diff --git a/ale/drivers/chandrayaan_drivers.py b/ale/drivers/chandrayaan_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..5f54d3e6b2da864db43261e42f12df63eb38de66
--- /dev/null
+++ b/ale/drivers/chandrayaan_drivers.py
@@ -0,0 +1,49 @@
+import spiceypy as spice
+
+from ale.base import Driver
+from ale.base.data_naif import NaifSpice
+from ale.base.label_isis import IsisLabel
+from ale.base.type_distortion import NoDistortion
+from ale.base.type_sensor import LineScanner
+
+class Chandrayaan1M3IsisLabelNaifSpiceDriver(LineScanner, IsisLabel, NaifSpice, NoDistortion, Driver):
+
+ @property
+ def instrument_id(self):
+ """
+ Returns the instrument id for chandrayaan moon mineralogy mapper
+
+ Returns
+ -------
+ : str
+ Frame Reference for chandrayaan moon mineralogy mapper
+ """
+ inst_id_lookup = {
+ "M3" : "CHANDRAYAAN-1_M3"
+ }
+ return inst_id_lookup[super().instrument_id]
+
+ @property
+ def ikid(self):
+ """
+ Returns the ikid/frame code from the ISIS label. This is attached
+ via chan1m3 on ingestion into an ISIS cube
+
+ Returns
+ -------
+ : int
+ ikid for chandrayaan moon mineralogy mapper
+ """
+ return spice.namfrm(self.instrument_id)
+
+ @property
+ def sensor_model_version(self):
+ """
+ The ISIS Sensor model number for Chandrayaan1M3 in ISIS. This is likely just 1
+
+ Returns
+ -------
+ : int
+ ISIS sensor model version
+ """
+ return 1
\ No newline at end of file
diff --git a/ale/util.py b/ale/util.py
index 1d645c8158df1dad021ea16d78e769f5d429e06b..e2834db7fc438b48866c70cda556eb07c91c785a 100644
--- a/ale/util.py
+++ b/ale/util.py
@@ -275,7 +275,7 @@ def get_kernels_from_isis_pvl(kernel_group, expand=True, format_as="list"):
if not "DataDirectory" in isisprefs:
warnings.warn("No IsisPreferences file found, is your ISISROOT env var set?")
- kernels = [expandvars(expandvars(k, dict_to_lower(isisprefs['DataDirectory']))) for k in kernels]
+ kernels = [expandvars(expandvars(k, isisprefs['DataDirectory'], case_sensitive=False)) for k in kernels]
# Ensure that the ISIS Addendum kernel is last in case it overrides
# some values from the default Instrument kernel
kernels = sorted(kernels, key=lambda x: "Addendum" in x)
@@ -287,7 +287,7 @@ def get_kernels_from_isis_pvl(kernel_group, expand=True, format_as="list"):
for kern_list in mk_paths:
for index, kern in enumerate(mk_paths[kern_list]):
if kern is not None:
- mk_paths[kern_list][index] = expandvars(expandvars(kern, dict_to_lower(isisprefs['DataDirectory'])))
+ mk_paths[kern_list][index] = expandvars(expandvars(kern, isisprefs['DataDirectory'], case_sensitive=False))
return mk_paths
else:
raise Exception(f'{format_as} is not a valid return format')
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/M3T20090630T083407_V03_L1B_nadir-jig_2016-04-29_0_sliced_-86000.xc b/tests/pytests/data/M3T20090630T083407_V03_RDN/M3T20090630T083407_V03_L1B_nadir-jig_2016-04-29_0_sliced_-86000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..2e392e322704775287ef863fb4d8ddd4a5fb74c4
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/M3T20090630T083407_V03_L1B_nadir-jig_2016-04-29_0_sliced_-86000.xc
@@ -0,0 +1,2023 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'USGS_CK_File '
+BEGIN_ARRAY 1 2001
+'M3T20090630T083407_V03_RDN '
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+'1^1'
+'18F^3'
+END_ARRAY 1 2001
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: ../chan_data/chan1m32isisTEMP.forwardAscending.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/M3T20090630T083407_V03_RDN_isis.lbl b/tests/pytests/data/M3T20090630T083407_V03_RDN/M3T20090630T083407_V03_RDN_isis.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..aeeb6d645a2ef9a641c47826cf7eb16faf418b46
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/M3T20090630T083407_V03_RDN_isis.lbl
@@ -0,0 +1,525 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 304
+ TileLines = 5
+
+ Group = Dimensions
+ Samples = 608
+ Lines = 5
+ Bands = 3
+ End_Group
+
+ Group = Pixels
+ Type = Real
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = CHANDRAYAAN-1
+ MissionId = CH1
+ InstrumentHostName = "CHANDRAYAAN-1 ORBITER"
+ InstrumentHostId = CH1-ORB
+ InstrumentName = "MOON MINERALOGY MAPPER"
+ InstrumentId = M3
+ TargetName = MOON
+ MissionPhaseName = "PRIMARY MISSION"
+ StartTime = 2009-06-30T08:34:35.424411
+ StopTime = 2009-06-30T08:34:35.678811
+ SpacecraftClockStartCount = 12/1759056.764
+ SpacecraftClockStopCount = 12/1759057.019
+ OrbitNumber = 2804
+ InstrumentModeId = TARGET
+ SpatialSumming = 1
+ LineExposureDuration = 50.88
+ SpacecraftYawDirection = FORWARD
+ OrbitLimbDirection = ASCENDING
+ SampleDisplayDirection = UNKNOWN
+ LineDisplayDirection = UNKNOWN
+ ProductType = CALIBRATED_IMAGE
+ End_Group
+
+ Group = Archive
+ DataSetId = CH1-ORB-L-M3-4-L1B-RADIANCE-V3.0
+ ProducerInstitutionName = "JET PROPULSION LABORATORY"
+ ProductId = M3T20090630T083407_V03_RDN
+ SourceProductId = M3T20090630T083407_V01_L0.IMG
+ ProductType = CALIBRATED_IMAGE
+ ProductCreationTime = 2009-05-10T18:01:10
+ ProductVersionType = ACTUAL
+ ProductVersionId = 3.0
+ SoftwareName = m3t_l1b_v07.exe
+ SoftwareVersionId = 07
+ Description = "M3 Level 1B data product which contains pixel
+ located, radiometrically-calibrated data."
+ End_Group
+
+ Group = BandBin
+ Center = (446.02, 456.00, 465.98, 475.96, 485.95, 495.93, 505.91,
+ 515.89, 525.87, 535.85, 545.83, 555.81, 565.79, 575.77,
+ 585.76, 595.74, 605.72, 615.70, 625.68, 635.66, 645.64,
+ 655.62, 665.60, 675.58, 685.56, 695.55, 705.53, 715.51,
+ 725.49, 735.47, 745.45, 755.43, 765.41, 775.39, 785.37,
+ 795.36, 805.34, 815.32, 825.30, 835.28, 845.26, 855.24,
+ 865.22, 875.20, 885.18, 895.17, 905.15, 915.13, 925.11,
+ 935.09, 945.07, 955.05, 965.03, 975.01, 984.99, 994.97,
+ 1004.96, 1014.94, 1024.92, 1034.90, 1044.88, 1054.86,
+ 1064.84, 1074.82, 1084.80, 1094.78, 1104.77, 1114.75,
+ 1124.73, 1134.71, 1144.69, 1154.67, 1164.65, 1174.63,
+ 1184.61, 1194.59, 1204.58, 1214.56, 1224.54, 1234.52,
+ 1244.50, 1254.48, 1264.46, 1274.44, 1284.42, 1294.40,
+ 1304.38, 1314.37, 1324.35, 1334.33, 1344.31, 1354.29,
+ 1364.27, 1374.25, 1384.23, 1394.21, 1404.19, 1414.18,
+ 1424.16, 1434.14, 1444.12, 1454.10, 1464.08, 1474.06,
+ 1484.04, 1494.02, 1504.00, 1513.99, 1523.97, 1533.95,
+ 1543.93, 1553.91, 1563.89, 1573.87, 1583.85, 1593.83,
+ 1603.81, 1613.80, 1623.78, 1633.76, 1643.74, 1653.72,
+ 1663.70, 1673.68, 1683.66, 1693.64, 1703.62, 1713.60,
+ 1723.59, 1733.57, 1743.55, 1753.53, 1763.51, 1773.49,
+ 1783.47, 1793.45, 1803.43, 1813.41, 1823.40, 1833.38,
+ 1843.36, 1853.34, 1863.32, 1873.30, 1883.28, 1893.26,
+ 1903.24, 1913.22, 1923.21, 1933.19, 1943.17, 1953.15,
+ 1963.13, 1973.11, 1983.09, 1993.07, 2003.05, 2013.03,
+ 2023.01, 2033.00, 2042.98, 2052.96, 2062.94, 2072.92,
+ 2082.90, 2092.88, 2102.86, 2112.84, 2122.82, 2132.81,
+ 2142.79, 2152.77, 2162.75, 2172.73, 2182.71, 2192.69,
+ 2202.67, 2212.65, 2222.63, 2232.62, 2242.60, 2252.58,
+ 2262.56, 2272.54, 2282.52, 2292.50, 2302.48, 2312.46,
+ 2322.44, 2332.42, 2342.41, 2352.39, 2362.37, 2372.35,
+ 2382.33, 2392.31, 2402.29, 2412.27, 2422.25, 2432.23,
+ 2442.22, 2452.20, 2462.18, 2472.16, 2482.14, 2492.12,
+ 2502.10, 2512.08, 2522.06, 2532.04, 2542.03, 2552.01,
+ 2561.99, 2571.97, 2581.95, 2591.93, 2601.91, 2611.89,
+ 2621.87, 2631.85, 2641.83, 2651.82, 2661.80, 2671.78,
+ 2681.76, 2691.74, 2701.72, 2711.70, 2721.68, 2731.66,
+ 2741.64, 2751.63, 2761.61, 2771.59, 2781.57, 2791.55,
+ 2801.53, 2811.51, 2821.49, 2831.47, 2841.45, 2851.44,
+ 2861.42, 2871.40, 2881.38, 2891.36, 2901.34, 2911.32,
+ 2921.30, 2931.28, 2941.26, 2951.25, 2961.23, 2971.21,
+ 2981.19, 2991.17)
+ Width = (12.31, 12.30, 12.30, 12.29, 12.29, 12.28, 12.28, 12.27,
+ 12.27, 12.26, 12.26, 12.26, 12.25, 12.25, 12.25, 12.24,
+ 12.24, 12.24, 12.24, 12.23, 12.23, 12.23, 12.23, 12.23,
+ 12.22, 12.22, 12.22, 12.22, 12.22, 12.22, 12.22, 12.22,
+ 12.22, 12.22, 12.22, 12.22, 12.22, 12.22, 12.22, 12.22,
+ 12.22, 12.23, 12.23, 12.23, 12.23, 12.23, 12.23, 12.24,
+ 12.24, 12.24, 12.24, 12.24, 12.25, 12.25, 12.25, 12.26,
+ 12.26, 12.26, 12.26, 12.27, 12.27, 12.27, 12.28, 12.28,
+ 12.29, 12.29, 12.29, 12.30, 12.30, 12.31, 12.31, 12.31,
+ 12.32, 12.32, 12.33, 12.33, 12.34, 12.34, 12.35, 12.35,
+ 12.36, 12.36, 12.37, 12.37, 12.38, 12.38, 12.39, 12.39,
+ 12.40, 12.40, 12.41, 12.41, 12.42, 12.42, 12.43, 12.43,
+ 12.44, 12.45, 12.45, 12.46, 12.46, 12.47, 12.47, 12.48,
+ 12.48, 12.49, 12.50, 12.50, 12.51, 12.51, 12.52, 12.52,
+ 12.53, 12.53, 12.54, 12.55, 12.55, 12.56, 12.56, 12.57,
+ 12.57, 12.58, 12.58, 12.59, 12.59, 12.60, 12.60, 12.61,
+ 12.61, 12.62, 12.62, 12.63, 12.63, 12.64, 12.64, 12.65,
+ 12.65, 12.66, 12.66, 12.67, 12.67, 12.68, 12.68, 12.68,
+ 12.69, 12.69, 12.70, 12.70, 12.70, 12.71, 12.71, 12.71,
+ 12.72, 12.72, 12.72, 12.73, 12.73, 12.73, 12.74, 12.74,
+ 12.74, 12.74, 12.75, 12.75, 12.75, 12.75, 12.76, 12.76,
+ 12.76, 12.76, 12.76, 12.76, 12.76, 12.76, 12.77, 12.77,
+ 12.77, 12.77, 12.77, 12.77, 12.77, 12.77, 12.77, 12.77,
+ 12.77, 12.77, 12.76, 12.76, 12.76, 12.76, 12.76, 12.76,
+ 12.75, 12.75, 12.75, 12.75, 12.74, 12.74, 12.74, 12.74,
+ 12.73, 12.73, 12.72, 12.72, 12.72, 12.71, 12.71, 12.70,
+ 12.70, 12.69, 12.69, 12.68, 12.67, 12.67, 12.66, 12.65,
+ 12.65, 12.64, 12.63, 12.63, 12.62, 12.61, 12.60, 12.59,
+ 12.58, 12.58, 12.57, 12.56, 12.55, 12.54, 12.53, 12.52,
+ 12.51, 12.50, 12.48, 12.47, 12.46, 12.45, 12.44, 12.42,
+ 12.41, 12.40, 12.38, 12.37, 12.36, 12.34, 12.33, 12.31,
+ 12.30, 12.28, 12.27, 12.25, 12.23, 12.22, 12.20, 12.18)
+ FilterNumber = (5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20,
+ 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35,
+ 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48, 49, 50,
+ 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65,
+ 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 80,
+ 81, 82, 83, 84, 85, 86, 87, 88, 89, 90, 91, 92, 93, 94, 95,
+ 96, 97, 98, 99, 100, 101, 102, 103, 104, 105, 106, 107,
+ 108, 109, 110, 111, 112, 113, 114, 115, 116, 117, 118, 119,
+ 120, 121, 122, 123, 124, 125, 126, 127, 128, 129, 130, 131,
+ 132, 133, 134, 135, 136, 137, 138, 139, 140, 141, 142, 143,
+ 144, 145, 146, 147, 148, 149, 150, 151, 152, 153, 154, 155,
+ 156, 157, 158, 159, 160, 161, 162, 163, 164, 165, 166, 167,
+ 168, 169, 170, 171, 172, 173, 174, 175, 176, 177, 178, 179,
+ 180, 181, 182, 183, 184, 185, 186, 187, 188, 189, 190, 191,
+ 192, 193, 194, 195, 196, 197, 198, 199, 200, 201, 202, 203,
+ 204, 205, 206, 207, 208, 209, 210, 211, 212, 213, 214, 215,
+ 216, 217, 218, 219, 220, 221, 222, 223, 224, 225, 226, 227,
+ 228, 229, 230, 231, 232, 233, 234, 235, 236, 237, 238, 239,
+ 240, 241, 242, 243, 244, 245, 246, 247, 248, 249, 250, 251,
+ 252, 253, 254, 255, 256, 257, 258, 259, 260)
+ OriginalBand = (1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17,
+ 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32,
+ 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47,
+ 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62,
+ 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77,
+ 78, 79, 80, 81, 82, 83, 84, 85, 86, 87, 88, 89, 90, 91, 92,
+ 93, 94, 95, 96, 97, 98, 99, 100, 101, 102, 103, 104, 105,
+ 106, 107, 108, 109, 110, 111, 112, 113, 114, 115, 116, 117,
+ 118, 119, 120, 121, 122, 123, 124, 125, 126, 127, 128, 129,
+ 130, 131, 132, 133, 134, 135, 136, 137, 138, 139, 140, 141,
+ 142, 143, 144, 145, 146, 147, 148, 149, 150, 151, 152, 153,
+ 154, 155, 156, 157, 158, 159, 160, 161, 162, 163, 164, 165,
+ 166, 167, 168, 169, 170, 171, 172, 173, 174, 175, 176, 177,
+ 178, 179, 180, 181, 182, 183, 184, 185, 186, 187, 188, 189,
+ 190, 191, 192, 193, 194, 195, 196, 197, 198, 199, 200, 201,
+ 202, 203, 204, 205, 206, 207, 208, 209, 210, 211, 212, 213,
+ 214, 215, 216, 217, 218, 219, 220, 221, 222, 223, 224, 225,
+ 226, 227, 228, 229, 230, 231, 232, 233, 234, 235, 236, 237,
+ 238, 239, 240, 241, 242, 243, 244, 245, 246, 247, 248, 249,
+ 250, 251, 252, 253, 254, 255, 256)
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -86520
+ LeapSecond = $base/kernels/lsk/naif0012.tls
+ TargetAttitudeShape = ($base/kernels/pck/pck00009.tpc,
+ $chandrayaan1/kernels/pck/moon_080317.tf,
+ $chandrayaan1/kernels/pck/moon_assoc_me.tf)
+ TargetPosition = (Table,
+ $Chandrayaan1/kernels/tspk/moon_pa_de421_1900-
+ -2050.bpc,
+ $Chandrayaan1/kernels/tspk/de421.bsp)
+ InstrumentPointing = (Table,
+ $chandrayaan1/kernels/ck/M3T20090630T083407_V-
+ 03_L1B_nadir-jig_2016-04-29.bc)
+ Instrument = Null
+ SpacecraftClock = $chandrayaan1/kernels/sclk/aig_ch1_sclk_compl-
+ ete_biased_m1p816.tsc
+ InstrumentPosition = (Table,
+ $chandrayaan1/kernels/spk/M3T20090630T083407_-
+ V03_L1B_nadir-jig_2016-04-29.bsp)
+ InstrumentAddendum = $chandrayaan1/kernels/iak/m3Addendum005.ti
+ ShapeModel = Null
+ InstrumentPositionQuality = Reconstructed
+ InstrumentPointingQuality = Reconstructed
+ CameraVersion = 1
+ Source = isis
+ End_Group
+
+ Group = RadiometricCalibration
+ Units = W/m2/um/sr
+ SolarDistance = 1.01711556761 <AU>
+ DetectorTemperature = 161.99
+ SpectralCalibrationFileName = M3T20070912_RDN_SPC.TAB
+ RadGainFactorFileName = M3T20070912_RDN_GAIN.TAB
+ GlobalBandpassFileName = M3T20070912_RDN_SPC.TAB
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = Table
+ Name = UtcFile
+ StartByte = 117804
+ Bytes = 250
+ Records = 5
+ ByteOrder = Lsb
+
+ Group = Field
+ Name = LineNumber
+ Type = Integer
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = UtcTime
+ Type = Text
+ Size = 26
+ End_Group
+
+ Group = Field
+ Name = Year
+ Type = Text
+ Size = 4
+ End_Group
+
+ Group = Field
+ Name = Ddoy
+ Type = Text
+ Size = 16
+ End_Group
+End_Object
+
+Object = Table
+ Name = InstrumentPointing
+ StartByte = 121420
+ Bytes = 280
+ Records = 7
+ ByteOrder = Lsb
+ TimeDependentFrames = (-86000, 1)
+ ConstantFrames = (-86520, -86000)
+ ConstantRotation = (1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 0.0, 1.0)
+ CkTableStartTime = 299622941.60815
+ CkTableEndTime = 299622941.86255
+ CkTableOriginalSize = 6
+ FrameTypeCode = 3
+ Description = "Created by spiceinit"
+ Kernels = $chandrayaan1/kernels/ck/M3T20090630T083407_V03_L1B_n-
+ adir-jig_2016-04-29.bc
+
+ Group = Field
+ Name = J2000Q0
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = InstrumentPosition
+ StartByte = 121700
+ Bytes = 168
+ Records = 3
+ ByteOrder = Lsb
+ CacheType = HermiteSpline
+ SpkTableStartTime = 299622941.60815
+ SpkTableEndTime = 299622941.86255
+ SpkTableOriginalSize = 6.0
+ Description = "Created by spiceinit"
+ Kernels = $chandrayaan1/kernels/spk/M3T20090630T083407_V03_L1B-
+ _nadir-jig_2016-04-29.bsp
+
+ Group = Field
+ Name = J2000X
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Y
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Z
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000XV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000YV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000ZV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = BodyRotation
+ StartByte = 126444
+ Bytes = 128
+ Records = 2
+ ByteOrder = Lsb
+ TimeDependentFrames = (31006, 1)
+ ConstantFrames = (31001, 31007, 31006)
+ ConstantRotation = (0.99999987325471, -3.29285422375571e-04,
+ 3.80869618671387e-04, 3.29286000210947e-04,
+ 0.99999994578431, -1.45444093783627e-06,
+ -3.80869119096078e-04, 1.57985578682691e-06,
+ 0.99999992746811)
+ CkTableStartTime = 299622941.60815
+ CkTableEndTime = 299622941.86255
+ CkTableOriginalSize = 2
+ FrameTypeCode = 6
+ Description = "Created by spiceinit"
+ Kernels = ($Chandrayaan1/kernels/tspk/moon_pa_de421_1900-2050.b-
+ pc, $Chandrayaan1/kernels/tspk/de421.bsp,
+ $base/kernels/pck/pck00009.tpc,
+ $chandrayaan1/kernels/pck/moon_080317.tf,
+ $chandrayaan1/kernels/pck/moon_assoc_me.tf)
+ SolarLongitude = 156.75392732777
+
+ Group = Field
+ Name = J2000Q0
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = SunPosition
+ StartByte = 132013
+ Bytes = 112
+ Records = 2
+ ByteOrder = Lsb
+ CacheType = Linear
+ SpkTableStartTime = 299622941.60815
+ SpkTableEndTime = 299622941.86255
+ SpkTableOriginalSize = 2.0
+ Description = "Created by spiceinit"
+ Kernels = ($Chandrayaan1/kernels/tspk/moon_pa_de421_1900-2050.-
+ bpc, $Chandrayaan1/kernels/tspk/de421.bsp)
+
+ Group = Field
+ Name = J2000X
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Y
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Z
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000XV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000YV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000ZV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 132125
+ Bytes = 6290
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 102017
+ Bytes = 15787
+End_Object
+
+Object = NaifKeywords
+ BODY_CODE = 301
+ BODY301_RADII = (1737.4, 1737.4, 1737.4)
+ BODY_FRAME_CODE = 31001
+ INS-86520_SWAP_OBSERVER_TARGET = TRUE
+ INS-86520_LIGHTTIME_CORRECTION = NONE
+ INS-86520_LT_SURFACE_CORRECT = TRUE
+ INS-86520_FOCAL_LENGTH = 39.63
+ INS-86520_PIXEL_PITCH = 0.027
+ CLOCK_ET_-86_12/1759056.764_COMPUTED = b7af9b1de2dbb141
+ INS-86520_TRANSX = (-0.64, -4.00552916405788e-05,
+ 0.026999970288384)
+ INS-86520_TRANSY = (-0.052, -0.026999970288384,
+ -4.00552916405788e-05)
+ INS-86520_ITRANSS = (-1.9610889460164,
+ -0.054945530371164, -37.036996280362)
+ INS-86520_ITRANSL = (23.700820451852, 37.036996280362,
+ -0.054945530371164)
+ INS-86520_BORESIGHT_SAMPLE = 304.5
+ INS-86520_BORESIGHT_LINE = 0.0
+ INS-86520_PP = (0.0, 0.0)
+ INS-86520_OD_K = (3.79921103637315e-04,
+ 2.13226448051461e-04,
+ -4.01862878758592e-08)
+ INS-86520_DECENTER = (0.004047, -5.0e-06)
+End_Object
+End
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/aig_ch1_sclk_complete_biased_m1p816_unix.tsc b/tests/pytests/data/M3T20090630T083407_V03_RDN/aig_ch1_sclk_complete_biased_m1p816_unix.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..568e766bb9c29de51fc128e3cd17aba5ac96f88f
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/aig_ch1_sclk_complete_biased_m1p816_unix.tsc
@@ -0,0 +1,623 @@
+KPL/SCLK
+
+This is a CHANDRAYAAN-1 SCLK file.
