -0.006144, + 0.006144, + 0.1204711614, + -0.006144, + -0.006144, + 0.1204711614, + 0.006144 + ], + "INS-130102_ITRANSS": [ + 0.0, + 83.33333333, + 0.0 + ], + "INS-130102_BORESIGHT": [ + 0.0, + 0.0, + 1.0 + ], + "INS-130102_UPVECTOR": [ + 0.0, + -1.0, + 0.0 + ], + "INS-130102_BORESIGHT_LINE": 511.5, + "INS-130102_BORESIGHT_SAMPLE": 511.5, + "TKFRAME_-130102_UNITS": "DEGREES", + "INS-130102_PIXEL_PITCH": 0.012, + "INS-130102_FOV_SHAPE": "POLYGON", + "INS-130102_TRANSX": [ + 0.0, + 0.012, + 0.0 + ], + "INS-130102_TRANSY": [ + 0.0, + 0.0, + -0.012 + ], + "INS-130102_OD_K": [ + 0.0, + 2.8e-05, + 0.0 + ], + "INS-130102_FOV_FRAME": "HAYABUSA_AMICA", + "TKFRAME_-130102_ANGLES": [ + -0.087, + -0.124, + -0.38 + ], + "FRAME_-130102_CENTER": -130.0, + "OBJECT_2025143_FRAME": "ITOKAWA_FIXED", + "FRAME_2025143_CLASS": 2.0, + "BODY2025143_PM": [ + 129.73, + 712.1437611, + 0.0 + ], + "BODY2025143_POLE_RA": [ + 90.02564, + 0.0, + 0.0 + ], + "FRAME_2025143_CLASS_ID": 2025143.0, + "BODY2025143_POLE_DEC": [ + -67.02704, + 0.0, + 0.0 + ], + "FRAME_2025143_CENTER": 2025143.0, + "BODY2025143_LONG_AXIS": 0.0, + "FRAME_2025143_NAME": "ITOKAWA_FIXED" + }, + "detector_sample_summing": 1, + "detector_line_summing": 1, + "focal_length_model": { + "focal_length": 0.1208 + }, + "detector_center": { + "line": 511.5, + "sample": 511.5 + }, + "focal2pixel_lines": [ + 0.0, + 0.0, + -83.33333333 + ], + "focal2pixel_samples": [ + 0.0, + 83.33333333, + 0.0 + ], + "optical_distortion": { + "radial": { + "coefficients": [ + 0.0, + 2.8e-05, + 0.0 + ] + } + }, + "starting_detector_line": 0, + "starting_detector_sample": 0, + "instrument_position": { + "spk_table_start_time": 182502855.87767982, + "spk_table_end_time": 182502855.87767982, + "spk_table_original_size": 1, + "ephemeris_times": [ + 182502855.87767982 + ], + "positions": [ + [ + 8.86672985554185, + 0.2413099824695155, + 0.0807100049795115 + ] + ], + "velocities": [ + [ + -1.7052270063544483e-07, + 3.570752676118616e-07, + 2.8761355905130292e-06 + ] + ], + "reference_frame": 1 + }, + "sun_position": { + "spk_table_start_time": 182502855.87767982, + "spk_table_end_time": 182502855.87767982, + "spk_table_original_size": 1, + "ephemeris_times": [ + 182502855.87767982 + ], + "positions": [ + [ + 154700502.11551195, + 5443988.583930893, + -2054766.29920961 + ] + ], + "velocities": [ + [ + -6.6574479060899465, + 28.813387859292327, + 13.032393923917786 + ] + ], + "reference_frame": 1 + } +} \ No newline at end of file diff --git a/tests/pytests/data/isds/mvic_mpf_isd.json b/tests/pytests/data/isds/mvic_mpf_isd.json index 2fe5cb56f46484556c4d338c05c424ecbf89dc90..938db665b90cc465f4e181bc0b28d4609c73abe8 100644 --- a/tests/pytests/data/isds/mvic_mpf_isd.json +++ b/tests/pytests/data/isds/mvic_mpf_isd.json @@ -12,8 +12,8 @@ "name_model": "USGS_ASTRO_FRAME_SENSOR_MODEL", "center_ephemeris_time": 486576443.42086315, "radii": { - "semimajor": 1195.0, - "semiminor": 1195.0, + "semimajor": 1188.3, + "semiminor": 1188.3, "unit": "km" }, "body_rotation": { @@ -1638,9 +1638,9 @@ }, "naif_keywords": { "BODY999_RADII": [ - 1195.0, - 1195.0, - 1195.0 + 1188.3, + 1188.3, + 1188.3 ], "BODY_FRAME_CODE": 10019, "BODY_CODE": 999, diff --git a/tests/pytests/data/isds/nhleisa_isd.json b/tests/pytests/data/isds/nhleisa_isd.json index 9121e7fce95bcb960ca0ca20a9a7901f3444d468..94714f7e05b49620b2af710ed50ab97035d8beb3 100644 --- a/tests/pytests/data/isds/nhleisa_isd.json +++ b/tests/pytests/data/isds/nhleisa_isd.json @@ -21,8 +21,8 @@ "starting_ephemeris_time": 487928588.0336103, "center_ephemeris_time": 487928745.5376103, "radii": { - "semimajor": 1195.0, - "semiminor": 1195.0, + "semimajor": 1188.3, + "semiminor": 1188.3, "unit": "km" }, "body_rotation": { @@ -4527,9 +4527,9 @@ }, "naif_keywords": { "BODY999_RADII": [ - 1195.0, - 1195.0, - 1195.0 + 1188.3, + 1188.3, + 1188.3 ], "BODY_FRAME_CODE": 10019, "BODY_CODE": 999, diff --git a/tests/pytests/data/st_2458542208_v/amica31.ti b/tests/pytests/data/st_2458542208_v/amica31.ti new file mode 100755 index 0000000000000000000000000000000000000000..a719856d7d64ce4d46e40fd88f006f73e143e25e --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/amica31.ti @@ -0,0 +1,322 @@ +KPL/IK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "amica31.ti" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = IK +PRODUCT_ID = "amica31.ti" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:41 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "HAYABUSA SPACECRAFT BUS" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "ASTEROID MULTI-BAND IMAGING CAMERA" +NAIF_INSTRUMENT_ID = -130102 +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = INSTRUMENT + DESCRIPTION = "SPICE I-Kernel (IK) file containing FOV and +reference frame definitions for the Hayabusa Asteroid Multi-band Imaging +CAmera (AMICA) instrument, created by the Hayabusa Joint Science Team. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Hayabusa NIRS Instrument and Frame Kernel Kile +=========================================================================== + + This instrument kernel (I-kernel) contains the frames and FOV + definitions for Hayabusa Asteroid Multi-band Imaging CAmera (AMICA). + + +Version and Date +--------------------------------------------------------------------------- + + Version 3.1 by Boris Semenov, NAIF/JPL, 23 Sep. 2009. + + Added miscellaneous comments. File name and version were not + changed. + + Version 3.1 by Naru Hirata, Univ. of Aizu, 25 Jul. 2008. + + ***** IMPORTANT ***** + This is a bug-fix release for v 3.0, which include wrong + pointing vector angles. + + Here is the corrected line. + TKFRAME_-130102_ANGLES = ( -0.087, -0.124, -0.380) + + PLEASE REPLACE the older version, v 3.0, with a new one + and DISCARD any results that depend on wrong values from + the older version. + + + Version 3.0 by Naru Hirata, Univ. of Aizu, 10 Apr. 2007. + + The alignments and the focal length are updated by results of + in-flight calibration. + + TKFRAME_-130102_ANGLES = ( -0.087, -0.124, 0.380) + INS-130102_FOCAL_LENGTH = ( 0.1208 ) + + Original efforts on in-flight calibration were done by Etsuko + Nemoto (Univ. of Aizu) and Masateru Ishiguro (Seoul National Univ.). + Details are described in a following paper. + + Ishiguro et al. (2007) + Calibration and Performance of Asteroid Multi-band Imaging + Camera (AMICA) onboard Hayabusa Spacecraft, + (in prep). + + Version 2.0 by Naru Hirata, Kobe University, 19 Oct. 2005. + + A definition of the camera boresight is again changed: + INS-130102_CENTER = ( 511.5, 511.5 ) + + Asignments of IDs are changed: + NAIF ID + ------------------------------------------------ + HAYABUSA -130 + HAYABUSA_SC_BUS_PRIME -130000 + + IDs for ONC/AMICA -1301xx + HAYABUSA_AMICA_IDEAL -130101 + HAYABUSA_AMICA -130102 + ------------------------------------------------ + + + Version 1.0 by Naru Hirata, Kobe University, 3 Sept. 2005. + + Modified the values of alignment and focal length: + + TKFRAME_-130001_RELATIVE = 'HAYABUSA_AMICA_IDEAL' + TKFRAME_-130001_ANGLES = ( -0.1047822858, -0.1069183120, -0.45) + TKFRAME_-130001_AXES = ( 1, 2, 3 ) + TKFRAME_-130001_UNITS = 'DEGREES' + + INS-130001_FOCAL_LENGTH = ( 0.1204711614 ) + INS-130001_F_NUMBER = ( 8.0 ) + + + Version 0.4 by Naru Hirata, Kobe University, 27 July 2005. + + Modified the values of alignment: + + TKFRAME_-130001_ANGLES = ( 0.0, 180.0, -90.0 ) + TKFRAME_-130001_AXES = ( 1, 2, 3 ) + + TKFRAME_-130001_ANGLES = ( -90.0, 180.0, 180.0 ) + TKFRAME_-130001_AXES = ( 3, 2, 3 ) + + + Version 0.3 (prototype) by Shingo Kobayashi, Univ. of Aizu, 21 July 2005. + + Added to a new item as follows: + + INS-130001_UPVECTOR = ( 0.0 -1.0 0.0 ) + + + Version 0.2 (prototype) by Naru Hirata, Kobe University, 24 June 2005. + + Added to some new items as follows: + + INS-130001_PIXEL_SAMPLES = ( 1024 ) + INS-130001_PIXEL_LINES = ( 1024 ) + INS-130001_CENTER = ( 512.5, 512.5 ) + INS-130001_PIXEL_SIZE = ( 0.000012 ) + + Version 0.1 (prototype) by Naru Hirata, Kobe University, 5 June 2004. + Version 0.0 (prototype) by Naru Hirata, Kobe University, 25 May 2004. + + +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. + The frame definitions information is accessed via any interfaces + utilizing SPICE frames subsystem (PXFORM, etc). + + This file was created with, and can be updated with a text editor or + word processor. + + +Conventions for Specifying Data +--------------------------------------------------------------------------- + + Instrument data