diff --git a/ale/drivers/mro_drivers.py b/ale/drivers/mro_drivers.py
index c1dfe4284939c89f41a3f51bd372b9f025d95fb0..1ad771d3e691b9dfc2f4cd85ffdb71af173fa5c5 100644
--- a/ale/drivers/mro_drivers.py
+++ b/ale/drivers/mro_drivers.py
@@ -1,8 +1,3 @@
-from glob import glob
-import os
-
-import numpy as np
-import pvl
import spiceypy as spice
from ale.base import Driver
diff --git a/ale/drivers/voyager_drivers.py b/ale/drivers/voyager_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..7b37fe3e7e574db18c6405992703b18f1e17fe42
--- /dev/null
+++ b/ale/drivers/voyager_drivers.py
@@ -0,0 +1,46 @@
+import spiceypy as spice
+
+import ale
+from ale.base.data_naif import NaifSpice
+from ale.base.label_isis import IsisLabel
+from ale.base.type_sensor import Framer
+from ale.base.base import Driver
+
+class Voyager2IssnacIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
+
+ @property
+ def sensor_model_version(self):
+ return 1
+
+ @property
+ def ikid(self):
+ return self.label['IsisCube']['Kernels']['NaifFrameCode']
+
+ @property
+ def spacecraft_name(self):
+ return super().spacecraft_name.replace('_', ' ')
+
+ @property
+ def pixel_size(self):
+ return spice.gdpool('INS{}_PIXEL_PITCH'.format(self.ikid), 0, 1)[0]
+
+ @property
+ def detector_center_sample(self):
+ return 499.5
+
+ @property
+ def detector_center_line(self):
+ return 499.5
+
+ @property
+ def ephemeris_start_time(self):
+ inital_time = spice.utc2et(self.utc_start_time.isoformat())
+ # To get shutter end (close) time, subtract 2 seconds from the start time
+ updated_time = inital_time - 2
+ # To get shutter start (open) time, take off the exposure duration from the end time.
+ start_time = updated_time - self.exposure_duration
+ return start_time
+
+ @property
+ def ephemeris_stop_time(self):
+ return self.ephemeris_start_time + self.exposure_duration
diff --git a/ale/formatters/isis_formatter.py b/ale/formatters/isis_formatter.py
index 019a3712889efb193db0af22aa87619e1281b34f..9ee2bd4c54fed1ab4eb6ff3d1a00b9f3ffde1d0b 100644
--- a/ale/formatters/isis_formatter.py
+++ b/ale/formatters/isis_formatter.py
@@ -26,6 +26,7 @@ def to_isis(driver):
frame_chain = driver.frame_chain
sensor_frame = driver.sensor_frame_id
+ target_frame = driver.target_frame_id
instrument_pointing = {}
source_frame, destination_frame, time_dependent_sensor_frame = frame_chain.last_time_dependent_frame_between(sensor_frame, 1)
@@ -39,7 +40,7 @@ def to_isis(driver):
instrument_pointing['CkTableEndTime'] = time_dependent_rotation.times[-1]
instrument_pointing['CkTableOriginalSize'] = len(time_dependent_rotation.times)
instrument_pointing['EphemerisTimes'] = time_dependent_rotation.times
- instrument_pointing['Quaternions'] = time_dependent_rotation.quats
+ instrument_pointing['Quaternions'] = time_dependent_rotation.quats[:, [3, 0, 1, 2]]
if source_frame != sensor_frame:
# Reverse the frame order because ISIS orders frames as
@@ -62,7 +63,7 @@ def to_isis(driver):
body_rotation['CkTableEndTime'] = time_dependent_rotation.times[-1]
body_rotation['CkTableOriginalSize'] = len(time_dependent_rotation.times)
body_rotation['EphemerisTimes'] = time_dependent_rotation.times
- body_rotation['Quaternions'] = time_dependent_rotation.quats
+ body_rotation['Quaternions'] = time_dependent_rotation.quats[:, [3, 0, 1, 2]]
if source_frame != target_frame:
# Reverse the frame order because ISIS orders frames as
@@ -72,13 +73,18 @@ def to_isis(driver):
body_rotation['ConstantRotation'] = constant_rotation.rotation_matrix()
meta_data['BodyRotation'] = body_rotation
+ j2000_rotation = frame_chain.compute_rotation(target_frame, 1)
+
instrument_position = {}
positions, velocities, times = driver.sensor_position
instrument_position['SpkTableStartTime'] = times[0]
instrument_position['SpkTableEndTime'] = times[-1]
instrument_position['SpkTableOriginalSize'] = len(times)
instrument_position['EphemerisTimes'] = times
+ # Rotate positions and velocities into J2000 then scale into kilometers
+ positions = j2000_rotation._rots.apply(positions) * 1/1000
instrument_position['Positions'] = positions
+ velocities = j2000_rotation._rots.apply(velocities) * 1/1000
instrument_position['Velocities'] = velocities
meta_data['InstrumentPosition'] = instrument_position
@@ -88,7 +94,10 @@ def to_isis(driver):
sun_position['SpkTableEndTime'] = times[-1]
sun_position['SpkTableOriginalSize'] = len(times)
sun_position['EphemerisTimes'] = times
+ # Rotate positions and velocities into J2000 then scale into kilometers
+ positions = j2000_rotation._rots.apply(positions) * 1/1000
sun_position['Positions'] = positions
+ velocities = j2000_rotation._rots.apply(velocities) * 1/1000
sun_position['Velocities'] = velocities
meta_data['SunPosition'] = sun_position
diff --git a/tests/pytests/conftest.py b/tests/pytests/conftest.py
index 2a6771a5d6efd4fadc9c868586b6c3d7b5650c46..4456088f2cd397b21b9b7104f6429a275bdd6b33 100644
--- a/tests/pytests/conftest.py
+++ b/tests/pytests/conftest.py
@@ -53,11 +53,16 @@ def compare_dicts(ldict, rdict):
elif isinstance(item, dict):
differences.extend(compare_dicts(item, rdict[key]))
elif isinstance(item, np.ndarray) or isinstance(item, list):
- if not np.allclose(item, rdict[key]):
+ if len(item) != len(rdict[key]):
+ differences.append(f'Array sizes of key {key} are not equal {item} : {rdict[key]}.')
+ elif not np.allclose(item, rdict[key]):
differences.append(f'Array values of key {key} are not almost equal {item} : {rdict[key]}.')
elif isinstance(item, str):
if item.lower() != rdict[key].lower():
differences.append(f'Values of key {key} are not equal {item} : {rdict[key]}.')
+ elif isinstance(item, float):
+ if not np.isclose(item, rdict[key]):
+ differences.append(f'Floating point values of key {key} are not close {item} : {rdict[key]}.')
else:
if item != rdict[key]:
differences.append(f'Values of key {key} are not equal {item} : {rdict[key]}.')
diff --git a/tests/pytests/data/c2065022/c2065022.spice_0.xsp b/tests/pytests/data/c2065022/c2065022.spice_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..758b13831b53724134dea574a86ccb4e077223ba
--- /dev/null
+++ b/tests/pytests/data/c2065022/c2065022.spice_0.xsp
@@ -0,0 +1,313 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 73
+'vgr2.jup230.nio '
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+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/acpaquette/kernel_split/c2065022.spice_0.bsp LOG FILE
+
+; Created 2019-09-04/15:36:34.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/acpaquette/kernel_split/c2065022.spice_0.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager2/kernels/spk//vgr2_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -32
+ BEGIN_TIME = 1979 JUL 09 14:27:35.688
+ END_TIME = 1979 JUL 09 14:29:25.095
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 502
+ BEGIN_TIME = 1979 JUL 09 14:27:35.688
+ END_TIME = 1979 JUL 09 14:29:25.095
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065022/c2065022.spice_1.xsp b/tests/pytests/data/c2065022/c2065022.spice_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..1656fdce61c736d32a8efb8383620cd38ccb8890
--- /dev/null
+++ b/tests/pytests/data/c2065022/c2065022.spice_1.xsp
@@ -0,0 +1,313 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 73
+'vgr2.jup230.nio '
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+'B813BB9FA07548^3'
+'73C1462D5A2244^1'
+'130D073312C932^-1'
+'97B4324F027A48^-3'
+'-6BF0B6117C3F6^-3'
+'58A2170564FEB4^-4'
+'-1068A5CDA2F449^-5'
+'-5AD2225860DF2^-6'
+'12F5C65C962E3E^-6'
+'-2252526866C9AA^-7'
+'-269B14C^8'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 2 39
+BEGIN_ARRAY 3 30
+'DE-0431LE-0431 '
+'-26867853D64DCA^8'
+'-268677E9D64DCC^8'
+'5'
+'0'
+'1'
+'2'
+30
+'-2685FCC^8'
+'1518^6'
+'-23095B332579FA^8'
+'-BD0582AF46C1A^6'
+'11F8B950533C7D^5'
+'E0CF1ED698767^2'
+'-DE910C6039DAB8^0'
+'-D0EC0A68256368^-3'
+'2EABE8DE25B6AA^-4'
+'C5A62EF855D028^-6'
+'1D1D34F9A2E441^8'
+'-B1003A8467DEE8^6'
+'-EEC155443E2CE^4'
+'10DD92E3CBAEA3^3'
+'68E3D00022799^0'
+'-79F7AC590D0B54^-2'
+'3AD219638752D^-4'
+'5C987F0EEBA05^-6'
+'D55803DFEFB728^7'
+'-47450EAF2DCFF4^6'
+'-6D5AB1CF7571C8^4'
+'6E33FF1B5945B^2'
+'3264EC9678848C^0'