+
+It has two fields, OBT seconds and milliseconds.
+It rolls over every 21 days resulting in a large number of partitions, each starting at 0 ticks
+and ending at 1814400000 ticks. The total of 40 partitions set in this
+file should allow conversions from the clock start up to 2010-DEC-31.
+
+This SCLK was built by Joe Boardman on September 10, 2009, from raw
+data provided by UmaDevi at ISRO. It spans the full mission. It tracks the OBT/Time to about 1 msec using multiple piecewise linear segments.
+
+This kernel DOES include the minus 1.816 second time bias required to lock with the ISRO SCLK due to frame buffering.
+
+The parallel time system is TDT.
+
+\begindata
+
+SCLK_KERNEL_ID = ( @2009-02-16 )
+
+SCLK_DATA_TYPE_86 = ( 1 )
+SCLK01_TIME_SYSTEM_86 = ( 2 )
+SCLK01_N_FIELDS_86 = ( 2 )
+SCLK01_MODULI_86 = ( 1814400 1000 )
+SCLK01_OFFSETS_86 = ( 0 0 )
+SCLK01_OUTPUT_DELIM_86 = ( 1 )
+
+SCLK_PARTITION_START_86 = (
+ 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
+ )
+
+SCLK_PARTITION_END_86 = (
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
+ 1814400000
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+\begintext
+
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/chan1m32isisTEMP.forwardAscending_0.xsp b/tests/pytests/data/M3T20090630T083407_V03_RDN/chan1m32isisTEMP.forwardAscending_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..65a3a85036540e16e3728a3ab35ae92454b492f9
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/chan1m32isisTEMP.forwardAscending_0.xsp
@@ -0,0 +1,183 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
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+
+; Created 2022-08-12/16:51:29.00.
+;
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+
+LEAPSECONDS_KERNEL = /Volumes/pkgs/isis3/isis_data//base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ../sliced_kernels/chan1m32isisTEMP.forwardAscending_0.bsp
+SOURCE_SPK_KERNEL = /Volumes/pkgs/isis3/isis_data//chandrayaan1/kernels/tspk/de421.bsp
+ INCLUDE_COMMENTS = NO
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+ BEGIN_TIME = 2009 JUN 30 08:24:07.876
+ END_TIME = 2009 JUN 30 08:28:10.258
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/chan1m32isisTEMP.forwardAscending_1.xsp b/tests/pytests/data/M3T20090630T083407_V03_RDN/chan1m32isisTEMP.forwardAscending_1.xsp
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--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/chan1m32isisTEMP.forwardAscending_1.xsp
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+'11DBE20ECD4F37^8'
+'11DBE20EDA55B^8'
+'11DBE20EE75C28^8'
+'11DBE20EF462A1^8'
+'11DBE20F01691A^8'
+'11DBE20F0E6F93^8'
+'11DBE20F1B760C^8'
+'11DBE20F287C84^8'
+'11DBE20F3582FD^8'
+'11DBE20F428976^8'
+'11DBE20F4F8FEE^8'
+'11DBE20F5C9667^8'
+'11DBE20F699CE^8'
+'11DBE20F76A359^8'
+'11DBE20F83A9D2^8'
+'11DBE20F90B04A^8'
+'11DBE20F9DB6C3^8'
+'11DBE20FAABD3C^8'
+'11DBE20FB7C3B4^8'
+'11DBE20FC4CA2D^8'
+'11DBE20FD1D0A6^8'
+'11DBE20FDED71F^8'
+'11DBE20FEBDD98^8'
+'11DBE20FF8E41^8'
+'11DBE21005EA89^8'
+'11DBE21012F102^8'
+'11DBE2101FF77A^8'
+'11DBE2102CFDF3^8'
+'11DBE2103A046C^8'
+'11DBE210470AE5^8'
+'11DBE21054115E^8'
+'11DBE2106117D6^8'
+'11DBE2106E1E4F^8'
+'11DBE2107B24C8^8'
+'11DBE210882B4^8'
+'11DBE2109531B9^8'
+'11DBE210A23832^8'
+'11DBE210AF3EAB^8'
+'11DBE210BC4524^8'
+'11DBE210C94B9C^8'
+'11DBE210D65215^8'
+'11DBE210E3588E^8'
+'11DBE210F05F06^8'
+'11DBE210FD657F^8'
+'11DBE2110A6BF8^8'
+'11DBE211177271^8'
+'11DBE2112478EA^8'
+'11DBE211317F62^8'
+'11DBE2113E85DB^8'
+'11DBE2114B8C54^8'
+'11DBE2115892CC^8'
+'11DBE211659945^8'
+'11DBE211729FBE^8'
+'11DBE2117FA637^8'
+'11DBE2118CACB^8'
+'11DBE21199B328^8'
+'11DBE211A6B9A1^8'
+'11DBE211B3C01A^8'
+'11DBE211C0C692^8'
+'11DBE211CDCD0B^8'
+'11DBE211DAD384^8'
+'11DBE211E7D9FD^8'
+'11DBE211F4E076^8'
+'11DBE21201E6EE^8'
+'11DBE2120EED67^8'
+'11DBE2121BF3E^8'
+'11DBE21228FA58^8'
+'11DBE2123600D1^8'
+'11DBE21243074A^8'
+'11DBE212500DC3^8'
+'11DBE2125D143C^8'
+'11DBE2126A1AB4^8'
+'11DBE21277212D^8'
+'11DBE2128427A6^8'
+'11DBE212912E1E^8'
+'11DBE2129E3497^8'
+'11DBE212AB3B1^8'
+'11DBE212B84189^8'
+'11DBE212C54802^8'
+'11DBE212D24E7A^8'
+'11DBE212DF54F3^8'
+'11DBE212EC5B6C^8'
+'11DBE212F961E4^8'
+'11DBE21306685D^8'
+'11DBE213136ED6^8'
+'11DBE21320754F^8'
+'11DBE2132D7BC8^8'
+'11DBE2133A824^8'
+'11DBE2134788B9^8'
+'11DBE213548F32^8'
+'11DBE2136195AA^8'
+'11DBE2136E9C23^8'
+'11DBE2137BA29C^8'
+'11DBE21388A915^8'
+'11DBE21395AF8E^8'
+'11DBE213A2B606^8'
+'11DBE213AFBC7F^8'
+'11DBE213BCC2F8^8'
+'11DBE213C9C97^8'
+'11DBE213D6CFE9^8'
+'11DBE213E3D662^8'
+'11DBE213F0DCDB^8'
+'11DBE213FDE354^8'
+'11DBE2140AE9CC^8'
+'11DBE21417F045^8'
+'11DBE21424F6BE^8'
+'11DBE21431FD36^8'
+'11DBE2143F03AF^8'
+'11DBE2144C0A28^8'
+'11DBE2145910A1^8'
+'11DBE21466171A^8'
+'11DBE214731D92^8'
+'11DBE21480240B^8'
+'11DBE2148D2A84^8'
+'11DBE2149A30FC^8'
+'11DBE214A73775^8'
+'11DBE214B43DEE^8'
+'11DBE214C14467^8'
+'11DBE214CE4AE^8'
+'11DBE214DB5158^8'
+'11DBE214E857D1^8'
+'11DBE214F55E4A^8'
+'11DBE2150264C2^8'
+'11DBE2150F6B3B^8'
+'11DBE2151C71B4^8'
+'11DBE21529782D^8'
+'11DBE215367EA6^8'
+'11DBE21543851E^8'
+'11DBE215508B97^8'
+'11DBE2155D921^8'
+'11DBE2156A9888^8'
+'11DBE215779F01^8'
+'11DBE21584A57A^8'
+'11DBE21591ABF3^8'
+'11DBE2159EB26C^8'
+'11DBE215ABB8E4^8'
+'11DBE215B8BF5D^8'
+'11DBE215C5C5D6^8'
+'11DBE215D2CC4E^8'
+'11DBE215DFD2C7^8'
+'11DBE215ECD94^8'
+'11DBE215F9DFB9^8'
+'11DBE21606E632^8'
+'11DBE21613ECAA^8'
+'11DBE21620F323^8'
+'11DBE2162DF99C^8'
+'11DBE2163B0014^8'
+'11DBE21648068D^8'
+'11DBE216550D06^8'
+'11DBE21662137F^8'
+'11DBE2166F19F8^8'
+'11DBE2167C207^8'
+'11DBE2168926E9^8'
+'11DBE216962D62^8'
+'11DBE216A333DA^8'
+'11DBE216B03A53^8'
+'11DBE216BD40CC^8'
+'11DBE216CA4745^8'
+'11DBE216D74DBE^8'
+'11DBE216E45436^8'
+'11DBE216F15AAF^8'
+'11DBE216FE6128^8'
+'11DBE2170B67A^8'
+'11DBE217186E19^8'
+'11DBE217257492^8'
+'11DBE217327B0B^8'
+'11DBE2173F8184^8'
+'11DBE2174C87FC^8'
+'11DBE217598E75^8'
+'11DBE2176694EE^8'
+'11DBE217739B66^8'
+'11DBE21780A1DF^8'
+'11DBE2178DA858^8'
+'11DBE2179AAED1^8'
+'11DBE217A7B54A^8'
+'11DBE217B4BBC2^8'
+'11DBE217C1C23B^8'
+'11DBE217CEC8B4^8'
+'11DBE217DBCF2C^8'
+'11DBE217E8D5A5^8'
+'11DBE217F5DC1E^8'
+'11DBE21802E297^8'
+'11DBE2180FE91^8'
+'11DBE2181CEF88^8'
+'11DBE21829F601^8'
+'11DBE21836FC7A^8'
+'11DBE2184402F2^8'
+'11DBE21851096B^8'
+'11DBE2185E0FE4^8'
+'11DBE2186B165D^8'
+'11DBE218781CD6^8'
+'11DBE21885234E^8'
+'11DBE2189229C7^8'
+'11DBE2189F304^8'
+'11DBE218AC36B8^8'
+'11DBE218B93D31^8'
+'11DBE218C643AA^8'
+'11DBE218D34A23^8'
+'11DBE218E0509C^8'
+'11DBE218ED5714^8'
+'11DBE218FA5D8D^8'
+'11DBE219076406^8'
+'11DBE219146A7E^8'
+'11DBE2192170F7^8'
+'11DBE2192E777^8'
+'11DBE2193B7DE9^8'
+'11DBE219488462^8'
+'11DBE219558ADA^8'
+'11DBE219629153^8'
+'11DBE2196F97CC^8'
+'11DBE2197C9E44^8'
+'11DBE21989A4BD^8'
+'11DBE21996AB36^8'
+'11DBE219A3B1AF^8'
+'11DBE219B0B828^8'
+'11DBE219BDBEA^8'
+'11DBE219CAC519^8'
+'11DBE219D7CB92^8'
+'11DBE219E4D20A^8'
+'11DBE219F1D883^8'
+'11DBE219FEDEFC^8'
+'11DBE21A0BE575^8'
+'11DBE21A18EBEE^8'
+'11DBE21A25F266^8'
+'11DBE21A32F8DF^8'
+'11DBE21A3FFF58^8'
+'11DBE21A4D05D^8'
+'11DBE21A5A0C49^8'
+'11DBE21A6712C2^8'
+'11DBE21A74193B^8'
+'11DBE21A811FB4^8'
+'11DBE21A8E262C^8'
+'11DBE21A9B2CA5^8'
+'11DBE21AA8331E^8'
+'11DBE21AB53996^8'
+'11DBE21AC2400F^8'
+'11DBE21ACF4688^8'
+'11DBE21ADC4D01^8'
+'11DBE21AE9537A^8'
+'11DBE21AF659F2^8'
+'11DBE21B03606B^8'
+'11DBE21B1066E4^8'
+'11DBE21B1D6D5C^8'
+'11DBE21B2A73D5^8'
+'11DBE21B377A4E^8'
+'11DBE21B4480C7^8'
+'11DBE21B51874^8'
+'11DBE21B5E8DB8^8'
+'11DBE21B6B9431^8'
+'11DBE21B789AAA^8'
+'11DBE21B85A122^8'
+'11DBE21B92A79B^8'
+'11DBE21B9FAE14^8'
+'11DBE21BACB48D^8'
+'11DBE21BB9BB06^8'
+'11DBE21BC6C17E^8'
+'11DBE21BD3C7F7^8'
+'11DBE21BE0CE7^8'
+'11DBE21BEDD4E8^8'
+'11DBE21BFADB61^8'
+'11DBE21C07E1DA^8'
+'11DBE21C14E853^8'
+'11DBE21C21EECC^8'
+'11DBE21C2EF544^8'
+'11DBE21C3BFBBD^8'
+'11DBE21C490236^8'
+'11DBE21C5608AE^8'
+'11DBE21C630F27^8'
+'11DBE21C7015A^8'
+'11DBE21C7D1C19^8'
+'11DBE21C8A2292^8'
+'11DBE21C97290A^8'
+'11DBE21CA42F83^8'
+'11DBE21CB135FC^8'
+'11DBE21CBE3C74^8'
+'11DBE21CCB42ED^8'
+'11DBE21CD84966^8'
+'11DBE21CE54FDF^8'
+'11DBE21CF25658^8'
+'11DBE21CFF5CD^8'
+'11DBE21D0C6349^8'
+'11DBE21D1969C2^8'
+'11DBE21D26703A^8'
+'11DBE21D3376B3^8'
+'11DBE21D407D2C^8'
+'11DBE21D4D83A5^8'
+'11DBE21D5A8A1E^8'
+'11DBE21D679096^8'
+'11DBE21D74970F^8'
+'11DBE21D819D88^8'
+'11DBE21D8EA4^8'
+'11DBE21D9BAA79^8'
+'11DBE21DA8B0F2^8'
+'11DBE21DB5B76B^8'
+'11DBE21DC2BDE4^8'
+'11DBE21DCFC45C^8'
+'11DBE21DDCCAD5^8'
+'11DBE21DDD8F71^8'
+'11DBE206270308^8'
+'11DBE20B3D8A32^8'
+'11DBE21054115E^8'
+'11DBE2156A9888^8'
+'11DBE21A811FB4^8'
+'7^1'
+'237^3'
+END_ARRAY 4 3976
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; ../sliced_kernels/chan1m32isisTEMP.forwardAscending_1.bsp LOG FILE
+
+; Created 2022-08-12/16:51:32.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Volumes/pkgs/isis3/isis_data//base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ../sliced_kernels/chan1m32isisTEMP.forwardAscending_1.bsp
+SOURCE_SPK_KERNEL = /Volumes/pkgs/isis3/isis_data//chandrayaan1/kernels/tspk/de421.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 3, 10, 301
+ BEGIN_TIME = 2009 JUN 30 08:32:35.424
+ END_TIME = 2009 JUN 30 08:36:35.678
+SOURCE_SPK_KERNEL = /Volumes/pkgs/isis3/isis_data//chandrayaan1/kernels/spk/M3T20090630T083407_V03_L1B_nadir-jig_2016-04-29.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -86
+ BEGIN_TIME = 2009 JUN 30 08:34:06.979
+ END_TIME = 2009 JUN 30 08:34:35.681
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/m3Addendum005.ti b/tests/pytests/data/M3T20090630T083407_V03_RDN/m3Addendum005.ti
new file mode 100644
index 0000000000000000000000000000000000000000..655c685f44ff38ae01f6ceacd7a9310f3303efe0
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/m3Addendum005.ti
@@ -0,0 +1,58 @@
+\begindata
+
+ FRAME_CH1_SPACECRAFT = -86000
+ FRAME_-86000_NAME = 'CH1_SPACECRAFT'
+ FRAME_-86000_CLASS = 3
+ FRAME_-86000_CLASS_ID = -86000
+ FRAME_-86000_CENTER = -86
+ CK_-86000_SCLK = -86
+ CK_-86000_SPK = -86
+
+
+ FRAME_CHANDRAYAAN-1_M3 = -86520
+ FRAME_-86520_NAME = 'CHANDRAYAAN-1_M3'
+ FRAME_-86520_CLASS = 4
+ FRAME_-86520_CLASS_ID = -86520
+ FRAME_-86520_CENTER = -86
+ TKFRAME_-86520_RELATIVE = 'CH1_SPACECRAFT'
+ TKFRAME_-86520_SPEC = 'ANGLES'
+ TKFRAME_-86520_ANGLES = ( 0.0 0.0 0.0 )
+ TKFRAME_-86520_AXES = ( 1, 2, 3 )
+ TKFRAME_-86520_UNITS = 'DEGREES'
+
+ INS-86520_PLATFORM_ID = ( -86000 )
+
+ INS-86520_PIXEL_PITCH = 0.027
+ INS-86520_FOCAL_LENGTH = 39.63
+
+ INS-86520_BORESIGHT_SAMPLE = 304.5
+ INS-86520_BORESIGHT_LINE = 0.0
+
+ INS-86520_TRANSX = ( -0.64, -0.0000400552916405788, 0.0269999702883839)
+ INS-86520_TRANSY = ( -0.052, -0.0269999702883839, -0.0000400552916405788)
+
+ INS-86520_ITRANSS = ( -1.96108894601637, -0.0549455303711644, -37.036996280362 )
+ INS-86520_ITRANSL = ( 23.7008204518524, 37.036996280362, -0.0549455303711644 )
+
+ INS-86520_PP = ( 0.0, 0.0 )
+ INS-86520_OD_K = ( 0.000379921103637315, 0.000213226448051461, -4.01862878758592E-08 )
+ INS-86520_DECENTER = ( 0.004047, -0.000005 )
+
+\begintext
+ These are the parameters required for writing c-kernels. For
+ the Chandrayaan1 spacecraft the ck frame is CH1_SPACECRAFT (-86000),
+ and the ck reference frame is J2000 (1).