items are specified using ``keyword=value'' + assignments. All keywords referencing instrument values in this + I-kernel start with the characters `INS' followed by the NAIF + instrument ID code for AMICA, -130102. The remainder of the keyword + is an underscore character followed by the unique name of the data + item. For example, AMICA boresight vector is specified by + + INS-130102_BORESIGHT + + The upper bound on the length of all keywords is 32 characters. + + +Hayabusa Spacecraft Frame Definition +--------------------------------------------------------------------------- + + This HAYABUSA_SC_BUS_PRIME frame definition is a copy of the + definition provided in the main Hayabusa FK file. It is included in + this IK file for historical reasons. + +\begindata + + FRAME_HAYABUSA_SC_BUS_PRIME = -130000 + FRAME_-130000_NAME = 'HAYABUSA_SC_BUS_PRIME' + FRAME_-130000_CLASS = 3 + FRAME_-130000_CLASS_ID = -130000 + FRAME_-130000_CENTER = -130 + CK_-130000_SCLK = -130 + CK_-130000_SPK = -130 + +\begintext + + +AMICA Frame Definitions +--------------------------------------------------------------------------- + + Two frames are defined for AMICA: HAYABUSA_AMICA_IDEAL and + HAYABUSA_AMICA. + + The HAYABUSA_AMICA_IDEAL frame incorporates the ideal fixed + instrument alignment relative to the spacecraft frame, + HAYABUSA_SC_BUS_PRIME. The +Z axis of the HAYABUSA_AMICA_IDEAL frame + is along the ideally-mounted instrument boresight. + + The HAYABUSA_AMICA frame incorporates the the actual instrument + misalignment relative to its ideal orientation represented by the + HAYABUSA_AMICA_IDEAL frame. The +Z axis of this frame is along the + actual instrument boresight. + + Both frames are defined as fixed offset frames with their + orientation specified using Euler angles. + + Note that angles in the frame definitions are specified for "from + instrument to base (relative to) frame" transformation. + + It is also noted that these instrument frames are different from the + frame definitions for mechanical design, which are officially referred + in printed materials. The boresight of the camera points the -Z axis in + the coordinates for mechanical design, while it points the +Z axis + in the SPICE instrument frame. + +\begindata + + FRAME_HAYABUSA_AMICA = -130102 + FRAME_-130102_NAME = 'HAYABUSA_AMICA' + FRAME_-130102_CLASS = 4 + FRAME_-130102_CLASS_ID = -130102 + FRAME_-130102_CENTER = -130 + TKFRAME_-130102_SPEC = 'ANGLES' + TKFRAME_-130102_RELATIVE = 'HAYABUSA_AMICA_IDEAL' + TKFRAME_-130102_ANGLES = ( -0.087, -0.124, -0.380) + TKFRAME_-130102_AXES = ( 1, 2, 3 ) + TKFRAME_-130102_UNITS = 'DEGREES' + + FRAME_HAYABUSA_AMICA_IDEAL = -130101 + FRAME_-130101_NAME = 'HAYABUSA_AMICA_IDEAL' + FRAME_-130101_CLASS = 4 + FRAME_-130101_CLASS_ID = -130101 + FRAME_-130101_CENTER = -130 + TKFRAME_-130101_SPEC = 'ANGLES' + TKFRAME_-130101_RELATIVE = 'HAYABUSA_SC_BUS_PRIME' + TKFRAME_-130101_ANGLES = ( 0.0, 180.0, -90.0 ) + TKFRAME_-130101_AXES = ( 1, 2, 3 ) + TKFRAME_-130101_UNITS = 'DEGREES' + +\begintext + + +AMICA Field-Of-View Definition +--------------------------------------------------------------------------- + + The AMICA FOV is defined using a corner-style definition as a 5.83 by + 5.83 degrees square pyramid centered around the boresight that points + along the +Z axis of the HAYABUSA_AMICA frame. FOV corner directions + are defined assuming that: + + - FOV has square shape with its sides along X and Y axes of the + instrument's frame; + + - FOV angular size in X direction is 5.83 degrees; in Y direction + -- 5.83 degrees; + + - boresight vector intersects FOV exactly in the center of the + rectangle; + + The FOV shape is set to 'POLYGON'; it could also have been set to + 'RECTANGLE'. Corner directions are given counterclockwise as seen + from boresight. + +\begindata + + INS-130102_PIXEL_SAMPLES = ( 1024 ) + INS-130102_PIXEL_LINES = ( 1024 ) + INS-130102_CENTER = ( 511.5, 511.5 ) + INS-130102_PIXEL_SIZE = ( 0.000012 ) + + INS-130102_FOV_FRAME = 'HAYABUSA_AMICA' + INS-130102_FOV_SHAPE = 'POLYGON' + INS-130102_BORESIGHT = ( 0.0 0.0 1.0 ) + INS-130102_UPVECTOR = ( 0.0 -1.0 0.0 ) + + INS-130102_FOV_BOUNDARY_CORNERS = ( + 0.006144 0.006144 0.1204711614 + -0.006144 0.006144 0.1204711614 + -0.006144 -0.006144 0.1204711614 + 0.006144 -0.006144 0.1204711614 + ) + +\begintext + + +AMICA Optical Parameters +--------------------------------------------------------------------------- + + The following table summarizes a camera optics parameters: + + ----------------------------------------------------------------- + parameter ONC-T(AMICA) + ----------------------------------------------------------------- + Focal Length, mm 120.8 + f/ratio f/8.0 + IFOV, arcsec/pixel 20.47 + Field of view (degree) + Horizontal 5.7 + Vertical 5.7 + ----------------------------------------------------------------- + + + These values are incorporated in the keywords below; focal lengths + and aperture are converted to METERS. + +\begindata + + INS-130102_FOCAL_LENGTH = ( 0.1208 ) + INS-130102_F_NUMBER = ( 8.0 ) + +\begintext + +End of IK file. diff --git a/tests/pytests/data/st_2458542208_v/amicaAddendum002.ti b/tests/pytests/data/st_2458542208_v/amicaAddendum002.ti new file mode 100755 index 0000000000000000000000000000000000000000..efa08086dc960f0236f8e08ec81d157efe011244 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/amicaAddendum002.ti @@ -0,0 +1,43 @@ +\begindata + + INS-130102_PIXEL_PITCH = 0.012 + INS-130102_BORESIGHT_SAMPLE = 511.5 + INS-130102_BORESIGHT_LINE = 511.5 + +\begintext + The AMICA orientientiation in ISIS camera model implemenation + is +Y = -LINE, +X = +SAMPLE, Z = +Z +\begindata + + INS-130102_TRANSY = (0.0, 0.0, -0.012) + INS-130102_TRANSX = (0.0, 0.012, 0.0) + INS-130102_ITRANSL = (0.0, 0.0, -83.33333333) + INS-130102_ITRANSS = (0.0, 83.33333333, 0.0) + +\begintext + The AMICA distortion uses the basic radial distortion model where + R**2 = x**2 + y **2. The distortion for X and Y is: + + Xc = X ( 1 + K1*R2) + Yc = Y ( 1 + K1*R2) + + ISIS implementation of the distortion model is slightly different but can be + used to implement this distortion model. + + For AMICA, only one term, K1 = -2.8x10**(-5), is used. Source for this + information is Ishiguro, Masateru, et al. "The Hayabusa Spacecraft Asteroid + Multi-band Imaging Camera (AMICA)". Icarus 207.2 (2010): 714-731. + +\begindata + + INS-130102_OD_K = ( 0.0, 0.000028, 0.0) + +\begintext +AMICA is very close to Itokawa so light time correction +and target/observer perspective are set as follows. + +\begindata + +INS-130102_SWAP_OBSERVER_TARGET = 'TRUE' +INS-130102_LIGHTTIME_CORRECTION = 'NONE' +INS-130102_LT_SURFACE_CORRECT = 'FALSE' diff --git a/tests/pytests/data/st_2458542208_v/hayabusa.tsc b/tests/pytests/data/st_2458542208_v/hayabusa.tsc new file mode 100755 index 0000000000000000000000000000000000000000..6db182f50dd1515dc1e0ac8db1f5497919f79af3 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/hayabusa.tsc @@ -0,0 +1,3462 @@ +KPL/SCLK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "hayabusa.tsc" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = SCLK +PRODUCT_ID = "hayabusa.tsc" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:43 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = CLOCK_COEFFICIENTS + DESCRIPTION = "SPICE Spacecraft Clock Kernel (SCLK) file +containing clock correlation data for the Hayabusa on-board clock, created +by the Hayabusa Joint Science Team. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Hayabusa SCLK File +=========================================================================== + + This file is a SPICE spacecraft clock (SCLK) kernel containing the + data necessary to convert between Hayabusa spacecraft on-board clock + time and ephemeris time. + + +Production/History of this SCLK file +-------------------------------------------------------- + + This file was produced by Dr. Naru Hirata of the Hayabusa Joint + Science Team. + + Although the SCLK_KERNEL_ID provided in the data section of the file + is set to September 6, 2005, the set of data included in the file + suggests that the file was created on or shortly after November 28, + 2005. + + The comments were added to the file by Boris Semenov, NAIF/JPL on + September 22, 2009, during preparation of Hayabusa SPICE data for + formal archiving in PDS. When the comments were added to the file, + the original file name (hayabusa.tsc) was not changed because no + data in the file were modified. + + +Usage +-------------------------------------------------------- + + This file must be loaded into the user's program by a call to the + FURNSH subroutine in order to use the SPICELIB SCLK family of + subroutines to convert Hayabusa 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: + + MMMMMMMMMMM:FFF + + where: + + MMMMMMMMMMM -- count of major on-board clock ticks (131086 ... + 39062500000); the nominal duration of one major + on-board clock tick is approximately 1/32 of a + second + + FFF -- count of minor on-board clock ticks (0 ... 