+'-33FB4F3A7AECDA^-2'
+'17333AFBD6BF22^-4'
+'2A595FECAAF3EA^-6'
+'-269B14C^8'
+'2A3^6'
+'1A^2'
+'1^1'
+END_ARRAY 3 30
+BEGIN_ARRAY 4 102
+'JUP310 '
+'-26867853D64DCA^8'
+'-268677E9D64DCC^8'
+'1F6'
+'5'
+'1'
+'3'
+102
+'-2686A58^8'
+'A8C^4'
+'80928DA8D49C48^5'
+'1A96D3AD15B1FF^5'
+'-1DD13A955C794E^5'
+'-F42565138B14D^3'
+'8600FC63A15AA^3'
+'2E359A8A2A6A^2'
+'-10F860113328^2'
+'-5F453D12F^0'
+'1AD15E13E^0'
+'A57AEA6E^-2'
+'-30C6904C^-2'
+'560B1EA^-3'
+'11E29E8^-3'
+'-EEEAC6^-4'
+'-3D4A48^-4'
+'22819^-4'
+'-18730B7666B72D^5'
+'7485590CE627A^5'
+'5A6A3A2E4E758^4'
+'-4174BDE7E297D8^4'
+'-1A7CBD49468ADC^3'
+'B746D05E3BAC^2'
+'3E2A1BCC211^1'
+'-136638FC9E^1'
+'-92491EAD^-1'
+'221601778^-1'
+'3179DB99^-2'
+'-471D2F8^-3'
+'-37C04^-3'
+'-40183^-4'
+'666966^-4'
+'1B2E08^-4'
+'-ACE8560407FC9^4'
+'382C29EC88D498^5'
+'27F4863216E25C^4'
+'-1F8EB6F1928054^4'
+'-BBFA4E9BFF61E^2'
+'58629BD36D6E^2'
+'1BE7BB88EB4^1'
+'-95C23E6648^0'
+'-438526F52^-1'
+'1053B1248^-1'
+'17D969F6C^-2'
+'-1D2A548^-3'
+'-1B04FC2^-3'
+'-29953C^-4'
+'3044E4^-4'
+'EBCBC^-5'
+'2414BC048F2984^1'
+'-AEA867604BB03^1'
+'-882F2B0F9C844^0'
+'64728DE93EA83^0'
+'2B52E4C49EDFC2^-1'
+'-13269A93F868AD^-1'
+'-7D52BC7C11111^-3'
+'28546E8856789A^-3'
+'123B83C5C28F5C^-4'
+'-5A95C1CEB24078^-5'
+'94CDC0DA740DA^-6'
+'1E877A4FA4FA5^-6'
+'-1EAD2FC3518A6E^-6'
+'-A2B6CA8641FDB8^-7'
+'622693E93E93E4^-7'
+'0^0'
+'9E7BF3CED5C448^1'
+'210D54DAF7665A^1'
+'-24908BD4F06EB^1'
+'-13D16EC42CD0A1^0'
+'AC2D9288826EB8^-1'
+'45E23BA79A375C^-2'
+'-1986A05EF08B91^-2'
+'-D87C6F4CD2DE4^-4'
+'39930050AFF9EC^-4'
+'56F445B302A7A^-5'
+'-9961C2F0734B7^-6'
+'-6DDF26D3A06D38^-6'
+'-50B17CC6BB5AA^-7'
+'10FE256789ABCE^-6'
+'4D4FBBBBBBBBB8^-7'
+'0^0'
+'4C66CFD04FC0C4^1'
+'E9AA34D6FD888^0'
+'-11A0DBC7C72359^1'
+'-8C9FE68E36C6B8^-1'
+'53084FDF433D6C^-1'
+'1F5C2AD53F17E5^-2'
+'-C510AC853A06D8^-3'
+'-63D0162E6AF37C^-4'
+'1B9CB7A02468AC^-4'
+'29E2120474CFD4^-5'
+'-409FA8641FDB94^-6'
+'-3579A7A1F1969^-6'
+'-3C97240795CEB^-7'
+'8025419CA252B^-7'
+'29EB5555555554^-7'
+'0^0'
+'-26874E4^8'
+'1518^5'
+'62^2'
+'1^1'
+END_ARRAY 4 102
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/acpaquette/kernel_split/c2065022.spice_1.bsp LOG FILE
+
+; Created 2019-09-04/15:36:34.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/acpaquette/kernel_split/c2065022.spice_1.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager2/kernels/spk//vgr2_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -32
+ BEGIN_TIME = 1979 JUL 09 15:11:53.979
+ END_TIME = 1979 JUL 09 15:13:39.979
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 502
+ BEGIN_TIME = 1979 JUL 09 15:11:53.979
+ END_TIME = 1979 JUL 09 15:13:39.979
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065022/c2065022_isis3.lbl b/tests/pytests/data/c2065022/c2065022_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..3c4a8f5572994aebc9fc841df25441d92e44e189
--- /dev/null
+++ b/tests/pytests/data/c2065022/c2065022_isis3.lbl
@@ -0,0 +1,139 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 800
+ TileLines = 800
+
+ Group = Dimensions
+ Samples = 800
+ Lines = 800
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftClockCount = 2065022
+ SpacecraftName = VOYAGER_2
+ TargetName = Europa
+ StartTime = 1979-07-09T15:11:58.979
+ InstrumentId = NARROW_ANGLE_CAMERA
+ ScanModeId = 2:1
+ ShutterModeId = BOTALT
+ GainModeId = LOW
+ EditModeId = 1:1
+ ExposureDuration = 0.1200 <seconds>
+ CameraState1 = 2
+ CameraState2 = 0
+ End_Group
+
+ Group = Archive
+ MissionPhaseName = JUPITER_ENCOUNTER
+ ProductId = 1255J2-001
+ End_Group
+
+ Group = BandBin
+ FilterName = CLEAR
+ FilterNumber = 0
+ Center = 0.460000 <micrometers>
+ Width = 0.360000 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -32101
+ End_Group
+
+ Group = Reseaus
+ Line = (12.6, 7.0, 4.0, -1.2, -4.6, -6.3, -8.0, -8.6, -8.9, -8.2,
+ -10.0, -3.2, 22.9, 26.0, 22.0, 18.0, 17.0, 15.0, 14.0, 13.0,
+ 13.0, 14.0, 8.0, 58.0, 55.1, 51.0, 48.0, 46.0, 44.0, 43.0,
+ 42.0, 41.0, 41.0, 43.0, 44.0, 94.0, 90.0, 88.0, 85.0, 84.0,
+ 82.0, 81.0, 81.0, 80.0, 81.0, 81.0, 131.9, 130.0, 118.7, 120.0,
+ 169.9, 167.1, 164.8, 164.0, 161.8, 160.7, 159.9, 160.0, 158.5,
+ 159.0, 159.0, 208.5, 208.0, 197.6, 197.6, 247.6, 245.5, 243.8,
+ 242.6, 241.6, 240.6, 239.9, 239.2, 238.4, 237.7, 237.3, 286.8,
+ 286.0, 277.2, 276.7, 326.4, 324.7, 323.3, 322.3, 321.5, 320.6,
+ 320.0, 319.3, 318.5, 317.5, 316.9, 366.0, 365.2, 357.0, 356.5,
+ 405.6, 404.2, 403.0, 402.1, 401.3, 400.6, 399.9, 399.1, 398.3,
+ 397.4, 396.4, 445.2, 444.6, 436.4, 435.6, 485.0, 483.7, 482.8,
+ 481.9, 481.1, 480.4, 479.6, 478.9, 478.0, 476.8, 475.5, 524.4,
+ 524.2, 515.6, 514.6, 564.4, 563.3, 562.4, 561.6, 560.8, 560.0,
+ 559.3, 558.4, 557.4, 556.0, 554.3, 603.5, 603.5, 593.0, 592.6,
+ 643.1, 642.5, 641.0, 641.0, 640.2, 638.0, 637.0, 636.0, 635.0,
+ 634.4, 630.0, 682.0, 682.0, 671.0, 669.3, 720.6, 720.9, 720.0,
+ 719.0, 718.0, 717.0, 716.0, 714.0, 712.0, 710.0, 706.0, 757.7,
+ 759.1, 758.0, 758.0, 757.0, 756.0, 755.0, 753.0, 752.0, 750.0,
+ 746.0, 743.4, 795.4, 787.0, 787.0, 786.0, 785.0, 784.0, 783.0,
+ 782.0, 780.0, 776.0, 778.0, 804.0, 810.7, 808.5, 808.5, 808.0,
+ 807.4, 806.1, 805.0, 801.0, 798.0, 798.5, 787.0, 120.0)
+ Sample = (0.4, 44.0, 119.0, 199.9, 278.0, 356.1, 433.9, 511.6, 588.5,
+ 664.1, 737.1, 784.4, 6.0, 81.0, 158.0, 236.0, 314.0, 393.0,
+ 471.0, 549.9, 626.3, 702.0, 772.0, -5.8, 43.0, 120.0, 199.0,
+ 276.0, 355.0, 433.0, 512.0, 589.0, 666.0, 740.0, 792.0, 15.0,
+ 81.0, 159.0, 238.0, 317.0, 395.0, 474.0, 551.0, 629.0, 705.0,
+ 769.0, -4.6, 43.0, 744.1, 793.0, 15.3, 82.3, 159.0, 238.0,
+ 318.1, 396.7, 475.2, 553.3, 631.0, 707.7, 773.5, -5.3, 43.0,
+ 746.8, 795.7, 15.3, 82.4, 160.8, 239.0, 318.0, 397.4, 475.9,
+ 554.3, 632.3, 709.6, 775.7, -5.1, 43.9, 748.7, 797.8, 15.6,
+ 82.9, 161.3, 240.1, 319.0, 397.8, 476.4, 555.0, 633.2, 710.9,
+ 777.5, -4.6, 44.4, 749.8, 799.3, 16.4, 83.4, 161.7, 240.4,
+ 319.3, 398.1, 476.9, 555.5, 633.8, 711.7, 778.5, -3.8, 45.3,
+ 750.4, 801.8, 17.5, 84.4, 162.3, 240.9, 319.7, 398.4, 477.2,
+ 555.9, 634.3, 712.3, 779.2, -2.3, 46.4, 751.0, 799.8, 19.0,
+ 85.4, 163.0, 241.4, 320.0, 398.9, 477.5, 556.4, 634.7, 712.7,
+ 779.4, -0.5, 48.0, 752.0, 800.0, 21.3, 86.9, 163.9, 242.0,
+ 320.6, 401.0, 479.0, 558.0, 636.0, 712.7, 778.0, 2.6, 50.4,
+ 752.0, 799.5, 26.0, 89.2, 166.0, 243.0, 322.0, 401.0, 480.0,
+ 559.0, 637.0, 714.0, 778.0, 4.5, 54.0, 129.0, 206.0, 284.0,
+ 362.0, 441.0, 519.0, 598.0, 675.0, 751.0, 800.0, 22.2, 93.0,
+ 168.0, 245.0, 323.0, 402.0, 481.0, 559.0, 637.0, 713.0, 785.0,
+ 11.0, 56.6, 129.6, 205.8, 283.3, 361.5, 439.8, 518.3, 599.0,
+ 675.6, 748.7, 794.0, 591.0)
+ Type = (5, 5, 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 0, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 5, 5, 5)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $voyager2/reseaus/vg2.issna.template.cub
+ Status = Nominal
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 705537
+ Bytes = 454
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 705991
+ Bytes = 2029
+End_Object
+End
diff --git a/tests/pytests/data/c2065022/naif0012.tls b/tests/pytests/data/c2065022/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/c2065022/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/c2065022/pck00008.tpc b/tests/pytests/data/c2065022/pck00008.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..cd1592038973a4d9b22412d031e735454ffcb32b
--- /dev/null
+++ b/tests/pytests/data/c2065022/pck00008.tpc
@@ -0,0 +1,3415 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "pck00008.tpc"
+MISSION_NAME = "MARS RECONNAISSANCE ORBITER"
+SPACECRAFT_NAME = "MARS RECONNAISSANCE ORBITER"
+DATA_SET_ID = "MRO-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = PCK
+PRODUCT_ID = "pck00008.tpc"
+PRODUCT_CREATION_TIME = 2007-06-05T13:50:45
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+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 = "Generic SPICE PCK file containing constants
+from the IAU 2000 report, created by NAIF, JPL. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2004 September 21
+
+
+File Organization
+--------------------------------------------------------
+
+ The contents of this file are as follows.
