From 8aa3b10ade682d45ccafe539057f7c6c0ede4fa8 Mon Sep 17 00:00:00 2001 From: Jacob Cain <115182890+jrcain-usgs@users.noreply.github.com> Date: Fri, 26 May 2023 15:23:56 -0700 Subject: [PATCH] Hayabusa NIRS (#532) * Changed hirise comment * Added NIRS driver * added nirs test isd * Added NIRS Tests * added NIRS test kernels * added NIRS changelog entry * remove projection/geotransform in truth ISD --- CHANGELOG.md | 3 +- ale/drivers/hayabusa_drivers.py | 70 +- .../2392975548_lvl3_0.ale_0.xsp | 151 + .../2392975548_lvl3_0.ale_1.xsp | 965 +++++ .../2392975548_lvl3_0_isis.lbl | 401 ++ .../data/2392975548_lvl3_0/hayabusa.tsc | 3462 ++++++++++++++++ .../data/2392975548_lvl3_0/hayabusa_hp.tf | 392 ++ ...itokawarendezvous_v02n_0_sliced_-130000.xc | 56 + ...itokawarendezvous_v02n_1_sliced_-130000.xc | 120 + .../data/2392975548_lvl3_0/itokawa_fixed.tf | 94 + .../2392975548_lvl3_0/itokawa_gaskell_n3.tpc | 115 + .../data/2392975548_lvl3_0/naif0012.tls | 152 + .../pytests/data/2392975548_lvl3_0/nirs10.ti | 184 + .../data/2392975548_lvl3_0/nirsAddendum002.ti | 34 + .../data/2392975548_lvl3_0/pck00009.tpc | 3639 +++++++++++++++++ tests/pytests/data/isds/hayabusanirs_isd.json | 260 ++ tests/pytests/test_hayabusa_drivers.py | 48 +- 17 files changed, 10141 insertions(+), 5 deletions(-) create mode 100644 tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp create mode 100644 tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp create mode 100644 tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl create mode 100755 tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc create mode 100755 tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf create mode 100644 tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc create mode 100644 tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc create mode 100755 tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf create mode 100755 tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc create mode 100755 tests/pytests/data/2392975548_lvl3_0/naif0012.tls create mode 100755 tests/pytests/data/2392975548_lvl3_0/nirs10.ti create mode 100755 tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti create mode 100755 tests/pytests/data/2392975548_lvl3_0/pck00009.tpc create mode 100644 tests/pytests/data/isds/hayabusanirs_isd.json diff --git a/CHANGELOG.md b/CHANGELOG.md index 595f0ff..9bc002d 100644 --- a/CHANGELOG.md +++ b/CHANGELOG.md @@ -52,4 +52,5 @@ release. - Msi IsisLabelNaifSpice Driver [#511](https://github.com/DOI-USGS/ale/pull/511) - MGS MOC WAC IsisLabelNaifSpice driver, tests, and test data [#516](https://github.com/DOI-USGS/ale/pull/516) - Chandrayaan1_mrffr IsisLabelNaifSpice driver, tests and test data [#519](https://github.com/DOI-USGS/ale/pull/519) -- MGS MOC Narrow Angle IsisLabelNaifSpice driver, tests, and test data [#517](https://github.com/DOI-USGS/ale/pull/517) \ No newline at end of file +- MGS MOC Narrow Angle IsisLabelNaifSpice driver, tests, and test data [#517](https://github.com/DOI-USGS/ale/pull/517) +- Hayabusa NIRS IsisLabelNaifSpice driver, tests and test data [#532](https://github.com/DOI-USGS/ale/pull/532) \ No newline at end of file diff --git a/ale/drivers/hayabusa_drivers.py b/ale/drivers/hayabusa_drivers.py index c4a2614..04b28b8 100644 --- a/ale/drivers/hayabusa_drivers.py +++ b/ale/drivers/hayabusa_drivers.py @@ -1,3 +1,4 @@ +import spiceypy as spice from ale.base.data_naif import NaifSpice from ale.base.label_isis import IsisLabel from ale.base.type_sensor import Framer @@ -22,7 +23,7 @@ class HayabusaAmicaIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Radial @property def sensor_model_version(self): """ - The ISIS Sensor model number for HiRise in ISIS. This is likely just 1 + The ISIS Sensor model number for Hayabusa Amica in ISIS. This is likely just 1 Returns ------- @@ -41,4 +42,69 @@ class HayabusaAmicaIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Radial : str Name of the sensor """ - return self.instrument_id \ No newline at end of file + return self.instrument_id + +class HayabusaNirsIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Driver): + + @property + def instrument_id(self): + """ + Returns the ID of the instrument + + Returns + ------- + : str + Name of the instrument + """ + lookup_table = {'NIRS': 'HAYABUSA_NIRS'} + return lookup_table[super().instrument_id] + + @property + def sensor_model_version(self): + """ + The ISIS Sensor model number for Hayabusa Nirs in ISIS. This is likely just 1 + + Returns + ------- + : int + ISIS sensor model version + """ + return 1 + + @property + def sensor_name(self): + """ + Returns the name of the instrument + + Returns + ------- + : str + Name of the sensor + """ + return self.instrument_id + + @property + def ephemeris_stop_time(self): + """ + Returns the exposure duration of the instrument + + Returns + ------- + : str + Exposure Duration + """ + + return spice.scs2e(self.spacecraft_id, self.spacecraft_clock_stop_count) + + @property + def exposure_duration(self): + """ + Returns the exposure duration of the instrument + + Returns + ------- + : str + Exposure Duration + """ + + return self.ephemeris_stop_time - self.ephemeris_start_time \ No newline at end of file diff --git a/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp new file mode 100644 index 0000000..0356b32 --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp @@ -0,0 +1,151 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/SPK ' +'2' +'6' +'SPKMERGE ' +BEGIN_ARRAY 1 33 +'ITOKAWA ' +'AC1FE9B5AB9B2^7' +'AC1FFCFB61E0C^7' +'1EE6B7' +'A' +'1' +'2' +33 +'AC164C^7' +'2A3^5' +'-96164580E2F96^7' +'-98AFDA22EDFAC8^5' +'7F8792164BF8^4' +'8E57FFDE00C6^2' +'-23C2C8BC^0' +'-18BFAFA64^-1' +'-2E9FC^-3' +'-199848^-5' +'E^-7' +'3265DFC23373^7' +'-480F9DC9F93DDC^6' +'-2ACF5A5F69F^4' +'7ABC039D108^2' +'FE2237B8^0' +'CCCE755^-2' +'-11C8C^-3' +'-507E4^-5' +'-68^-7' +'1ACE10954DD2DE^7' +'-1FD5B586354A57^6' +'-16C533CA1634^4' +'3291BBCE2D5^2' +'7247BDBD8^0' +'66BB89F8^-2' +'-692A^-4' +'-231B4^-5' +'-28^-7' +'ABEC1C^7' +'546^5' +'1D^2' +'1^1' +END_ARRAY 1 33 +BEGIN_ARRAY 2 16 +'HAYABUSA Traj. by HJSC; with NAIF mods ' +'AC1FE9B5AB9B2^7' +'AC1FFCFB61E0C^7' +'-82' +'1EE6B7' +'1' +'9' +16 +'FD0D130C3E5CF8^1' +'-32CEAB825B452A^1' +'-1C8AE979EBDB0B^1' +'18997317907C75^-3' +'-11922DF762C049^-4' +'-DDCD8152470B9^-5' +'10C1B09DB1E9EB^2' +'-337AB8D362FE0C^1' +'-1D12A714AB578D^1' +'160C4781A00001^-3' +'-5E8A965C^-5' +'-74440DFD^-5' +'AC164E001A362^7' +'AC2018B41E4B28^7' +'1^1' +'2^1' +END_ARRAY 2 16 +BEGIN_ARRAY 3 39 +'DE-0403LE-0403 ' +'AC1FE9B5AB9B2^7' +'AC1FFCFB61E0C^7' +'A' +'0' +'1' +'2' +39 +'ACA9F4^7' +'A8C^5' +'95D530B0708338^5' +'-954848CD8FCCC8^3' +'-1237A4B9E50726^2' +'27BC5CD97A7B14^0' +'-A008B2350BB548^-2' +'-D2B620BE6E8188^-3' +'1CCEE01A24443C^-3' +'-2DD8F01365A4FA^-4' +'36287C4B50D55A^-5' +'-1FE65DFD04A91B^-6' +'-6A58460956428^-7' +'36DF7F7552069^5' +'1C5529660F3CE4^4' +'-A946527ED81378^1' +'9A0E242217DF6^-1' +'16FE20CDC8E56B^-1' +'-1292E9468DA1ED^-2' +'BAEA14DDB07C4^-4' +'6342B3BBC0991C^-5' +'-2DB7DC8B183E78^-5' +'628F2A73E43B98^-6' +'-B29DC397F7128^-7' +'1327760ADD39C3^5' +'C31C168F8BEC^3' +'-42418DABAB8A8^1' +'E630651E16D2E^-2' +'BD018994D52C78^-2' +'-878B623FBBAAB^-3' +'35FD3ECDACEEC2^-4' +'81103383568628^-5' +'-1E099CC4A97B08^-5' +'38632AEF23BA6^-6' +'-544DDE19114234^-7' +'AC0134^7' +'1518^6' +'23^2' +'1^1' +END_ARRAY 3 39 +TOTAL_ARRAYS 3 + ~NAIF/SPC BEGIN COMMENTS~ + +; Created 2023-05-05/16:06:04.00. +; +; BEGIN SPKMERGE COMMANDS + +LEAPSECONDS_KERNEL = ~/remotedata/isis_data/base/kernels/lsk/naif0012.tls + +SPK_KERNEL = ~/data/isistestdata/hayabusa/nirs/out/2392975548_lvl3_0.ale_0.bsp +SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/sb_25143_140.bsp + INCLUDE_COMMENTS = NO + BODIES = 2025143 + BEGIN_TIME = 2005 SEP 20 10:55:23.172 + END_TIME = 2005 SEP 20 11:00:31.529 +SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp + INCLUDE_COMMENTS = NO + BODIES = -130 + BEGIN_TIME = 2005 SEP 20 10:55:23.172 + END_TIME = 2005 SEP 20 11:00:31.529 +SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/de403s.bsp + INCLUDE_COMMENTS = NO + BODIES = 10 + BEGIN_TIME = 2005 SEP 20 10:55:23.172 + END_TIME = 2005 SEP 20 11:00:31.529 + +; END SPKMERGE COMMANDS + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp new file mode 100644 index 0000000..a7b0e8a --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp @@ -0,0 +1,965 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/SPK ' +'2' +'6' +'SPKMERGE ' +BEGIN_ARRAY 1 33 +'ITOKAWA ' +'AC200CC268059^7' +'AC201FED9F515^7' +'1EE6B7' +'A' +'1' +'2' +33 +'AC164C^7' +'2A3^5' +'-96164580E2F96^7' +'-98AFDA22EDFAC8^5' +'7F8792164BF8^4' +'8E57FFDE00C6^2' +'-23C2C8BC^0' +'-18BFAFA64^-1' +'-2E9FC^-3' +'-199848^-5' +'E^-7' +'3265DFC23373^7' +'-480F9DC9F93DDC^6' +'-2ACF5A5F69F^4' +'7ABC039D108^2' +'FE2237B8^0' +'CCCE755^-2' +'-11C8C^-3' +'-507E4^-5' +'-68^-7' +'1ACE10954DD2DE^7' +'-1FD5B586354A57^6' +'-16C533CA1634^4' +'3291BBCE2D5^2' +'7247BDBD8^0' +'66BB89F8^-2' +'-692A^-4' +'-231B4^-5' +'-28^-7' +'ABEC1C^7' +'546^5' +'1D^2' +'1^1' +END_ARRAY 1 33 +BEGIN_ARRAY 2 829 +'HAYABUSA Traj. by HJSC; with NAIF mods ' +'AC200CC268059^7' +'AC201FED9F515^7' +'-82' +'1EE6B7' +'1' +'9' +829 +'FD0D130C3E5CF8^1' +'-32CEAB825B452A^1' +'-1C8AE979EBDB0B^1' +'18997317907C75^-3' +'-11922DF762C049^-4' +'-DDCD8152470B9^-5' +'10C1B09DB1E9EB^2' +'-337AB8D362FE0C^1' +'-1D12A714AB578D^1' +'160C4781A00001^-3' +'-5E8A965C^-5' +'-74440DFD^-5' +'10C1B1FE766205^2' +'-337AB931ED9468^1' +'-1D12A788EF658A^1' +'160C3F30FFFFFF^-3' +'-5E881D10000004^-5' +'-7442AE24^-5' +'10C1B35F3A5515^2' +'-337AB99075B178^1' +'-1D12A7FD3213AE^1' +'160C36CEBFFFFF^-3' +'-5E85D882^-5' +'-74415FE6^-5' +'10C1B4BFFDC201^2' +'-337AB9EEFB89FA^1' +'-1D12A871737394^1' +'160C2E7E2^-3' +'-5E835F3^-5' +'-7440000C000004^-5' +'10C1B620C0A9E3^2' +'-337ABA4D7EE92A^1' +'-1D12A8E5B373A^1' +'160C262D5FFFFF^-3' +'-5E810910000004^-5' +'-743EB1CBFFFFFC^-5' +'10C1B781830CB9^2' +'-337ABAABFFF23A^1' +'-1D12A959F2256C^1' +'160C1DDCCFFFFF^-3' +'-5E7EA153FFFFFC^-5' +'-743D405D^-5' +'10C1B8E244EA86^2' +'-337ABB0A7E938E^1' +'-1D12A9CE2F65C9^1' +'160C157A8FFFFF^-3' +'-5E7C4B32^-5' +'-743C03B4^-5' +'10C1BA4306422F^2' +'-337ABB68FADEC^1' +'-1D12AA426B697D^1' +'160C0D29CFFFFF^-3' +'-5E79D1E1FFFFFC^-5' +'-743A9244^-5' +'10C1BBA3C714CC^2' +'-337ABBC774B0A2^1' +'-1D12AAB6A5FBC1^1' +'160C04C7B^-3' +'-5E778D56^-5' +'-74394404^-5' +'10C1BD04876147^2' +'-337ABC25EC3DF8^1' +'-1D12AB2ADF3FC5^1' +'1611A2D2578ACA^-3' +'-5E8D487F040C04^-5' +'-7455BDCB13218C^-5' +'10C1BE654729D^2' +'-337ABC846151FE^1' +'-1D12AB9F173589^1' +'160BF4263FFFFF^-3' +'-5E72BDE1FFFFFC^-5' +'-74368453^-5' +'10C1BFC6066C34^2' +'-337ABCE2D40FE^1' +'-1D12AC134DB9DC^1' +'160BEBC42^-3' +'-5E705627FFFFFC^-5' +'-743547ABFFFFFC^-5' +'10C1C126C52876^2' +'-337ABD41446608^1' +'-1D12AC87830188^1' +'160BE385^-3' +'-5E6E0006^-5' +'-7433D63AFFFFFC^-5' +'10C1C2878360C6^2' +'-337ABD9FB2660E^1' +'-1D12ACFBB6D7C3^1' +'160BDB22C^-3' +'-5E6B984A^-5' +'-743287FAFFFFFC^-5' +'10C1C3E84112F2^2' +'-337ABDFE1DFE58^1' +'-1D12AD6FE95FBE^1' +'160BD2D2200002^-3' +'-5E693094000004^-5' +'-743139BB^-5' +'10C1C548FE4014^2' +'-337ABE5C872EEC^1' +'-1D12ADE41A9979^1' +'160BCA6FE00001^-3' +'-5E66C8D6000004^-5' +'-742FC84B^-5' +'10C1C6A9BAE712^2' +'-337ABEBAEDF7C2^1' +'-1D12AE584A61C4^1' +'160BC21F3^-3' +'-5E6472B6^-5' +'-742E8BA2000004^-5' +'10C1C80A770905^2' +'-337ABF19526A78^1' +'-1D12AECC78ED66^1' +'160BB9CEA^-3' +'-5E620AFC^-5' +'-742D1A33^-5' +'10C1C96B32A5EF^2' +'-337ABF77B47574^1' +'-1D12AF40A60799^1' +'160BB17DDFFFFF^-3' +'-5E5FB4D6^-5' +'-742BCBF2^-5' +'10C1CACBEDBDCD^2' +'-337ABFD6142A4A^1' +'-1D12AFB4D1D38B^1' +'160BA91BAFFFFF^-3' +'-5E5D4D22^-5' +'-742A7DB2^-5' +'10C1CC2CA84F88^2' +'-337AC03471776C^1' +'-1D12B028FC513D^1' +'160BA0CB000001^-3' +'-5E5AE564^-5' +'-74290C42^-5' +'10C1CD8D625C38^2' +'-337AC092CC5CD^1' +'-1D12B09D255D7F^1' +'160B987A4FFFFF^-3' +'-5E588F42^-5' +'-7427CF9A^-5' +'10C1CEEE1BE3DD^2' +'-337AC0F124EC12^1' +'-1D12B1114D2D19^1' +'160B9018200002^-3' +'-5E562789FFFFFC^-5' +'-74265E2B^-5' +'10C1D04ED4E55F^2' +'-337AC14F7B139C^1' +'-1D12B185738B44^1' +'160B87C77^-3' +'-5E53BFCE^-5' +'-74250FE9000004^-5' +'10C1D1AF8D61D6^2' +'-337AC1ADCED36A^1' +'-1D12B1F9989B2D^1' +'160B7F76D00001^-3' +'-5E5169AA000004^-5' +'-7423C1A8FFFFFC^-5' +'10C1D310455943^2' +'-337AC20C203D14^1' +'-1D12B26DBC5CD6^1' +'160B77147FFFFF^-3' +'-5E4F01F2000004^-5' +'-7422503A000004^-5' +'10C1D470FCCA8B^2' +'-337AC26A6F3F06^1' +'-1D12B2E1DEAD1^1' +'160B6EC3EFFFFE^-3' +'-5E4C9A3A000004^-5' +'-742101F8^-5' +'10C1D5D1B3B6CA^2' +'-337AC2C8BBD94^1' +'-1D12B355FFAF08^1' +'160B66734^-3' +'-5E4A4416^-5' +'-741FB3B9^-5' +'10C1D7326A1DFE^2' +'-337AC327061D56^1' +'-1D12B3CA1F62C1^1' +'160B5E228FFFFF^-3' +'-5E47DC5C^-5' +'-741E53E2^-5' +'10C1D893200027^2' +'-337AC3854DF9B2^1' +'-1D12B43E3DB6A3^1' +'160B55C04FFFFF^-3' +'-5E4574A2^-5' +'-741CF409000004^-5' +'10C1D9F3D55C2C^2' +'-337AC3E3936E54^1' +'-1D12B4B25AAAAC^1' +'160B4D6FB00001^-3' +'-5E431E80000004^-5' +'-741BA5C6FFFFFC^-5' +'10C1DB548A3327^2' +'-337AC441D68CD4^1' 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+'-337AE30EA36C3^1' +'-1D12DB2CBE013C^1' +'160888DEA00001^-3' +'-5D78ABEA^-5' +'-73A92933^-5' +'10C250692559AE^2' +'-337AE36C1C181A^1' +'-1D12DBA0672A6F^1' +'1608808E100001^-3' +'-5D764432000004^-5' +'-73A7C95B000004^-5' +'AC164E001A362^7' +'AC2018B41E4B28^7' +'AC2018C41E4B28^7' +'AC2018D41E4B28^7' +'AC2018E41E4B28^7' +'AC2018F41E4B28^7' +'AC2019041E4B28^7' +'AC2019141E4B28^7' +'AC2019241E4B28^7' +'AC2019341E4B28^7' +'AC2019441E4B28^7' +'AC2019541A3298^7' +'AC2019641A3298^7' +'AC2019741A3298^7' +'AC2019841A3298^7' +'AC2019941A3298^7' +'AC2019A41A3298^7' +'AC2019B41A3298^7' +'AC2019C41A3298^7' +'AC2019D41A3298^7' +'AC2019E41A3298^7' +'AC2019F41A3298^7' +'AC201A041A3298^7' +'AC201A141A3298^7' +'AC201A241A3298^7' +'AC201A341A3298^7' +'AC201A441