+
+\begindata
+ INS-86520_CK_FRAME_ID=-86000
+ INS-86520_CK_REFERENCE_ID=1
+
+\begintext
+ These parameters control the light time, stelar aberation, and observer swap
+ The parameters are set for best results with the low altitude of Chan-1
+
+\begindata
+ INS-86520_SWAP_OBSERVER_TARGET = 'TRUE'
+ INS-86520_LIGHTTIME_CORRECTION = 'NONE'
+ INS-86520_LT_SURFACE_CORRECT = 'TRUE'
+
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_080317.tf b/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_080317.tf
new file mode 100644
index 0000000000000000000000000000000000000000..79b7c73bab4b32d67cb35c7818f57d09c652743f
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_080317.tf
@@ -0,0 +1,599 @@
+KPL/FK
+
+
+ SPICE Lunar Reference Frame Specification Kernel
+ =====================================================================
+
+ Original file name: moon_080317.tf
+ Creation date: 2008 March 17 20:10
+ Created by: Nat Bachman (NAIF/JPL)
+ Date of last revision: 2008 March 21 16:07
+ Purpose of revision:
+
+ Changed names of PA system and frame from "principal axis" to
+ "principal axes."
+
+
+ Version description:
+
+ This frame kernel contains lunar frame specifications compatible
+ with the current lunar binary PCK file
+
+ moon_pa_de421_1900-2050.bpc
+
+ The above PCK contains lunar orientation data from the DE-421 JPL
+ Planetary Ephemeris.
+
+ The previous NAIF lunar frame specification kernel was
+
+ moon_071218.tf
+
+ That kernel is compatible with the DE-418-based lunar binary PCK
+ file
+
+ moon_pa_de418_1950-2050.bpc
+
+ The comment section below titled "Lunar body-fixed frame
+ associations" discusses lunar frame association kernels. These
+ kernels direct portions of the SPICE system that rely on default
+ body-fixed reference frames to associate with the Moon either the
+ MOON_ME or MOON_PA reference frames.
+
+
+ This file was modified on 26-FEB-2009 by Nat Bachman. The initial
+ blank line was removed and this change description was added.
+ Nothing else has been changed.
+
+
+ Frames Specified by this Kernel
+ =====================================================================
+
+ Frame Name Relative to Type Frame ID
+ -------------- ----------------- ----- --------
+ MOON_PA MOON_PA_DE421 FIXED 31000
+ MOON_ME MOON_ME_DE421 FIXED 31001
+ MOON_PA_DE421 ICRF/J2000 PCK 31006
+ MOON_ME_DE421 MOON_PA_DE421 FIXED 31007
+
+
+ Introduction
+ =====================================================================
+
+ This kernel specifies lunar body-fixed reference frames for use by
+ SPICE-based application software. These reference frames are
+ associated with high-accuracy lunar orientation data provided by the
+ JPL Solar System Dynamics Group's planetary ephemerides (both
+ trajectory and lunar orientation data are stored in these ephemeris
+ files). These ephemerides have names of the form DE-nnn (DE stands
+ for "developmental ephemeris").
+
+ The frames specified by this kernel are realizations of two different
+ lunar reference systems:
+
+ Principal Axes (PA) system
+ --------------------------
+ The axes of this system are defined by the principal axes of the
+ Moon. Due to the nature of the Moon's orbit and
+ rotation, the Z axis of this system does not coincide with the
+ Moon's mean spin axis, nor does the X axis coincide with the mean
+ direction to the center of the Earth (in contrast with the ME
+ system defined below).
+
+ Lunar principal axes frames realizing the lunar PA system and
+ specified by this kernel are associated with JPL planetary
+ ephemerides. Each new JPL planetary ephemeris can (but does not
+ necessarily) define a new realization of the lunar principal axes
+ system. Coordinates of lunar surface features expressed in lunar
+ PA frames can change slightly from one lunar ephemeris version to
+ the next.
+
+
+ Mean Earth/Polar Axis (ME) system
+ ---------------------------------
+ The Lunar mean Earth/polar axis system is a lunar body-fixed
+ reference system used in the IAU/IAG Working Group Report [2] to
+ describe the orientation of the Moon relative to the ICRF frame.
+ The +Z axis of this system is aligned with the north mean lunar
+ rotation axis, while the prime meridian contains the the mean
+ Earth direction.
+
+ This system is also sometimes called the "mean Earth/mean
+ rotation axis" system or "mean Earth" system.
+
+ The mean directions used to define the axes of a mean Earth/polar
+ axis reference frame realizing the lunar ME system and specified
+ by this kernel are associated with a given JPL planetary
+ ephemeris version. The rotation between the mean Earth frame for
+ a given ephemeris version and the associated principal axes frame
+ is given by a constant matrix (see [1]).
+
+
+ For the current JPL planetary ephemeris (DE), this kernel includes
+ specifications of the corresponding principal axes and mean Earth/
+ polar axis frames. The names of these frames have the form
+
+ MOON_PA_DEnnn
+
+ and
+
+ MOON_ME_DEnnn
+
+ respectively, where nnn is the version number of the DE. The set of
+ DE-dependent frame specifications will grow over time; frame
+ specifications pertaining to older DEs can be obtained from earlier
+ versions of this frame kernel.
+
+ For each of the two reference systems, there is a corresponding
+ "generic" frame specification: these generic frames are simply
+ aliases for the PA and ME frames associated with the latest DE. The
+ generic frame names are
+
+ MOON_PA
+ MOON_ME
+
+ These generic frame names are provided to enable SPICE-based
+ applications to refer to the latest DE-based (or other) lunar
+ rotation data without requiring code modifications as new kernels
+ become available. SPICE users may, if they wish, modify this kernel
+ to assign these frame aliases to other frames than those selected
+ here, for example, older DE-based frames. NAIF recommends that, if
+ this frame kernel is modified, the name of this file also be changed
+ to avoid confusion.
+
+
+ Comparison of PA and ME frames
+ ------------------------------
+
+ The rotation between the mean Earth frame for a given DE and the
+ associated principal axes frame for the same DE is given by a
+ constant matrix (see [1]). For DE-421, the rotation angle of this
+ matrix is approximately 0.0288473 degrees; this is equivalent to
+ approximately 875 m when expressed as a displacement along a great
+ circle on the Moon's surface.
+
+
+ Comparison of DE-based and IAU/IAG report-based ME frames
+ ---------------------------------------------------------
+
+ Within the SPICE system, a lunar ME frame specified by the
+ rotational elements from the IAU/IAG Working Group report [2] is
+ given the name IAU_MOON; the data defining this frame are provided
+ in a generic text PCK.
+
+ The orientation of the lunar ME frame obtained by applying the
+ DE-based PA-to-ME rotation described above to the DE-based lunar
+ libration data does not agree closely with the lunar ME frame
+ orientation given by the rotational elements from the IAU/IAG
+ Working Group report (that is, the IAU_MOON frame). The difference
+ is due to truncation of the libration series used in the report's
+ formula for lunar orientation (see [1]).
+
+ In the case of DE-421, for the time period ~2000-2020, the
+ time-dependent difference of these ME frame implementations has an
+ amplitude of approximately 0.0051 degrees, which is equivalent to
+ approximately 155 m, measured along a great circle on the Moon's
+ surface, while the average value is approximately 0.00249 degrees,
+ or 76 m.
+
+
+ Comparison of DE-421 and DE-418 Lunar Reference Frames
+ ======================================================
+
+ The magnitudes of the rotational offsets between the
+ DE-418 and DE-421 realizations of the MOON_PA and MOON_ME
+ frames are discussed below.
+
+ Note that the angle ranges shown below are ordered as signed values,
+ *not* by absolute value.
+
+ MOON_PA frame orientation differences
+ -------------------------------------
+
+ Tests performed by NAIF indicate an approximately 0.45 microradian
+ maximum rotation between the MOON_PA_DE418 and MOON_PA_DE421 frames,
+ based on a sampling of orientation data over the time period
+ 2000-2020. This offset corresponds to a displacement of about 0.79 m
+ along a great circle on the Moon's surface.
+
+ When the transformation from the MOON_PA_DE418 frame to the
+ MOON_PA_DE421 frame is decomposed as a 1-2-3 Euler angle sequence,
+ the offset angle ranges for each axis are:
+
+ X axis: -3.8063e-07 to -2.9746e-07 radians
+ Y axis: -2.5322e-07 to -1.8399e-07 radians
+ Z axis: -9.9373e-08 to 6.0046e-08 radians
+
+
+ MOON_ME frame orientation differences
+ -------------------------------------
+
+ Tests performed by NAIF indicate an approximately 0.27 microradian
+ maximum rotation between the MOON_ME_DE418 and MOON_ME_DE421 frames,
+ based on a sampling of orientation data over the time period
+ 2000-2020. This offset corresponds to a displacement of about 0.46 m
+ along a great circle on the Moon's surface.
+
+ When the transformation from the MOON_ME_DE418 frame to the
+ MOON_ME_DE421 frame is decomposed as a 1-2-3 Euler angle sequence,
+ the offset angle ranges for each axis are:
+
+ X axis: 7.2260e-09 to 9.0391e-08 radians
+ Y axis: 3.7643e-08 to 1.0691e-07 radians
+ Z axis: -2.4471e-07 to -8.5296e-08 radians
+
+
+ Regarding Use of the ICRF in SPICE
+ ==================================
+
+ The IERS Celestial Reference Frame (ICRF) is offset from the J2000
+ reference frame (equivalent to EME 2000) by a small rotation: the
+ J2000 pole offset magnitude is about 18 milliarcseconds (mas) and
+ the equinox offset magnitude is approximately 78 milliarcseconds
+ (see [3]).
+
+ Certain SPICE data products use the frame label "J2000" for data
+ that actually are referenced to the ICRF. This is the case for SPK
+ files containing JPL version DE-4nn planetary ephemerides, for
+ orientation data from generic text PCKs, and for binary PCKs,
+ including binary lunar PCKs used in conjunction with this lunar
+ frame kernel.
+
+ Consequently, when SPICE computes the rotation between the "J2000"
+ frame and either of the lunar PA or ME frames, what's computed is
+ actually the rotation between the ICRF and the respective lunar
+ frame.
+
+ Similarly, when SPICE is used to compute the state given by a JPL DE
+ planetary ephemeris SPK file of one ephemeris object relative to
+ another (for example, the state of the Moon with respect to the
+ Earth), expressed relative to the frame "J2000," the state is
+ actually expressed relative to the ICRF.
+
+ Because SPICE is already using the ICRF, users normally need not
+ use the J2000-to-ICRF transformation to adjust results computed
+ with SPICE.
+
+ Lunar body-fixed frame associations
+ =====================================================================
+
+ By default, the SPICE system considers the body-fixed reference
+ frame associated with the Moon to be the one named IAU_MOON. This
+ body-frame association affects the outputs of the SPICE frame system
+ routines
+
+ CIDFRM
+ CNMFRM
+
+ and of the SPICE time conversion and geometry routines
+
+ ET2LST
+ ILLUM
+ SRFXPT
+ SUBPT
+ SUBSOL
+
+ Also, any code that calls these routines to obtain results involving
+ lunar body-fixed frames are affected. Within SPICE, the only
+ higher-level system that is affected is the dynamic frame system.
+
+ NAIF provides "frame association" kernels that simplify changing the
+ body-fixed frame associated with the Moon. Using FURNSH to load
+ either of the kernels named below changes the Moon's body-fixed
+ frame from its current value, which initially is IAU_MOON, to that
+ shown in the right-hand column:
+
+ Kernel name Lunar body-fixed frame
+ ----------- ----------------------
+ moon_assoc_me.tf MOON_ME
+ moon_assoc_pa.tf MOON_PA
+
+ For further information see the in-line comments in the association
+ kernels themselves. Also see the Frames Required Reading section
+ titled "Connecting an Object to its Body-fixed Frame."
+
+ In the N0062 SPICE Toolkit, the routines
+
+ ILLUM
+ SRFXPT
+ SUBPT
+ SUBSOL
+
+ are superseded, respectively, by the routines
+
+ ILUMIN
+ SINCPT
+ SUBPNT
+ SUBSLR
+
+ The newer routines don't require frame association kernels: the name
+ of the target body's body-fixed reference frame is an input argument
+ to these routines.
+
+
+ Using this Kernel
+ =====================================================================
+
+ In order for a SPICE-based application to use reference frames
+ specified by this kernel, the application must load both this kernel
+ and a binary lunar PCK containing lunar orientation data for the
+ time of interest. Normally the kernels need be loaded only once
+ during program initialization.
+
+ SPICE users may find it convenient to use a meta-kernel (also called
+ a "FURNSH kernel") to name the kernels to be loaded. Below, we show
+ an example of such a meta-kernel, as well as the source code of a
+ small Fortran program that uses lunar body fixed frames. The
+ program's output is included as well.
+
+ The kernel names shown here are simply used as examples; users must
+ select the kernels appropriate for their applications.
+
+ Numeric results shown below may differ very slightly from those
+ obtained on users' computer systems.
+
+
+ Meta-kernel
+ -----------
+
+
+ KPL/MK
+
+
+ Example meta-kernel showing use of
+
+ - binary lunar PCK
+ - generic lunar frame kernel (FK)
+ - leapseconds kernel (LSK)
+ - planetary SPK
+
+ 17-MAR-2008 (NJB)
+
+ Note: to actually use this kernel, replace the @ characters
+ below with backslashes (\). The backslash character cannot be
+ used here, within the comments of this frame kernel, because the
+ begindata and begintext strings would be interpreted as
+ directives bracketing actual load commands.
+
+ This meta-kernel assumes that the referenced kernels exist
+ in the user's current working directory.
+
+ @begindata
+
+ KERNELS_TO_LOAD = ( 'moon_pa_de421_1900-2050.bpc'
+ 'moon_080317.tf'
+ 'leapseconds.ker'
+ 'de421.bsp' )
+
+ @begintext
+
+
+ Example program
+ ---------------
+
+ PROGRAM EX1
+ IMPLICIT NONE
+
+ INTEGER FILSIZ
+ PARAMETER ( FILSIZ = 255 )
+
+ CHARACTER*(FILSIZ) META
+
+ DOUBLE PRECISION ET
+ DOUBLE PRECISION LT
+ DOUBLE PRECISION STME ( 6 )
+ DOUBLE PRECISION STPA ( 6 )
+
+ C
+ C Prompt user for meta-kernel name.