+
+ Introductory Information:
+
+ -- File Organization
+
+ -- Version description
+
+ -- Disclaimer
+
+ -- Sources
+
+ -- Explanation
+
+ -- 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 Gaspra, Ida,
+ Vesta, and Eros
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Gaspra, Ida, Kleopatra, and Eros
+
+
+
+Version description
+--------------------------------------------------------
+
+ This file was created on September 21, 2004. This version
+ incorporates data from reference [2]: "Report of the IAU/IAG
+ Working Group on Cartographic Coordinates and Rotational Elements
+ of the Planets and Satellites: 2000." Note that the 2003
+ version of this report is as yet unpublished.
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, plus data
+ for the asteroids Vesta, Kleopatra, and Eros.
+
+
+Disclaimer
+--------------------------------------------------------
+
+
+Applicability of Data
+
+ This constants file may not contain the parameter values that
+ you prefer. Note that this file may be readily modified by
+ you or anyone else. NAIF suggests that you inspect this file
+ visually before proceeding with any critical or extended
+ data processing.
+
+File Modifications by Users
+
+ NAIF requests that you update the "by line" and date if you
+ modify this file.
+
+Known Limitations and Caveats
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG Working Group Report [2] to be accurate to 0.1 degree
+ ([2], p.85). 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.
+
+
+ NAIF strongly cautions against using the earth rotation model
+ (from [2]) given here 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 section 335 produces a new
+ earth orientation parameter (EOP) file, a new PCK is produced.
+ These PCKs cover a 12-month time span starting about nine
+ months prior to the current date. 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 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 back to 1972
+ and *low accuracy* predicted earth orientation to 2023 are also
+ available in the same location.
+
+ How does the rotation model used in the long term predict
+ binary earth PCK compare to that used in this file? Because of
+ the unpredictability of the earth's orientation, in particular
+ of its spin, it's not possible to answer with certainty.
+ However, we can make these observations:
+
+ - The long term predict binary PCK presumably does a better
+ job of predicting the orientation of the earth's equator
+ since the binary PCK accounts for nutation and the model
+ from [2] does not.
+
+ - The prime meridian error in the model from [2] amounts
+ to, at a minimum, about 10 seconds of rotation. It should
+ take years for the spin error of the binary long term
+ predict PCK to grow as large.
+
+ Characteristics and names of the binary kernels described here
+ are subject to change. Contact NAIF for details concerning
+ binary earth PCKs.
+
+
+ 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 the geomagnetic field model
+ from which these values were derived, including a discussion of
+ the model's accuracy, see [13].
+
+
+ The Mars prime meridian offset given by [10] 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.
+
+
+ SPICE Toolkits prior to version N0057 cannot make use of
+ trigonometric polynomial terms in the formulas for orientation of
+ the planets. The only planet for which such terms are used is
+ Neptune. Use of trigonometric polynomial terms for natural
+ satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+
+
+
+
+Sources
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+ [1] 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," Unpublished.
+
+ [2] Seidelmann, P.K., Abalakin, V.K., Bursa, M., Davies, M.E.,
+ Bergh, C. de, Lieske, J.H., Oberst, J., Simon, J.L.,
+ Standish, E.M., Stooke, P., and Thomas, P.C. (2002).
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2000," Celestial Mechanics and Dynamical
+ Astronomy, v.82, Issue 1, pp. 83-111.
+
+ [3] Davies, M.E., Abalakin, V.K., Bursa, M., Kinoshita, H.,
+ Kirk, R.L., Lieske, J.H., Marov, M.Ya., Seidelmann, P.K.,
+ and Simon, J.-L. "Report of the IAU/IAG/COSPAR Working
+ Group on Cartographic Coordinates and Rotational Elements
+ of the Planets and Satellites: 1997," Unpublished.
+
+ [4] Davies, M.E., Abalakin, V.K., Bursa, M., Lieske, J.H.,
+ Morando, B., Morrison, D., Seidelmann, P.K., Sinclair,
+ A.T., Yallop, B., and Tjuflin, Y.S. (1996). "Report of
+ the IAU/IAG/COSPAR Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 1994," Celestial Mechanics and Dynamical
+ Astronomy, v.63, pp. 127-148.
+
+ [5] Davies, M.E., Abalakin, V.K., Brahic, A., Bursa, M.,
+ Chovitz., B.H., Lieske, J.H., Seidelmann, P.K.,
+ Sinclair, A.T., and Tiuflin, I.S. (1992). "Report of the
+ IAU/IAG/COSPAR Working Group on Cartographic Coordinates
+ and Rotational Elements of the Planets and Satellites:
+ 1991," Celestial Mechanics and Dynamical Astronomy,
+ v.53, no.4, pp. 377-397.
+
+ [6] 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.
+
+ [7] Nautical Almanac Office, United States Naval Observatory
+ and H.M. Nautical Almanac Office, Rutherford Appleton
+ Laboratory (2005). "The Astronomical Almanac for
+ the Year 2005," U.S. Government Printing Office,
+ Washington, D.C.: and The Stationary Office, London.
+
+ [8] 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.
+
+ [9] Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+ Conventions," presentation to the Mars Express Data
+ Archive Working Group, Dec. 14, 2001.
+
+ [10] 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.
+
+ [11] Russell, C.T. (1971). "Geophysical Coordinate
+ Transformations," Cosmic Electrodynamics 2 184-186.
+ NAIF document 181.0.
+
+ [12] 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>.
+
+ [13] 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>.
+
+ [14] Duxbury, Thomas C. (1979). "Planetary Geodetic Control
+ Using Satellite Imaging," Journal of Geophysical Research,
+ vol. 84, no. B3. This paper is cataloged as NAIF
+ document 190.0.
+
+ [15] Letter from Thomas C. Duxbury to Dr. Ephraim Lazeryevich
+ Akim, Keldish Institute of Applied Mathematics, USSR
+ Academy of Sciences, Moscow, USSR. This letter is
+ cataloged as NAIF document number 195.0.
+
+ [16] "Placeholder" values were supplied by NAIF for some radii
+ of the bodies listed below:
+
+ Body NAIF ID code
+ ---- ------------
+ Metis 516
+ Helene 612
+ Larissa 807
+
+ See the discussion below for further information.
+
+
+ Most values are from [2]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [7].
+
+ -- 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.
+
+ -- For several satellites, the 2000 IAU report either gives
+ a single radius value or a polar radius and a single
+ equatorial radius. SPICE Toolkit software that uses body
+ radii expects to find three radii whenever these data are
+ read from the kernel pool. In the cases listed below,
+ NAIF has used the mean radius value for all three radii.
+ Wherever this was done, the fact has been noted.
+
+ The affected satellites are:
+
+ Body NAIF ID code
+ ---- ------------
+ Metis 516
+ Helene 612
+ Larissa 807
+
+ -- Earth north geomagnetic centered dipole values are from
+ [12]. The article [10] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [13] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [9].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ dated April 24, 2000. Most of these values came from the
+ 1994 IAU report [4].
+
+
+
+
+Explanation
+--------------------------------------------------------
+
+ The SPICE Toolkit software that uses this file is documented in
+ the SPICE "Required Reading" file pck.req. For a terse
+ description of the PCK file format, see the section below titled
+ "File Format." See the SPICE "Required Reading" file 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.
+
+ 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, and satellites. 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.
+
+
+File Format
+
+ 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 token shown
+ here 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 comment block
+ 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
+ sign 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 make the file unreadable by
+ SPICE software.
+
+
+Time systems and reference frames
+
+ The 2000 IAU/IAG Working Group Report [1] states that, to the
+ accuracy of the formulas given, the time system used may be
+ regarded as any of TDB (Barycentric Dynamical Time), TT
+ (Terrestrial time, formerly called TDT), or T_eph (the independent
+ variable of the JPL planetary ephemerides). Reference [2], from
+ which most data in this report were taken, erroneously identifies
+ the time system as TCB (Barycentric Coordinate Time).