A3298^7' +'AC201A541A3298^7' +'AC201A641A3298^7' +'AC201A741A3298^7' +'AC201A841A3298^7' +'AC201A941A3298^7' +'AC201AA41A3298^7' +'AC201AB41A3298^7' +'AC201AC41A3298^7' +'AC201AD41A3298^7' +'AC201AE41A3298^7' +'AC201AF41A3298^7' +'AC201B041A3298^7' +'AC201B141A3298^7' +'AC201B241A3298^7' +'AC201B341A3298^7' +'AC201B441A3298^7' +'AC201B541A3298^7' +'AC201B641A3298^7' +'AC201B741A3298^7' +'AC201B841A3298^7' +'AC201B941A3298^7' +'AC201BA41A3298^7' +'AC201BB41A3298^7' +'AC201BC41A3298^7' +'AC201BD4161A08^7' +'AC201BE4161A08^7' +'AC201BF4161A08^7' +'AC201C04161A08^7' +'AC201C14161A08^7' +'AC201C24161A08^7' +'AC201C34161A08^7' +'AC201C44161A08^7' +'AC201C54161A08^7' +'AC201C64161A08^7' +'AC201C74161A08^7' +'AC201C84161A08^7' +'AC201C94161A08^7' +'AC201CA4161A08^7' +'AC201CB4161A08^7' +'AC201CC4161A08^7' +'AC201CD4161A08^7' +'AC201CE4161A08^7' +'AC201CF4161A08^7' +'AC201D04161A08^7' +'AC201D14161A08^7' +'AC201D24161A08^7' +'AC201D34161A08^7' +'AC201D44161A08^7' +'AC201D54161A08^7' +'AC201D64161A08^7' +'AC201D74161A08^7' +'AC201D84161A08^7' +'AC201D94161A08^7' +'AC201DA4161A08^7' +'AC201DB4161A08^7' +'AC201DC4161A08^7' +'AC201DD4161A08^7' +'AC201DE4161A08^7' +'AC201DF4161A08^7' +'AC201E04161A08^7' +'AC201E14161A08^7' +'AC201E24161A08^7' +'AC201E34161A08^7' +'AC201E44161A08^7' +'AC201E5412017^7' +'AC201E6412017^7' +'AC201E7412017^7' +'AC201E8412017^7' +'AC201E9412017^7' +'AC201EA412017^7' +'AC201EB412017^7' +'AC201EC412017^7' +'AC201ED412017^7' +'AC201EE412017^7' +'AC201EF412017^7' +'AC201F0412017^7' +'AC201F1412017^7' +'AC201F2412017^7' +'AC201F3412017^7' +'AC201F4412017^7' +'AC201F5412017^7' +'AC201F6412017^7' +'AC201F7412017^7' +'AC201F8412017^7' +'AC201F9412017^7' +'AC201FA412017^7' +'AC201FB412017^7' +'AC201FC412017^7' +'AC201FD412017^7' +'AC201FE412017^7' +'AC201FF412017^7' +'AC201ED412017^7' +'1^1' +'76^2' +END_ARRAY 2 829 +BEGIN_ARRAY 3 39 +'DE-0403LE-0403 ' +'AC200CC268059^7' +'AC201FED9F515^7' +'A' +'0' +'1' +'2' +39 +'ACA9F4^7' +'A8C^5' +'95D530B0708338^5' +'-954848CD8FCCC8^3' +'-1237A4B9E50726^2' +'27BC5CD97A7B14^0' +'-A008B2350BB548^-2' +'-D2B620BE6E8188^-3' +'1CCEE01A24443C^-3' +'-2DD8F01365A4FA^-4' +'36287C4B50D55A^-5' +'-1FE65DFD04A91B^-6' +'-6A58460956428^-7' +'36DF7F7552069^5' +'1C5529660F3CE4^4' +'-A946527ED81378^1' +'9A0E242217DF6^-1' +'16FE20CDC8E56B^-1' +'-1292E9468DA1ED^-2' +'BAEA14DDB07C4^-4' +'6342B3BBC0991C^-5' +'-2DB7DC8B183E78^-5' +'628F2A73E43B98^-6' +'-B29DC397F7128^-7' +'1327760ADD39C3^5' +'C31C168F8BEC^3' +'-42418DABAB8A8^1' +'E630651E16D2E^-2' +'BD018994D52C78^-2' +'-878B623FBBAAB^-3' +'35FD3ECDACEEC2^-4' +'81103383568628^-5' +'-1E099CC4A97B08^-5' +'38632AEF23BA6^-6' +'-544DDE19114234^-7' +'AC0134^7' +'1518^6' +'23^2' +'1^1' +END_ARRAY 3 39 +TOTAL_ARRAYS 3 + ~NAIF/SPC BEGIN COMMENTS~ +; ~/data/isistestdata/hayabusa/nirs/out/2392975548_lvl3_0.ale_1.bsp LOG FILE + +; Created 2023-05-05/16:06:10.00. +; +; BEGIN SPKMERGE COMMANDS + +LEAPSECONDS_KERNEL = ~/remotedata/isis_data/base/kernels/lsk/naif0012.tls + +SPK_KERNEL = ~/data/isistestdata/hayabusa/nirs/out/2392975548_lvl3_0.ale_1.bsp +SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/sb_25143_140.bsp + INCLUDE_COMMENTS = NO + BODIES = 2025143 + BEGIN_TIME = 2005 SEP 20 11:04:43.968 + END_TIME = 2005 SEP 20 11:09:50.669 +SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp + INCLUDE_COMMENTS = NO + BODIES = -130 + BEGIN_TIME = 2005 SEP 20 11:04:43.968 + END_TIME = 2005 SEP 20 11:09:50.669 +SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/de403s.bsp + INCLUDE_COMMENTS = NO + BODIES = 10 + BEGIN_TIME = 2005 SEP 20 11:04:43.968 + END_TIME = 2005 SEP 20 11:09:50.669 + +; END SPKMERGE COMMANDS + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl new file mode 100644 index 0000000..98b3250 --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl @@ -0,0 +1,401 @@ +Object = IsisCube + Object = Core + StartByte = 65537 + Format = Tile + TileSamples = 1 + TileLines = 1 + + Group = Dimensions + Samples = 1 + Lines = 1 + Bands = 64 + End_Group + + Group = Pixels + Type = Real + ByteOrder = Lsb + Base = 0.0 + Multiplier = 1.0 + End_Group + End_Object + + Group = Instrument + SpacecraftName = HAYABUSA + InstrumentId = NIRS + SpacecraftClockStartCount = 1/2392973413.133 + SpacecraftClockStopCount = 1/2392975548.000 + StartTime = 2005-09-20T11:06:43 + StopTime = 2005-09-20T11:07:50 + TotalIntegrationTime = 13.10720 <SECOND> + IntegrationTime = 25.6 <msec> + TargetName = ITOKAWA + End_Group + + Group = Archive + Pixel0Wavelength = 787.16 <nm> + WavelengthInterval = 23.56 <nm> + StackingEndTime = 2392975548 <decimal> + SWHistMode = Pixel + SWLIDARMode = Normal + SWFLashMode = Normal + SWRawMode = STACK + SWDeviationOutput = ON + SWMinMaxOutput = ON + HWPower = ON + HWChopper = ON + HWChopperMode = CHOP + HWTEC = ON + HWTECModeV = "CLOSE:-9.5 deg" <V> + HWTECModeC = -9.5 <C> + HWLamp = OFF + HWLED = OFF + DarkCurrentSubtraction = YES + YearDoy = 2005263 + End_Group + + Group = BandBin + Width = 0.02356 <micrometers> + Unit = Micrometers + FilterNumber = (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) + Center = (0.7636, 0.78716, 0.81072, 0.83428, 0.85784, 0.8814, + 0.90496, 0.92852, 0.95208, 0.97564, 0.9992, 1.02276, + 1.04632, 1.06988, 1.09344, 1.117, 1.14056, 1.16412, + 1.18768, 1.21124, 1.2348, 1.25836, 1.28192, 1.30548, + 1.32904, 1.3526, 1.37616, 1.39972, 1.42328, 1.44684, + 1.4704, 1.49396, 1.51752, 1.54108, 1.56464, 1.5882, + 1.61176, 1.63532, 1.65888, 1.68244, 1.706, 1.72956, + 1.75312, 1.77668, 1.80024, 1.8238, 1.84736, 1.87092, + 1.89448, 1.91804, 1.9416, 1.96516, 1.98872, 2.01228, + 2.03584, 2.0594, 2.08296, 2.10652, 2.13008, 2.15364, + 2.1772, 2.20076, 2.22432, 2.24788) + End_Group + + Group = Kernels + NaifFrameCode = -130200 + LeapSecond = $base/kernels/lsk/naif0012.tls + TargetAttitudeShape = ($base/kernels/pck/pck00009.tpc, + $hayabusa/kernels/pck/itokawa_gaskell_n3.tpc) + TargetPosition = (Table, $hayabusa/kernels/tspk/de403s.bsp, + $hayabusa/kernels/tspk/sb_25143_140.bsp) + InstrumentPointing = (Table, + $hayabusa/kernels/ck/hayabusa_itokawarendezvo- + us_v02n.bc, + $hayabusa/kernels/fk/hayabusa_hp.tf, + $hayabusa/kernels/fk/itokawa_fixed.tf) + Instrument = $hayabusa/kernels/ik/nirs10.ti + SpacecraftClock = $hayabusa/kernels/sclk/hayabusa.tsc + InstrumentPosition = (Table, + $hayabusa/kernels/spk/hay_osbj_050911_051118_- + v1n.bsp) + InstrumentAddendum = $hayabusa/kernels/iak/nirsAddendum002.ti + ShapeModel = Null + InstrumentPositionQuality = Reconstructed + InstrumentPointingQuality = Reconstructed + CameraVersion = 1 + Source = isis + End_Group + + Group = MissionData + PhaseAngle = 8.38 <DEGREE> + IncidenceAngle = 59.38 <DEGREE> + EmissionAngle = 60.91 <DEGREE> + CenterLatitude = 36.23 <DEGREE> + CenterLongitude = 345.79 <DEGREE> + CornersLatitude = (N/A, 29.62 <DEGREE>, 30.33 <DEGREE>, N/A) + CornersLongitude = (N/A, 346.92 <DEGREE>, 336.00 <DEGREE>, N/A) + End_Group +End_Object + +Object = Label + Bytes = 65536 +End_Object + +Object = Table + Name = InstrumentPointing + StartByte = 72978 + Bytes = 64 + Records = 1 + ByteOrder = Lsb + TimeDependentFrames = (-130000, 1) + ConstantFrames = (-130200, -130201, -130000) + ConstantRotation = (4.16716354675321e-08, 0.99999999978068, + 2.09439095658742e-05, 0.99999802059666, + 6.12322187538694e-17, -0.0019896740344835, + -0.0019896740340471, 2.09439510224007e-05, + -0.99999802037734) + CkTableStartTime = 180486501.50057 + CkTableEndTime = 180486501.50057 + CkTableOriginalSize = 1 + FrameTypeCode = 3 + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/ck/hayabusa_itokawarendezvous_v02n- + .bc, $hayabusa/kernels/fk/hayabusa_hp.tf, + $hayabusa/kernels/fk/itokawa_fixed.tf) + + Group = Field + Name = J2000Q0 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = Table + Name = InstrumentPosition + StartByte = 73042 + Bytes = 56 + Records = 1 + ByteOrder = Lsb + CacheType = Linear + SpkTableStartTime = 180486501.50057 + SpkTableEndTime = 180486501.50057 + SpkTableOriginalSize = 1.0 + Description = "Created by spiceinit" + Kernels = $hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp + + Group = Field + Name = J2000X + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Y + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Z + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000XV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000YV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000ZV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = Table + Name = BodyRotation + StartByte = 73098 + Bytes = 64 + Records = 1 + ByteOrder = Lsb + TimeDependentFrames = (2025143, 1) + CkTableStartTime = 180486501.50057 + CkTableEndTime = 180486501.50057 + CkTableOriginalSize = 1 + FrameTypeCode = 2 + PoleRa = (90.02564, 0.0, 0.0) + PoleDec = (-67.02704, 0.0, 0.0) + PrimeMeridian = (129.73, 712.1437611, 0.0) + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/tspk/de403s.bsp, + $hayabusa/kernels/tspk/sb_25143_140.bsp, + $base/kernels/pck/pck00009.tpc, + $hayabusa/kernels/pck/itokawa_gaskell_n3.tpc) + SolarLongitude = 104.40427844844 + + Group = Field + Name = J2000Q0 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Q3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV1 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV2 