+ C
+ CALL PROMPT ( 'Enter name of meta-kernel > ', META )
+
+ C
+ C Load lunar PCK, generic lunar frame kernel,
+ C leapseconds kernel, and planetary ephemeris
+ C via metakernel.
+ C
+ CALL FURNSH ( META )
+
+ C
+ C Convert a time of interest from UTC to ET.
+ C
+ CALL STR2ET ( '2008 MAR 17 20:10:00', ET )
+
+ WRITE (*,*) 'ET (sec past J2000 TDB): ', ET
+ WRITE (*,*) ' State of Earth relative to Moon'
+
+ C
+ C Find the geometric state of the Earth relative to the
+ C Moon at ET, expressed relative to the ME frame.
+ C
+ CALL SPKEZR ( 'Earth', ET, 'MOON_ME',
+ . 'NONE', 'Moon', STME, LT )
+
+ WRITE (*,*) ' In MOON_ME frame:'
+ WRITE (*,*) STME
+
+ C
+ C Find the geometric state of the Earth relative to the
+ C Moon at ET, expressed relative to the PA frame.
+ C
+ CALL SPKEZR ( 'Earth', ET, 'MOON_PA',
+ . 'NONE', 'Moon', STPA, LT )
+
+ WRITE (*,*) ' In MOON_PA frame:'
+ WRITE (*,*) STPA
+
+ END
+
+
+ Program output
+ --------------
+
+ Enter name of meta-kernel > meta
+ ET (sec past J2000 TDB): 259056665.
+ State of Earth relative to Moon
+ In MOON_ME frame:
+ 379892.825 33510.118 -12661.5278 0.0400357582 0.0117963334 0.115130508
+ In MOON_PA frame:
+ 379908.634 33385.003 -12516.8859 0.0399957879 0.0117833314 0.115145731
+
+
+
+ References
+ =====================================================================
+
+ [1] J.G. Williams, D.H. Boggs and W.M. Folkner. "DE421 Lunar
+ Orbit, Physical Librations, and Surface Coordinates,"
+ preprint of JPL IOM 335-JW,DB,WF-20080314-001, dated
+ March 14, 2008.
+
+ [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] Roncoli, R. (2005). "Lunar Constants and Models Document,"
+ JPL D-32296.
+
+
+ Frame Specifications
+ =====================================================================
+
+ MOON_PA is the name of the generic lunar principal axes (PA) reference
+ frame. This frame is an alias for the principal axes frame defined
+ by the latest version of the JPL Solar System Dynamics Group's
+ planetary ephemeris.
+
+ In this instance of the lunar reference frames kernel, MOON_PA is an
+ alias for the lunar principal axes frame associated with the
+ planetary ephemeris DE-421.
+
+ \begindata
+
+ FRAME_MOON_PA = 31000
+ FRAME_31000_NAME = 'MOON_PA'
+ FRAME_31000_CLASS = 4
+ FRAME_31000_CLASS_ID = 31000
+ FRAME_31000_CENTER = 301
+
+ TKFRAME_31000_SPEC = 'MATRIX'
+ TKFRAME_31000_RELATIVE = 'MOON_PA_DE421'
+ TKFRAME_31000_MATRIX = ( 1 0 0
+ 0 1 0
+ 0 0 1 )
+
+ \begintext
+
+ MOON_ME is the name of the generic lunar mean Earth/polar axis (ME)
+ reference frame. This frame is an alias for the mean Earth/polar
+ axis frame defined by the latest version of the JPL Solar System
+ Dynamics Group's planetary ephemeris.
+
+ In this instance of the lunar reference frames kernel, MOON_ME is an
+ alias for the lunar mean Earth/polar axis frame associated with the
+ planetary ephemeris DE-421.
+
+ \begindata
+
+ FRAME_MOON_ME = 31001
+ FRAME_31001_NAME = 'MOON_ME'
+ FRAME_31001_CLASS = 4
+ FRAME_31001_CLASS_ID = 31001
+ FRAME_31001_CENTER = 301
+
+ TKFRAME_31001_SPEC = 'MATRIX'
+ TKFRAME_31001_RELATIVE = 'MOON_ME_DE421'
+ TKFRAME_31001_MATRIX = ( 1 0 0
+ 0 1 0
+ 0 0 1 )
+
+
+ \begintext
+
+
+ MOON_PA_DE421 is the name of the lunar principal axes
+ reference frame defined by JPL's DE-421 planetary ephemeris.
+
+ \begindata
+
+ FRAME_MOON_PA_DE421 = 31006
+ FRAME_31006_NAME = 'MOON_PA_DE421'
+ FRAME_31006_CLASS = 2
+ FRAME_31006_CLASS_ID = 31006
+ FRAME_31006_CENTER = 301
+
+
+ \begintext
+
+ MOON_ME_DE421 is the name of the lunar mean Earth/polar
+ axis reference frame defined by JPL's DE-421 planetary ephemeris.
+
+ Rotation angles are from reference [1].
+
+ \begindata
+
+ FRAME_MOON_ME_DE421 = 31007
+ FRAME_31007_NAME = 'MOON_ME_DE421'
+ FRAME_31007_CLASS = 4
+ FRAME_31007_CLASS_ID = 31007
+ FRAME_31007_CENTER = 301
+
+ TKFRAME_31007_SPEC = 'ANGLES'
+ TKFRAME_31007_RELATIVE = 'MOON_PA_DE421'
+ TKFRAME_31007_ANGLES = ( 67.92 78.56 0.30 )
+ TKFRAME_31007_AXES = ( 3, 2, 1 )
+ TKFRAME_31007_UNITS = 'ARCSECONDS'
+
+ \begintext
+
+
+ Updating this Kernel
+ --------------------
+
+ When a new JPL DE providing lunar rotation data becomes available,
+ the new lunar PA frame associated with that data set will be named
+
+ MOON_PA_DEnnn
+
+ where nnn is the version number of the DE.
+
+ The PCK body ID code associated with that data set will be
+
+ 31008
+
+ The frame ID and class ID for this frame will also be 31008.
+
+ The generic PA frame specification will be updated to point to the
+ new DE-specific PA frame. The rest of this frame specification
+ is unchanged.
+
+ The ME frame name associated with the new data set will be named
+
+ MOON_ME_DEnnn
+
+ The frame ID and class ID for this frame will be
+
+ 31009
+
+ The rotational offset between this frame and the new DE-specific PA
+ frame will need to be updated; this offset is DE-dependent.
+
+ The generic ME frame specification will be updated to point to the
+ new DE-specific ME frame. The rest of this frame specification
+ is unchanged.
+
+
+
+ =====================================================================
+ End of kernel
+
+
+
+
+
+
+
+
+
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_assoc_me.tf b/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_assoc_me.tf
new file mode 100644
index 0000000000000000000000000000000000000000..b589b93f18d7bfdefdabc6307b250855b8f7ec58
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_assoc_me.tf
@@ -0,0 +1,272 @@
+KPL/FK
+
+
+ SPICE Lunar ME Reference Frame/Body Association Kernel
+ =====================================================================
+
+ Original file name: moon_assoc_me.tf
+ Creation date: 2007 February 13 17:24
+ Created by: Nat Bachman (NAIF/JPL)
+ Last updated: 2008 March 18 22:15
+ Purpose of update:
+
+ Documentation now refers to DE421 kernels. Deprecated SPICE
+ routines and their replacements are noted.
+
+
+ Overview
+ =====================================================================
+
+ In the SPICE system, the default body-fixed reference frame
+ associated with the Moon is named
+
+ IAU_MOON
+
+ The IAU_MOON reference frame is implemented via approximate formulas
+ provided by the IAU report [1] and is not suitable for high-accuracy
+ work.
+
+ This kernel directs the SPICE system to associate the lunar "mean
+ Earth" reference frame
+
+ MOON_ME
+
+ with the Moon.
+
+ When this kernel is loaded via FURNSH, the SPICE frame system
+ routines CNMFRM and CIDFRM, which identify the reference frame
+ associated with a specified body, will indicate that the MOON_ME
+ frame is associated with the Moon. In addition, higher-level SPICE
+ geometry routines that rely on the CNMFRM or CIDFRM routines will
+ use the MOON_ME frame where applicable. As of the release date of
+ this kernel, these SPICE routines are:
+
+ ET2LST
+ LSPCN
+
+ Any code that calls these routines to obtain results
+ involving lunar body-fixed frames are affected. Within SPICE, the
+ only higher-level system that is affected is the dynamic frame
+ system.
+
+ The deprecated (as of the N0062 SPICE Toolkit release) routines
+
+ ILLUM
+ SRFXPT
+ SUBPT
+ SUBSOL
+
+ also make use of this kernel; however NAIF recommends that
+ users instead call the following routines which, respectively,
+ supersede those listed above:
+
+ ILUMIN
+ SINCPT
+ SUBPNT
+ SUBSLR
+
+ The newer routines don't make use of frame association kernels;
+ these routines accept the name of the target body-fixed
+ frame as an input argument.
+
+ Note: to direct SPICE to associate the lunar principal axis frame
+
+ MOON_PA
+
+ with the Moon, load the kernel
+
+ moon_assoc_pa.tf
+
+ rather than this one.
+
+
+
+ Using this kernel
+ =====================================================================
+
+ This kernel must be loaded together with a lunar frame specification
+ kernel and a binary lunar PCK. Below an example meta-kernel that
+ loads these files and a small program illustrating use of the
+ meta-kernel are shown. The names of the kernels used here are
+ current as of the release date of this kernel, but should not be
+ assumed to be current at later dates.
+
+
+ Example meta-kernel
+ -------------------
+
+ To use the meta-kernel shown below, the '@' characters must be
+ replaced with backslash '\' characters. Backslashes cannot be
+ used in this comment block because they would confuse the SPICE
+ text kernel parser.
+
+
+
+ KPL/FK
+
+ @begintext
+
+ Kernels to load are:
+
+ Lunar kernels
+ -------------
+ Binary lunar PCK: moon_pa_de421_1900-2050.bpc
+ Lunar FK: moon_080317.tf
+ Frame association kernel: moon_assoc_me.tf
+
+ Additional kernels to support sub-point computation
+ ---------------------------------------------------
+ Text PCK for lunar radii: pck00008.tpc
+
+ Leapseconds kernel (for
+ time conversion): naif0008.tls
+
+ Planetary ephemeris (for
+ sub-Earth computation): de421.bsp
+
+ @begindata
+
+ KERNELS_TO_LOAD = ( 'moon_pa_de421_1900-2050.bpc'
+ 'moon_080317.tf'
+ 'moon_assoc_me.tf'
+ 'pck00008.tpc'
+ 'naif0008.tls'
+ 'de421.bsp' )
+ @begintext
+
+ End of kernel
+
+
+
+ Example code
+ ------------
+
+ Find the geometric (without light time and stellar aberration
+ corrections) sub-Earth point on the Moon at a given UTC time,
+ using the MOON_ME reference frame. Display the name of the
+ body-fixed lunar frame used for the computation.
+
+
+ PROGRAM EX
+ IMPLICIT NONE
+
+ DOUBLE PRECISION DPR
+
+ INTEGER FILEN
+ PARAMETER ( FILEN = 255 )
+
+ INTEGER FRNMLN
+ PARAMETER ( FRNMLN = 32 )
+
+ INTEGER TIMLEN
+ PARAMETER ( TIMLEN = 50 )
+
+ CHARACTER*(FRNMLN) FRNAME
+ CHARACTER*(FILEN) META
+ CHARACTER*(TIMLEN) TIMSTR
+
+ DOUBLE PRECISION ALT
+ DOUBLE PRECISION ET
+ DOUBLE PRECISION LAT
+ DOUBLE PRECISION LON
+ DOUBLE PRECISION RADIUS
+ DOUBLE PRECISION SPOINT ( 3 )
+
+ INTEGER FRCODE
+
+ LOGICAL FOUND
+
+ C
+ C Obtain name of meta-kernel; load kernel.
+ C
+ CALL PROMPT ( 'Enter meta-kernel name > ', META )
+ CALL FURNSH ( META )
+
+ C
+ C Obtain input time and convert to seconds past J2000 TDB.
+ C
+ CALL PROMPT ( 'Enter observation time > ', TIMSTR )
+ CALL STR2ET ( TIMSTR, ET )
+
+ C
+ C Find the closest point on the Moon to the center
+ C of the Earth at ET.
+ C
+ CALL SUBPT ( 'Near point', 'MOON', ET, 'NONE',
+ . 'EARTH', SPOINT, ALT )
+ .
+ C
+ C Express the sub-observer point in latitudinal
+ C coordinates.
+ C
+ CALL RECLAT ( SPOINT, RADIUS, LON, LAT )
+
+ C
+ C Look up the name of the lunar body-fixed frame.
+ C
+ CALL CNMFRM ( 'MOON', FRCODE, FRNAME, FOUND )
+
+ C
+ C Always check the "found" flag. Signal an error if we
+ C don't find a frame name.
+ C
+ IF ( .NOT. FOUND ) THEN
+ CALL SETMSG ( 'No body-fixed frame found for the Moon.' )
+ CALL SIGERR ( 'SPICE(NOFRAME)' )
+ END IF
+
+ WRITE(*,*) 'Lunar body-fixed frame is ', FRNAME
+ WRITE(*,*) 'Sub-Earth planetocentric longitude (deg):',
+ . LON*DPR()
+ WRITE(*,*) 'Sub-Earth planetocentric latitude (deg):',
+ . LAT*DPR()
+ END
+
+
+ Example program output
+ ----------------------
+
+ Numeric results and output formatting shown below should be
+ expected to differ somewhat across different computing platforms.
+
+ When the above example program is run using the example meta-kernel,
+ and the (arbitrary) date 2008 Mar 18 00:00:00 UTC is used
+ as the observation time, the output will be:
+
+ Lunar body-fixed frame is MOON_ME
+ Sub-Earth planetocentric longitude (deg): 5.05523767
+ Sub-Earth planetocentric latitude (deg): -1.65932776
+
+
+ References
+ =====================================================================
+ [1] 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.
+
+
+
+ Data
+ =====================================================================
+
+ The assignment below directs the SPICE system to associate the MOON_ME
+ reference frame with the Moon.
+
+ For further information, see the Frames Required Reading section
+ titled "Connecting an Object to its Body-fixed Frame."
+
+ \begindata
+
+ OBJECT_MOON_FRAME = 'MOON_ME'
+
+ \begintext
+
+
+ End of kernel
+ =====================================================================
+
+
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_pa_de421_1900-2050.bpc b/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_pa_de421_1900-2050.bpc
new file mode 100644
index 0000000000000000000000000000000000000000..10e35ab7694a103bb1265ec591a96bf4772e6be2
Binary files /dev/null and b/tests/pytests/data/M3T20090630T083407_V03_RDN/moon_pa_de421_1900-2050.bpc differ
diff --git a/tests/pytests/data/M3T20090630T083407_V03_RDN/naif0012.tls b/tests/pytests/data/M3T20090630T083407_V03_RDN/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/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/M3T20090630T083407_V03_RDN/pck00009.tpc b/tests/pytests/data/M3T20090630T083407_V03_RDN/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/M3T20090630T083407_V03_RDN/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+Purpose
+--------------------------------------------------------
+
+ This file makes available for use in SPICE-based application
+ software orientation and size/shape data for natural bodies. The
+ principal source of the data is a published report by the IAU/IAG
+ Working Group on Cartographic Coordinates and Rotational Elements [1].
+
+ Orientation and size/shape data not provided by this file may be
+ available in mission-specific PCK files. Such PCKs may be the preferred
+ data source for mission-related applications. Mission-specific PCKs can
+ be found in PDS archives or on the NAIF web site at URL:
+
+ http://naif.jpl.nasa.gov
+
+
+File Organization
+--------------------------------------------------------
+
+ The contents of this file are as follows.
+
+ Introductory Information:
+
+ -- Purpose
+
+ -- File Organization
+
+ -- Version description
+
+ -- Disclaimer
+
+ -- Sources
+
+ -- Explanatory notes
+
+ -- Body numbers and names
+
+
+ PcK Data:
+
+
+ Orientation Data
+ ----------------
+
+ -- Orientation constants for the Sun and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+Disclaimer
+--------------------------------------------------------
+
+Applicability of Data
+
+ This P_constants file may not contain the parameter values that
+ you prefer. NAIF suggests that you inspect this file visually
+ before proceeding with any critical or extended data processing.
+
+File Modifications by Users
+
+ Note that this file may be readily modified by you to change
+ values or add/delete parameters. NAIF requests that you update the
+ "by line," date, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG Working Group Report [1] to be accurate to 0.1 degree
+ ([1], p.158). However, NAIF notes that orientation models for
+ natural satellites and asteroids have in some cases changed
+ substantially with the availability of new observational data, so
+ users are urged to investigate the suitability for their
+ applications of the models presented here.
+
+ Earth orientation
+ -----------------
+
+ NAIF strongly cautions against using the earth rotation model
+ (from [1]) for work demanding high accuracy. This model has been
+ determined by NAIF to have an error in the prime meridian location
+ of magnitude at least 150 arcseconds, with a local minimum
+ occurring during the year 1999. Regarding availability of better
+ earth orientation data for use with the SPICE system:
+
+ Earth orientation data are available from NAIF in the form of
+ binary earth PCK files. NAIF employs an automated process to
+ create these files; each time JPL's Tracking Systems and
+ Applications Section produces a new earth orientation parameter
+ (EOP) file, a new PCK is produced. These PCKs cover a roughly
+ 10 year time span starting at Jan. 1, 2000. In these PCK files,
+ the following effects are accounted for in modeling the earth's
+ rotation:
+
+ - Precession: 1976 IAU model
+
+ - Nutation: 1980 IAU model, plus interpolated
+ EOP nutation corrections
+
+ - Polar motion: interpolated from EOP file
+
+ - True sidereal time:
+
+ UT1 - UT1R (if needed): given by analytic formula
+ + TAI - UT1 (or UT1R): interpolated from EOP file
+ + UT1 - GMST: given by analytic formula
+ + equation of equinoxes: given by analytic formula
+
+ where
+
+ TAI = International Atomic Time
+ UT1 = Greenwich hour angle of computed mean sun - 12h
+ UT1R = Regularized UT1
+ GMST = Greenwich mean sidereal time
+
+ These kernels are available from the NAIF web site
+
+ http://naif.jpl.nasa.gov
+
+ (follow the links to Data, generic_kernels, and PCK data) or
+
+ ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck
+
+ or via anonymous ftp from the server
+
+ naif.jpl.nasa.gov
+
+ The kernels are in the path
+
+ pub/naif/generic_kernels/pck
+
+ At this time, these kernels have file names of the form
+
+ earth_000101_yymmdd_yymmdd.bpc
+
+ The second and third dates are, respectively, the file's
+ coverage end time and the epoch of the last datum.