+
+ SPICE software treats the time system used in this file as T_eph,
+ but for historical reasons SPICE documentation refers to the time
+ system as both "ET" and "TDB." For consistency, documentation in
+ this version of the file retains use of the name TDB.
+
+ The origin of the time system is 2000 January 1 12:00:00 (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.
+
+ The inertial reference frame used for the rotational elements in
+ this file is identified by [1] as the ICRF (International
+ Celestial Reference Frame). In this file, the frame is treated
+ as J2000. 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
+ body orientation. To be precise, the Euler angles 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 J2000 (also called "EME2000"), but other
+ frames can be specified in the file. See the PCK Required Reading
+ for details.
+
+ The first two angles, in order, are the J2000 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 the Sun and planets, 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. Some
+ coefficients may be zero. Currently Neptune is the only planet
+ for which trigonometric polynomial terms are used.
+
+ 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.
+
+ Example: 1991 IAU Model for orientation of the Earth. Note that
+ these values are used as an example only; see the data area below
+ for current values.
+
+
+ alpha = 0.00 - 0.641 T ( RA )
+ 0
+
+ delta = 90.0 - 0.557 T ( DEC )
+ 0
+
+ W = 190.16 + 360.9856235 d ( Prime meridian )
+
+
+ T represents centuries past J2000 ( TDB ),
+
+ d represents days past J2000 ( TDB ).
+
+ In this file, the polynomials' coefficients above are assigned to the
+ symbols
+
+ BODY399_POLE_RA
+ BODY399_POLE_DEC
+ BODY399_POLE_PM
+
+ as follows:
+
+ BODY399_POLE_RA = ( 0. -0.641 0. )
+ BODY399_POLE_DEC = ( 90. -0.557 0. )
+ BODY399_PM = ( 190.16 360.9856235 0. )
+
+ Note the number "399"; this is the NAIF ID code for the Earth.
+
+ You'll see an additional symbol grouped with the ones listed here; it
+ is
+
+ BODY399_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 and the prime meridian
+ of the body.
+
+ Expressions for satellites are a little more complicated; in addition
+ to polynomial terms, there are 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."
+
+ In this file, the polynomial expressions for the nutation precession
+ angles are listed along with the planet's RA, DEC, and prime meridian
+ terms.
+
+ Example: 1991 IAU nutation precession angles for Earth. Note that these
+ values are used as an example only; see the data area below for current
+ values.
+
+ E1 = 125.045 - 0.052992 d
+ E2 = 250.090 - 0.105984 d
+ E3 = 260.008 + 13.012001 d
+ E4 = 176.625 + 13.340716 d
+ E5 = 357.529 + 0.985600 d
+
+ d represents days past J2000 ( TDB )
+
+ Because the SPICE Toolkit software expects the time units for the
+ angles to be CENTURIES (as in the IAU models for most bodies--the
+ Earth is an exception), the linear coefficients are scaled by
+ 36525.0 (days/century) in the assignments:
+
+ BODY3_NUT_PREC_ANGLES = ( 125.045 -1935.5328
+ 250.090 -3871.0656
+ 260.008 475263.336525
+ 176.625 487269.6519
+ 357.529 35999.04 )
+
+ As stated above, the satellite orientation models use polynomial and
+ trigonometric terms, where the arguments of the trigonometric terms
+ are the "nutation precession angles."
+
+ Example: 1988 IAU values for the Moon. Again, these values are used
+ as an example only; see the data area below for current values.
+
+
+ alpha = 270.000 + 0.003 T - 3.878 sin(E1) - 0.120 sin(E2)
+ 0
+ + 0.070 sin(E3) - 0.017 sin(E4) (RA)
+
+
+ delta = 66.541 + 0.013 T + 1.543 cos(E1) + 0.024 cos(E2)
+ 0
+ - 0.028 cos(E3) + 0.007 cos(E4) (DEC)
+
+
+ W = 38.317 + 13.1763582 d + 3.558 sin(E1)
+
+ + 0.121 sin(E2)
+
+ - 0.064 sin(E3)
+
+ + 0.016 sin(E4)
+
+ + 0.025 sin(E5) ( Prime
+ meridian )
+
+ d represents days past J2000.
+
+ E1--E5 are the nutation precession angles.
+
+ The polynomial terms are assigned to symbols by the statements
+
+ BODY301_POLE_RA = ( 270.000 0.003 0. )
+ BODY301_POLE_DEC = ( 66.541 0.013 0. )
+ BODY301_PM = ( 38.317 13.1763582 0. )
+
+ The coefficients of the trigonometric terms are assigned to symbols by
+ the statements
+
+ BODY301_NUT_PREC_RA = ( -3.878 -0.120 0.070 -0.017 0. )
+ BODY301_NUT_PREC_DEC = ( 1.543 0.024 -0.028 0.007 0. )
+ BODY301_NUT_PREC_PM = ( 3.558 0.121 -0.064 0.016 0.025 )
+
+ Note that for the RA and PM (prime meridian) assignments, the ith term
+ is the coefficient of sin(Ei) in the expression used in the IAU model,
+ while for the DEC assignment, the ith term is the coefficient of
+ cos(Ei) in the expression used in the IAU model.
+
+ 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 2000 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
+
+ While not relevant to the P_constants kernel, we note here for
+ completeness that 0 is used to represent the solar system
+ barycenter.
+
+ 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
+
+
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000433 Asteroid Eros
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation constants for the Sun and planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+Mercury
+
+ Old values:
+
+ body199_pole_ra = ( 281.01, -0.033, 0. )
+ body199_pole_dec = ( 61.45, -0.005, 0. )
+ body199_pm = ( 329.55 6.1385025 0. )
+
+ body199_long_axis = ( 0. )
+
+
+ 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 2000 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 shown are from the 1994 IAU report [4].
+
+ body399_pole_ra = ( 0. -0.641 0. )
+ body399_pole_dec = ( 90. -0.557 0. )
+ body399_pm = ( 190.16 360.9856235 0. )
+ body399_long_axis = ( 0. )
+
+ Nutation precession angles are unchanged in the 2000 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 [11]. 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 [12], 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 [10], [12], and [13] 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 [12]. 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 shown are from the 1994 IAU report [4].
+
+ body499_pole_ra = ( 317.681 -0.108 0. )
+ body499_pole_dec = ( 52.886 -0.061 0. )
+ body499_pm = ( 176.901 350.8919830 0. )
+
+ Nutation precession angles are unchanged in the 2000 IAU report.
+
+ Old lambda_a values were specified as POSITIVE WEST LONGITUDE.
+ Reference [14] gave the value
+
+ body499_long_axis = ( 110. )
+
+ and reference [15] gave the value
+
+ body499_long_axis = ( 104.9194 )
+
+
+ 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 [9] 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
+ [2] gives equal values for both equatorial radii, so the
+ lambda_a offset does not apply to the IAU model.
+
+ The 2000 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:
+
+ 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
+ 352.25 +2382.6
+ 113.35 +6070.0
+ 146.64 +182945.8
+ 49.24 +90274.4 )
+
+ Current values:
+
+ The number of nutation precession angles is ten. The ninth and
+ tenth are twice the first and second, respectively.
+
+ \begindata
+
+
+ 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 )
+ \begintext
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2000 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 2000 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 2000 IAU report. However,
+ the kernel variables used to store the values have changed.
+ See note immediately below.
+
+ Current values:
+
+ The kernel variables
+
+ BODY899_NUT_PREC_RA
+ BODY899_NUT_PREC_DEC
+ BODY899_NUT_PREC_PM
+
+ are new in this PCK version (dated October 17, 2003).
+ These variables capture trigonometric terms in the expressions
+ for Neptune's pole direction and prime meridian location.
+ Version N0057 of the SPICE Toolkit uses these variables;
+ earlier versions can read them but ignore them when
+ computing Neptune's orientation.
+
+ \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 unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are from the 1988 IAU report.
+
+ body301_pole_ra = ( 270.000 0. 0. )
+ body301_pole_dec = ( 66.534 0. 0. )
+ body301_pm = ( 38.314 13.1763581 0. )
+ body301_long_axis = ( 0. )
+
+ body301_nut_prec_ra = ( -3.878 -0.120 0.070 -0.017 0. )
+ body301_nut_prec_dec = ( 1.543 0.024 -0.028 0.007 0. )
+ body301_nut_prec_pm = ( 3.558 0.121 -0.064 0.016 0.025 )
+
+ 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. 0.0072 0. 0.
+ 0. -0.0052 0. 0.
+ 0.0043 )
+
+ BODY301_NUT_PREC_DEC = ( 1.5419 0.0239 -0.0278 0.0068
+ 0. -0.0029 0.0009 0.
+ 0. 0.0008 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 )
+
+ 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 2000 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. 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 2000 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 2000 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:
+
+ 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:
+
+ body503_pole_ra = ( 268.20 -0.009 0. )
+ body503_pole_dec = ( +64.57 +0.003 0. )
+ body503_pm = ( 44.04 +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 )
+
+ 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:
+
+ body504_pole_ra = ( 268.72 -0.009 0. )
+ body504_pole_dec = ( +64.83 +0.003 0. )
+ body504_pm = ( 259.73 +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 )
+
+ 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Janus
+
+
+ Old values:
+
+ Values are unchanged in the 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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. 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 2000 report [2] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (note (j), p.99).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2000 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 2000 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 2000 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 2000 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 2000 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 2000 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 unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+Orientation constants for Asteroids Gaspra, Ida, Vesta, and Eros
+--------------------------------------------------------
+
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2000 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
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2431010_POLE_RA = ( 348.76 0. 0. )
+ BODY2431010_POLE_DEC = ( 87.12 0. 0. )
+ BODY2431010_PM = ( 265.95 -1864.6280070 0. )
+ BODY2431010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Vesta
+
+ 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
+
+ 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
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [7], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2000 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 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2000 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 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2000 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:
+
+ Old values for Io, Europa, Ganymede, Callisto and Amalthea.
+ These are from the 1997 IAU report.