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = AV3 + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = Table + Name = SunPosition + StartByte = 73162 + Bytes = 56 + Records = 1 + ByteOrder = Lsb + CacheType = Linear + SpkTableStartTime = 180486501.50057 + SpkTableEndTime = 180486501.50057 + SpkTableOriginalSize = 1.0 + Description = "Created by spiceinit" + Kernels = ($hayabusa/kernels/tspk/de403s.bsp, + $hayabusa/kernels/tspk/sb_25143_140.bsp) + + Group = Field + Name = J2000X + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Y + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000Z + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000XV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000YV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = J2000ZV + Type = Double + Size = 1 + End_Group + + Group = Field + Name = ET + Type = Double + Size = 1 + End_Group +End_Object + +Object = History + Name = IsisCube + StartByte = 73218 + Bytes = 1384 +End_Object + +Object = OriginalLabel + Name = IsisCube + StartByte = 66287 + Bytes = 6691 +End_Object + +Object = NaifKeywords + BODY_CODE = 2025143 + BODY2025143_RADII = (0.274, 0.156, 0.138) + BODY_FRAME_CODE = 2025143 + INS-130200_SWAP_OBSERVER_TARGET = TRUE + INS-130200_LIGHTTIME_CORRECTION = NONE + INS-130200_LT_SURFACE_CORRECT = FALSE + INS-130200_FOCAL_LENGTH = 0.0272 + INS-130200_PIXEL_PITCH = 0.047472922 + CLOCK_ET_-130_1/2392973413.133_COMPUTED = 0fe04c880284a541 + CLOCK_ET_-130_1/2392975548.000_COMPUTED = 1fb5b30d0384a541 + INS-130200_TRANSX = (0.0, 0.0, -0.047472922) + INS-130200_TRANSY = (0.0, 0.047472922, 0.0) + INS-130200_ITRANSS = (0.0, 0.0, 21.064639754005) + INS-130200_ITRANSL = (0.0, -21.064639754005, 0.0) + INS-130200_BORESIGHT_LINE = 0.0 + INS-130200_BORESIGHT_SAMPLE = 0.0 +End_Object +End diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc b/tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc new file mode 100755 index 0000000..6db182f --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc @@ -0,0 +1,3462 @@ +KPL/SCLK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "hayabusa.tsc" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = SCLK +PRODUCT_ID = "hayabusa.tsc" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:43 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = CLOCK_COEFFICIENTS + DESCRIPTION = "SPICE Spacecraft Clock Kernel (SCLK) file +containing clock correlation data for the Hayabusa on-board clock, created +by the Hayabusa Joint Science Team. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Hayabusa SCLK File +=========================================================================== + + This file is a SPICE spacecraft clock (SCLK) kernel containing the + data necessary to convert between Hayabusa spacecraft on-board clock + time and ephemeris time. + + +Production/History of this SCLK file +-------------------------------------------------------- + + This file was produced by Dr. Naru Hirata of the Hayabusa Joint + Science Team. + + Although the SCLK_KERNEL_ID provided in the data section of the file + is set to September 6, 2005, the set of data included in the file + suggests that the file was created on or shortly after November 28, + 2005. + + The comments were added to the file by Boris Semenov, NAIF/JPL on + September 22, 2009, during preparation of Hayabusa SPICE data for + formal archiving in PDS. When the comments were added to the file, + the original file name (hayabusa.tsc) was not changed because no + data in the file were modified. + + +Usage +-------------------------------------------------------- + + This file must be loaded into the user's program by a call to the + FURNSH subroutine in order to use the SPICELIB SCLK family of + subroutines to convert Hayabusa spacecraft on-board clock to ET and + vice versa. + + +SCLK Format +-------------------------------------------------------- + + The on-board clock, the conversion for which is provided by this + SCLK file, consists of two fields: + + MMMMMMMMMMM:FFF + + where: + + MMMMMMMMMMM -- count of major on-board clock ticks (131086 ... + 39062500000); the nominal duration of one major + on-board clock tick is approximately 1/32 of a + second + + FFF -- count of minor on-board clock ticks (0 ... 