255); + the nominal duration of one minor on-board clock + tick is approximately 1/8192 of a second + + +Inquiries +-------------------------------------------------------- + + If you have any questions regarding this file contact + + Naru Hirata + naru@u-aizu.ac.jp + Department of Computer Software + The University of Aizu, Japan + + or + + Boris V. Semenov + (818) 354-8136 + Boris.Semenov@jpl.nasa.gov + + +Kernel Data +-------------------------------------------------------- + +\begintext + +DESCRIPTION =" + +This file contains the data necessary to convert between Hayabusa +spacecraft clock time and ephemeris time. " + + +\begindata + +SCLK_KERNEL_ID = ( @2005-09-06 ) + +SCLK_DATA_TYPE_130 = ( 1 ) +SCLK01_TIME_SYSTEM_130 = ( 1 ) +SCLK01_N_FIELDS_130 = ( 2 ) +SCLK01_MODULI_130 = ( 4294967296 256) +SCLK01_OFFSETS_130 = ( 0 0) +SCLK01_OUTPUT_DELIM_130 = ( 2 ) +SCLK_PARTITION_START_130 = ( 0.0000000000000E+00 ) +SCLK_PARTITION_END_130 = ( 1.0000000000000E+13 ) + +SCLK01_COEFFICIENTS_130 = ( + + 3.35581810000000e+07 1.05712107715935e+08 3.12498634281155e-02 + 6.71126130000000e+07 1.05716203698034e+08 3.12498779238695e-02 + 1.00667045000000e+08 1.05720299682034e+08 3.12498580876763e-02 + 1.34221477000000e+08 1.05724395663433e+08 3.12495364015456e-02 + 3.35548581000000e+08 1.05748971361343e+08 3.12490928669149e-02 + 3.69103013000000e+08 1.05753067242443e+08 3.12490227679518e-02 + 4.36211877000000e+08 1.05761258986268e+08 3.12489858340541e-02 + 4.69766309000000e+08 1.05765354853339e+08 3.12489689042947e-02 + 5.03328933000000e+08 1.05769451718158e+08 3.12490054922567e-02 + 5.36899749000000e+08 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1.86319328703516e+08 3.12491125359696e-02 + 6.60418635072000e+11 1.86323420087322e+08 3.12492306675267e-02 + 6.60452189504000e+11 1.86327515986484e+08 3.12492277380443e-02 + + +) +\begintext diff --git a/tests/pytests/data/st_2458542208_v/hayabusa_hp.tf b/tests/pytests/data/st_2458542208_v/hayabusa_hp.tf new file mode 100755 index 0000000000000000000000000000000000000000..fd7d0fd00181bdedd8392dd887e135c9a450466f --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/hayabusa_hp.tf @@ -0,0 +1,392 @@ +KPL/FK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "hayabusa_hp.tf" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = FK +PRODUCT_ID = "hayabusa_hp.tf" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:41 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = FRAMES + DESCRIPTION = "SPICE Frames Kernel (FK) file containing +the definitions of the Hayabusa spacecraft frame and mission-specific +dynamic frames, created by the Hayabusa Joint Science Team. The original +name of this file was HAYABUSA_HP.TF. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Hayabusa Frames Definition Kernel +=========================================================================== + + This frame kernel contains a set of frame definitions for the + Hayabusa mission. It also contains NAIF name-ID mappings for + Hayabusa instruments. + + +Version and Date +--------------------------------------------------------------------------- + + Version 1.0 -- Sep. 22, 2009 -- Boris Semenov, NAIF/JPL. + + Lowercased file name (HAYABUSA_HP.TF -> hayabusa_hp.tf); + + Corrected spacecraft name to be consistent with the duplicate + definitions provided in IKs (HAYABUSA_SC_BUS -> + HAYABUSA_SC_BUS_PRIME); + + Added name-ID mapping keywords for science instruments; + + Added comments describing frames defined in the IK and + Itokawa FK; + + Added other miscellaneous comments. + + Version 1.0 -- Sep. 19, 2005 -- Naru Hirata, Aizu Univ. + + +Hayabusa NAIF IDs +--------------------------------------------------------------------------- + + The following names and NAIF ID codes are assigned to the Hayabusa + spacecraft, its structures, and science instruments: + + NAME NAIF ID + ----------------------------------------------- + HAYABUSA -130 + HAYABUSA_AMICA -130102 + HAYABUSA_NIRS -130200 + HAYABUSA_LIDAR -130300 + HAYABUSA_XRS -130400 + + The keywords below implement the Hayabusa name-ID mappings. + + \begindata + + NAIF_BODY_NAME += ( 'HAYABUSA' ) + NAIF_BODY_CODE += ( -130 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_AMICA' ) + NAIF_BODY_CODE += ( -130102 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_NIRS' ) + NAIF_BODY_CODE += ( -130200 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_LIDAR' ) + NAIF_BODY_CODE += ( -130300 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_XRS' ) + NAIF_BODY_CODE += ( -130400 ) + + \begintext + + +Hayabusa Reference Frames +--------------------------------------------------------------------------- + + The following reference frames for Hayabusa spacecraft, its + structures, and science instruments are defined in this FK and other + Hayabusa kernels (Itokawa FK, PCKs, and IKs): + + + Itokawa body-fixed frame (defined in a separate FK and PCKs): + ------------------------------------------------------------- + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + ITOKAWA_FIXED J2000 PCK 2025143 + + + Hayabusa spacecraft frame (duplicated in the IKs): + ---------------------------------------------------- + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + HAYABUSA_SC_BUS_PRIME J2000 CK -130000 + + + Hayabusa Science instrument frames (defined in the instrument IK files): + ------------------------------------------------------------------------ + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + HAYABUSA_AMICA_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130101 + HAYABUSA_AMICA HAYABUSA_AMICA FIXED -130102 + + HAYABUSA_NIRS_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130201 + HAYABUSA_NIRS HAYABUSA_NIRS_IDEAL FIXED -130200 + + HAYABUSA_LIDAR_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130301 + HAYABUSA_LIDAR HAYABUSA_LIDAR_IDEAL FIXED -130300 + + HAYABUSA_XRS_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130410 + HAYABUSA_XRS HAYABUSA_XRS_IDEAL FIXED -130400 + + + Hayabusa-specific dynamic frames: + --------------------------------- + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + HAYABUSA_HP_FRAME J2000 DYNAMIC -130900 + ITOKAWA_-Z_SUN_+X J2000 DYNAMIC -130910 + EARTH_ITOKAWA_P J2000 DYNAMIC -130920 + + +Hayabusa Reference Frame Tree +--------------------------------------------------------------------------- + + + This diagram shows the Hayabusa frame tree: + + + "J2000" INERTIAL + +-----------------------------------------------------------+ + | | | | | + |<-dynamic | | | dynamic->| + | | | | | + V | | | V + "HAYABUSA_HP_FRAME" | | | "ITOKAWA_-Z_SUN_+X" + ------------------- | | | ------------------- + | | | + | | | + dynamic->| | |<-pck + | | | + V | V + "EARTH_ITOKAWA_P" | "ITOKAWA_FIXED" + ----------------- | --------------- + | + | + |<-ck + | + V + "HAYABUSA_SC_BUS_PRIME" + +-----------------------------------------------------------+ + | | | | + | |<-fixed | |<-fixed + | | | | + | V | V + | "HAYABUSA_NIRS_IDEAL" | "HAYABUSA_XRS_IDEAL" + | --------------------- | -------------------- + | | | | + | |<-fixed | |<-fixed + | | | | + | V | V + | "HAYABUSA_NIRS" | "HAYABUSA_XRS" + | --------------- | -------------- + | | + | | + |<-fixed |<-fixed + | | + V V + "HAYABUSA_AMICA_IDEAL" "HAYABUSA_LIDAR_IDEAL" + ---------------------- ---------------------- + | | + |<-fixed |<-fixed + | | + V V + "HAYABUSA_AMICA" "HAYABUSA_LIDAR" + ---------------- ---------------- + + +Itokawa Body-Fixed Frame +--------------------------------------------------------------------------- + + The Itokawa body-fixed frame, ITOKAWA_FIXED, is defined in a + separate FK file (itokawa_fixed.tf). Its definition is also + duplicated in some of the Itokawa PCK files. + + +Hayabusa Spacecraft Frame +--------------------------------------------------------------------------- + + The Hayabusa spacecraft frame, HAYABUSA_SC_BUS_PRIME, is defined + as follows: + + - +Z axis is parallel to