+
+ body501_radii = ( 1826. 1815. 1812. )
+ body502_radii = ( 1562. 1560. 1559. )
+ body503_radii = ( 2635. 2633. 2633. )
+ body504_radii = ( 2409. 2409. 2409. )
+ body505_radii = ( 131. 73. 67. )
+ 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 = ( 50 50 50 )
+ body515_radii = ( 13 10 8 )
+ body516_radii = ( 20 20 20 )
+
+
+ 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 2000 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
+ 2000 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:
+
+ body601_radii = ( 210.3 197.4 192.6 )
+ body602_radii = ( 256.2 247.3 244.0 )
+ 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 = ( 180. 140. 112.5 )
+ body608_radii = ( 718. 718. 718. )
+ body609_radii = ( 115. 110. 105. )
+ body610_radii = ( 97. 95. 77. )
+ body611_radii = ( 69. 55. 55. )
+ body612_radii = ( 16 16 16 )
+ body613_radii = ( 15 12.5 7.5 )
+ body614_radii = ( 15 8 8 )
+ body615_radii = ( 18.5 17.2 13.5 )
+ body616_radii = ( 74 50 34 )
+ body617_radii = ( 55 44 31 )
+ body618_radii = ( 10 10 10 )
+
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+ Only the first equatorial radius for Helene (body 612) is given in the
+ 2000 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 = ( 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 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2000 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2000 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 2000 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 unchanged in the 2000 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 593 593 593 )
+
+ \begintext
+
+
+
+Radii of Selected Asteroids
+--------------------------------------------------------
+
+
+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
+
+
+
+
+Kleopatra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000216_RADII = ( 108.5 47 40.5 )
+
+ \begintext
+
+
+
+Eros
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 7.311 7.311 7.311 )
+
+ \begintext
+
+
+===========================================================================
+End of file pck00008.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/c2065022/vg200011.tsc b/tests/pytests/data/c2065022/vg200011.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..12511cd3643e3c138dd49df21d22d04f74b657b1
--- /dev/null
+++ b/tests/pytests/data/c2065022/vg200011.tsc
@@ -0,0 +1,1391 @@
+KPL/SCLK
+
+
+\beginlabel
+
+MISSION_NAME = VOYAGER
+SPACECRAFT_NAME = VG2
+SPICE_DATA_TYPE = SCLK
+DATA_SET_ID = "VG2-X-SPICE-6-SCLK-V2.0"
+FILE_NAME = "VG200011.TSC"
+PRODUCT_ID = "VG200011.TSC"
+SOURCE_PRODUCT_ID = { "SCLK.SCET.32 version B100719,
+dated 2010-07-19T13:34:27", "SCLK_SCET.32 version B060714,
+dated 2006-07-14T14:46:43", "SCLK_SCET.32 version B000623,
+dated 2000-06-23T14:00:23", "FDSC/SCE FILE, DATED 1999-07-16T15:20:53" }
+SOFTWARE_NAME = "MAKVSK, by Nat Bachman of NAIF"
+PRODUCT_CREATION _TIME = 2010-07-20T02:40
+PRODUCER_ID = NAIF, N. Bachman
+MISSION_PHASE_TYPE = {"CRUISE","ENCOUNTER","EXTENDED MISSION"}
+MISSION_PHASE_NAME = {"CRUISE","JUPITER ENCOUNTER","SATURN
+ENCOUNTER","URANUS ENCOUNTER","NEPTUNE ENCOUNTER","EXTENDED MISSION"}
+PRODUCT_VERSION_TYPE = RECONSTRUCTION
+START_TIME = 1977-08-20T15:42:18
+STOP_TIME = 2010-10-16T18:06:30
+SPACECRAFT_CLOCK_START_COUNT = "1/00011:00:001"
+SPACECRAFT_CLOCK_STOP_COUNT = "7/46460:00:247"
+NOTE = "Calibrated data cover from launch to 2010-JUL-19 (2010//199),
+but the file may be used in predict mode through 2060 MAY 18,
+(SCLK =15/65535:59:800). Records for partitions 1-4 were derived from the
+SCLKvSCET file dated 1999-07-16. Records for partition 5 start at UTC epoch
+1994-08-04T00:34:09. These records were derived from the SCLKvSCET file
+having version ID B000623. Records for partition 6 start at UTC epoch
+2000-07-27T13:17:47. These records were derived from the SCLKvSCET file
+having version ID B060714. Records for partition 7 start at UTC epoch
+2006-07-21T02:01:22.573 These records were derived from the SCLKvSCET file
+having version ID B100719. The portion of partition 7 following
+2010-199T18:06:30 and partitions 8-15 constitute the predict region."
+
+\endlabel
+
+
+Voyager 2 SPICE SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between Voyager 2
+ spacecraft clock time (SCLK) and ephemeris time.
+
+ NAIF suggests that you do not modify this file. If you do modify it,
+ be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ This file is VG2 version 00011, produced July 20, 2010 by NAIF
+ (N. Bachman).
+
+ See the label above for list of source SCLKvSCET coefficient files.
+
+
+Implementation notes
+--------------------------------------------------------
+
+ You must load this file into the kernel pool before using any of the
+ SPICELIB SCLK routines. The code fragment
+
+ CALL FURNSH ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also need
+ to load a leapseconds kernel. The additional call to FURNSH,
+
+ CALL FURNSH ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names of
+ the files used on your system as arguments to FURNSH. Because the file
+ names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading files.
+ The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+
+
+\begindata
+
+SCLK_KERNEL_ID = ( @20-JUL-2010/02:13 )
+
+SCLK_DATA_TYPE_32 = ( 1 )
+SCLK01_N_FIELDS_32 = ( 3 )
+SCLK01_MODULI_32 = ( 65536 60 800 )
+SCLK01_OFFSETS_32 = ( 0 0 1 )
+SCLK01_OUTPUT_DELIM_32 = ( 2 )
+
+SCLK_PARTITION_START_32 = ( 5.2800000000000E+05
+ 1.9254560000000E+08
+ 0.0000000000000E+00
+ 2.4800000000000E+04
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00 )
+
+SCLK_PARTITION_END_32 = ( 1.9254558300000E+08
+ 3.1457280010000E+09
+ 2.6261048310000E+09
+ 3.1457280000000E+09
+ 3.1457280000000E+09
+ 3.1457280170000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09 )
+
+SCLK01_COEFFICIENTS_32 = (
+
+ 0.00000000000000 -7.0578821346618E+08 2.8800040800000E+03
+ 240000.00000000 -7.0577381347419E+08 2.8800040800000E+03
+ 2352000.0000000 -7.0564709329522E+08 2.8799977800000E+03
+ 2592000.0000000 -7.0563269330622E+08 2.8800028800000E+03
+ 7872000.0000000 -7.0531589298929E+08 2.8800005400000E+03
+ 9312000.0000000 -7.0522949297430E+08 2.8800024600000E+03
+ 13392000.000000 -7.0498469276535E+08 2.8800004200000E+03
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+ 17242224032.000 3.2874473526887E+08 3.8640761400000E+03
+ 17242704032.000 3.2878337603086E+08 2.8799946600000E+03
+ 17281104032.000 3.3108737179916E+08 1.9487581800000E+03
+ 17281584032.000 3.3110685938115E+08 2.8799939400000E+03
+ 17308464032.000 3.3271965600463E+08 2.8800307800000E+03
+ 17308944032.000 3.3274845631262E+08 2.8799945400000E+03 )
+
+\begintext
diff --git a/tests/pytests/data/c2065022/vg2_issna_v02.ti b/tests/pytests/data/c2065022/vg2_issna_v02.ti
new file mode 100644
index 0000000000000000000000000000000000000000..d5a294659e68dad44f717ef3e3063b6e4707e7ca
--- /dev/null
+++ b/tests/pytests/data/c2065022/vg2_issna_v02.ti
@@ -0,0 +1,51 @@
+KPL/IK
+
+Voyager 2 Imaging Subsytem Narrow Angle camera (ISSNA)
+----------------------------------------------------------------
+
+ Version 2 by Jeff Bytof -- 27 November 2000.
+
+ Changed shape from POLYGON to RECTANGLE.
+
+
+ Version 1.0 by Jeff Bytof, NAIF/JPL, 31 March 2000.
+
+ Provide the corner vector directions of the ISSNA
+ field of view.
+
+
+\begintext
+
+ Field of view description
+ -------------------------
+
+ - FOV is square with its sides along X and Y
+ axes of the instrument's frame;
+
+ - full FOV angular size in X and Y directions is 0.424 degrees;
+
+ - boresight vector intersects FOV exactly in the center of
+ the square;
+
+
+\begindata
+
+
+ INS-32101_FOV_FRAME = 'VG2_ISSNA'
+
+ INS-32101_FOV_SHAPE = 'RECTANGLE'
+
+ INS-32101_BORESIGHT = ( 0.0 0.0 1.0 )
+
+
+ INS-32101_FOV_BOUNDARY_CORNERS = (
+
+ .003700098 .003700098 1.0
+ -.003700098 .003700098 1.0
+ -.003700098 -.003700098 1.0
+ .003700098 -.003700098 1.0
+
+ )
+
+\begintext
+
diff --git a/tests/pytests/data/c2065022/vg2_jup_qmw_na_fc-32100_t2_0_sliced_-32100.xc b/tests/pytests/data/c2065022/vg2_jup_qmw_na_fc-32100_t2_0_sliced_-32100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..c63ac28e96b3edb5bd2c1f9e76e45bedb6a3513f
--- /dev/null
+++ b/tests/pytests/data/c2065022/vg2_jup_qmw_na_fc-32100_t2_0_sliced_-32100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG2 JUP SEDR QMW IMAGE NAV POINTING: NA '
+'3B0C0BCB^8'
+'3B0C12EA^8'
+'-7D64'
+'2'
+'2'
+'1'
+10
+'606DF80471D628^0'
+'20607B6F8BC582^0'
+'B1A1EDCD5867C^0'
+'-99BD3FE24F64A8^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'3B0C0EBE^8'
+'3B0C11DE^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/acpaquette/voyager/c2065022.spice.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065022/vg2_jup_qmw_na_fc-32100_t2_1_sliced_-32100.xc b/tests/pytests/data/c2065022/vg2_jup_qmw_na_fc-32100_t2_1_sliced_-32100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..7a4f655347a3ce3486416fa000ad205a87942a95
--- /dev/null
+++ b/tests/pytests/data/c2065022/vg2_jup_qmw_na_fc-32100_t2_1_sliced_-32100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG2 JUP SEDR QMW IMAGE NAV POINTING: NA '
+'3B0CB8DC^8'
+'3B0CBFC2^8'
+'-7D64'
+'2'
+'2'
+'1'
+10
+'58839FB314C034^0'
+'1696292F466A35^0'
+'B237FA488C87B^0'
+'-9F7721867D92B^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'3B0CB8DC^8'
+'3B0CBA9E^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/acpaquette/voyager/c2065022.spice.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065022/vg2_v02.tf b/tests/pytests/data/c2065022/vg2_v02.tf
new file mode 100644
index 0000000000000000000000000000000000000000..dfae5d6790ad479614ec7d32759c79c80063677b
--- /dev/null
+++ b/tests/pytests/data/c2065022/vg2_v02.tf
@@ -0,0 +1,339 @@
+KPL/FK
+
+Voyager-2 Frame Kernel
+===========================================================================
+
+ This file contains various frame definitions for Voyager-2,
+ related to the spacecraft body and the scan platform.