+
+ These binary PCK files are very accurate (error < 0.1
+ microradian) for epochs preceding the epoch of the last datum.
+ For later epochs, the error rises to several microradians.
+
+ Binary PCK files giving accurate earth orientation from 1972 to
+ 2007 and *low accuracy* predicted earth orientation from
+ 2007 to 2037 are also available in the same location. See the
+ aareadme.txt file at the "pck" URL above for details.
+
+ Characteristics and names of the binary kernels described here
+ are subject to change. See the "pck" URL above for information
+ on current binary earth PCKs.
+
+
+ Lunar orientation
+ -----------------
+
+ The lunar orientation formula provided by this file is a
+ trigonometric polynomial approximation yielding the orientation of
+ the lunar "Mean Earth/Polar Axis" (ME) reference frame. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which are available on the NAIF web site (see URLS above)
+ and in the NAIF server's ftp area. The lunar frame kernel
+ is located in the path
+
+ pub/naif/generic_kernels/fk/satellites
+
+ and has a name of the form
+
+ moon_yymmdd.tf
+
+ The binary lunar PCK is in the path
+
+ pub/naif/generic_kernels/pck
+
+ and has a name of the form
+
+ moon_pa_dennn_yyyy-yyyy.bpc
+
+ See the "aareadme.txt" files in the paths shown above for details
+ on file contents and versions. We also suggest you refer to the
+ SPICE tutorial named "lunar_earth_pck-fk," which is available from
+ the NAIF web site.
+
+
+ Earth geomagnetic dipole
+ ------------------------
+
+ The SPICE Toolkit doesn't currently contain software to model the
+ earth's north geomagnetic centered dipole as a function of time.
+ As a convenience for users, the north dipole location from the
+ J2000 epoch was selected as a representative datum, and the
+ planetocentric longitude and latitude of this location have been
+ associated with the keywords
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT
+
+ Values for the earth's north geomagnetic centered dipole are
+ presented in comments as a discrete time series for the time range
+ 1945-2000. For details concerning the geomagnetic field model from
+ which these values were derived, including a discussion of the
+ model's accuracy, see [9].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value is provided for informational
+ purposes only.
+
+
+ Software limitations
+ --------------------
+
+ SPICE Toolkits prior to version N0057 cannot make use of
+ trigonometric polynomial terms in the formulas for orientation of
+ the planets. The only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ The second nutation precession angle (M2) for Mars is represented
+ by a quadratic polynomial in the 2006 IAU report. The SPICELIB
+ subroutine BODEUL can not handle this term (which is extremely
+ small), so we truncate the polynomial to a linear one. The
+ resulting orientation error has a maximum magnitude of less
+ than 0.0032 degrees over the time span 1996-2015 and less than
+ 0.0082 degrees over the time span 1986-2025.
+
+
+Sources
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Conrad, A., Consolmagno, G.J., Hestroffer, D.,
+ Hilton, J.L., Krasinsky, G.A., Neumann, G.,
+ Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J.,
+ and Thomas, P.C. "Report of the IAU/IAG Working Group
+ on cartographic coordinates and rotational elements: 2006."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] Nautical Almanac Office, United States Naval Observatory
+ and H.M. Nautical Almanac Office, Rutherford Appleton
+ Laboratory (2010). "The Astronomical Almanac for
+ the Year 2010," U.S. Government Printing Office,
+ Washington, D.C.: and The Stationary Office, London.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [5] Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+ Conventions," presentation to the Mars Express Data
+ Archive Working Group, Dec. 14, 2001.
+
+ [6] Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic
+ Field and Magnetosphere." <http://www-ssc.igpp.ucla.
+ edu/personnel/russell/papers/earth_mag>. Originally
+ published in "Encyclopedia of Planetary Sciences," J.H.
+ Shirley and R.W. Fainbridge, eds. Chapman and Hall,
+ New York, pp 208-211.
+
+ [7] Russell, C.T. (1971). "Geophysical Coordinate
+ Transformations," Cosmic Electrodynamics 2 184-186.
+ NAIF document 181.0.
+
+ [8] ESA/ESTEC Space Environment Information System (SPENVIS)
+ (2003). Web page: "Dipole approximations of the
+ geomagnetic field." <http://www.spenvis.oma.be/spenvis/
+ help/background/magfield/cd.html>.
+
+ [9] International Association of Geomagnetism and Aeronomy
+ and International Union of Geodesy and Geophysics (2004).
+ Web page: "The 9th Generation International Geomagnetic
+ Reference Field." <http://www.ngdc.noaa.gov/
+ IAGA/vmod/igrf.html>.
+
+ [10] Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
+ and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
+ Working Group on Cartographic Coordinates and Rotational
+ Elements of the Planets and Satellites: 1988," Celestial
+ Mechanics and Dynamical Astronomy, v.46, no.2, pp.
+ 187-204.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- The second nutation precession angle (M2) for Mars is
+ represented by a quadratic polynomial in the 2000
+ IAU report. The SPICELIB subroutine BODEUL can not
+ handle this term (which is extremely small), so we
+ truncate the polynomial to a linear one.
+
+ -- Earth north geomagnetic centered dipole values are from
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+Explanatory Notes
+--------------------------------------------------------
+
+ This file, which is logically part of the SPICE P-kernel, contains
+ constants used to model the orientation, size and shape of the
+ Sun, planets, natural satellites, and selected comets and
+ asteroids. The orientation models express the direction of the
+ pole and location of the prime meridian of a body as a function of
+ time. The size/shape models ("shape models" for short) represent
+ all bodies as ellipsoids, using two equatorial radii and a polar
+ radius. Spheroids and spheres are obtained when two or all three
+ radii are equal.
+
+ The SPICE Toolkit routines that use this file are documented in
+ the SPICE "Required Reading" file pck.req. They are also
+ documented in the "PCK" SPICE tutorial, which is available on
+ the NAIF web site.
+
+File Format
+
+ A terse description of the PCK file format is given here. See the
+ SPICE "Required Reading" files pck.req and kernel.req for a
+ detailed explanation of the SPICE text kernel file format. The
+ files pck.req and kernel.req are included in the documentation
+ provided with the SPICE Toolkit.
+
+ The file starts out with the ``ID word'' string
+
+ KPL/PCK
+
+ This string identifies the file as a text kernel containing PCK
+ data.
+
+ This file consists of a series of comment blocks and data blocks.
+ Comment blocks, which contain free-form descriptive or explanatory
+ text, are preceded by a \begintext token. Data blocks follow a
+ \begindata token. In order to be recognized, each of these tokens
+ must be placed on a line by itself.
+
+ The portion of the file preceding the first data block is treated
+ as a comment block; it doesn't require an initial \begintext
+ token.
+
+ This file identifies data using a series of
+
+ KEYWORD = VALUE
+
+ assignments. The left hand side of each assignment is a
+ "kernel variable" name; the right hand side is an associated value
+ or list of values. The SPICE subroutine API allows SPICE routines
+ and user applications to retrieve the set of values associated
+ with each kernel variable name.
+
+ Kernel variable names are case-sensitive and are limited to
+ 32 characters in length.
+
+ Numeric values may be integer or floating point. String values
+ are normally limited to 80 characters in length; however, SPICE
+ provides a mechanism for identifying longer, "continued" strings.
+ See the SPICE routine STPOOL for details.
+
+ String values are single quoted.
+
+ When the right hand side of an assignment is a list of values,
+ the list items may be separated by commas or simply by blanks.
+ The list must be bracketed by parentheses. Example:
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ This file may contain blank lines anywhere. Non-printing
+ characters including TAB should not be present in the file: the
+ presence of such characters may cause formatting errors when the
+ file is viewed.
+
+Time systems and reference frames
+
+ The 2006 IAU/IAG Working Group Report [1] states the time scale
+ used as the independent variable for the rotation formulas is
+ Barycentric Dynamical Time (TDB) and that the epoch of variable
+ quantities is J2000 TDB (2000 Jan 1 12:00 TDB). Throughout SPICE
+ documentation and in this file, we use the names "J2000 TDB" and
+ "J2000" for this epoch. The name "J2000.0" is equivalent.
+
+ SPICE documentation refers to the time system used in this file
+ as either "ET" or "TDB." SPICE software makes no distinction
+ between TDB and the time system associated with the independent
+ variable of the JPL planetary ephemerides T_eph.
+
+ The inertial reference frame used for the rotational elements in
+ this file is identified by [1] as the ICRF (International
+ Celestial Reference Frame).
+
+ The SPICE PCK software that reads this file uses the label "J2000"
+ to refer to the ICRF; this is actually a mislabeling which has
+ been retained in the interest of backward compatibility. Using
+ data from this file, by means of calls to the SPICE frame
+ transformation routines, will actually compute orientation
+ relative to the ICRF.
+
+ The difference between the J2000 frame and the ICRF is
+ on the order of tens of milliarcseconds and is well below the
+ accuracy level of the formulas in this file.
+
+Orientation models
+
+ All of the orientation models use three Euler angles to describe
+ the orientation of the coordinate axes of the "Body Equator and
+ Prime Meridian" system with respect to an inertial system. By
+ default, the inertial system is the ICRF (labeled as "J2000"), but
+ other frames can be specified in the file. See the PCK Required
+ Reading for details.
+
+ The first two angles, in order, are the ICRF right ascension and
+ declination (henceforth RA and DEC) of the north pole of a body as
+ a function of time. The third angle is the prime meridian location
+ (represented by "W"), which is expressed as a rotation about the
+ north pole, and is also a function of time.
+
+ For each body, the expressions for the north pole's right
+ ascension and declination, as well as prime meridian location, are
+ sums (as far as the models that appear in this file are concerned)
+ of quadratic polynomials and trigonometric polynomials, where the
+ independent variable is time.
+
+ In this file, the time arguments in expressions always refer to
+ Barycentric Dynamical Time (TDB), measured in centuries or days
+ past a reference epoch. By default, the reference epoch is the
+ J2000 epoch, which is Julian ephemeris date 2451545.0, but other
+ epochs can be specified in the file. See the PCK Required Reading
+ for details.
+
+ Orientation models for satellites and some planets (including
+ Jupiter) involve both polynomial terms and trigonometric terms.
+ The arguments of the trigonometric terms are linear polynomials.
+ In this file, we call the arguments of these trigonometric terms
+ "nutation precession angles."
+
+ Example: 2006 IAU Model for orientation of Jupiter. Note that
+ these values are used as an example only; see the data area below
+ for current values.
+
+ Right ascension
+ ---------------
+
+ alpha = 268.056595 - 0.006499 T + 0.000117 sin(Ja)
+ 0 + 0.000938 sin(Jb) + 0.001432 sin(Jc)
+ + 0.000030 sin(Jd) + 0.002150 sin(Je)
+
+ Declination
+ -----------
+
+ delta = 64.495303 + 0.002413 T + 0.000050 cos(Ja)
+ 0 + 0.000404 cos(Jb) + 0.000617 cos(Jc)
+ - 0.000013 cos(Jd) + 0.000926 cos(Je)
+
+ Prime meridian
+ --------------
+
+ W = 284.95 + 870.5366420 d
+
+
+ Here
+
+ T represents centuries past J2000 ( TDB ),
+
+ d represents days past J2000 ( TDB ).
+
+ Ja-Je are nutation precession angles.
+
+ In this file, the polynomials' coefficients above are assigned
+ to kernel variable names (left-hand-side symbols) as follows
+
+ BODY599_POLE_RA = ( 268.056595 -0.006499 0. )
+ BODY599_POLE_DEC = ( 64.495303 0.002413 0. )
+ BODY599_PM = ( 284.95 870.5366420 0. )
+
+ and the trigonometric polynomials' coefficients are assigned
+ as follows
+
+ BODY599_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117
+ 0.000938
+ 0.001432
+ 0.000030
+ 0.002150 )
+
+ BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050
+ 0.000404
+ 0.000617
+ -0.000013
+ 0.000926 )
+
+ BODY599_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0 )
+
+ Note the number "599"; this is the NAIF ID code for Jupiter.
+
+ In this file, the polynomial expressions for the nutation
+ precession angles are listed along with the planet's RA, DEC, and
+ prime meridian terms. Below are the 2006 IAU nutation precession
+ angles for the Jupiter system.
+
+ J1 = 73.32 + 91472.9 T
+ J2 = 24.62 + 45137.2 T
+ J3 = 283.90 + 4850.7 T
+ J4 = 355.80 + 1191.3 T
+ J5 = 119.90 + 262.1 T
+ J6 = 229.80 + 64.3 T
+ J7 = 352.25 + 2382.6 T
+ J8 = 113.35 + 6070.0 T
+
+ J9 = 146.64 + 182945.8 T
+ J10 = 49.24 + 90274.4 T
+
+ Ja = 99.360714 + 4850.4046 T
+ Jb = 175.895369 + 1191.9605 T
+ Jc = 300.323162 + 262.5475 T
+ Jd = 114.012305 + 6070.2476 T
+ Je = 49.511251 + 64.3000 T
+
+ Here
+
+ T represents centuries past J2000 ( TDB )
+
+ J1-J10 and Ja-Je are the nutation precession angles. The angles
+ J9 and J10 are equal to 2*J1 and 2*J2, respectively.
+
+ Angles J9 and J10 are not present in [1]; they have been added
+ to fit the terms 2*J1 and 2*J2, which appear in the orientation
+ models of several satellites, into a form that can be accepted
+ by the PCK system.
+
+ The assignment of the nutation precession angles for the
+ Jupiter system is as follows:
+
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.25 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4
+ 99.360714 4850.4046
+ 175.895369 1191.9605
+ 300.323162 262.5475
+ 114.012305 6070.2476
+ 49.511251 64.3000 )
+
+ You'll see an additional symbol grouped with the ones listed
+ above; it is
+
+ BODY599_LONG_AXIS
+
+ This term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ The pattern of the formulas for satellite orientation is similar
+ to that for Jupiter. Example: 2006 IAU values for Io. Again, these
+ values are used as an example only; see the data area below for
+ current values.
+
+ Right ascension
+ ---------------
+
+ alpha = 268.05 - 0.009 T + 0.094 sin(J3) + 0.024 sin(J4)
+ 0
+
+ Declination
+ -----------
+
+ delta = 64.50 + 0.003 T + 0.040 cos(J3) + 0.011 cos(J4)
+ 0
+
+ Prime meridian
+ --------------
+
+ W = 200.39 + 203.4889538 d - 0.085 sin(J3) - 0.022 sin(J4)
+
+
+ d represents days past J2000.
+
+ J3 and J4 are nutation precession angles.
+
+ The polynomial terms are assigned to symbols by the statements
+
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( 64.50 0.003 0. )
+ BODY501_PM = ( 200.39 203.4889538 0. )
+
+ The coefficients of the trigonometric terms are assigned to symbols by
+ the statements
+
+ BODY501_NUT_PREC_RA = ( 0. 0. 0.094 0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. 0.040 0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+
+ 501 is the NAIF ID code for Io.
+
+ SPICE software expects the models for satellite orientation to
+ follow the form of the model shown here: the polynomial portions of the
+ RA, DEC, and W expressions are expected to be quadratic, the
+ trigonometric terms for RA and W (satellite prime meridian) are expected
+ to be linear combinations of sines of nutation precession angles, the
+ trigonometric terms for DEC are expected to be linear combinations of
+ cosines of nutation precession angles, and the polynomials for the
+ nutation precession angles themselves are expected to be linear.
+
+ Eventually, the software will handle more complex expressions, we
+ expect.
+
+
+Shape models
+
+ There is only one kind of shape model supported by the SPICE Toolkit
+ software at present: the triaxial ellipsoid. The 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ For each body, three radii are listed: The first number is
+ the largest equatorial radius (the length of the semi-axis
+ containing the prime meridian), the second number is the smaller
+ equatorial radius, and the third is the polar radius.
+
+ Example: Radii of the Earth.
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers and Names
+--------------------------------------------------------
+
+
+ 1 Mercury barycenter
+ 2 Venus barycenter
+ 3 Earth barycenter
+ 4 Mars barycenter
+ 5 Jupiter barycenter
+ 6 Saturn barycenter
+ 7 Uranus barycenter
+ 8 Neptune barycenter
+ 9 Pluto barycenter
+ 10 Sun
+
+
+ 199 Mercury
+
+
+ 299 Venus
+
+
+ 399 Earth
+
+ 301 Moon
+
+
+ 499 Mars
+
+ 401 Phobos 402 Deimos
+
+
+ 599 Jupiter
+
+ 501 Io 502 Europa 503 Ganymede 504 Callisto
+ 505 Amalthea 506 Himalia 507 Elara 508 Pasiphae
+ 509 Sinope 510 Lysithea 511 Carme 512 Ananke
+ 513 Leda 514 Thebe 515 Adrastea 516 Metis
+
+
+ 699 Saturn
+
+ 601 Mimas 602 Enceladus 603 Tethys 604 Dione
+ 605 Rhea 606 Titan 607 Hyperion 608 Iapetus
+ 609 Phoebe 610 Janus 611 Epimetheus 612 Helene
+ 613 Telesto 614 Calypso 615 Atlas 616 Prometheus
+ 617 Pandora 618 Pan
+
+
+ 799 Uranus
+
+ 701 Ariel 702 Umbriel 703 Titania 704 Oberon
+ 705 Miranda 706 Cordelia 707 Ophelia 708 Bianca
+ 709 Cressida 710 Desdemona 711 Juliet 712 Portia
+ 713 Rosalind 714 Belinda 715 Puck
+
+
+ 899 Neptune
+
+ 801 Triton 802 Nereid 803 Naiad 804 Thalassa
+ 805 Despina 806 Galatea 807 Larissa 808 Proteus
+
+
+ 999 Pluto
+
+ 901 Charon
+
+
+ 1000005 Comet 19P/Borrelly
+ 1000036 Comet Halley
+ 1000093 Comet 9P/Tempel 1
+ 1000107 Comet 81P/Wild 2
+
+ 2000001 Asteroid Ceres
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body10_pole_ra = ( 286.13 0. 0. )
+ body10_pole_dec = ( 63.87 0. 0. )
+ body10_pm = ( 84.10 14.18440 0. )
+ body10_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY10_POLE_RA = ( 286.13 0. 0. )
+ BODY10_POLE_DEC = ( 63.87 0. 0. )
+ BODY10_PM = ( 84.176 14.18440 0. )
+ BODY10_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_POLE_RA = ( 272.76 0. 0. )
+ BODY299_POLE_DEC = ( 67.16 0. 0. )
+ BODY299_PM = ( 160.20 -1.4813688 0. )
+
+ BODY299_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY399_POLE_RA = ( 0. -0.641 0. )
+ BODY399_POLE_DEC = ( 90. -0.557 0. )
+ BODY399_PM = ( 190.147 360.9856235 0. )
+ BODY399_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Nutation precession angles for the Earth-Moon system:
+
+ The linear coefficients have been scaled up from degrees/day
+ to degrees/century, because the SPICELIB PCK reader expects
+ these units. The original constants were:
+
+ 125.045D0 -0.0529921D0
+ 250.089D0 -0.1059842D0
+ 260.008D0 13.0120009D0
+ 176.625D0 13.3407154D0
+ 357.529D0 0.9856003D0
+ 311.589D0 26.4057084D0
+ 134.963D0 13.0649930D0
+ 276.617D0 0.3287146D0
+ 34.226D0 1.7484877D0
+ 15.134D0 -0.1589763D0
+ 119.743D0 0.0036096D0
+ 239.961D0 0.1643573D0
+ 25.053D0 12.9590088D0
+
+
+ \begindata
+
+
+ BODY3_NUT_PREC_ANGLES = ( 125.045 -1935.5364525000
+ 250.089 -3871.0729050000
+ 260.008 475263.3328725000
+ 176.625 487269.6299850000
+ 357.529 35999.0509575000
+ 311.589 964468.4993100000
+ 134.963 477198.8693250000
+ 276.617 12006.3007650000
+ 34.226 63863.5132425000
+ 15.134 -5806.6093575000
+ 119.743 131.8406400000
+ 239.961 6003.1503825000
+ 25.053 473327.7964200000 )
+
+
+ \begintext
+
+
+ Earth north geomagnetic centered dipole:
+
+ Old values:
+
+ Values are from [7]. Note the year of publication was 1971.