the nominal HGA boresight; + + - +X axis is parallel to the ion engines thrust vector; + + - +Y axis completes the right-handed frame; + + The Hayabusa spacecraft frame shown on this diagram: + + ^ + | HGA Boresight + | + + ^ + / \ HGA + -------------------- + \ / + \ +Z / + -------- ^ --------- + | | | Ion Engines + | | |_ + | | +X |_] + | x-----> |_] -----> + _| +Y | Thrust Vector + NIRS | | | + ----| |---------------| |- + | | LIDAR XRS + | | + Sample | | | + horn | | | Science Instrument + / \ V Boresights + + + This frame is defined as a CK-based frame below. The frame + definition is also duplicated in Hayabusa science instrument IKs. + + \begindata + + FRAME_HAYABUSA_SC_BUS_PRIME = -130000 + FRAME_-130000_NAME = 'HAYABUSA_SC_BUS_PRIME' + FRAME_-130000_CLASS = 3 + FRAME_-130000_CLASS_ID = -130000 + FRAME_-130000_CENTER = -130 + CK_-130000_SCLK = -130 + CK_-130000_SPK = -130 + + \begintext + + +Hayabusa Science Instrument Frames +--------------------------------------------------------------------------- + + Hayabusa science instrument frames are defined in the IK files. + + +Hayabusa-Specific Dynamic Frames +--------------------------------------------------------------------------- + + The HAYABUSA_HP_FRAME frame, used as the reference frame in the + Hayabusa SPKs produces by JAXA, is defined as follows: + + - +Z axis is along the geometric direction from Itokawa to the + Earth + + - +X axis is as close as possible to the geometric direction + from Itokawa to the Sun + + - +Y axis completes the right-handed frame; + + This frame is defined as a two-vector style dynamic frame below. + + \begindata + + FRAME_HAYABUSA_HP = -130900 + FRAME_-130900_NAME = 'HAYABUSA_HP' + FRAME_-130900_CLASS = 5 + FRAME_-130900_CLASS_ID = -130900 + FRAME_-130900_CENTER = 2025143 + FRAME_-130900_RELATIVE = 'J2000' + FRAME_-130900_DEF_STYLE = 'PARAMETERIZED' + FRAME_-130900_FAMILY = 'TWO-VECTOR' + FRAME_-130900_PRI_AXIS = 'Z' + FRAME_-130900_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130900_PRI_OBSERVER = 2025143 + FRAME_-130900_PRI_TARGET = 'EARTH' + FRAME_-130900_PRI_ABCORR = 'NONE' + FRAME_-130900_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130900_SEC_OBSERVER = 2025143 + FRAME_-130900_SEC_TARGET = 'SUN' + FRAME_-130900_SEC_AXIS = 'X' + FRAME_-130900_SEC_ABCORR = 'NONE' + + \begintext + + + The ITOKAWA_-Z_SUN_+X frame, representing the nominal Itokawa-pointed + orientation, is defined as follows: + + - -Z axis is along the geometric direction from Hayabusa to + Itokawa + + - +X axis is as close as possible to the geometric direction from + Hayabusa to the Sun + + - +Y axis completes the right-handed frame; + + This frame is defined as a two-vector style dynamic frame below. + + \begindata + + FRAME_ITOKAWA_-Z_SUN_+X = -130910 + FRAME_-130910_NAME = 'ITOKAWA_-Z_SUN_+X' + FRAME_-130910_CLASS = 5 + FRAME_-130910_CLASS_ID = -130910 + FRAME_-130910_CENTER = -130 + FRAME_-130910_RELATIVE = 'J2000' + FRAME_-130910_DEF_STYLE = 'PARAMETERIZED' + FRAME_-130910_FAMILY = 'TWO-VECTOR' + FRAME_-130910_PRI_AXIS = '-Z' + FRAME_-130910_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130910_PRI_OBSERVER = -130 + FRAME_-130910_PRI_TARGET = 2025143 + FRAME_-130910_PRI_ABCORR = 'NONE' + FRAME_-130910_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130910_SEC_OBSERVER = -130 + FRAME_-130910_SEC_TARGET = 'SUN' + FRAME_-130910_SEC_AXIS = 'X' + FRAME_-130910_SEC_ABCORR = 'NONE' + + \begintext + + + The EARTH_ITOKAWA_P frame is defined as follows: + + - +Z axis is along the geometric direction from the Earth to + Itokawa + + - +Y axis is as close as possible to the geometric direction from + the Earth to the Sun + + - +X axis completes the right-handed frame; + + This frame is defined as a two-vector style dynamic frame below. + + \begindata + + FRAME_EARTH_ITOKAWA_P = -130920 + FRAME_-130920_NAME = 'EARTH_ITOKAWA_P' + FRAME_-130920_CLASS = 5 + FRAME_-130920_CLASS_ID = -130920 + FRAME_-130920_CENTER = 399 + FRAME_-130920_RELATIVE = 'J2000' + FRAME_-130920_DEF_STYLE = 'PARAMETERIZED' + FRAME_-130920_FAMILY = 'TWO-VECTOR' + FRAME_-130920_PRI_AXIS = 'Z' + FRAME_-130920_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130920_PRI_OBSERVER = 'EARTH' + FRAME_-130920_PRI_TARGET = 2025143 + FRAME_-130920_PRI_ABCORR = 'NONE' + FRAME_-130920_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130920_SEC_OBSERVER = 'EARTH' + FRAME_-130920_SEC_TARGET = 'SUN' + FRAME_-130920_SEC_AXIS = 'Y' + FRAME_-130920_SEC_ABCORR = 'NONE' + + \begintext + + +End of FK file. diff --git a/tests/pytests/data/st_2458542208_v/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc b/tests/pytests/data/st_2458542208_v/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc new file mode 100644 index 0000000000000000000000000000000000000000..c273b85e0b980cb1954fa33af2a2fa3b6f17dab8 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc @@ -0,0 +1,192 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/CK ' +'2' +'6' +'HAYABUSA S/C ATTITUDE ' +BEGIN_ARRAY 1 171 +'HAYABUSA S/C ATTITUDE ' +'927A277516^A' +'927A488148^A' +'-1FBD0' +'1' +'3' +'1' +171 +'5AF67FA56758E4^0' +'-9A5236475B2798^0' +'-5F54E2FD0AAF08^0' +'-9C128FC7B1E81^0' +'-39317E7633275E^-4' +'-F184F21C6525A^-4' +'1D3CB82DEED556^-3' +'5AF5775759E64C^0' +'-9A507A37E01AD^0' +'-5F557EE8CC923C^0' +'-9C1481A2B1C4C8^0' +'-84201140D07998^-4' +'-EC165A98193D38^-4' +'21D5CF1FB7C69C^-3' +'5AF3093BDCF004^0' +'-9A4A9BAE0F8CD8^0' +'-5F5A534B2DEA8^0' +'-9C18C64606823^0' +'203C10C00E7638^-4' 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+'927A44D50323E^A' +'927A46D4FDB4F^A' +'927A47E0013178^A' +'927A488148^A' +'927A277516^A' +'1^1' +'15^2' +END_ARRAY 1 171 +TOTAL_ARRAYS 1 + ~NAIF/SPC BEGIN COMMENTS~ +This CK is for testing with the image: ../../../data/isistestdata/hayabusa/st_2458542208_v.ale.cub + +This CK was generated using the following command: {} + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/st_2458542208_v/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc b/tests/pytests/data/st_2458542208_v/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc new file mode 100644 index 0000000000000000000000000000000000000000..c2bcac3306f921827ee34d7a99cd74dd2518396f --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc @@ -0,0 +1,192 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/CK ' +'2' +'6' +'HAYABUSA S/C ATTITUDE ' +BEGIN_ARRAY 1 171 +'HAYABUSA S/C ATTITUDE ' +'927A6801EB^A' +'927A88CC7^A' +'-1FBD0' +'1' +'3' +'1' +171 +'5C70D766D707D4^0' +'-997646A23F2CD8^0' +'-5DC882D28D3B0C^0' +'-9CFC96314D23C^0' +'-9819C56C06A41^-4' +'64BFA3A7A17894^-3' +'ADF8DA8CF601D8^-3' +'5C53B23D3A8AA4^0' +'-9974C5EEC9B65^0' +'-5DE77A14ABC33^0' +'-9CFCB23E00E408^0' +'-7AD008DDB287FC^-4' +'61A4DF7521986C^-3' +'8ADDB81731E28^-3' +'5C197E5A7A3288^0' +'-9977D3766FA778^0' +'-5E2508EF32ECA4^0' +'-9CF707CB6AE1C^0' +'-3052E2BEB8EFB4^-4' +'6BD9C8CB7479C4^-3' +'7D04E94B1DF53^-3' +'5BE038B880C1E^0' +'-998153D872DE48^0' +'-5E5ED0CC85A568^0' +'-9CEC9ABF6EBEA^0' +'-2410936D373D4E^-4' +'6D62AA8FAE60B4^-3' +'79F0195A002764^-3' +'5BA7582628D28C^0' +'-998BF163C82F9^0' +'-5E97ACCF6DBD6C^0' +'-9CE13E516540D^0' +'-777470CF4E625C^-4' +'74852558FCE6C^-3' +'6E7D531A4438D^-3' +'5B722FEA3F3058^0' +'-9999DD8C0403F^0' +'-5ECFEF45289CC8^0' +'-9CD0AB7E6F8C48^0' +'-3A4FF21DCA067A^-4' +'89380018030C68^-3' +'59339D0C630868^-3' +'5B3E880E26046C^0' +'-99B2B157118228^0' +'-5F044CF6DCA60C^0' +'-9CB6BACDBAAE3^0' +'-55B038D73FC66^-4' +'5880CBB1B0A0E^-3' +'1A338CCF2E9AA6^-3' +'5B27B06F99F71C^0' +'-99C7F48C0963^0' +'-5F1D924E6C3C6C^0' +'-9C9FD3CD836AB8^0' +'4A8522D996021C^-4' +'-2E6897B30AE0E8^-4' +'-337CF7549C284A^-3' +'5B3693B46BD644^0' +'-99D1756650CBB^0' +'-5F0C2A35704F58^0' +'-9C9864F167FA58^0' +'114EB3DD399CC4^-4' +'-7857A5C5789318^-4' +'-263D988FD8E8BE^-3' +'5B3D3C1AA0504^0' +'-99D40FA1BE875^0' +'-5F054D51BC49F^0' +'-9C961FC9EDC178^0' +'-7A6047469C1BB^-4' +'-9112D212398A48^-4' +'-4228565A6749F^-3' +'5B48D2065AE948^0' +'-99D7F4B14D4CA8^0' +'-5EFC22EB3C6468^0' +'-9C911B262EC9E8^0' +'-3322606C81FFE6^-4' +'-11C0DE232A89A1^-3' +'-3365154411E5EC^-3' +'5B5CC9DBC7CA94^0' +'-99DB7D06B9AD28^0' +'-5EEA80E0E095F4^0' +'-9C8CAE5446FAA^0' +'2D32258FAA9414^-4' +'-1DB6FE1DF80845^-3' +'-24943378911E5C^-3' +'5B6CA1531A6B38^0' +'-99D9AF7B22E6C^0' +'-5ED9584443E8E4^0' +'-9C8F9AA034BCB^0' +'571FC930F61E7C^-4' +'-1934347E19D438^-3' +'-28D832F8EC3D0C^-3' +'5B7C26A72161E^0' +'-99DA83C45BB3F^0' +'-5EC6E77D27958^0' +'-9C90E3E4618968^0' +'-11B6C87C9846AE^-5' +'-176E1B38B7119