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 2 -- 27 Nov. 2000 -- Jeff Bytof
+
+ Changed base frame of instruments to VG2_SCAN_PLATFORM.
+
+ Eliminated multiple frames for PPS. That can
+ be handled in the PPS instrument kernel.
+
+
+ Version 1.2 -- 16 Aug. 2000 -- Jeff Bytof
+
+ Added additional frame definitions for the PPS instrument
+ because it has multiple fields of view.
+
+
+ Version 1.1 -- 8 March 2000 -- Jeff Bytof
+
+ Added the spacecraft high-gain antenna frame, FRAME_VG2_HGA.
+
+ Added -100 to all scan platform instrument ID codes, to
+ associate them to the scan platform ID code of -32100.
+
+
+ Version 1.0 -- 4 November 1999 -- Jeff Bytof
+
+ Initial Release.
+
+
+References
+--------------------------------------------------------
+
+ (1) Frames Required Reading (NAIF document).
+
+ (2) C Kernel Required Reading (NAIF document).
+
+
+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 LDPOOL loads a kernel file into the pool as shown below.
+
+
+ CALL LDPOOL ( kernel_name )
+
+
+ In order for a program or subroutine to extract data from the pool,
+ the SPICELIB routines GDPOOL and GIPOOL are used. See [3] for more
+ details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Naming Conventions
+--------------------------------------------------------
+
+ All names referencing values in this frame kernel start with the
+ characters `FRAME', 'CK' or `TKFRAME' followed by the Voyager-2
+ spacecraft bus ID number (-32000) added to the instrument or
+ alternate frame index number.
+
+ The remainder of the name is an underscore character followed by the
+ unique name of the data item. For example, the Voyager-2 cone/clock
+ offsets relative to the spacecraft frame, given as three Euler angles,
+ are specified using two items:
+
+ TKFRAME_-32200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-32200_AXES = ( 3, 2, 1 )
+
+ The upper bound on the length of the name of any data item is 32
+ characters.
+
+ If the same item is included in more then one file, or if the same
+ item appears more than once within a single file, the latest value
+ supersedes any earlier values.
+
+
+TKFRAME Keyword Description
+--------------------------------------------------------
+
+ This section describes the TKFRAME keywords. The rotational offsets
+ can be given as three angles -- ROLL, PITCH and YAW, from which
+ a rotation matrix can be constructed that will transform the components
+ of a vector expressed in the spacecraft frame to components expressed
+ in the antenna fixed frame. For example, if x, y and z are the
+ components of a vector expressed in the spacecraft frame, X, Y and Z
+ will be the components of the same vector expressed in the antenna
+ fixed frame:
+
+
+ [ X ] [ ] [ x ]
+ | Y | = | ROT | | y |
+ [ Z ] [ ] [ z ]
+
+
+ where ROT is the rotation matrix constructed from the rotation angles
+ as follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ YAW ] [ PITCH ] [ ROLL ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where each of three matrixes on the right side represent a coordinate
+ frame rotation by the given angle around the indicated axis. See the
+ SPICELIB routine EUL2M for more information about constructing
+ a rotation matrix from a set of rotation angles.
+
+ Following are some examples of use of the TKFRAME keywords:
+
+ The keyword that indicates which frame the axis rotations are
+ referred to is:
+
+ TKFRAME_-32200_RELATIVE = 'VG2_SC_BUS'
+
+
+ The keyword TKFRAME_-91000_ANGLES contain these values, in radians,
+ in the following order:
+
+ ``ROLL'' ``PITCH'' ``YAW''
+ TKFRAME_-32200_ANGLES = ( 55.0, 0.0, 180.0 )
+
+
+ The keyword TKFRAME_-32200_AXES contains integer codes of the
+ corresponding axes of rotations (1 -- X, 2 -- Y, 3 -- Z).
+
+ TKFRAME_-32200_AXES = ( 3, 2, 1 )
+
+
+ The keyword TKFRAME_-32200_UNITS gives the units of the angles.
+
+ TKFRAME_-32202_UNITS = 'DEGREES'
+
+
+
+Spacecraft Bus
+--------------------------------------------------------
+
+ The following data represents the basic spacecraft bus, and
+ the scan platform. Spacecraft bus attitude with respect to an inertial
+ frame is provided by a C kernel (see [2] for more information).
+ Scan platform orientation with respect to an inertial frame
+ is also provided by a C-kernel. Each instrument mounted
+ on the scan platform may have measureable offsets from the
+ nominal scan platform orientation. The Narrow Angle camera
+ has been chosen as representative of the scan platform orientation.
+
+\begindata
+
+ FRAME_VG2_SC_BUS = -32000
+ FRAME_-32000_NAME = 'VG2_SC_BUS'
+ FRAME_-32000_CLASS = 3
+ FRAME_-32000_CLASS_ID = -32000
+ FRAME_-32000_CENTER = -32
+ CK_-32000_SCLK = -32
+ CK_-32000_SPK = -32
+
+ FRAME_VG2_SCAN_PLATFORM = -32100
+ FRAME_-32100_NAME = 'VG2_SCAN_PLATFORM'
+ FRAME_-32100_CLASS = 3
+ FRAME_-32100_CLASS_ID = -32100
+ FRAME_-32100_CENTER = -32
+ CK_-32100_SCLK = -32
+ CK_-32100_SPK = -32
+
+\begintext
+
+
+Frame Definitions
+--------------------------------------------------------
+
+ Here are the antenna frame definitions for Voyager 2. These will be
+ utilized by SPICE's FRAMES subsystem to provide automatic state
+ transformations to/from the Voyager-2 frame. Note that SPICE toolkit
+ version N0047 or higher is required to use fixed-offset frames.
+
+ Note that angles in the frame definitions are specified for the "from
+ instrument to base (relative to) frame" transformation.
+
+
+ Spacecraft body-fixed frames:
+
+
+\begindata
+
+ FRAME_VG2_CONE_CLOCK = -32200
+ FRAME_-32200_NAME = 'VG2_CONE_CLOCK'
+ FRAME_-32200_CLASS = 4
+ FRAME_-32200_CLASS_ID = -32200
+ FRAME_-32200_CENTER = -32
+ TKFRAME_-32200_SPEC = 'ANGLES'
+ TKFRAME_-32200_RELATIVE = 'VG2_SC_BUS'
+ TKFRAME_-32200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-32200_AXES = ( 3, 2, 1 )
+ TKFRAME_-32200_UNITS = 'DEGREES'
+
+ FRAME_VG2_AZ_EL = -32300
+ FRAME_-32300_NAME = 'VG2_AZ_EL'
+ FRAME_-32300_CLASS = 4
+ FRAME_-32300_CLASS_ID = -32300
+ FRAME_-32300_CENTER = -32
+ TKFRAME_-32300_SPEC = 'ANGLES'
+ TKFRAME_-32300_RELATIVE = 'VG2_SC_BUS'
+ TKFRAME_-32300_ANGLES = ( -173.0, 0.0, 180.0 )
+ TKFRAME_-32300_AXES = ( 1, 2, 3 )
+ TKFRAME_-32300_UNITS = 'DEGREES'
+
+
+\begintext
+
+ The boresight of the antenna is the +Z axis.
+
+\begindata
+
+ FRAME_VG2_HGA = -32400
+ FRAME_-32400_NAME = 'VG2_HGA'
+ FRAME_-32400_CLASS = 4
+ FRAME_-32400_CLASS_ID = -32400
+ FRAME_-32400_CENTER = -32
+ TKFRAME_-32400_SPEC = 'ANGLES'
+ TKFRAME_-32400_RELATIVE = 'VG2_SC_BUS'
+ TKFRAME_-32400_ANGLES = ( 180.0, 0.0, 0.0 )
+ TKFRAME_-32400_AXES = ( 1, 2, 3 )
+ TKFRAME_-32400_UNITS = 'DEGREES'
+
+\begintext
+
+ Voyager-2 scan platform instrument frame definitions.
+
+ The Euler angles of rotation given below are
+ referred to the ISSNA frame of reference which
+ in this case is considered the equivalent of the
+ scan platform's frame.
+
+ Boresights are +Z in each instrument frame.