255); + the nominal duration of one minor on-board clock + tick is approximately 1/8192 of a second + + +Inquiries +-------------------------------------------------------- + + If you have any questions regarding this file contact + + Naru Hirata + naru@u-aizu.ac.jp + Department of Computer Software + The University of Aizu, Japan + + or + + Boris V. Semenov + (818) 354-8136 + Boris.Semenov@jpl.nasa.gov + + +Kernel Data +-------------------------------------------------------- + +\begintext + +DESCRIPTION =" + +This file contains the data necessary to convert between Hayabusa +spacecraft clock time and ephemeris time. " + + +\begindata + +SCLK_KERNEL_ID = ( @2005-09-06 ) + +SCLK_DATA_TYPE_130 = ( 1 ) +SCLK01_TIME_SYSTEM_130 = ( 1 ) +SCLK01_N_FIELDS_130 = ( 2 ) +SCLK01_MODULI_130 = ( 4294967296 256) +SCLK01_OFFSETS_130 = ( 0 0) +SCLK01_OUTPUT_DELIM_130 = ( 2 ) +SCLK_PARTITION_START_130 = ( 0.0000000000000E+00 ) +SCLK_PARTITION_END_130 = ( 1.0000000000000E+13 ) + +SCLK01_COEFFICIENTS_130 = ( + + 3.35581810000000e+07 1.05712107715935e+08 3.12498634281155e-02 + 6.71126130000000e+07 1.05716203698034e+08 3.12498779238695e-02 + 1.00667045000000e+08 1.05720299682034e+08 3.12498580876763e-02 + 1.34221477000000e+08 1.05724395663433e+08 3.12495364015456e-02 + 3.35548581000000e+08 1.05748971361343e+08 3.12490928669149e-02 + 3.69103013000000e+08 1.05753067242443e+08 3.12490227679518e-02 + 4.36211877000000e+08 1.05761258986268e+08 3.12489858340541e-02 + 4.69766309000000e+08 1.05765354853339e+08 3.12489689042947e-02 + 5.03328933000000e+08 1.05769451718158e+08 3.12490054922567e-02 + 5.36899749000000e+08 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6.57633402192000e+11 1.85983434358455e+08 3.12501471207235e-02 + 6.57700435573000e+11 1.85991617182745e+08 3.12492753077650e-02 + 6.58226259573000e+11 1.86055803194227e+08 3.12492793506543e-02 + 6.58237331061000e+11 1.86057154663061e+08 3.12492849752620e-02 + 6.58304509557000e+11 1.86065354975427e+08 3.12492753944304e-02 + 6.58934069109000e+11 1.86142203724714e+08 3.12492826401815e-02 + 6.58941937525000e+11 1.86143164202666e+08 3.12474973568453e-02 + 6.58975612240000e+11 1.86147274556447e+08 3.12509908827777e-02 + 6.59009049557000e+11 1.86151356389606e+08 3.12492801747339e-02 + 6.59042603989000e+11 1.86155452295257e+08 3.12492827458755e-02 + 6.59076158421000e+11 1.86159548201245e+08 3.12492867130914e-02 + 6.59109712853000e+11 1.86163644107753e+08 3.12492912601101e-02 + 6.59143267285000e+11 1.86167740014857e+08 3.12492134526939e-02 + 6.59680329040000e+11 1.86233297661026e+08 3.12502873000298e-02 + 6.59747336149000e+11 1.86241477314961e+08 3.12488838278250e-02 + 6.60385117504000e+11 1.86319328703516e+08 3.12491125359696e-02 + 6.60418635072000e+11 1.86323420087322e+08 3.12492306675267e-02 + 6.60452189504000e+11 1.86327515986484e+08 3.12492277380443e-02 + + +) +\begintext diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf b/tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf new file mode 100755 index 0000000..fd7d0fd --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf @@ -0,0 +1,392 @@ +KPL/FK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "hayabusa_hp.tf" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = FK +PRODUCT_ID = "hayabusa_hp.tf" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:41 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = FRAMES + DESCRIPTION = "SPICE Frames Kernel (FK) file containing +the definitions of the Hayabusa spacecraft frame and mission-specific +dynamic frames, created by the Hayabusa Joint Science Team. The original +name of this file was HAYABUSA_HP.TF. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Hayabusa Frames Definition Kernel +=========================================================================== + + This frame kernel contains a set of frame definitions for the + Hayabusa mission. It also contains NAIF name-ID mappings for + Hayabusa instruments. + + +Version and Date +--------------------------------------------------------------------------- + + Version 1.0 -- Sep. 22, 2009 -- Boris Semenov, NAIF/JPL. + + Lowercased file name (HAYABUSA_HP.TF -> hayabusa_hp.tf); + + Corrected spacecraft name to be consistent with the duplicate + definitions provided in IKs (HAYABUSA_SC_BUS -> + HAYABUSA_SC_BUS_PRIME); + + Added name-ID mapping keywords for science instruments; + + Added comments describing frames defined in the IK and + Itokawa FK; + + Added other miscellaneous comments. + + Version 1.0 -- Sep. 19, 2005 -- Naru Hirata, Aizu Univ. + + +Hayabusa NAIF IDs +--------------------------------------------------------------------------- + + The following names and NAIF ID codes are assigned to the Hayabusa + spacecraft, its structures, and science instruments: + + NAME NAIF ID + ----------------------------------------------- + HAYABUSA -130 + HAYABUSA_AMICA -130102 + HAYABUSA_NIRS -130200 + HAYABUSA_LIDAR -130300 + HAYABUSA_XRS -130400 + + The