B^-3' +'-13BA277C72E097^-3' +'5B81919A00E87C^0' +'-99D8AD17D9FFC8^0' +'-5EC1A41C27D4CC^0' +'-9C92B76AC60948^0' +'-2FFB9950DE230A^-4' +'-342F5094B3A39^-3' +'-3AD8DE99FBCEAA^-3' +'5B8F3BAB849CE4^0' +'-99D5FE2CD60138^0' +'-5EB527456B2A7C^0' +'-9C94EB8DFFAD6^0' +'DF00A1651EF4F^-5' +'-23377CCD1109CE^-3' +'-26924CA3D3264^-3' +'5BA14757CD9F54^0' +'-99D282AAA11DE^0' +'-5EA2FFD0E2758C^0' +'-9C98C2EF8AB9A^0' +'1464C566BB48D2^-4' +'-2AAD03D536B0B^-3' +'-212C0B613A6F9^-3' +'5BB2ED77F3F1E8^0' +'-99CBD067408E38^0' +'-5E9100FEC23BB^0' +'-9C9FE0D868834^0' +'4B48F61CF671A^-5' +'-282D0245B0619C^-3' +'-17D1E03510A69F^-3' +'5BC18B7FAC5424^0' +'-99C3F9440C4528^0' +'-5E828FD5368A94^0' +'-9CA7BB6A4A5C88^0' +'21F269F4F9B21E^-4' +'-29F6E4240B129E^-3' +'-FD069CF91C57F8^-4' +'5BC7C6441F136^0' +'-99BEFF94238F78^0' +'-5E7BD333F07CC8^0' +'-9CAD078D5FDBF^0' +'-873AF1F202BE8^-4' +'-37472D98483C76^-3' +'-19C3F46F69EF88^-3' +'5BD14C29C5A81^0' +'-99B8AE9D923698^0' +'-5E74DEBC80D594^0' +'-9CB1D73B9D359^0' +'74D917F69CB14^-4' +'-2998993BAE8A44^-3' +'-E3144D82A47338^-4' +'927A6801EB^A' +'927A68D503A43^A' +'927A6AD4FE353^A' +'927A6CD500F76^A' +'927A6ED503B99^A' +'927A70D4FE4A98^A' +'927A72D5010CC8^A' +'927A74D503CEF8^A' +'927A76D4FE5FF^A' +'927A77E001DC88^A' +'927A78D501222^A' +'927A7AD503E45^A' +'927A7CD4FE7558^A' +'927A7ED5013788^A' +'927A7FDFFC82E8^A' +'927A80D503F9B8^A' +'927A82D4FE8AB^A' +'927A84D5014CE^A' +'927A86D5040F1^A' +'927A87DFFF5A7^A' +'927A88CC7^A' +'927A6801EB^A' +'1^1' +'15^2' +END_ARRAY 1 171 +TOTAL_ARRAYS 1 + ~NAIF/SPC BEGIN COMMENTS~ +This CK is for testing with the image: ../../../data/isistestdata/hayabusa/st_2458542208_v.ale.cub + +This CK was generated using the following command: {} + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/st_2458542208_v/itokawa_fixed.tf b/tests/pytests/data/st_2458542208_v/itokawa_fixed.tf new file mode 100755 index 0000000000000000000000000000000000000000..1a6630f4945ec137408f6860ee477af3c5d8209e --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/itokawa_fixed.tf @@ -0,0 +1,94 @@ +KPL/FK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "itokawa_fixed.tf" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = FK +PRODUCT_ID = "itokawa_fixed.tf" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:41 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = FRAMES + DESCRIPTION = "SPICE Frames Kernel (FK) file containing +the definition of the asteroid Itokawa body-fixed frame, created by the +Hayabusa Joint Science Team. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +ITOKAWA Body-Fixed Frame Definition Kernel +=========================================================================== + + This frame kernel contains asteroid ITOKAWA body-fixed frame definition. + + +Version and Date +-------------------------------------------------------- + + Version 1.0 -- May 25, 2004 -- Naru Hirata + + Initial release. + + +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. Loading the kernel associates data items with their + names in a data structure called the `kernel pool'. The SPICELIB + routine FURNSH loads a kernel file into the pool as shown below. + + CALL FURNSH ( frame_kernel_name ) + + This file was created and may be updated with a text editor or word + processor. + + +ITOKAWA Body-Fixed Frame +-------------------------------------------------------- + + This kernel file defines asteroid ITOKAWA body-frame, ITOKAWA_FIXED, with + the frame ID code 2025143 in the same as any other PCK frame: + + * +Z along asteroid's North pole; + + * +X along asteroid's prime meridian; + + * +Y complements to the right hand frame; + + * the origin of this frame is at the center of the asteroid ellipsoid. + + As for any PCK frame orientation of this frame is computed by evaluating + corresponding rotation constants provided in a PCK file. + + \begindata + + FRAME_ITOKAWA_FIXED = 2025143 + FRAME_2025143_NAME = 'ITOKAWA_FIXED' + FRAME_2025143_CLASS = 2 + FRAME_2025143_CLASS_ID = 2025143 + FRAME_2025143_CENTER = 2025143 + + OBJECT_2025143_FRAME = 'ITOKAWA_FIXED' + + \begintext + diff --git a/tests/pytests/data/st_2458542208_v/itokawa_gaskell_n3.tpc b/tests/pytests/data/st_2458542208_v/itokawa_gaskell_n3.tpc new file mode 100755 index 0000000000000000000000000000000000000000..e8abb4dbe97d6f350c0b718f1cb036d1812a8700 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/itokawa_gaskell_n3.tpc @@ -0,0 +1,115 @@ +KPL/PCK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "itokawa_gaskell_n3.tpc" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = PCK +PRODUCT_ID = "itokawa_gaskell_n3.tpc" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:42 +PRODUCER_ID = "R.GASKELL/PSI" +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +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 Planetary Constants Kernel (PCK) file +containing the asteroid Itokawa radii values, body-fixed frame definition, +and rotation constants derived by Dr. Robert W. Gaskell, PSI. The original +name of this files was Itokawa_Gaskell_n3.tpc. It contains the rotation +constants consistent with the Itokawa shape models archived in the PDS data +set HAY-A-AMICA-5-ITOKAWASHAPE-V1.0. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Asteroid Itokawa P_constants (PcK) SPICE kernel file +=========================================================================== + + By Hayabusa Joint Science Team, <unknown date>; miscellaneous comments + added by Boris Semenov, NAIF/JPL, on September 24, 2009. + + +Summary +-------------------------------------------------------- + + This PCK file contains Itokawa rotation constants, radii and + the definition of the Itokawa body-fixed frame, ITOKAWA_FIXED. + + The Itokawa rotation constants provided in this PCK are + from the data set catalog file for the Itokawa shape model + data set (HAY-A-AMICA-5-ITOKAWASHAPE-V1.0) by the Dr. Robert W. + Gaskell, PSI. + + +Rotation constants for asteroid Itokawa +-------------------------------------------------------- + + Itokawa rotation constants are provided in the keywords below. + + \begindata + + BODY2025143_POLE_RA = ( 90.02564 0.0 0.0 ) + BODY2025143_POLE_DEC = (-67.02704 0.0 0.0 ) + BODY2025143_PM = (129.73000 712.14376110 0.0 ) + + \begintext + + +Radii for asteroid ITOKAWA +-------------------------------------------------------- + + The Itokawa radii are provided in the keyword below. + + \begindata + + BODY2025143_RADII = ( 0.274 0.156 0.138 ) + + \begintext + + +ITOKAWA_FIXED Frame Definition +-------------------------------------------------------- + + The ITOKAWA fixed frame is defined in the same as any other PCK + frame: + + * +Z along the North pole; + + * +X toward the prime meridian; + + * +Y 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 this PCK file. + + \begindata + + FRAME_ITOKAWA_FIXED = 2025143 + FRAME_2025143_NAME = 'ITOKAWA_FIXED' + FRAME_2025143_CLASS = 2 + FRAME_2025143_CLASS_ID = 2025143 + FRAME_2025143_CENTER = 2025143 + + OBJECT_2025143_FRAME = 'ITOKAWA_FIXED' + + \begintext + + +End of PCK file. diff --git a/tests/pytests/data/st_2458542208_v/naif0012.tls b/tests/pytests/data/st_2458542208_v/naif0012.tls new file mode 100755 index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/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/st_2458542208_v/pck00009.tpc b/tests/pytests/data/st_2458542208_v/pck00009.tpc new file mode 100755 index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/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/st_2458542208_v/st_2458542208_v.ale_0.xsp b/tests/pytests/data/st_2458542208_v/st_2458542208_v.ale_0.xsp new file mode 100644 index 0000000000000000000000000000000000000000..4ae8e40372b4d415ae817bbb55291b199e497924 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/st_2458542208_v.ale_0.xsp @@ -0,0 +1,853 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/SPK ' +'2' +'6' 