+
+
+\begindata
+
+
+ FRAME_VG2_ISSNA = -32101
+ FRAME_-32101_NAME = 'VG2_ISSNA'
+ FRAME_-32101_CLASS = 4
+ FRAME_-32101_CLASS_ID = -32101
+ FRAME_-32101_CENTER = -32
+ TKFRAME_-32101_SPEC = 'ANGLES'
+ TKFRAME_-32101_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32101_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-32101_AXES = ( 1, 2, 3 )
+ TKFRAME_-32101_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_ISSWA = -32102
+ FRAME_-32102_NAME = 'VG2_ISSWA'
+ FRAME_-32102_CLASS = 4
+ FRAME_-32102_CLASS_ID = -32102
+ FRAME_-32102_CENTER = -32
+ TKFRAME_-32102_SPEC = 'ANGLES'
+ TKFRAME_-32102_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32102_ANGLES = ( 0.171102, 0.0068, -0.0308 )
+ TKFRAME_-32102_AXES = ( 3, 1, 2 )
+ TKFRAME_-32102_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_PPS = -32103
+ FRAME_-32103_NAME = 'VG2_PPS'
+ FRAME_-32103_CLASS = 4
+ FRAME_-32103_CLASS_ID = -32103
+ FRAME_-32103_CENTER = -32
+ TKFRAME_-32103_SPEC = 'ANGLES'
+ TKFRAME_-32103_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32103_ANGLES = ( 0.0, -0.003, -0.060 )
+ TKFRAME_-32103_AXES = ( 3, 1, 2 )
+ TKFRAME_-32103_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_UVS = -32104
+ FRAME_-32104_NAME = 'VG2_UVS'
+ FRAME_-32104_CLASS = 4
+ FRAME_-32104_CLASS_ID = -32104
+ FRAME_-32104_CENTER = -32
+ TKFRAME_-32104_SPEC = 'ANGLES'
+ TKFRAME_-32104_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32104_ANGLES = ( 0.0, -0.08, 0.0 )
+ TKFRAME_-32104_AXES = ( 3, 1, 2 )
+ TKFRAME_-32104_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_UVSOCC = -32105
+ FRAME_-32105_NAME = 'VG2_UVSOCC'
+ FRAME_-32105_CLASS = 4
+ FRAME_-32105_CLASS_ID = -32105
+ FRAME_-32105_CENTER = -32
+ TKFRAME_-32105_SPEC = 'ANGLES'
+ TKFRAME_-32105_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32105_ANGLES = ( 0.0, 0.0, -19.26 )
+ TKFRAME_-32105_AXES = ( 3, 1, 2 )
+ TKFRAME_-32105_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_IRIS = -32106
+ FRAME_-32106_NAME = 'VG2_IRIS'
+ FRAME_-32106_CLASS = 4
+ FRAME_-32106_CLASS_ID = -32106
+ FRAME_-32106_CENTER = -32
+ TKFRAME_-32106_SPEC = 'ANGLES'
+ TKFRAME_-32106_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32106_ANGLES = ( 0.0, 0.009 , 0.016 )
+ TKFRAME_-32106_AXES = ( 3, 1, 2 )
+ TKFRAME_-32106_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_IRISOCC = -32107
+ FRAME_-32107_NAME = 'VG2_IRISOCC'
+ FRAME_-32107_CLASS = 4
+ FRAME_-32107_CLASS_ID = -32107
+ FRAME_-32107_CENTER = -32
+ TKFRAME_-32107_SPEC = 'ANGLES'
+ TKFRAME_-32107_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32107_ANGLES = ( 0.0, 0.0, -20.8 )
+ TKFRAME_-32107_AXES = ( 3, 1, 2 )
+ TKFRAME_-32107_UNITS = 'DEGREES'
+
+\begintext
diff --git a/tests/pytests/data/c2065022/voyagerAddendum004.ti b/tests/pytests/data/c2065022/voyagerAddendum004.ti
new file mode 100644
index 0000000000000000000000000000000000000000..1bab47031b34785ada4f0c3ef4609cb27bd82215
--- /dev/null
+++ b/tests/pytests/data/c2065022/voyagerAddendum004.ti
@@ -0,0 +1,36 @@
+\begindata
+INS-32101_SPK_TIME_BIAS = 0.0
+INS-32101_CK_TIME_BIAS = 0.0
+INS-32101_CK_TIME_TOLERANCE = 2000
+INS-32101_PIXEL_PITCH = 0.011789473651194
+INS-32101_FOCAL_LENGTH = 1503.49
+
+INS-32101_TRANSX = ( 0.0, 0.011789473651194, 0.0)
+INS-32101_TRANSY = ( 0.0, 0.0, 0.011789473651194)
+INS-32101_ITRANSS = ( 0.0, 84.8214288089711, 0.0)
+INS-32101_ITRANSL = ( 0.0, 0.0, 84.8214288089711)
+INS-32101_PLATFORM_ID = -32001
+
+INS-32102_SPK_TIME_BIAS = 0.0
+INS-32102_CK_TIME_BIAS = 0.0
+INS-32102_CK_TIME_TOLERANCE = 2000
+INS-32102_PIXEL_PITCH = 0.0116661644275479
+INS-32102_FOCAL_LENGTH = 200.770
+
+INS-32102_TRANSX = ( 0.0, 0.0116661644275479, 0.0)
+INS-32102_TRANSY = ( 0.0, 0.0, 0.0116661644275479)
+INS-32102_ITRANSS = ( 0.0, 85.7179757931961, 0.0)
+INS-32102_ITRANSL = ( 0.0, 0.0, 85.7179757931961)
+INS-32102_PLATFORM_ID = -32002
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Voyager 2 the ck
+instrument frame is VG1_SCAN_PLATFORM (-32100) and the ck reference frame
+is B1950 (2).
+
+\begindata
+INS-32101_CK_FRAME_ID=-32100
+INS-32101_CK_REFERENCE_ID=2
+INS-32102_CK_FRAME_ID=-32100
+INS-32102_CK_REFERENCE_ID=2
diff --git a/tests/pytests/test_isis_formatter.py b/tests/pytests/test_isis_formatter.py
index 667d25e903583df85214cae83c8c267a6bac91a6..cc41939ff333522c5f300a94bb1463f3e3bba5ff 100644
--- a/tests/pytests/test_isis_formatter.py
+++ b/tests/pytests/test_isis_formatter.py
@@ -169,7 +169,7 @@ def test_instrument_pointing(driver):
assert pointing['CkTableEndTime'] == 1
assert pointing['CkTableOriginalSize'] == 2
np.testing.assert_equal(pointing['EphemerisTimes'], np.array([0, 1]))
- np.testing.assert_equal(pointing['Quaternions'], np.array([[0, 0, 0, -1], [0, 0, 0, -1]]))
+ np.testing.assert_equal(pointing['Quaternions'], np.array([[-1, 0, 0, 0], [-1, 0, 0, 0]]))
def test_instrument_position(driver):
meta_data = isis_formatter.to_isis(driver)
@@ -178,8 +178,8 @@ def test_instrument_position(driver):
assert position['SpkTableEndTime'] == 900
assert position['SpkTableOriginalSize'] == 2
np.testing.assert_equal(position['EphemerisTimes'], np.array([800, 900]))
- np.testing.assert_equal(position['Positions'], np.array([[0, 1, 2], [3, 4, 5]]))
- np.testing.assert_equal(position['Velocities'], np.array([[0, -1, -2], [-3, -4, -5]]))
+ np.testing.assert_equal(position['Positions'], np.array([[0, 0.001, 0.002], [0.003, 0.004, 0.005]]))
+ np.testing.assert_equal(position['Velocities'], np.array([[0, -0.001, -0.002], [-0.003, -0.004, -0.005]]))
def test_body_rotation(driver):
meta_data = isis_formatter.to_isis(driver)
@@ -189,7 +189,7 @@ def test_body_rotation(driver):
assert rotation['CkTableEndTime'] == 1
assert rotation['CkTableOriginalSize'] == 2
np.testing.assert_equal(rotation['EphemerisTimes'], np.array([0, 1]))
- np.testing.assert_equal(rotation['Quaternions'], np.array([[0, 0, 0, -1], [0, 0, 0, -1]]))
+ np.testing.assert_equal(rotation['Quaternions'], np.array([[-1, 0, 0, 0], [-1, 0, 0, 0]]))
def test_sun_position(driver):
meta_data = isis_formatter.to_isis(driver)
@@ -198,8 +198,8 @@ def test_sun_position(driver):
assert position['SpkTableEndTime'] == 700
assert position['SpkTableOriginalSize'] == 2
np.testing.assert_equal(position['EphemerisTimes'], np.array([600, 700]))
- np.testing.assert_equal(position['Positions'], np.array([[0, 1, 2], [3, 4, 5]]))
- np.testing.assert_equal(position['Velocities'], np.array([[0, -1, -2], [-3, -4, -5]]))
+ np.testing.assert_equal(position['Positions'], np.array([[0, 0.001, 0.002], [0.003, 0.004, 0.005]]))
+ np.testing.assert_equal(position['Velocities'], np.array([[0, -0.001, -0.002], [-0.003, -0.004, -0.005]]))
def test_naif_keywords(driver):
meta_data = isis_formatter.to_isis(driver)
diff --git a/tests/pytests/test_mro_drivers.py b/tests/pytests/test_mro_drivers.py
index a10eb4aa48d86f3d44e4777f2c27554b89c86b40..7f8aaf1f6e959b17f08d99e300f2c8b9798e6226 100644
--- a/tests/pytests/test_mro_drivers.py
+++ b/tests/pytests/test_mro_drivers.py
@@ -79,45 +79,55 @@ def isis_compare_dict():
'CkTableEndTime': 297088762.9923841,
'CkTableOriginalSize': 6,
'EphemerisTimes': [297088762.24158406, 297088762.3917441, 297088762.5419041, 297088762.69206405, 297088762.84222406, 297088762.9923841],
- 'Quaternions': [[0.18648266589041404, -0.2396394764713814, 0.8548690179951135, 0.42070904282056604],
- [0.18654399941209654, -0.23960773322048612, 0.8548589519568615, 0.4207203854384721],
- [0.18660480854159617, -0.2395758135567815, 0.8548483051723957, 0.42073322917454875],
- [0.18666593205145582, -0.23954391528431818, 0.8548379212197076, 0.4207453753832475],
- [0.18672709386922662, -0.2395120269907863, 0.8548277995612382, 0.4207569541186571],
- [0.18678728502603456, -0.23948004737140324, 0.8548176086382281, 0.4207691445740938]]},
+ 'Quaternions': [[0.42070904282056604, 0.18648266589041404, -0.2396394764713814, 0.8548690179951135],
+ [0.4207203854384721, 0.18654399941209654, -0.23960773322048612, 0.8548589519568615],
+ [0.42073322917454875, 0.18660480854159617, -0.2395758135567815, 0.8548483051723957],