+
+ body399_mag_north_pole_lon = ( -69.761 )
+ body399_mag_north_pole_lat = ( 78.565 )
+
+
+ Current values:
+
+ The north dipole location is time-varying. The values shown
+ below, taken from [8], represent a discrete sampling of the
+ north dipole location from 1945 to 2000. The terms DGRF and
+ IGRF refer to, respectively, "Definitive Geomagnetic
+ Reference Field" and "International Geomagnetic Reference
+ Field." See references [6], [8], and [9] for details.
+
+ Coordinates are planetocentric.
+
+ Data source Lat Lon
+ ----------- ----- ------
+ DGRF 1945 78.47 291.47
+ DGRF 1950 78.47 291.15
+ DGRF 1955 78.46 290.84
+ DGRF 1960 78.51 290.53
+ DGRF 1965 78.53 290.15
+ DGRF 1970 78.59 289.82
+ DGRF 1975 78.69 289.53
+ DGRF 1980 78.81 289.24
+ DGRF 1985 78.97 289.10
+ DGRF 1990 79.13 288.89
+ IGRF 1995 79.30 288.59
+ IGRF 2000 79.54 288.43
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY499_POLE_RA = ( 317.68143 -0.1061 0. )
+ BODY499_POLE_DEC = ( 52.88650 -0.0609 0. )
+ BODY499_PM = ( 176.630 350.89198226 0. )
+
+ \begintext
+
+ Source [5] specifies the following value for the lambda_a term
+ (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
+ LONGITUDE, measured from the prime meridian, of the meridian
+ containing the longest axis of the reference ellipsoid.
+ (CAUTION: previous values were POSITIVE WEST.)
+
+ body499_long_axis = ( 252. )
+
+ We list this lambda_a value for completeness. The IAU report
+ [1] gives equal values for both equatorial radii, so the
+ lambda_a offset does not apply to the IAU model.
+
+ The 2003 IAU report defines M2, the second nutation precession angle,
+ by:
+
+ 2
+ 192.93 + 1128.4096700 d + 8.864 T
+
+ We truncate the M2 series to a linear expression, because the PCK
+ software cannot handle the quadratic term.
+
+ Again, the linear terms are scaled by 36525.0:
+
+ -0.4357640000000000 --> -15916.28010000000
+ 1128.409670000000 --> 41215163.19675000
+ -1.8151000000000000E-02 --> -662.9652750000000
+
+ We also introduce a fourth nutation precession angle, which
+ is the pi/2-complement of the third angle. This angle is used
+ in computing the prime meridian location for Deimos. See the
+ discussion of this angle below in the section containing orientation
+ constants for Deimos.
+
+ \begindata
+
+ BODY4_NUT_PREC_ANGLES = ( 169.51 -15916.2801
+ 192.93 41215163.19675
+ 53.47 -662.965275
+ 36.53 662.965275 )
+
+ \begintext
+
+
+Jupiter
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body599_pole_ra = ( 268.05 -0.009 0. )
+ body599_pole_dec = ( 64.49 0.003 0. )
+ body599_pm = ( 284.95 870.5366420 0. )
+ body599_long_axis = ( 0. )
+
+ body5_nut_prec_angles = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.35 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4 )
+
+
+
+ Current values:
+
+ The number of nutation precession angles is 15. The ninth and
+ tenth are twice the first and second, respectively. The
+ eleventh through fifteenth correspond to angles JA-JE in
+ the 2006 IAU report; angles JA-JE were not used prior to that
+ report.
+
+ \begindata
+
+
+ BODY599_POLE_RA = ( 268.056595 -0.006499 0. )
+ BODY599_POLE_DEC = ( 64.495303 0.002413 0. )
+ BODY599_PM = ( 284.95 870.5366420 0. )
+ BODY599_LONG_AXIS = ( 0. )
+
+ BODY599_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117
+ 0.000938
+ 0.001432
+ 0.000030
+ 0.002150 )
+
+ BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050
+ 0.000404
+ 0.000617
+ -0.000013
+ 0.000926 )
+
+ BODY599_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0 )
+
+
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.25 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4
+ 99.360714 4850.4046
+ 175.895369 1191.9605
+ 300.323162 262.5475
+ 114.012305 6070.2476
+ 49.511251 64.3000 )
+ \begintext
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_POLE_RA = ( 40.589 -0.036 0. )
+ BODY699_POLE_DEC = ( 83.537 -0.004 0. )
+ BODY699_PM = ( 38.90 810.7939024 0. )
+ BODY699_LONG_AXIS = ( 0. )
+
+ \begintext
+
+ The first seven angles given here are the angles S1
+ through S7 from the 2000 report; the eighth and
+ ninth angles are 2*S1 and 2*S2, respectively.
+
+
+ \begindata
+
+ BODY6_NUT_PREC_ANGLES = ( 353.32 75706.7
+ 28.72 75706.7
+ 177.40 -36505.5
+ 300.00 -7225.9
+ 316.45 506.2
+ 345.20 -1016.3
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_POLE_RA = ( 257.311 0. 0. )
+ BODY799_POLE_DEC = ( -15.175 0. 0. )
+ BODY799_PM = ( 203.81 -501.1600928 0. )
+ BODY799_LONG_AXIS = ( 0. )
+
+ \begintext
+
+ The first 16 angles given here are the angles U1
+ through U16 from the 2000 report; the 17th and
+ 18th angles are 2*U11 and 2*U12, respectively.
+
+ \begindata
+
+ BODY7_NUT_PREC_ANGLES = ( 115.75 54991.87
+ 141.69 41887.66
+ 135.03 29927.35
+ 61.77 25733.59
+ 249.32 24471.46
+ 43.86 22278.41
+ 77.66 20289.42
+ 157.36 16652.76
+ 101.81 12872.63
+ 138.64 8061.81
+ 102.23 -2024.22
+ 316.41 2863.96
+ 304.01 -51.94
+ 308.71 -93.17
+ 340.82 -75.32
+ 259.14 -504.81
+ 204.46 -4048.44
+ 632.82 5727.92 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY899_POLE_RA = ( 299.36 0. 0. )
+ BODY899_POLE_DEC = ( 43.46 0. 0. )
+ BODY899_PM = ( 253.18 536.3128492 0. )
+ BODY899_LONG_AXIS = ( 0. )
+
+
+ BODY899_NUT_PREC_RA = ( 0.70 0. 0. 0. 0. 0. 0. 0. )
+ BODY899_NUT_PREC_DEC = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
+ BODY899_NUT_PREC_PM = ( -0.48 0. 0. 0. 0. 0. 0. 0. )
+
+ \begintext
+
+ The 2000 report defines the nutation precession angles
+
+ N, N1, N2, ... , N7
+
+ and also uses the multiples of N1 and N7
+
+ 2*N1
+
+ and
+
+ 2*N7, 3*N7, ..., 9*N7
+
+ In this file, we treat the angles and their multiples as
+ separate angles. In the kernel variable
+
+ BODY8_NUT_PREC_ANGLES
+
+ the order of the angles is
+
+ N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
+
+ Each angle is defined by a linear polynomial, so two
+ consecutive array elements are allocated for each
+ angle. The first term of each pair is the constant term,
+ the second is the linear term.
+
+ \begindata
+
+ BODY8_NUT_PREC_ANGLES = ( 357.85 52.316
+ 323.92 62606.6
+ 220.51 55064.2
+ 354.27 46564.5
+ 75.31 26109.4
+ 35.36 14325.4
+ 142.61 2824.6
+ 177.85 52.316
+ 647.840 125213.200
+ 355.700 104.632
+ 533.550 156.948
+ 711.400 209.264
+ 889.250 261.580
+ 1067.100 313.896
+ 1244.950 366.212
+ 1422.800 418.528
+ 1600.650 470.844 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY999_POLE_RA = ( 312.993 0. 0. )
+ BODY999_POLE_DEC = ( 6.163 0. 0. )
+ BODY999_PM = ( 237.305 -56.3625225 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ New values:
+
+ \begindata
+
+
+
+
+
+ BODY301_POLE_RA = ( 269.9949 0.0031 0. )
+ BODY301_POLE_DEC = ( 66.5392 0.0130 0. )
+ BODY301_PM = ( 38.3213 13.17635815 -1.4D-12 )
+ BODY301_LONG_AXIS = ( 0. )
+
+ BODY301_NUT_PREC_RA = ( -3.8787 -0.1204 0.0700 -0.0172
+ 0.0 0.0072 0.0 0.0
+ 0.0 -0.0052 0.0 0.0
+ 0.0043 )
+
+ BODY301_NUT_PREC_DEC = ( 1.5419 0.0239 -0.0278 0.0068
+ 0.0 -0.0029 0.0009 0.0
+ 0.0 0.0008 0.0 0.0
+ -0.0009 )
+
+ BODY301_NUT_PREC_PM = ( 3.5610 0.1208 -0.0642 0.0158
+ 0.0252 -0.0066 -0.0047 -0.0046
+ 0.0028 0.0052 0.0040 0.0019
+ -0.0044 )
+ \begintext
+
+
+
+Satellites of Mars
+
+
+ Phobos
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ The quadratic prime meridian term is scaled by 1/36525**2:
+
+ 8.864000000000000 ---> 6.6443009930565219E-09
+
+ \begindata
+
+ BODY401_POLE_RA = ( 317.68 -0.108 0. )
+ BODY401_POLE_DEC = ( 52.90 -0.061 0. )
+ BODY401_PM = ( 35.06 1128.8445850 6.6443009930565219E-09 )
+
+ BODY401_LONG_AXIS = ( 0. )
+
+ BODY401_NUT_PREC_RA = ( 1.79 0. 0. 0. )
+ BODY401_NUT_PREC_DEC = ( -1.08 0. 0. 0. )
+ BODY401_NUT_PREC_PM = ( -1.42 -0.78 0. 0. )
+
+
+ \begintext
+
+
+ Deimos
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ New values:
+
+ The Deimos prime meridian expression is:
+
+
+ 2
+ W = 79.41 + 285.1618970 d - 0.520 T - 2.58 sin M
+ 3
+
+ + 0.19 cos M .
+ 3
+
+
+ At the present time, the PCK kernel software (the routine
+ BODEUL in particular) cannot handle the cosine term directly,
+ but we can represent it as
+
+ 0.19 sin M
+ 4
+
+ where
+
+ M = 90.D0 - M
+ 4 3
+
+ Therefore, the nutation precession angle assignments for Phobos
+ and Deimos contain four coefficients rather than three.
+
+ The quadratic prime meridian term is scaled by 1/36525**2:
+
+ -0.5200000000000000 ---> -3.8978300049519307E-10
+
+ \begindata
+
+ BODY402_POLE_RA = ( 316.65 -0.108 0. )
+ BODY402_POLE_DEC = ( 53.52 -0.061 0. )
+ BODY402_PM = ( 79.41 285.1618970 -3.897830D-10 )
+ BODY402_LONG_AXIS = ( 0. )
+
+ BODY402_NUT_PREC_RA = ( 0. 0. 2.98 0. )
+ BODY402_NUT_PREC_DEC = ( 0. 0. -1.78 0. )
+ BODY402_NUT_PREC_PM = ( 0. 0. -2.58 0.19 )
+
+ \begintext
+
+
+
+
+Satellites of Jupiter
+
+
+ Io
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( 64.50 0.003 0. )
+ BODY501_PM = ( 200.39 203.4889538 0. )
+ BODY501_LONG_AXIS = ( 0. )
+
+ BODY501_NUT_PREC_RA = ( 0. 0. 0.094 0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. 0.040 0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+
+ \begintext
+
+
+
+ Europa
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 0. )
+ body502_long_axis = ( 0. )
+
+ body502_nut_prec_ra = ( 0. 0. 0. 1.086 0.060 0.015 0.009 )
+ body502_nut_prec_dec = ( 0. 0. 0. 0.468 0.026 0.007 0.002 )
+ body502_nut_prec_pm = ( 0. 0. 0. -0.980 -0.054 -0.014 -0.008 )
+
+
+ Current values:
+
+ \begindata
+
+ BODY502_POLE_RA = ( 268.08 -0.009 0. )
+ BODY502_POLE_DEC = ( 64.51 0.003 0. )
+ BODY502_PM = ( 36.022 101.3747235 0. )
+ BODY502_LONG_AXIS = ( 0. )
+
+ BODY502_NUT_PREC_RA = ( 0. 0. 0. 1.086 0.060 0.015 0.009 )
+ BODY502_NUT_PREC_DEC = ( 0. 0. 0. 0.468 0.026 0.007 0.002 )
+ BODY502_NUT_PREC_PM = ( 0. 0. 0. -0.980 -0.054 -0.014 -0.008 )
+
+ \begintext
+
+
+ Ganymede
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY503_POLE_RA = ( 268.20 -0.009 0. )
+ BODY503_POLE_DEC = ( 64.57 0.003 0. )
+ BODY503_PM = ( 44.064 50.3176081 0. )
+ BODY503_LONG_AXIS = ( 0. )
+
+ BODY503_NUT_PREC_RA = ( 0. 0. 0. -0.037 0.431 0.091 )
+ BODY503_NUT_PREC_DEC = ( 0. 0. 0. -0.016 0.186 0.039 )
+ BODY503_NUT_PREC_PM = ( 0. 0. 0. 0.033 -0.389 -0.082 )
+
+ \begintext
+
+
+ Callisto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY504_POLE_RA = ( 268.72 -0.009 0. )
+ BODY504_POLE_DEC = ( 64.83 0.003 0. )
+ BODY504_PM = ( 259.51 21.5710715 0. )
+ BODY504_LONG_AXIS = ( 0. )
+
+ BODY504_NUT_PREC_RA = ( 0. 0. 0. 0. -0.068 0.590 0. 0.010 )
+ BODY504_NUT_PREC_DEC = ( 0. 0. 0. 0. -0.029 0.254 0. -0.004 )
+ BODY504_NUT_PREC_PM = ( 0. 0. 0. 0. 0.061 -0.533 0. -0.009 )
+
+ \begintext
+
+
+ Amalthea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY505_POLE_RA = ( 268.05 -0.009 0. )
+ BODY505_POLE_DEC = ( 64.49 0.003 0. )
+ BODY505_PM = ( 231.67 722.6314560 0. )
+ BODY505_LONG_AXIS = ( 0. )
+
+ BODY505_NUT_PREC_RA = ( -0.84 0. 0. 0. 0. 0. 0. 0. 0.01 0. )
+ BODY505_NUT_PREC_DEC = ( -0.36 0. 0. 0. 0. 0. 0. 0. 0. 0. )
+ BODY505_NUT_PREC_PM = ( 0.76 0. 0. 0. 0. 0. 0. 0. -0.01 0. )
+
+ \begintext
+
+
+ Thebe
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY514_POLE_RA = ( 268.05 -0.009 0. )
+ BODY514_POLE_DEC = ( 64.49 0.003 0. )
+ BODY514_PM = ( 8.56 533.7004100 0. )
+ BODY514_LONG_AXIS = ( 0. )
+
+ BODY514_NUT_PREC_RA = ( 0. -2.11 0. 0. 0. 0. 0. 0. 0. 0.04 )
+ BODY514_NUT_PREC_DEC = ( 0. -0.91 0. 0. 0. 0. 0. 0. 0. 0.01 )
+ BODY514_NUT_PREC_PM = ( 0. 1.91 0. 0. 0. 0. 0. 0. 0. -0.04 )
+
+ \begintext
+
+
+ Adrastea
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+
+ BODY515_POLE_RA = ( 268.05 -0.009 0. )
+ BODY515_POLE_DEC = ( 64.49 0.003 0. )
+ BODY515_PM = ( 33.29 1206.9986602 0. )
+ BODY515_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Metis
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY516_POLE_RA = ( 268.05 -0.009 0. )
+ BODY516_POLE_DEC = ( 64.49 0.003 0. )
+ BODY516_PM = ( 346.09 1221.2547301 0. )
+ BODY516_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Mimas
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY601_POLE_RA = ( 40.66 -0.036 0. )
+ BODY601_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY601_PM = ( 337.46 381.9945550 0. )
+ BODY601_LONG_AXIS = ( 0. )
+
+ BODY601_NUT_PREC_RA = ( 0. 0. 13.56 0. 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_DEC = ( 0. 0. -1.53 0. 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_PM = ( 0. 0. -13.48 0. -44.85 0. 0. 0. 0. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY602_POLE_RA = ( 40.66 -0.036 0. )
+ BODY602_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY602_PM = ( 2.82 262.7318996 0. )
+ BODY602_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY603_POLE_RA = ( 40.66 -0.036 0. )
+ BODY603_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY603_PM = ( 10.45 190.6979085 0. )
+ BODY603_LONG_AXIS = ( 0. )
+
+ BODY603_NUT_PREC_RA = ( 0. 0. 0. 9.66 0. 0. 0. 0. 0. )
+ BODY603_NUT_PREC_DEC = ( 0. 0. 0. -1.09 0. 0. 0. 0. 0. )
+ BODY603_NUT_PREC_PM = ( 0. 0. 0. -9.60 2.23 0. 0. 0. 0. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY604_POLE_RA = ( 40.66 -0.036 0. )
+ BODY604_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY604_PM = ( 357.00 131.5349316 0. )
+ BODY604_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY605_POLE_RA = ( 40.38 -0.036 0. )
+ BODY605_POLE_DEC = ( 83.55 -0.004 0. )
+ BODY605_PM = ( 235.16 79.6900478 0. )
+ BODY605_LONG_AXIS = ( 0. )
+
+ BODY605_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 3.10 0. 0. 0. )
+ BODY605_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. -0.35 0. 0. 0. )
+ BODY605_NUT_PREC_PM = ( 0. 0. 0. 0. 0. -3.08 0. 0. 0. )
+
+ \begintext
+
+
+
+ Titan
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY606_POLE_RA = ( 36.41 -0.036 0. )
+ BODY606_POLE_DEC = ( 83.94 -0.004 0. )
+ BODY606_PM = ( 189.64 22.5769768 0. )
+ BODY606_LONG_AXIS = ( 0. )
+
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 2.66 0. 0 )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. -0.30 0. 0 )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. -2.64 0. 0 )
+
+ \begintext
+
+
+
+ Hyperion
+
+ The IAU report does not give an orientation model for Hyperion.