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+'AE0C403786994^7' +'AE0C404786994^7' +'AE0C405786994^7' +'AE0C406786994^7' +'AE0C407786994^7' +'AE0C408786994^7' +'AE0C409786994^7' +'AE0C40A786994^7' +'AE0C40B786994^7' +'AE0C40C786994^7' +'AE0C40D78280B^7' +'AE0C40E78280B^7' +'AE0C40F78280B^7' +'AE0C41078280B^7' +'AE0C41178280B^7' +'AE0C41278280B^7' +'AE0C41378280B^7' +'AE0C41478280B^7' +'AE0C41578280B^7' +'AE0C41678280B^7' +'AE0C41778280B^7' +'AE0C41878280B^7' +'AE0C41978280B^7' +'AE0C41A78280B^7' +'AE0C41B78280B^7' +'AE0C41C78280B^7' +'AE0C41D78280B^7' +'AE0C41E78280B^7' +'AE0C41F78280B^7' +'AE0C42078280B^7' +'AE0C42178280B^7' +'AE0C42278280B^7' +'AE0C42378280B^7' +'AE0C42478280B^7' +'AE0C42578280B^7' +'AE0C42678280B^7' +'AE0C42778280B^7' +'AE0C42878280B^7' +'AE0C42978280B^7' +'AE0C42A78280B^7' +'AE0C42B78280B^7' +'AE0C42C78280B^7' +'AE0C42D78280B^7' +'AE0C42E78280B^7' +'AE0C42F78280B^7' +'AE0C43078280B^7' +'AE0C43178280B^7' +'AE0C43278280B^7' +'AE0C43378280B^7' +'AE0C43478280B^7' +'AE0C43578280B^7' +'AE0C43678280B^7' +'AE0C43778280B^7' +'AE0C43878280B^7' +'AE0C43978280B^7' +'AE0C43A78280B^7' +'AE0C43B78280B^7' +'AE0C43C77E682^7' +'AE0C43D77E682^7' +'AE0C43E77E682^7' +'AE0C43F77E682^7' +'AE0C44077E682^7' +'AE0C44177E682^7' +'AE0C44277E6828^7' +'AE0C44377E6828^7' +'AE0C44477E6828^7' +'AE0C44577E6828^7' +'AE0C44677E6828^7' +'AE0C44777E6828^7' +'AE0C44877E6828^7' +'AE0C44977E6828^7' +'AE0C44A77E6828^7' +'AE0C44B77E6828^7' +'AE0C44C77E6828^7' +'AE0C44D77E6828^7' +'AE0C44E77E6828^7' +'AE0C44F77E6828^7' +'AE0C45077E6828^7' +'AE0C45177E6828^7' +'AE0C45277E6828^7' +'AE0C45377E6828^7' +'AE0C45477E6828^7' +'AE0C45277E6828^7' +'1^1' +'66^2' +END_ARRAY 2 717 +BEGIN_ARRAY 3 39 +'DE-0403LE-0403 ' +'AE0C34B79F2CB8^7' +'AE0C453DA3455^7' +'A' +'0' +'1' +'2' +39 +'ADFB74^7' +'A8C^5' +'94A1D96FDC9538^5' +'-9DFA14C450E87^3' +'-10A6F90CC55C8E^2' +'1A8DB36D7919A4^0' +'-DBA82D668F68^-2' +'1943E04814A3A9^-3' +'2D2DBBB0F8889A^-4' +'-13328359B6AFED^-5' +'2D4395828FC13A^-6' +'-166EB5C923E47F^-6' +'-50E6C5C4989A2^-8' +'3A64FEEA808364^5' +'1C038412106FEF^4' +'-9BB7059785BE3^1' +'1869B5AA252882^0' +'934A2C3016BD4^-2' +'-56AB4C415E9828^-3' +'595353E6116C3C^-4' +'-6E4C3AE2B464E^-6' +'6454B33CA4F478^-6' +'-E159348A215B38^-7' +'-8B8F3AF4B6392^-8' +'14ABA56F833013^5' +'C116B04BE71DE8^3' +'-3E3EECFB165A0E^1' +'8BF8BF3538E55^-1' +'50D54F66499DF4^-2' +'-2CBDB1CB1D95C2^-3' +'2CD23EAB3A0576^-4' +'-1CDE56A5F1B23D^-6' +'30DE3A636A3FE2^-6' +'-4C3AEEAC5F8958^-7' +'-42223050A58024^-8' +'AD52B4^7' +'1518^6' +'23^2' +'1^1' +END_ARRAY 3 39 +TOTAL_ARRAYS 3 + ~NAIF/SPC BEGIN COMMENTS~ +; ../../../data/isistestdata/hayabusa/out/st_2458542208_v.ale_0.bsp LOG FILE + +; Created 2023-02-16/02:11:21.00. +; +; BEGIN SPKMERGE COMMANDS + +LEAPSECONDS_KERNEL = ../../../remotedata/isis_data/base/kernels/lsk/naif0012.tls + +SPK_KERNEL = ../../../data/isistestdata/hayabusa/out/st_2458542208_v.ale_0.bsp +SOURCE_SPK_KERNEL = ../../../remotedata/isis_data/hayabusa/kernels/tspk/sb_25143_140.bsp + INCLUDE_COMMENTS = NO + BODIES = 2025143 + BEGIN_TIME = 2005 OCT 13 19:02:35.294 + END_TIME = 2005 OCT 13 19:06:59.670 +SOURCE_SPK_KERNEL = ../../../remotedata/isis_data/hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp + INCLUDE_COMMENTS = NO + BODIES = -130 + BEGIN_TIME = 2005 OCT 13 19:02:35.294 + END_TIME = 2005 OCT 13 19:06:59.670 +SOURCE_SPK_KERNEL = ../../../remotedata/isis_data/hayabusa/kernels/tspk/de403s.bsp + INCLUDE_COMMENTS = NO + BODIES = 10 + BEGIN_TIME = 2005 OCT 13 19:02:35.294 + END_TIME = 2005 OCT 13 19:06:59.670 + +; END SPKMERGE COMMANDS + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/st_2458542208_v/st_2458542208_v.ale_1.xsp b/tests/pytests/data/st_2458542208_v/st_2458542208_v.ale_1.xsp new file mode 100644 index 0000000000000000000000000000000000000000..8a7e30e5e98df58ce4506f6f037f8afa7325444f --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/st_2458542208_v.ale_1.xsp @@ -0,0 +1,1989 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/SPK ' +'2' +'6' +'SPKMERGE ' +BEGIN_ARRAY 1 33 +'ITOKAWA ' +'AE0C54FDDC9D6^7' +'AE0C65630BB8^7' +'1EE6B7' +'A' +'1' +'2' +33 +'AE108C^7' +'2A3^5' +'-9362655229C478^7' +'11D114E68B4532^6' +'A18750D88088^4' +'51BD20950E1^2' +'-13D12E948^1' +'-2F3B42A8C^-1' +'-B90C^-4' +'AAB79^-5' +'2^-6' +'-5ACF5E84FB1CC8^6' +'-4BF3EE662F4E08^6' +'63C6F9E67CA8^3' +'E31CD5A4DEF^2' +'10A094D49^1' +'-10A636D5^-1' +'-5A27CA^-3' +'-63F4C^-5' +'CF^-7' +'1BD5954A382803^6' +'-225C8A47DDF064^6' +'-1E648043D30C^3' +'62D62CED7CF^2' +'7FBB718D7^0' +'-60D15FD8^-2' +'-27D6E4^-3' +'-31786^-5' +'4FC^-7' +'ADE65C^7' +'546^5' +'1D^2' +'1^1' +END_ARRAY 1 33 +BEGIN_ARRAY 2 1852 +'HAYABUSA Traj. by HJSC; with NAIF mods ' +'AE0C54FDDC9D6^7' +'AE0C65630BB8^7' +'-82' +'1EE6B7' +'1' +'9' +1024 +'8DDE344AA251E^1' +'3DC3AF8C2BA2CE^0' +'1492B81055B3DB^0' +'-2804D64FFFFFFC^-5' +'5EFFAF75^-5' +'303AD643FFFFFE^-4' +'8DDE34229D7B9^1' +'3DC3B57C269A1E^0' +'1492E84B2BF7DB^0' +'-2811233FFFFFFE^-5' +'5F0178DAA00004^-5' +'303AE375B2FFFE^-4' +'8DDE33FA8C585^1' +'3DC3BB6C3E27C8^0' +'149318860F6D8E^0' +'-281D5EB0000002^-5' +'5F0353D7A^-5' +'303AEF8DED0002^-4' +'8DDE33D26EF9A^1' +'3DC3C15C736542^0' +'149348C0FEFB7B^0' +'-2829888^-5' +'5F052ED5^-5' +'303AFCBFA00002^-4' +'8DDE33AA45712^1' +'3DC3C74CC65292^0' +'149378FBFBBB1B^0' +'-2835D58^-5' +'5F06E6A2C^-5' +'303B09F151FFFC^-4' +'8DDE33820F9BA^1' +'3DC3CD3D34BCBE^0' +'1493A93705AC6D^0' +'-284210EFFFFFFC^-5' +'5F08C1A02^-5' +'303B1723060004^-4' +'8DDE3359CD8AB^1' +'3DC3D32DC0D6C^0' +'1493D9721CCF73^0' +'-284E4C50000002^-5' +'5F0A9C9D4^-5' +'303B233B4^-4' +'8DDE33317F3E6^1' +'3DC3D91E6AA094^0' +'149409AD400AB3^0' +'-285A87BFFFFFFE^-5' +'5F0C6603000004^-5' +'303B306CF10002^-4' +'8DDE330924B6A^1' +'3DC3DF0F3100C4^0' +'149439E87077A4^0' +'-2866C32^-5' +'5F0E2F684^-5' +'303B3D9EA8^-4' +'8DDE32E0BDF38^1' +'3DC3E50013F748^0' +'14946A23AE164C^0' +'-287D5C0F763146^-5' +'5F2854F8488348^-5' +'3047A6D80D24F8^-4' +'8DDE32B84AF4F^1' +'3DC3EAF113842A^0' +'14949A5EF8E6A4^0' +'-287F39F7FFFFFC^-5' +'5F11D3CB400004^-5' +'303B56E893^-4' +'8DDE328FCBBAF8^1' +'3DC3F0E230C0DE^0' +'1494CA9A4FCF37^0' +'-288B755FFFFFFE^-5' +'5F13AEC86^-5' +'303B641A450002^-4' +'8DDE3267404598^1' +'3DC3F6D36BAD64^0' +'1494FAD5B3E97C^0' +'-2897B0C^-5' +'5F1566966^-5' +'303B714BF7^-4' +'8DDE323EA894D8^1' +'3DC3FCC4C216CA^0' +'14952B11253573^0' +'-28A3FDD0000004^-5' +'5F1741939FFFFC^-5' +'303B7D6433^-4' +'8DDE3216049708^1' +'3DC402B6363004^0' +'14955B4CA299A6^0' +'-28B02797FFFFFC^-5' +'5F191C90E^-5' +'303B8BAF5EFFFC^-4' +'8DDE31ED546F7^1' +'3DC408A7C7F912^0' +'14958B882E4905^0' +'-28BC6300000004^-5' +'5F1AE5F65FFFFC^-5' +'303B97C799FFFE^-4' +'8DDE31C4980C7^1' +'3DC40E99765878^0' +'1495BBC3C6109F^0' +'-28C8B008000002^-5' +'5F1CAF5BE^-5' +'303BA4F94B^-4' +'8DDE319BCF5C68^1' +'3DC4148B414E36^0' +'1495EBFF6B09EA^0' +'-28D4D9D0000004^-5' +'5F1E8A594^-5' +'303BB11184FFFE^-4' +'8DDE3172FA8298^1' +'3DC41A7D29F3CA^0' +'14961C3B1C1B6F^0' +'-28E1154^-5' +'5F2053BEC^-5' +'303BBE43390004^-4' +'8DDE314A196D58^1' +'3DC4206F2F2FB6^0' +'14964C76DA5EA8^0' +'-28ED6237FFFFFC^-5' +'5F221D246^-5' +'303BCB74EA^-4' +'8DDE31212C0B2^1' +'3DC426615101FC^0' +'14967CB2A5D392^0' +'-28F99DA8000002^-5' +'5F23F8215FFFFC^-5' +'303BD8A69F^-4' +'8DDE30F8326D78^1' +'3DC42C53908412^0' +'1496ACEE7E7A31^0' +'-2905C778^-5' +'5F25C1872^-5' +'303BE5D8520002^-4' +'8DDE30CF2CA6^1' +'3DC43245EC9C84^0' +'1496DD2A645283^0' +'-29121478^-5' +'5F279C846^-5' +'303BF1F08B^-4' +'8DDE30A61A9188^1' +'3DC438386664CA^0' +'14970D6656430E^0' +'-291E4FE^-5' +'5F2965E9E^-5' +'303BFF223DFFFE^-4' +'8DDE307CFC41A8^1' +'3DC43E2AFCC368^0' +'14973DA255654C^0' +'-292A79B^-5' +'5F2B2F4F8^-5' +'303C0B3A770002^-4' +'8DDE3053D1C7F8^1' +'3DC4441DAFB86^0' +'14976DDE609FC3^0' +'-2936C6B^-5' +'5F2D0A4CA^-5' +'303C1985A60002^-4' +'8DDE302A9B0148^1' +'3DC44A10805D2A^0' +'14979E1A7A2569^0' +'-29430218^-5' +'5F2ED3B25FFFFC^-5' +'303C259DDC^-4' +'8DDE300157FF3^1' +'3DC450036D985^0' +'1497CE569FC345^0' +'-294F3D8^-5' +'5F309D17C00004^-5' +'303C32CF92FFFE^-4' +'8DDE2FD808C1B^1' +'3DC455F67769CC^0' +'1497FE92D292D8^0' +'-295B78EFFFFFFE^-5' +'5F327815200004^-5' +'303C400144^-4' +'8DDE2FAEAD48C^1' +'3DC45BE99EEB1E^0' +'14982ECF12941C^0' +'-2967B45^-5' +'5F34417AC^-5' +'303C4C197DFFFE^-4' +'8DDE2F8545947^1' +'3DC461DCE302CA^0' +'14985F0B5EAD9A^0' +'-2973EFBFFFFFFE^-5' +'5F361C77A^-5' +'303C594B30FFFC^-4' +'8DDE2F5BD1A4B^1' +'3DC467D044CA44^0' +'14988F47B7F8CB^0' +'-29802B27FFFFFE^-5' +'5F37E5DD8^-5' +'303C667CE4^-4' +'8DDE2F32517988^1' +'3DC46DC3C3281C^0' +'1498BF841E75AF^0' +'-298C6688^-5' +'5F39AF432^-5' +'303C73AE96FFFE^-4' +'8DDE2F08C513^1' +'3DC473B75E1C4E^0' +'1498EFC0922446^0' +'-2998A1F7FFFFFA^-5' +'5F3B8A40200004^-5' +'303C7FC6D0FFFC^-4' +'8DDE2EDF2C7108^1' +'3DC479AB16C05^0' +'14991FFD11EB17^0' +'-29A4EEF7FFFFFE^-5' +'5F3D53A5BFFFFC^-5' +'303C8CF8840002^-4' +'8DDE2EB587821^1' +'3DC47F9EEBFAAC^0' +'149950399EE39B^0' +'-29B118C8000006^-5' +'5F3F1D0B600004^-5' +'303C9A2A36FFFE^-4' +'8DDE2E8BD66948^1' +'3DC48592DDCB62^0' +'14998076390DD2^0' +'-29BD5430000002^-5' +'5F40F808A^-5' +'303CA64271^-4' +'8DDE2E62191518^1' +'3DC48B86ED4BEC^0' +'1499B0B2DF5043^0' +'-29C9