+ [0.4207453753832475, 0.18666593205145582, -0.23954391528431818, 0.8548379212197076],
+ [0.4207569541186571, 0.18672709386922662, -0.2395120269907863, 0.8548277995612382],
+ [0.4207691445740938, 0.18678728502603456, -0.23948004737140324, 0.8548176086382281]]},
'BodyRotation': {'TimeDependentFrames': [10014, 1],
'CkTableStartTime': 297088762.24158406,
'CkTableEndTime': 297088762.9923841,
'CkTableOriginalSize': 6,
'EphemerisTimes': [297088762.24158406, 297088762.3917441, 297088762.5419041, 297088762.69206405, 297088762.84222406, 297088762.9923841],
- 'Quaternions': [[-0.2996928944391797, -0.10720760458181891, -0.4448811306448063, 0.8371209459443085],
- [-0.2996934649760026, -0.1072060096645597, -0.4448855856569007, 0.8371185783490869],
- [-0.2996940355045328, -0.10720441474371896, -0.44489004065791765, 0.8371162107293473],
- [-0.2996946060241849, -0.1072028198209324, -0.44489449564328926, 0.8371138430875174],
- [-0.2996951765357392, -0.10720122489401934, -0.44489895061910595, 0.8371114754203602],
- [-0.29969574703861046, -0.10719962996461516, -0.4449034055807993, 0.8371091077303039]]},
+ 'Quaternions': [[0.8371209459443085, -0.2996928944391797, -0.10720760458181891, -0.4448811306448063],
+ [0.8371185783490869, -0.2996934649760026, -0.1072060096645597, -0.4448855856569007],
+ [0.8371162107293473, -0.2996940355045328, -0.10720441474371896, -0.44489004065791765],
+ [0.8371138430875174, -0.2996946060241849, -0.1072028198209324, -0.44489449564328926],
+ [0.8371114754203602, -0.2996951765357392, -0.10720122489401934, -0.44489895061910595],
+ [0.8371091077303039, -0.29969574703861046, -0.10719962996461516, -0.4449034055807993]]},
'InstrumentPosition': {'SpkTableStartTime': 297088762.24158406,
'SpkTableEndTime': 297088762.9923841,
'SpkTableOriginalSize': 6,
'EphemerisTimes': [297088762.24158406, 297088762.3917441, 297088762.5419041, 297088762.69206405, 297088762.84222406, 297088762.9923841],
- 'Positions': [[-615012.0886971647, -97968.2345594813, -3573947.032011338],
- [-615520.6109230528, -97906.4784443392, -3573862.281296898],
- [-616029.119550515, -97844.70954517406, -3573777.458632478],
- [-616537.6144124779, -97782.9278549998, -3573692.564075001],
- [-617046.0958326485, -97721.13339810426, -3573607.5975138554],
- [-617554.5636389386, -97659.32615734483, -3573522.559012526]],
- 'Velocities': [[-3386.5803072965314, 411.22659677341727, 564.1630407502585],
- [-3386.489840800698, 411.311733889654, 564.6421991490199],
- [-3386.3993050250588, 411.39686089830735, 565.121345962894],
- [-3386.308700009319, 411.48197773049435, 565.6004809915789],
- [-3386.2180256890892, 411.567084441927, 566.0796046059958],
- [-3386.127282097941, 411.652181012709, 566.5587166058317]]},
+ 'Positions': [[-1885.2595574396726, 913.1466129090919, -2961.9072734074616],
+ [-1885.5542519556852, 912.7250080871751, -2961.850963369567],
+ [-1885.8489085311885, 912.3033848578856, -2961.794593708069],
+ [-1886.1435271048538, 911.8817433844737, -2961.7381644454717],
+ [-1886.4381077924143, 911.4600833470981, -2961.681675541305],
+ [-1886.732650539467, 911.0384049200497, -2961.6251270167986]],
+ 'Velocities': [[-1.996367491737628, -2.7947535723103862, 0.40022835507075183],
+ [-1.9961370953858215, -2.7948577920481075, 0.40064724633288534],
+ [-1.995906659162522, -2.7949619556787955, 0.40106612935145375],
+ [-1.9956761831571486, -2.7950660631619337, 0.40148500394594044],
+ [-1.995445667175973, -2.795170114597101, 0.40190387042237496],
+ [-1.995215111338196, -2.7952741099180174, 0.4023227286300164]]},
'SunPosition': {'SpkTableStartTime': 297088762.61698407,
'SpkTableEndTime': 297088762.61698407,
'SpkTableOriginalSize': 1,
'EphemerisTimes': [297088762.61698407],
- 'Positions': [[-127052102329.16032, 139728839049.65073, -88111530293.94502]],
- 'Velocities': [[9883868.06162645, 8989183.29614645, 881.9339912834714]]}}
+ 'Positions': [[-208246783.16649625, -7672643.572718078, 2105891.871806553],
+ [-208246727.14724845, -7674420.97378656, 2104954.712096058],
+ [-208246671.10884315, -7676198.370536743, 2104017.543867386],
+ [-208246615.05133778, -7677975.761145981, 2103080.368081583],
+ [-208246558.97465575, -7679753.148044037, 2102143.183457432],
+ [-208246502.87885448, -7681530.529408173, 2101205.9909560373]],
+ 'Velocities': [[-373.21084988516105, 11812.830032566408, 6230.090308526069],
+ [-373.3380528336456, 11812.79727998301, 6230.144788806889],
+ [-373.4652557832692, 11812.764526050134, 6230.199268400618],
+ [-373.59245860358607, 11812.731770801367, 6230.253747251377],
+ [-373.71966146848814, 11812.69901419193, 6230.308225433648],
+ [-373.846864247526, 11812.666256255417, 6230.362702891557]]}}
@pytest.fixture(scope='module')
def test_kernels():
@@ -134,6 +144,7 @@ def test_mro_load(test_kernels, label_type, formatter, usgscsm_compare_dict, isi
usgscsm_isd_str = ale.loads(label_file, props={'kernels': test_kernels}, formatter=formatter)
usgscsm_isd_obj = json.loads(usgscsm_isd_str)
+ print(usgscsm_isd_obj)
if formatter=='usgscsm':
# Check to change the line based on ISIS vs PDS3
diff --git a/tests/pytests/test_voyager_drivers.py b/tests/pytests/test_voyager_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..1306e81e1102c1b68f40b657856d0f3beeb5f784
--- /dev/null
+++ b/tests/pytests/test_voyager_drivers.py
@@ -0,0 +1,70 @@
+import os
+import json
+import unittest
+from unittest.mock import patch
+
+import pytest
+import numpy as np
+import spiceypy as spice
+
+import ale
+from ale.drivers.mro_drivers import MroCtxPds3LabelNaifSpiceDriver, MroCtxIsisLabelNaifSpiceDriver, MroCtxIsisLabelIsisSpiceDriver
+
+from conftest import get_image_kernels, convert_kernels, get_image_label, compare_dicts
+
+@pytest.fixture()
+def isis_compare_dict():
+ return {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY502_RADII': [1564.13, 1561.23, 1560.93],
+ 'BODY_FRAME_CODE': 10024,
+ 'INS-32101_PIXEL_SIZE': 0.011789473651194,
+ 'INS-32101_ITRANSL': [0.0, 0.0, 84.821428808971],
+ 'INS-32101_ITRANSS': [0.0, 84.821428808971, 0.0],
+ 'INS-32101_FOCAL_LENGTH': 1503.49,
+ 'INS-32101_BORESIGHT_SAMPLE': 500,
+ 'INS-32101_BORESIGHT_LINE': 500},
+ 'InstrumentPointing': {'TimeDependentFrames': [-32100, 2, 1],
+ 'ConstantFrames': [-32101, -32100],
+ 'CkTableStartTime': -646346832.89712,
+ 'CkTableEndTime': -646346832.89712,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.89712],
+ 'Quaternions': [[0.34057881936764,0.085849252725072,0.69748691965044,-0.62461825983655]]},
+ 'BodyRotation': {'TimeDependentFrames': [10024, 1],
+ 'CkTableStartTime': -646346832.89712,
+ 'CkTableEndTime': -646346832.89712,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.89712],
+ 'Quaternions': [[0.029536586623089,-0.01009726603285,-0.22183796921534,0.97458378330636]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -646346832.89712,
+ 'SpkTableEndTime': -646346832.89712,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.89712],
+ 'Positions': [[133425.48293894,184605.07752753,-3162.2190909154]],
+ 'Velocities': [[-10.722770423744,2.0367821121285,-0.64314600586812]]},
+ 'SunPosition': {'SpkTableStartTime': -646346832.8971245,
+ 'SpkTableEndTime': -646346832.8971245,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.8971245],
+ 'Positions': [[588004836.49532,-489060608.67696,-224000895.4511]],
+ 'Velocities': [[9.1115543713942,-4.4506204607189,-2.785930492615]]}}
+
+@pytest.fixture(scope='module')
+def test_kernels():
+ kernels = get_image_kernels('c2065022')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+@pytest.mark.parametrize("label_type", ['isis3'])
+@pytest.mark.parametrize("formatter", ['isis'])
+@pytest.mark.skip(reason="Fails due to angular velocity problems")
+def test_voyager_load(test_kernels, label_type, formatter, isis_compare_dict):
+ label_file = get_image_label('c2065022', label_type)
+
+ usgscsm_isd_str = ale.loads(label_file, props={'kernels': test_kernels}, formatter=formatter)
+ usgscsm_isd_obj = json.loads(usgscsm_isd_str)
+
+ assert compare_dicts(usgscsm_isd_obj, isis_compare_dict) == []