+ Hyperion's rotation is in chaotic and is not predictable for
+ long periods.
+
+
+ Iapetus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY608_POLE_RA = ( 318.16 -3.949 0. )
+ BODY608_POLE_DEC = ( 75.03 -1.143 0. )
+ BODY608_PM = ( 350.20 4.5379572 0. )
+ BODY608_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY609_POLE_RA = ( 356.90 0. 0. )
+ BODY609_POLE_DEC = ( 77.80 0. 0. )
+ BODY609_PM = ( 178.58 931.639 0. )
+ BODY609_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Janus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY610_POLE_RA = ( 40.58 -0.036 0. )
+ BODY610_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY610_PM = ( 58.83 518.2359876 0. )
+ BODY610_LONG_AXIS = ( 0. )
+
+ BODY610_NUT_PREC_RA = ( 0. -1.623 0. 0. 0. 0. 0. 0. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY611_POLE_RA = ( 40.58 -0.036 0. )
+ BODY611_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY611_PM = ( 293.87 518.4907239 0. )
+ BODY611_LONG_AXIS = ( 0. )
+
+ BODY611_NUT_PREC_RA = ( -3.153 0. 0. 0. 0. 0. 0. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY612_POLE_RA = ( 40.85 -0.036 0. )
+ BODY612_POLE_DEC = ( 83.34 -0.004 0. )
+ BODY612_PM = ( 245.12 131.6174056 0. )
+ BODY612_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Telesto
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY613_POLE_RA = ( 50.51 -0.036 0. )
+ BODY613_POLE_DEC = ( 84.06 -0.004 0. )
+ BODY613_PM = ( 56.88 190.6979332 0. )
+ BODY613_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Calypso
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY614_POLE_RA = ( 36.41 -0.036 0. )
+ BODY614_POLE_DEC = ( 85.04 -0.004 0. )
+ BODY614_PM = ( 153.51 190.6742373 0. )
+ BODY614_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Atlas
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY615_POLE_RA = ( 40.58 -0.036 0. )
+ BODY615_POLE_DEC = ( 83.53 -0.004 0. )
+ BODY615_PM = ( 137.88 598.3060000 0. )
+ BODY615_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Prometheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY616_POLE_RA = ( 40.58 -0.036 )
+ BODY616_POLE_DEC = ( 83.53 -0.004 )
+ BODY616_PM = ( 296.14 587.289000 )
+ BODY616_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Pandora
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY617_POLE_RA = ( 40.58 -0.036 0. )
+ BODY617_POLE_DEC = ( 83.53 -0.004 0. )
+ BODY617_PM = ( 162.92 572.7891000 0. )
+ BODY617_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Pan
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY618_POLE_RA = ( 40.6 -0.036 0. )
+ BODY618_POLE_DEC = ( 83.5 -0.004 0. )
+ BODY618_PM = ( 48.8 626.0440000 0. )
+ BODY618_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+
+Satellites of Uranus
+
+
+
+ Ariel
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY701_POLE_RA = ( 257.43 0. 0. )
+ BODY701_POLE_DEC = ( -15.10 0. 0. )
+ BODY701_PM = ( 156.22 -142.8356681 0. )
+ BODY701_LONG_AXIS = ( 0. )
+
+ BODY701_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0.29 )
+
+ BODY701_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0.28 )
+
+ BODY701_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0.05 0.08 )
+ \begintext
+
+
+
+ Umbriel
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY702_POLE_RA = ( 257.43 0. 0. )
+ BODY702_POLE_DEC = ( -15.10 0. 0. )
+ BODY702_PM = ( 108.05 -86.8688923 0. )
+ BODY702_LONG_AXIS = ( 0. )
+
+ BODY702_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0.21 )
+
+ BODY702_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0.20 )
+
+ BODY702_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. -0.09 0. 0.06 )
+
+ \begintext
+
+
+
+ Titania
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY703_POLE_RA = ( 257.43 0. 0. )
+ BODY703_POLE_DEC = ( -15.10 0. 0. )
+ BODY703_PM = ( 77.74 -41.3514316 0. )
+ BODY703_LONG_AXIS = ( 0. )
+
+ BODY703_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.29 )
+
+ BODY703_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.28 )
+
+ BODY703_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.08 )
+ \begintext
+
+
+
+ Oberon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY704_POLE_RA = ( 257.43 0. 0. )
+ BODY704_POLE_DEC = ( -15.10 0. 0. )
+ BODY704_PM = ( 6.77 -26.7394932 0. )
+ BODY704_LONG_AXIS = ( 0. )
+
+
+ BODY704_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.16 )
+
+ BODY704_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.16 )
+
+ BODY704_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.04 )
+ \begintext
+
+
+
+ Miranda
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+ BODY705_POLE_RA = ( 257.43 0. 0. )
+ BODY705_POLE_DEC = ( -15.08 0. 0. )
+ BODY705_PM = ( 30.70 -254.6906892 0. )
+ BODY705_LONG_AXIS = ( 0. )
+
+ BODY705_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 4.41 0. 0. 0. 0.
+ 0. -0.04 0. )
+
+ BODY705_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 4.25 0. 0. 0. 0.
+ 0. -0.02 0. )
+
+ BODY705_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 1.15 -1.27 0. 0. 0.
+ 0. -0.09 0.15 )
+ \begintext
+
+
+
+ Cordelia
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY706_POLE_RA = ( 257.31 0. 0. )
+ BODY706_POLE_DEC = ( -15.18 0. 0. )
+ BODY706_PM = ( 127.69 -1074.5205730 0. )
+ BODY706_LONG_AXIS = ( 0. )
+
+ BODY706_NUT_PREC_RA = ( -0.15 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY706_NUT_PREC_DEC = ( 0.14 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY706_NUT_PREC_PM = ( -0.04 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Ophelia
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY707_POLE_RA = ( 257.31 0. 0. )
+ BODY707_POLE_DEC = ( -15.18 0. 0. )
+ BODY707_PM = ( 130.35 -956.4068150 0. )
+ BODY707_LONG_AXIS = ( 0. )
+
+ BODY707_NUT_PREC_RA = ( 0. -0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY707_NUT_PREC_DEC = ( 0. 0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY707_NUT_PREC_PM = ( 0. -0.03 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Bianca
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY708_POLE_RA = ( 257.31 0. 0. )
+ BODY708_POLE_DEC = ( -15.18 0. 0. )
+ BODY708_PM = ( 105.46 -828.3914760 0. )
+ BODY708_LONG_AXIS = ( 0. )
+
+ BODY708_NUT_PREC_RA = ( 0. 0. -0.16 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY708_NUT_PREC_DEC = ( 0. 0. 0.16 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY708_NUT_PREC_PM = ( 0. 0. -0.04 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Cressida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+ BODY709_POLE_RA = ( 257.31 0. 0. )
+ BODY709_POLE_DEC = ( -15.18 0. 0. )
+ BODY709_PM = ( 59.16 -776.5816320 0. )
+ BODY709_LONG_AXIS = ( 0. )
+
+
+ BODY709_NUT_PREC_RA = ( 0. 0. 0. -0.04 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ BODY709_NUT_PREC_DEC = ( 0. 0. 0. 0.04 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ BODY709_NUT_PREC_PM = ( 0. 0. 0. -0.01 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ \begintext
+
+
+
+ Desdemona
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY710_POLE_RA = ( 257.31 0. 0. )
+ BODY710_POLE_DEC = ( -15.18 0. 0. )
+ BODY710_PM = ( 95.08 -760.0531690 0. )
+ BODY710_LONG_AXIS = ( 0. )
+
+ BODY710_NUT_PREC_RA = ( 0. 0. 0. 0. -0.17
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY710_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.16
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY710_NUT_PREC_PM = ( 0. 0. 0. 0. -0.04
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Juliet
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY711_POLE_RA = ( 257.31 0. 0. )
+ BODY711_POLE_DEC = ( -15.18 0. 0. )
+ BODY711_PM = ( 302.56 -730.1253660 0. )
+ BODY711_LONG_AXIS = ( 0. )
+
+ BODY711_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ -0.06 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY711_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0.06 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY711_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ -0.02 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Portia
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY712_POLE_RA = ( 257.31 0. 0. )
+ BODY712_POLE_DEC = ( -15.18 0. 0. )
+ BODY712_PM = ( 25.03 -701.4865870 0. )
+ BODY712_LONG_AXIS = ( 0. )
+
+ BODY712_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. -0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY712_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY712_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. -0.02 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Rosalind
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY713_POLE_RA = ( 257.31 0. 0. )
+ BODY713_POLE_DEC = ( -15.18 0. 0. )
+ BODY713_PM = ( 314.90 -644.6311260 0. )
+ BODY713_LONG_AXIS = ( 0. )
+
+ BODY713_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. -0.29 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY713_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0.28 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY713_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. -0.08 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Belinda
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY714_POLE_RA = ( 257.31 0. 0. )
+ BODY714_POLE_DEC = ( -15.18 0. 0. )
+ BODY714_PM = ( 297.46 -577.3628170 0. )
+ BODY714_LONG_AXIS = ( 0. )
+
+ BODY714_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. -0.03 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY714_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0.03 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY714_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. -0.01 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+ \begintext
+
+
+
+ Puck
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY715_POLE_RA = ( 257.31 0. 0. )
+ BODY715_POLE_DEC = ( -15.18 0. 0. )
+ BODY715_PM = ( 91.24 -472.5450690 0. )
+ BODY715_LONG_AXIS = ( 0. )
+
+ BODY715_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. -0.33
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY715_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.31
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY715_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. -0.09
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+
+Satellites of Neptune
+
+
+ Triton
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY801_POLE_RA = ( 299.36 0. 0. )
+ BODY801_POLE_DEC = ( 41.17 0. 0. )
+ BODY801_PM = ( 296.53 -61.2572637 0. )
+ BODY801_LONG_AXIS = ( 0. )
+
+
+ BODY801_NUT_PREC_RA = ( 0. 0. 0. 0.
+ 0. 0. 0. -32.35
+ 0. -6.28 -2.08 -0.74
+ -0.28 -0.11 -0.07 -0.02
+ -0.01 )
+
+
+ BODY801_NUT_PREC_DEC = ( 0. 0. 0. 0.
+ 0. 0. 0. 22.55
+ 0. 2.10 0.55 0.16
+ 0.05 0.02 0.01 0.
+ 0. )
+
+
+ BODY801_NUT_PREC_PM = ( 0. 0. 0. 0.
+ 0. 0. 0. 22.25
+ 0. 6.73 2.05 0.74
+ 0.28 0.11 0.05 0.02
+ 0.01 )
+
+ \begintext
+
+
+
+
+ Nereid
+
+ Old values:
+
+ Values are from the 1988 IAU report [10]. Note that this
+ rotation model pre-dated the 1989 Voyager 2 Neptune
+ encounter.
+
+
+ body802_pole_ra = ( 273.48 0. 0. )
+ body802_pole_dec = ( 67.22 0. 0. )
+ body802_pm = ( 237.22 0.9996465 0. )
+ body802_long_axis = ( 0. )
+
+
+ The report seems to have a typo: in the nut_prec_ra expression,
+ where the report gives -0.51 sin 3N3, we use -0.51 3N2.
+
+ body802_nut_prec_ra = ( 0. -17.81
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ 2.56 -0.51 0.11 -0.03 )
+
+ body802_nut_prec_dec = ( 0. -6.67
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ 0.47 -0.07 0.01 )
+
+ body802_nut_prec_pm = ( 0. 16.48
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ -2.57 0.51 -0.11 0.02 )
+
+
+
+ Current values:
+
+ The 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY803_POLE_RA = ( 299.36 0. 0. )
+ BODY803_POLE_DEC = ( 43.36 0. 0. )
+ BODY803_PM = ( 254.06 +1222.8441209 0. )
+ BODY803_LONG_AXIS = ( 0. )
+
+
+ BODY803_NUT_PREC_RA = ( 0.70 -6.49 0. 0.
+ 0. 0. 0. 0.
+ 0.25 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY803_NUT_PREC_DEC = ( -0.51 -4.75 0. 0.
+ 0. 0. 0. 0.
+ 0.09 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY803_NUT_PREC_PM = ( -0.48 4.40 0. 0.
+ 0. 0. 0. 0.
+ -0.27 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+
+ Thalassa
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY804_POLE_RA = ( 299.36 0. 0. )
+ BODY804_POLE_DEC = ( 43.45 0. 0. )
+ BODY804_PM = ( 102.06 1155.7555612 0. )
+ BODY804_LONG_AXIS = ( 0. )
+
+
+ BODY804_NUT_PREC_RA = ( 0.70 0. -0.28 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+
+ BODY804_NUT_PREC_DEC = ( -0.51 0. -0.21 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY804_NUT_PREC_PM = ( -0.48 0. 0.19 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+ Despina
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY805_POLE_RA = ( 299.36 0. 0. )
+ BODY805_POLE_DEC = ( 43.45 0. 0. )
+ BODY805_PM = ( 306.51 +1075.7341562 0. )
+ BODY805_LONG_AXIS = ( 0. )
+
+
+ BODY805_NUT_PREC_RA = ( 0.70 0. 0. -0.09
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY805_NUT_PREC_DEC = ( -0.51 0. 0. -0.07
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY805_NUT_PREC_PM = ( -0.49 0. 0. 0.06
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+
+ Galatea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY806_POLE_RA = ( 299.36 0. 0. )
+ BODY806_POLE_DEC = ( 43.43 0. 0. )
+ BODY806_PM = ( 258.09 839.6597686 0. )
+ BODY806_LONG_AXIS = ( 0. )
+
+
+ BODY806_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ -0.07 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY806_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ -0.05 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY806_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0.05 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+ Larissa
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY807_POLE_RA = ( 299.36 0. 0. )
+ BODY807_POLE_DEC = ( 43.41 0. 0. )
+ BODY807_PM = ( 179.41 +649.0534470 0. )
+ BODY807_LONG_AXIS = ( 0. )
+
+
+ BODY807_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ 0. -0.27 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY807_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ 0. -0.20 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY807_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0. 0.19 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+
+ Proteus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY808_POLE_RA = ( 299.27 0. 0. )
+ BODY808_POLE_DEC = ( 42.91 0. 0. )
+ BODY808_PM = ( 93.38 +320.7654228 0. )
+ BODY808_LONG_AXIS = ( 0. )
+
+
+ BODY808_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ 0. 0. -0.05 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY808_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ 0. 0. -0.04 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY808_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0. 0. 0.04 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+
+
+Satellites of Pluto
+
+ Charon
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY901_POLE_RA = ( 312.993 0. 0. )
+ BODY901_POLE_DEC = ( 6.163 0. 0. )
+ BODY901_PM = ( 57.305 -56.3625225 0. )
+ BODY901_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000005_POLE_RA = ( 218.5 0. 0. )
+ BODY1000005_POLE_DEC = ( -12.5 0. 0. )
+ BODY1000005_PM = ( 000. 390.0 0. )
+ BODY1000005_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000093_POLE_RA = ( 294. 0. 0. )
+ BODY1000093_POLE_DEC = ( 73. 0. 0. )
+ BODY1000093_PM = ( 252.63 212.064 0. )
+ BODY1000093_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000433_POLE_RA = ( 11.35 0. 0. )
+ BODY2000433_POLE_DEC = ( 17.22 0. 0. )
+ BODY2000433_PM = ( 326.07 1639.38864745 0. )
+ BODY2000433_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+ \begindata
+
+ BODY2025143_POLE_RA = ( 90.53 0. 0. )
+ BODY2025143_POLE_DEC = ( -66.30 0. 0. )
+ BODY2025143_PM = ( 000.0 712.143 0. )
+ BODY2025143_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2431010_POLE_RA = ( 168.76 0. 0. )
+ BODY2431010_POLE_DEC = ( -2.88 0. 0. )
+ BODY2431010_PM = ( 265.95 +1864.6280070 0. )
+ BODY2431010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY9511010_POLE_RA = ( 9.47 0. 0. )
+ BODY9511010_POLE_DEC = ( 26.70 0. 0. )
+ BODY9511010_PM = ( 83.67 1226.9114850 0. )
+ BODY9511010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values as the polar radius for
+ the triaxial model.
+
+ \begindata
+
+ BODY499_RADII = ( 3396.19 3396.19 3376.20 )
+
+ \begintext
+
+
+
+Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ BODY505_RADII = ( 125 73 64 )
+
+ \begintext
+
+ Only mean radii are available in the 2003 IAU report for bodies
+ 506-513.