A138^-5' +'5F42D305C00004^-5' +'303CB48D9D^-4' +'8DDE2E384F73E^1' +'3DC4917B1A7C48^0' +'1499E0EF93DDE^0' +'-29D5CB00000002^-5' +'5F448AD3C00004^-5' +'303CC0A5D70002^-4' +'8DDE2E0E79A8E^1' +'3DC4976F632984^0' +'149A112C5483B7^0' +'-29E20668000006^-5' +'5F4665D1^-5' +'303CCDD789FFFE^-4' +'8DDE2DE497A278^1' +'3DC49D63C98694^0' +'149A4169225B41^0' +'-29EE537^-5' +'5F4840CE^-5' +'303CD9EFC30002^-4' +'8DDE2DBAA94F08^1' +'3DC4A3584D9374^0' +'149A71A5FC4B04^0' +'-29FA8ECFFFFFFE^-5' +'5F4A0A33C^-5' +'303CE72177^-4' +'8DDE2D90AEC038^1' +'3DC4A94CEE36B^0' +'149AA1E2E36C7B^0' +'-2A06B8A8^-5' +'5F4BD399600004^-5' +'303CF4532A^-4' +'8DDE2D66A8079^1' +'3DC4AF41AB7046^0' +'149AD21FD7BFA5^0' +'-2A1305A8000002^-5' +'5F4D9CFEFFFFFC^-5' +'303D0184DC0002^-4' +'8DDE2D3C9501E8^1' +'3DC4B536854036^0' +'149B025CD94481^0' +'-2A1F4108000006^-5' +'5F4F77FC^-5' +'303D0EB6910002^-4' +'8DDE2D1275C0E^1' +'3DC4BB2B7CBFF6^0' +'149B3299E7FB12^0' +'-2A2B6AE8000006^-5' +'5F5152F94^-5' +'303D1ACECA^-4' +'8DDE2CE84A55F8^1' +'3DC4C12091EF8A^0' +'149B62D702C9DC^0' +'-2A37B7E^-5' +'5F530AC74^-5' +'303D28007C0002^-4' +'8DDE2CBE129E18^1' +'3DC4C715C29BFE^0' +'149B93142ACA58^0' +'-2A43F348^-5' +'5F54E5C47FFFFC^-5' +'303D3532300002^-4' +'8DDE2C93CEAAD^1' +'3DC4CD0B10F846^0' +'149BC3515FFC88^0' +'-2A502EB^-5' +'5F56C0C1A^-5' +'303D414A68FFFE^-4' +'8DDE2C697E7C2^1' +'3DC4D3007D046^0' +'149BF38EA146F1^0' +'-2A5C6A18^-5' +'5F588A274^-5' +'303D4E7C1CFFFE^-4' +'8DDE2C3F221208^1' +'3DC4D8F605A6D4^0' +'149C23CBEFC30E^0' +'-2A68A587FFFFFE^-5' +'5F5A538CE^-5' +'303D5BADCF^-4' +'8DDE2C14B96C8^1' +'3DC4DEEBAADFA2^0' +'149C54094B70DD^0' +'-2A74E0E0000002^-5' +'5F5C2E8A^-5' +'303D68DF83^-4' +'8DDE2BEA448BA^1' +'3DC4E4E16DC842^0' +'149C8446B4506^0' +'-2A811C6^-5' +'5F5DF7EFA^-5' +'303D74F7BBFFFE^-4' +'8DDE2BBFC36F4^1' +'3DC4EAD74D473C^0' +'149CB48429481C^0' +'-2A8D57C0000006^-5' +'5F5FC1554^-5' 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+'14C3299C0F2B51^0' +'-344D4D8^-5' +'60D1AC121FFFFC^-5' +'3047CB7E010002^-4' +'8DDE05C530BCE8^1' +'3DC9BA13D2CE5E^0' +'14C359E3DAA952^0' +'-34599A88^-5' +'60D363DFE^-5' +'3047D8AFB20004^-4' +'8DDE0590D7226^1' +'3DC9C021090C5C^0' +'14C38A2BB35904^0' +'-3465D5F^-5' +'60D55074E00004^-5' +'3047E4C7F^-4' +'8DDE055C714C7^1' +'3DC9C62E5E13AA^0' +'14C3BA739820F4^0' +'-34721160000002^-5' +'60D70842C^-5' +'3047F3131A^-4' +'8DDE0527FF3B1^1' +'3DC9CC3BCE97D6^0' +'14C3EABB8B340E^0' +'-347E5E58^-5' +'60D8E34^-5' +'3047FF2B52FFFC^-4' +'8DDE04F380DCB8^1' +'3DC9D2495CCBD6^0' +'14C41B038A5F61^0' +'-348A8827FFFFFE^-5' +'60DAACA5A^-5' +'30480B438EFFFE^-4' +'8DDE04BEF6549^1' +'3DC9D85707963^0' +'14C44B4B95A2F^0' +'-3496C398000002^-5' +'60DC87A29FFFFC^-5' +'3048198EBB0002^-4' +'AE0C54F769ED4^7' +'AE0C550769ED4^7' +'AE0C551769ED4^7' +'AE0C552769ED4^7' +'AE0C553769ED4^7' +'AE0C554769ED4^7' +'AE0C555769ED4^7' +'AE0C556769ED4^7' +'AE0C557769ED4^7' +'AE0C558769ED4^7' +'AE0C559765D4B^7' +'AE0C55A765D4B^7' 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+'AE0C58F761BC2^7' +'AE0C590761BC2^7' +'AE0C591761BC2^7' +'AE0C592761BC2^7' +'AE0C593761BC2^7' +'AE0C594761BC2^7' +'AE0C595761BC2^7' +'AE0C596761BC2^7' +'AE0C597761BC2^7' +'AE0C598761BC2^7' +'AE0C599761BC2^7' +'AE0C59A761BC2^7' +'AE0C59B761BC2^7' +'AE0C59C761BC2^7' +'AE0C59D761BC2^7' +'AE0C59E761BC2^7' +'AE0C59F761BC2^7' +'AE0C5A0761BC2^7' +'AE0C5A1761BC2^7' +'AE0C5A2761BC2^7' +'AE0C5A3761BC2^7' +'AE0C5A4761BC2^7' +'AE0C5A5761BC2^7' +'AE0C5A6761BC2^7' +'AE0C5A7761BC2^7' +'AE0C5A8761BC2^7' +'AE0C5A9761BC2^7' +'AE0C5AA761BC2^7' +'AE0C5AB761BC2^7' +'AE0C5AC761BC2^7' +'AE0C5AD761BC2^7' +'AE0C5AE761BC2^7' +'AE0C5AF761BC2^7' +'AE0C5B0761BC2^7' +'AE0C5B1761BC2^7' +'AE0C5B2761BC2^7' +'AE0C5B3761BC2^7' +'AE0C5B4761BC2^7' +'AE0C5B5761BC2^7' +'AE0C5B6761BC2^7' +'AE0C5B7761BC2^7' +'AE0C5B875DA388^7' +'AE0C5B975DA388^7' +'AE0C5BA75DA388^7' +'AE0C5BB75DA388^7' +'AE0C5BC75DA388^7' +'AE0C5BD75DA388^7' +'AE0C5BE75DA388^7' +'AE0C5BF75DA388^7' +'AE0C5C075DA388^7' +'AE0C5C175DA388^7' +'AE0C5C275DA388^7' +'AE0C5C375DA388^7' +'AE0C5C475DA388^7' +'AE0C5C575DA388^7' +'AE0C5C675DA388^7' +'AE0C5C775DA388^7' +'AE0C5C875DA388^7' +'AE0C5C975DA388^7' +'AE0C5CA75DA388^7' +'AE0C5CB75DA388^7' +'AE0C5CC75DA388^7' +'AE0C5CD75DA388^7' +'AE0C5CE75DA388^7' +'AE0C5CF75DA388^7' +'AE0C5D075DA388^7' +'AE0C5D175DA388^7' +'AE0C5D275DA388^7' +'AE0C5D375DA388^7' +'AE0C5D475DA388^7' +'AE0C5D575DA388^7' +'AE0C5D675DA388^7' +'AE0C5D775DA388^7' +'AE0C5D875DA388^7' +'AE0C5D975DA388^7' +'AE0C5DA75DA388^7' +'AE0C5DB75DA388^7' +'AE0C5DC75DA388^7' +'AE0C5DD75DA388^7' +'AE0C5DE75DA388^7' +'AE0C5DF75DA388^7' +'AE0C5E075DA388^7' +'AE0C5E175DA388^7' +'AE0C5E275DA388^7' +'AE0C5E375DA388^7' +'AE0C5E475DA388^7' +'AE0C5E575DA388^7' +'AE0C5E675DA388^7' +'AE0C5E775DA388^7' +'AE0C5E87598AF8^7' +'AE0C5E97598AF8^7' +'AE0C5EA7598AF8^7' +'AE0C5EB7598AF8^7' +'AE0C5EC7598AF8^7' +'AE0C5ED7598AF8^7' +'AE0C5EE7598AF8^7' +'AE0C5EF7598AF8^7' +'AE0C5F07598AF8^7' +'AE0C5F17598AF8^7' +'AE0C5F27598AF8^7' +'AE0C5F37598AF8^7' +'AE0C5F47598AF8^7' +'AE0C5F57598AF8^7' +'AE0C5F67598AF8^7' +'AE0C5F77598AF8^7' +'AE0C5F87598AF8^7' +'AE0C5F97598AF8^7' +'AE0C5FA7598AF8^7' +'AE0C5FB7598AF8^7' +'AE0C5FC7598AF8^7' +'AE0C5FD7598AF8^7' +'AE0C5FE7598AF8^7' +'AE0C5FF7598AF8^7' +'AE0C6007598AF8^7' +'AE0C6017598AF8^7' +'AE0C6027598AF8^7' +'AE0C6037598AF8^7' +'AE0C6047598AF8^7' +'AE0C6057598AF8^7' +'AE0C6067598AF8^7' +'AE0C6077598AF8^7' +'AE0C6087598AF8^7' +'AE0C6097598AF8^7' +'AE0C60A7598AF8^7' +'AE0C60B7598AF8^7' +'AE0C60C7598AF8^7' +'AE0C60D7598AF8^7' +'AE0C60E7598AF8^7' +'AE0C60F7598AF8^7' +'AE0C6107598AF8^7' +'AE0C6117598AF8^7' +'AE0C6127598AF8^7' +'AE0C6137598AF8^7' +'AE0C6147598AF8^7' +'AE0C6157598AF8^7' +'AE0C6167598AF8^7' +'AE0C617755726^7' +'AE0C618755726^7' +'AE0C619755726^7' +'AE0C61A755726^7' +'AE0C61B755726^7' +'AE0C61C755726^7' +'AE0C61D755726^7' +'AE0C61E755726^7' +'AE0C61F755726^7' +'AE0C620755726^7' +'AE0C621755726^7' +'AE0C622755726^7' +'AE0C623755726^7' +'AE0C624755726^7' +'AE0C625755726^7' +'AE0C626755726^7' +'AE0C627755726^7' +'AE0C628755726^7' +'AE0C629755726^7' +'AE0C62A755726^7' +'AE0C62B755726^7' +'AE0C62C755726^7' +'AE0C62D755726^7' +'AE0C62E755726^7' +'AE0C62F755726^7' +'AE0C630755726^7' +'AE0C631755726^7' +'AE0C632755726^7' +'AE0C633755726^7' +'AE0C634755726^7' +'AE0C635755726^7' +'AE0C636755726^7' +'AE0C637755726^7' +'AE0C638755726^7' +'AE0C639755726^7' +'AE0C63A755726^7' +'AE0C63B755726^7' +'AE0C63C755726^7' +'AE0C63D755726^7' +'AE0C63E755726^7' +'AE0C63F755726^7' +'AE0C640755726^7' +'AE0C641755726^7' +'AE0C642755726^7' +'AE0C643755726^7' +'AE0C644755726^7' +'AE0C645755726^7' +'AE0C646755726^7' +'AE0C64775159D^7' +'AE0C64875159D^7' +'AE0C64975159D^7' +'AE0C64A75159D^7' +'AE0C64B75159D^7' +'AE0C64C75159D^7' +'AE0C64D75159D^7' +'AE0C64E75159D^7' +'AE0C64F75159D^7' +'AE0C65075159D^7' +'AE0C65175159D^7' +'AE0C65275159D^7' +'AE0C65375159D^7' +'AE0C65475159D^7' +'AE0C65575159D^7' +'AE0C65675159D^7' +'AE0C5B2761BC2^7' +'AE0C6167598AF8^7' +'1^1' +'108^3' +END_ARRAY 2 1852 +BEGIN_ARRAY 3 39 +'DE-0403LE-0403 ' +'AE0C54FDDC9D6^7' +'AE0C65630BB8^7' +'A' +'0' +'1' +'2' +39 +'ADFB74^7' +'A8C^5' +'94A1D96FDC9538^5' +'-9DFA14C450E87^3' +'-10A6F90CC55C8E^2' +'1A8DB36D7919A4^0' +'-DBA82D668F68^-2' +'1943E04814A3A9^-3' +'2D2DBBB0F8889A^-4' +'-13328359B6AFED^-5' +'2D4395828FC13A^-6' +'-166EB5C923E47F^-6' +'-50E6C5C4989A2^-8' +'3A64FEEA808364^5' +'1C038412106FEF^4' +'-9BB7059785BE3^1' +'1869B5AA252882^0' +'934A2C3016BD4^-2' +'-56AB4C415E9828^-3' +'595353E6116C3C^-4' +'-6E4C3AE2B464E^-6' +'6454B33CA4F478^-6' +'-E159348A215B38^-7' +'-8B8F3AF4B6392^-8' +'14ABA56F833013^5' +'C116B04BE71DE8^3' +'-3E3EECFB165A0E^1' +'8BF8BF3538E55^-1' +'50D54F66499DF4^-2' +'-2CBDB1CB1D95C2^-3' +'2CD23EAB3A0576^-4' +'-1CDE56A5F1B23D^-6' +'30DE3A636A3FE2^-6' +'-4C3AEEAC5F8958^-7' +'-42223050A58024^-8' +'AD52B4^7' +'1518^6' +'23^2' +'1^1' +END_ARRAY 3 39 +TOTAL_ARRAYS 3 + ~NAIF/SPC BEGIN COMMENTS~ +; ../../../data/isistestdata/hayabusa/out/st_2458542208_v.ale_1.bsp LOG FILE + +; Created 2023-02-16/02:11:29.00. +; +; BEGIN SPKMERGE COMMANDS + +LEAPSECONDS_KERNEL = ../../../remotedata/isis_data/base/kernels/lsk/naif0012.tls + +SPK_KERNEL = ../../../data/isistestdata/hayabusa/out/st_2458542208_v.ale_1.bsp +SOURCE_SPK_KERNEL = ../../../remotedata/isis_data/hayabusa/kernels/tspk/sb_25143_140.bsp + INCLUDE_COMMENTS = NO + BODIES = 2025143 + BEGIN_TIME = 2005 OCT 13 19:11:11.684 + END_TIME = 2005 OCT 13 19:15:34.008 +SOURCE_SPK_KERNEL = ../../../remotedata/isis_data/hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp + INCLUDE_COMMENTS = NO + BODIES = -130 + BEGIN_TIME = 2005 OCT 13 19:11:11.684 + END_TIME = 2005 OCT 13 19:15:34.008 +SOURCE_SPK_KERNEL = ../../../remotedata/isis_data/hayabusa/kernels/tspk/de403s.bsp + INCLUDE_COMMENTS = NO + BODIES = 10 + BEGIN_TIME = 2005 OCT 13 19:11:11.684 + END_TIME = 2005 OCT 13 19:15:34.008 + +; END SPKMERGE COMMANDS + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/st_2458542208_v/st_2458542208_v_isis.lbl b/tests/pytests/data/st_2458542208_v/st_2458542208_v_isis.lbl new file mode 100644 index 0000000000000000000000000000000000000000..017f3de4350bdff66f204225631c98b828c08ae0 --- /dev/null +++ b/tests/pytests/data/st_2458542208_v/st_2458542208_v_isis.lbl @@ -0,0 +1,385 @@ +Object = IsisCube + Object = Core + StartByte = 65537 + Format = Tile + TileSamples = 512 + TileLines = 512 + + Group = Dimensions + Samples = 1024 + Lines = 1024 + Bands = 1 + End_Group + + Group = Pixels + Type = Real + ByteOrder = Lsb + Base = 0.0 + Multiplier = 1.0 + End_Group + End_Object + + Group = Instrument + SpacecraftName = HAYABUSA + InstrumentId = AMICA + SpacecraftClockStartCount = 2457499394 <1/32sec> + SpacecraftClockStopCount = 2457499873 <1/32sec> + StartTime = 2005-10-13T19:13:11 + StopTime = 2005-10-13T19:13:11 + ExposureDuration = .0218 <SECOND> + TargetName = ITOKAWA + TargetType = ASTEROID + OriginalTargetName = "25143 ITOKAWA" + Binning = 1 + FirstLine = 0 + LastLine = 1023 + FirstSample = 0 + LastSample = 1023 + CcdTemperature = -26.86 + End_Group + + Group = Archive + FileName = st_2458542208_v.fit + DataSetId = HAY-A-AMICA-3-HAYAMICA-V1.0 + ProductId = 20051013_ST_2458542208_V_FIT + ProductName = 20051013:ST_2458542208_V.FIT + ProductCreationTime = 2008-04-08 + SubImageCount = 2 + Image1Number = 34 + DataType = SCIENCE + OutputMode = LOSSY + OperationType = MEAN + LutNumber = 0 + QualityFlag = 0 + QualityDesc = GOOD + YearDoy = 2005286 + End_Group + + Group = BandBin + OriginalBand = 1 + Name = V + Number = 3 + Center = 553 <nanometers> + Width = 72 <nanometers> + Unit = Nanometers + End_Group + + Group = Kernels + NaifFrameCode = -130102 + LeapSecond = $base/kernels/lsk/naif0012.tls + TargetAttitudeShape = ($base/kernels/pck/pck00009.tpc, + $hayabusa/kernels/pck/itokawa_gaskell_n3.tpc) + TargetPosition = (Table, $hayabusa/kernels/tspk/de403s.bsp, + $hayabusa/kernels/tspk/sb_25143_140.bsp) + InstrumentPointing = (Table, + $hayabusa/kernels/ck/hayabusa_itokawarendezvo- + us_v02n.bc, + $hayabusa/kernels/fk/hayabusa_hp.tf, + $hayabusa/kernels/fk/itokawa_fixed.tf) + Instrument = $hayabusa/kernels/ik/amica31.ti + SpacecraftClock = $hayabusa/kernels/sclk/hayabusa.tsc + InstrumentPosition = (Table, + $hayabusa/kernels/spk/hay_jaxa_050916_051119_- + v1n.bsp, + $hayabusa/kernels/spk/hay_osbj_050911_051118_- + v1n.bsp) + InstrumentAddendum = $hayabusa/kernels/iak/amicaAddendum002.ti + ShapeModel = Null + InstrumentPositionQuality = Reconstructed + InstrumentPointingQuality = Reconstructed + CameraVersion = 1 + Source = isis + End_Group +End_Object + +Object = Label + Bytes = 65536 +End_Object + +Object = Table + Name = InstrumentPointing + StartByte = 4265673 + Bytes = 64 + Records = 1 + ByteOrder = Lsb + TimeDependentFrames = (-130000, 1) + ConstantFrames = (-130102, -130101, -130000) + ConstantRotation = (0.0066354810266741, 0.99997566485661, + 0.0021540859158883, 0.99997683210906, + -0.0066321870038765, -0.0015327559101681, + -0.0015184323097167, 0.0021642065830212, + -0.99999650528049) + CkTableStartTime = 182502855.87768 + CkTableEndTime = 182502855.87768 + CkTableOriginalSize = 1 + FrameTypeCode = 3 + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/ck/hayabusa_itokawarendezvous_v02n- + .bc, $hayabusa/kernels/fk/hayabusa_hp.tf, + $hayabusa/kernels/fk/itokawa_fixed.tf) + + Group = Field + Name = J2000Q0 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = Table + Name = InstrumentPosition + StartByte = 4265737 + Bytes = 56 + Records = 1 + ByteOrder = Lsb + CacheType = Linear + SpkTableStartTime = 182502855.87768 + SpkTableEndTime = 182502855.87768 + SpkTableOriginalSize = 1.0 + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/spk/hay_jaxa_050916_051119_v1n.bs- + p, + $hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp) + + Group = Field + Name = J2000X + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Y + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Z + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000XV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000YV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000ZV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = Table + Name = BodyRotation + StartByte = 4265793 + Bytes = 64 + Records = 1 + ByteOrder = Lsb + TimeDependentFrames = (2025143, 1) + CkTableStartTime = 182502855.87768 + CkTableEndTime = 182502855.87768 + CkTableOriginalSize = 1 + FrameTypeCode = 2 + PoleRa = (90.02564, 0.0, 0.0) + PoleDec = (-67.02704, 0.0, 0.0) + PrimeMeridian = (129.73, 712.1437611, 0.0) + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/tspk/de403s.bsp, + $hayabusa/kernels/tspk/sb_25143_140.bsp, + $base/kernels/pck/pck00009.tpc, + $hayabusa/kernels/pck/itokawa_gaskell_n3.tpc) + SolarLongitude = 126.31213271325 + + Group = Field + Name = J2000Q0 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = Table + Name = SunPosition + StartByte = 4265857 + Bytes = 56 + Records = 1 + ByteOrder = Lsb + CacheType = Linear + SpkTableStartTime = 182502855.87768 + SpkTableEndTime = 182502855.87768 + SpkTableOriginalSize = 1.0 + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/tspk/de403s.bsp, + $hayabusa/kernels/tspk/sb_25143_140.bsp) + + Group = Field + Name = J2000X + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Y + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Z + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000XV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000YV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000ZV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = History + Name = IsisCube + StartByte = 4265913 + Bytes = 1357 +End_Object + +Object = OriginalLabel + Name = IsisCube + StartByte = 4260310 + Bytes = 5363 +End_Object + +Object = NaifKeywords + BODY_CODE = 2025143 + BODY2025143_RADII = (0.274, 0.156, 0.138) + BODY_FRAME_CODE = 2025143 + INS-130102_SWAP_OBSERVER_TARGET = TRUE + INS-130102_LIGHTTIME_CORRECTION = NONE + INS-130102_LT_SURFACE_CORRECT = FALSE + INS-130102_FOCAL_LENGTH = 0.1208 + INS-130102_PIXEL_PITCH = 0.012 + CLOCK_ET_-130_2457499394_COMPUTED = 90cabb8f8bc1a541 + INS-130102_TRANSX = (0.0, 0.012, 0.0) + INS-130102_TRANSY = (0.0, 0.0, -0.012) + INS-130102_ITRANSS = (0.0, 83.33333333, 0.0) + INS-130102_ITRANSL = (0.0, 0.0, -83.33333333) + INS-130102_BORESIGHT_LINE = 511.5 + INS-130102_BORESIGHT_SAMPLE = 511.5 + INS-130102_OD_K = (0.0, 2.8e-05, 0.0) +End_Object +End diff --git a/tests/pytests/test_hayabusa_drivers.py b/tests/pytests/test_hayabusa_drivers.py new file mode 100644 index 0000000000000000000000000000000000000000..2da7df85fd3efa87785d4cb095bcd467b2249fb7 --- /dev/null +++ b/tests/pytests/test_hayabusa_drivers.py @@ -0,0 +1,44 @@ +import pytest +import numpy as np +import os +import unittest +from unittest.mock import MagicMock, PropertyMock, patch +import spiceypy as spice +import json + +from conftest import get_image, get_image_label, get_isd, get_image_kernels, convert_kernels, compare_dicts +import ale +from ale.drivers.hayabusa_drivers import HayabusaAmicaIsisLabelNaifSpiceDriver +from ale import util + + +@pytest.fixture(scope='module') +def test_amica_kernels(): + kernels = get_image_kernels('st_2458542208_v') + updated_kernels, binary_kernels = convert_kernels(kernels) + yield updated_kernels + for kern in binary_kernels: + os.remove(kern) + +def test_amica_load(test_amica_kernels): + label_file = get_image_label('st_2458542208_v', 'isis') + compare_dict = get_isd("hayabusaamica") + + isd_str = ale.loads(label_file, props={'kernels': test_amica_kernels}) + isd_obj = json.loads(isd_str) + assert compare_dicts(isd_obj, compare_dict) == [] + + +class test_nac_isis_naif(unittest.TestCase): + def setUp(self): + label = get_image_label("st_2458542208_v", "isis") + self.driver = HayabusaAmicaIsisLabelNaifSpiceDriver(label) + + def test_instrument_id(self): + assert self.driver.instrument_id == "HAYABUSA_AMICA" + + def test_sensor_model_version(self): + assert self.driver.sensor_model_version == 1 + + def test_sensor_name(self): + assert self.driver.sensor_name == "HAYABUSA_AMICA"