+
+ \begindata
+
+ BODY506_RADII = ( 85 85 85 )
+ BODY507_RADII = ( 40 40 40 )
+ BODY508_RADII = ( 18 18 18 )
+ BODY509_RADII = ( 14 14 14 )
+ BODY510_RADII = ( 12 12 12 )
+ BODY511_RADII = ( 15 15 15 )
+ BODY512_RADII = ( 10 10 10 )
+ BODY513_RADII = ( 5 5 5 )
+ BODY514_RADII = ( 58 49 42 )
+ BODY515_RADII = ( 10 8 7 )
+
+ \begintext
+
+ The value for the second radius for body 516 is not given in
+ 2003 IAU report. The values given are:
+
+ BODY516_RADII = ( 30 --- 20 )
+
+ For use within the SPICE system, we use only the mean radius.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ body610_radii = ( 97.0 95.0 77.0 )
+ body611_radii = ( 69.0 55.0 55.0 )
+
+
+ Only the first equatorial radius for Helene (body 612) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ body613_radii = ( 15 12.5 7.5 )
+ body614_radii = ( 15.0 8.0 8.0 )
+ body615_radii = ( 18.5 17.2 13.5 )
+ body616_radii = ( 74.0 50.0 34.0 )
+ body617_radii = ( 55.0 44.0 31.0 )
+
+
+
+ Current values:
+
+ \begindata
+
+ BODY601_RADII = ( 207.4 196.8 190.6 )
+ BODY602_RADII = ( 256.6 251.4 248.3 )
+ BODY603_RADII = ( 540.4 531.1 527.5 )
+ BODY604_RADII = ( 563.8 561.0 560.3 )
+ BODY605_RADII = ( 767.2 762.5 763.1 )
+ BODY606_RADII = ( 2575 2575 2575 )
+ BODY607_RADII = ( 164 130 107 )
+ BODY608_RADII = ( 747.4 747.4 712.4 )
+ BODY609_RADII = ( 108.6 107.7 101.5 )
+ BODY610_RADII = ( 97.0 95.0 77.0 )
+ BODY611_RADII = ( 69.0 55.0 55.0 )
+
+ \begintext
+
+ Only the first equatorial radius for Helene (body 612) is given in the
+ 2006 IAU report:
+
+ BODY612_RADII = ( 17.5 --- --- )
+
+ The mean radius is 16km; we use this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ \begindata
+
+ BODY612_RADII = ( 17.5 17.5 17.5 )
+ BODY613_RADII = ( 15 12.5 7.5 )
+ BODY614_RADII = ( 15.0 8.0 8.0 )
+ BODY615_RADII = ( 18.5 17.2 13.5 )
+ BODY616_RADII = ( 74.0 50.0 34.0 )
+ BODY617_RADII = ( 55.0 44.0 31.0 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY701_RADII = ( 581.1 577.9 577.7 )
+ BODY702_RADII = ( 584.7 584.7 584.7 )
+ BODY703_RADII = ( 788.9 788.9 788.9 )
+ BODY704_RADII = ( 761.4 761.4 761.4 )
+ BODY705_RADII = ( 240.4 234.2 232.9 )
+
+ \begintext
+
+ The 2000 report gives only mean radii for satellites 706--715.
+
+ \begindata
+
+ BODY706_RADII = ( 13 13 13 )
+ BODY707_RADII = ( 15 15 15 )
+ BODY708_RADII = ( 21 21 21 )
+ BODY709_RADII = ( 31 31 31 )
+ BODY710_RADII = ( 27 27 27 )
+ BODY711_RADII = ( 42 42 42 )
+ BODY712_RADII = ( 54 54 54 )
+ BODY713_RADII = ( 27 27 27 )
+ BODY714_RADII = ( 33 33 33 )
+ BODY715_RADII = ( 77 77 77 )
+
+ \begintext
+
+
+
+
+Satellites of Neptune
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ The 2000 report gives mean radii only for bodies 801-806.
+
+ \begindata
+
+ BODY801_RADII = ( 1352.6 1352.6 1352.6 )
+ BODY802_RADII = ( 170 170 170 )
+ BODY803_RADII = ( 29 29 29 )
+ BODY804_RADII = ( 40 40 40 )
+ BODY805_RADII = ( 74 74 74 )
+ BODY806_RADII = ( 79 79 79 )
+
+ \begintext
+
+
+ The second equatorial radius for Larissa is not given in the 2000
+ report. The available values are:
+
+ BODY807_RADII = ( 104 --- 89 )
+
+ For use within the SPICE system, we use only the mean radius.
+ \begindata
+
+ BODY807_RADII = ( 96 96 96 )
+ BODY808_RADII = ( 218 208 201 )
+
+ \begintext
+
+
+
+
+Satellites of Pluto
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ Current values:
+
+
+ The value in the data assignment below is the
+ "effective radius."
+
+ The first principal axis length is
+
+ 3.5 km
+
+ The lengths of the other semi-axes are not provided
+ by [1].
+
+ \begindata
+
+ BODY1000005_RADII = ( 4.22 4.22 4.22 )
+
+ \begintext
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Current values:
+
+
+ The value in the data assignment below is the
+ "effective radius."
+
+ According to [1]:
+
+ The maximum and minimum radii are not properly
+ the values of the principal semi-axes, they
+ are half the maximum and minimum values of the
+ diameter. Due to the large deviations from a
+ simple ellipsoid, they may not correspond with
+ measurements along the principal axes, or be
+ orthogonal to each other.
+
+ \begindata
+
+ BODY1000093_RADII = ( 3.0 3.0 3.0 )
+
+ \begintext
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \begintext
+
+
+Kleopatra
+
+
+ Old values:
+
+ Values are from the 2003 report.
+
+
+ body2000216_radii = ( 108.5 47 40.5 )
+
+
+ Current values:
+
+
+ No values are provided in the 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/isds/chandrayannM3_isd.json b/tests/pytests/data/isds/chandrayannM3_isd.json
new file mode 100644
index 0000000000000000000000000000000000000000..eb7c86c3f077f13206a060af012de5696d5f3771
--- /dev/null
+++ b/tests/pytests/data/isds/chandrayannM3_isd.json
@@ -0,0 +1,415 @@
+{
+ "isis_camera_version": 1,
+ "image_lines": 5,
+ "image_samples": 608,
+ "name_platform": "CHANDRAYAAN-1",
+ "name_sensor": "MOON MINERALOGY MAPPER",
+ "reference_height": {
+ "maxheight": 1000,
+ "minheight": -1000,
+ "unit": "m"
+ },
+ "name_model": "USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL",
+ "interpolation_method": "lagrange",
+ "line_scan_rate": [
+ [
+ 0.5,
+ -0.12720000743865967,
+ 0.05088
+ ]
+ ],
+ "starting_ephemeris_time": 299622941.60814995,
+ "center_ephemeris_time": 299622941.73534995,
+ "radii": {
+ "semimajor": 1737.4,
+ "semiminor": 1737.4,
+ "unit": "km"
+ },
+ "body_rotation": {
+ "time_dependent_frames": [
+ 31006,
+ 1
+ ],
+ "ck_table_start_time": 299622941.60814995,
+ "ck_table_end_time": 299622941.86254996,
+ "ck_table_original_size": 2,
+ "ephemeris_times": [
+ 299622941.60814995,
+ 299622941.86254996
+ ],
+ "quaternions": [
+ [
+ -0.9747735513065916,
+ 0.19646555501476617,
+ -0.009172349392417702,
+ 0.1055162422212761
+ ],
+ [
+ -0.9747735156174205,
+ 0.196465551731104,
+ -0.009172415802241563,
+ 0.10551657226330902
+ ]
+ ],
+ "angular_velocities": [
+ [
+ 6.124937754497467e-08,
+ -1.0239801705539717e-06,
+ 2.4560118095097265e-06
+ ],
+ [
+ 6.12493776573662e-08,
+ -1.0239801709466094e-06,
+ 2.456011809503279e-06
+ ]
+ ],
+ "constant_frames": [
+ 31001,
+ 31007,
+ 31006
+ ],
+ "constant_rotation": [
+ 0.9999998732547144,
+ -0.00032928542237557133,
+ 0.00038086961867138755,
+ 0.00032928600021094723,
+ 0.9999999457843062,
+ -1.4544409378362713e-06,
+ -0.00038086911909607826,
+ 1.5798557868269087e-06,
+ 0.9999999274681067
+ ],
+ "reference_frame": 1
+ },
+ "instrument_pointing": {
+ "time_dependent_frames": [
+ -86000,
+ 1
+ ],
+ "ck_table_start_time": 299622941.60806996,
+ "ck_table_end_time": 299622941.86547,
+ "ck_table_original_size": 7,
+ "ephemeris_times": [
+ 299622941.60806996,
+ 299622941.65895,
+ 299622941.70983,
+ 299622941.76071,
+ 299622941.81158996,
+ 299622941.86247,
+ 299622941.86547
+ ],
+ "quaternions": [
+ [
+ -0.07932458945117579,
+ 0.6686267050477891,
+ -0.7382516883292113,
+ 0.04037800743484437
+ ],
+ [
+ -0.07931136277253394,
+ 0.6686270378355014,
+ -0.7382536542422642,
+ 0.040362532235106274
+ ],
+ [
+ -0.07929816903614584,
+ 0.6686273679739351,
+ -0.7382556180070331,
+ 0.0403470651326279
+ ],
+ [
+ -0.07928500836507205,
+ 0.6686276954564626,
+ -0.7382575796169487,
+ 0.04033160615764239
+ ],
+ [
+ -0.07927188089774231,
+ 0.6686280202760814,
+ -0.7382595390631518,
+ 0.0403161553584303
+ ],
+ [
+ -0.07925878672648098,
+ 0.6686283424269328,
+ -0.7382614963436729,
+ 0.04030071272892822
+ ],
+ [
+ -0.07925878672648098,
+ 0.6686283424269328,
+ -0.7382614963436729,
+ 0.04030071272892822
+ ]
+ ],
+ "angular_velocities": null,
+ "reference_frame": 1,
+ "constant_frames": [
+ -86520,
+ -86000
+ ],
+ "constant_rotation": [
+ 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0,
+ 0.0,
+ 0.0,
+ 0.0,
+ 1.0
+ ]
+ },
+ "naif_keywords": {
+ "BODY301_RADII": [
+ 1737.4,
+ 1737.4,
+ 1737.4
+ ],
+ "BODY_FRAME_CODE": 31001,
+ "BODY_CODE": 301,
+ "INS-86520_ITRANSS": [
+ -1.9610889460163698,
+ -0.054945530371164404,
+ -37.036996280362
+ ],
+ "INS-86520_BORESIGHT_SAMPLE": 304.5,
+ "TKFRAME_-86520_RELATIVE": "CH1_SPACECRAFT",
+ "INS-86520_OD_K": [
+ 0.000379921103637315,
+ 0.000213226448051461,
+ -4.0186287875859195e-08
+ ],
+ "FRAME_-86520_CLASS": 4.0,
+ "INS-86520_DECENTER": [
+ 0.004047,
+ -5e-06
+ ],
+ "INS-86520_CK_REFERENCE_ID": 1.0,
+ "INS-86520_PLATFORM_ID": -86000.0,
+ "TKFRAME_-86520_UNITS": "DEGREES",
+ "INS-86520_LT_SURFACE_CORRECT": "TRUE",
+ "INS-86520_SWAP_OBSERVER_TARGET": "TRUE",
+ "TKFRAME_-86520_ANGLES": [
+ 0.0,
+ 0.0,
+ 0.0
+ ],
+ "FRAME_-86520_CENTER": -86.0,
+ "INS-86520_LIGHTTIME_CORRECTION": "NONE",
+ "INS-86520_PIXEL_PITCH": 0.027,
+ "FRAME_-86520_NAME": "CHANDRAYAAN-1_M3",
+ "TKFRAME_-86520_AXES": [
+ 1.0,
+ 2.0,
+ 3.0
+ ],
+ "TKFRAME_-86520_SPEC": "ANGLES",
+ "INS-86520_TRANSX": [
+ -0.64,
+ -4.00552916405788e-05,
+ 0.0269999702883839
+ ],
+ "INS-86520_TRANSY": [
+ -0.052,
+ -0.0269999702883839,
+ -4.00552916405788e-05
+ ],
+ "FRAME_-86520_CLASS_ID": -86520.0,
+ "INS-86520_CK_FRAME_ID": -86000.0,
+ "INS-86520_BORESIGHT_LINE": 0.0,
+ "INS-86520_FOCAL_LENGTH": 39.63,
+ "INS-86520_PP": [
+ 0.0,
+ 0.0
+ ],
+ "INS-86520_ITRANSL": [
+ 23.7008204518524,
+ 37.036996280362,
+ -0.054945530371164404
+ ],
+ "BODY301_POLE_RA": [
+ 269.9949,
+ 0.0031,
+ 0.0
+ ],
+ "BODY301_NUT_PREC_PM": [
+ 3.561,
+ 0.1208,
+ -0.0642,
+ 0.0158,
+ 0.0252,
+ -0.0066,
+ -0.0047,
+ -0.0046,
+ 0.0028,
+ 0.0052
+ ],
+ "BODY301_NUT_PREC_RA": [
+ -3.8787000000000003,
+ -0.1204,
+ 0.07,
+ -0.0172,
+ 0.0,
+ 0.0072,
+ 0.0,
+ 0.0,
+ 0.0,
+ -0.0052
+ ],
+ "BODY301_LONG_AXIS": 0.0,
+ "BODY301_NUT_PREC_DEC": [
+ 1.5419,
+ 0.0239,
+ -0.0278,
+ 0.0068,
+ 0.0,
+ -0.0029,
+ 0.0009,
+ 0.0,
+ 0.0,
+ 0.0008
+ ],
+ "BODY301_POLE_DEC": [
+ 66.5392,
+ 0.013,
+ 0.0
+ ],
+ "BODY301_PM": [
+ 38.3213,
+ 13.17635815,
+ -1.3999999999999999e-12
+ ]
+ },
+ "detector_sample_summing": 1,
+ "detector_line_summing": 1,
+ "focal_length_model": {
+ "focal_length": 39.63
+ },
+ "detector_center": {
+ "line": 0.0,
+ "sample": 304.5
+ },
+ "focal2pixel_lines": [
+ 23.7008204518524,
+ 37.036996280362,
+ -0.054945530371164404
+ ],
+ "focal2pixel_samples": [
+ -1.9610889460163698,
+ -0.054945530371164404,
+ -37.036996280362
+ ],
+ "optical_distortion": {
+ "radial": {
+ "coefficients": [
+ 0.0,
+ 0.0,
+ 0.0
+ ]
+ }
+ },
+ "starting_detector_line": 0,
+ "starting_detector_sample": 0,
+ "instrument_position": {
+ "spk_table_start_time": 299622941.60814995,
+ "spk_table_end_time": 299622941.86254996,
+ "spk_table_original_size": 6,
+ "ephemeris_times": [
+ 299622941.60814995,
+ 299622941.65902996,
+ 299622941.70991,
+ 299622941.76078993,
+ 299622941.81166995,
+ 299622941.86254996
+ ],
+ "positions": [
+ [
+ 87.43803283072197,
+ 170.58382785758494,
+ 1937.3684802589921
+ ],
+ [
+ 87.43510506145041,
+ 170.5039141771109,
+ 1937.376298445722
+ ],
+ [
+ 87.43218518920048,
+ 170.42401232587338,
+ 1937.3841107949745
+ ],
+ [
+ 87.42927324562292,
+ 170.3441224440555,
+ 1937.3919172883918
+ ],
+ [
+ 87.42636925235688,
+ 170.26424439143332,
+ 1937.3997179348762
+ ],
+ [
+ 87.42347324097756,
+ 170.18437830744463,
+ 1937.4075127164092
+ ]
+ ],
+ "velocities": [
+ [
+ -0.05762002410373986,
+ -1.5707459933015884,
+ 0.1537165891795824
+ ],
+ [
+ -0.05746510464914588,
+ -1.5705139595332909,
+ 0.1536019506461352
+ ],
+ [
+ -0.05730961271290819,
+ -1.5702809919216132,
+ 0.15348712189335625
+ ],
+ [
+ -0.05715359501832903,
+ -1.570047160550427,
+ 0.1533721371829534
+ ],
+ [
+ -0.0569969401442109,
+ -1.569812298292768,
+ 0.1532569148111189
+ ],
+ [
+ -0.056840025211490175,
+ -1.5695769708168128,
+ 0.15314173131318826
+ ]
+ ],
+ "reference_frame": 1
+ },
+ "sun_position": {
+ "spk_table_start_time": 299622941.73534995,
+ "spk_table_end_time": 299622941.73534995,
+ "spk_table_original_size": 1,
+ "ephemeris_times": [
+ 299622941.73534995
+ ],
+ "positions": [
+ [
+ -22279396.272817865,
+ 138086310.683749,
+ 59901633.861951254
+ ]
+ ],
+ "velocities": [
+ [
+ -29.247063986944152,
+ -3.0931661850381134,
+ -1.3160268288136903
+ ]
+ ],
+ "reference_frame": 1
+ }
+}
\ No newline at end of file
diff --git a/tests/pytests/test_chandrayaan_driver.py b/tests/pytests/test_chandrayaan_driver.py
new file mode 100644
index 0000000000000000000000000000000000000000..43a9779a6ee8063d955db62a87a82cf6348113c2
--- /dev/null
+++ b/tests/pytests/test_chandrayaan_driver.py
@@ -0,0 +1,48 @@
+from cgi import test
+import pytest
+import ale
+import os
+import pvl
+
+import numpy as np
+from ale.drivers import co_drivers
+from ale.formatters.formatter import to_isd
+import unittest
+from unittest.mock import PropertyMock, patch
+import json
+from conftest import get_image_label, get_image_kernels, get_isd, convert_kernels, compare_dicts, get_table_data
+
+from ale.drivers.chandrayaan_drivers import Chandrayaan1M3IsisLabelNaifSpiceDriver
+
+@pytest.fixture()
+def m3_kernels(scope="module", autouse=True):
+ kernels = get_image_kernels("M3T20090630T083407_V03_RDN")
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+def test_chandrayaan_load(m3_kernels):
+ label_file = get_image_label("M3T20090630T083407_V03_RDN", label_type="isis")
+ compare_dict = get_isd("chandrayannM3")
+
+ isd_str = ale.loads(label_file, props={"kernels": m3_kernels}, verbose=True)
+ isd_obj = json.loads(isd_str)
+ x = compare_dicts(isd_obj, compare_dict)
+ assert x == []
+
+# ========= Test chandrayaan isislabel and naifspice driver =========
+class test_chandrayaan_isis_naif(unittest.TestCase):
+
+ def setUp(self):
+ label = get_image_label("M3T20090630T083407_V03_RDN", "isis")
+ self.driver = Chandrayaan1M3IsisLabelNaifSpiceDriver(label)
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "CHANDRAYAAN-1_M3"
+
+ def test_ikid_id(self):
+ assert self.driver.spacecraft_id == -86
+
+ def test_sensor_model_version(self):
+ assert self.driver.sensor_model_version == 1
\ No newline at end of file