keywords below implement the Hayabusa name-ID mappings. + + \begindata + + NAIF_BODY_NAME += ( 'HAYABUSA' ) + NAIF_BODY_CODE += ( -130 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_AMICA' ) + NAIF_BODY_CODE += ( -130102 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_NIRS' ) + NAIF_BODY_CODE += ( -130200 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_LIDAR' ) + NAIF_BODY_CODE += ( -130300 ) + + NAIF_BODY_NAME += ( 'HAYABUSA_XRS' ) + NAIF_BODY_CODE += ( -130400 ) + + \begintext + + +Hayabusa Reference Frames +--------------------------------------------------------------------------- + + The following reference frames for Hayabusa spacecraft, its + structures, and science instruments are defined in this FK and other + Hayabusa kernels (Itokawa FK, PCKs, and IKs): + + + Itokawa body-fixed frame (defined in a separate FK and PCKs): + ------------------------------------------------------------- + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + ITOKAWA_FIXED J2000 PCK 2025143 + + + Hayabusa spacecraft frame (duplicated in the IKs): + ---------------------------------------------------- + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + HAYABUSA_SC_BUS_PRIME J2000 CK -130000 + + + Hayabusa Science instrument frames (defined in the instrument IK files): + ------------------------------------------------------------------------ + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + HAYABUSA_AMICA_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130101 + HAYABUSA_AMICA HAYABUSA_AMICA FIXED -130102 + + HAYABUSA_NIRS_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130201 + HAYABUSA_NIRS HAYABUSA_NIRS_IDEAL FIXED -130200 + + HAYABUSA_LIDAR_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130301 + HAYABUSA_LIDAR HAYABUSA_LIDAR_IDEAL FIXED -130300 + + HAYABUSA_XRS_IDEAL HAYABUSA_SC_BUS_PRIME FIXED -130410 + HAYABUSA_XRS HAYABUSA_XRS_IDEAL FIXED -130400 + + + Hayabusa-specific dynamic frames: + --------------------------------- + + Name Relative to Type Frame ID + ====================== ===================== ============ ======== + HAYABUSA_HP_FRAME J2000 DYNAMIC -130900 + ITOKAWA_-Z_SUN_+X J2000 DYNAMIC -130910 + EARTH_ITOKAWA_P J2000 DYNAMIC -130920 + + +Hayabusa Reference Frame Tree +--------------------------------------------------------------------------- + + + This diagram shows the Hayabusa frame tree: + + + "J2000" INERTIAL + +-----------------------------------------------------------+ + | | | | | + |<-dynamic | | | dynamic->| + | | | | | + V | | | V + "HAYABUSA_HP_FRAME" | | | "ITOKAWA_-Z_SUN_+X" + ------------------- | | | ------------------- + | | | + | | | + dynamic->| | |<-pck + | | | + V | V + "EARTH_ITOKAWA_P" | "ITOKAWA_FIXED" + ----------------- | --------------- + | + | + |<-ck + | + V + "HAYABUSA_SC_BUS_PRIME" + +-----------------------------------------------------------+ + | | | | + | |<-fixed | |<-fixed + | | | | + | V | V + | "HAYABUSA_NIRS_IDEAL" | "HAYABUSA_XRS_IDEAL" + | --------------------- | -------------------- + | | | | + | |<-fixed | |<-fixed + | | | | + | V | V + | "HAYABUSA_NIRS" | "HAYABUSA_XRS" + | --------------- | -------------- + | | + | | + |<-fixed |<-fixed + | | + V V + "HAYABUSA_AMICA_IDEAL" "HAYABUSA_LIDAR_IDEAL" + ---------------------- ---------------------- + | | + |<-fixed |<-fixed + | | + V V + "HAYABUSA_AMICA" "HAYABUSA_LIDAR" + ---------------- ---------------- + + +Itokawa Body-Fixed Frame +--------------------------------------------------------------------------- + + The Itokawa body-fixed frame, ITOKAWA_FIXED, is defined in a + separate FK file (itokawa_fixed.tf). Its definition is also + duplicated in some of the Itokawa PCK files. + + +Hayabusa Spacecraft Frame +--------------------------------------------------------------------------- + + The Hayabusa spacecraft frame, HAYABUSA_SC_BUS_PRIME, is defined + as follows: + + - +Z axis is parallel to the nominal HGA boresight; + + - +X axis is parallel to the ion engines thrust vector; + + - +Y axis completes the right-handed frame; + + The Hayabusa spacecraft frame shown on this diagram: + + ^ + | HGA Boresight + | + + ^ + / \ HGA + -------------------- + \ / + \ +Z / + -------- ^ --------- + | | | Ion Engines + | | |_ + | | +X |_] + | x-----> |_] -----> + _| +Y | Thrust Vector + NIRS | | | + ----| |---------------| |- + | | LIDAR XRS + | | + Sample | | | + horn | | | Science Instrument + / \ V Boresights + + + This frame is defined as a CK-based frame below. The frame + definition is also duplicated in Hayabusa science instrument IKs. + + \begindata + + FRAME_HAYABUSA_SC_BUS_PRIME = -130000 + FRAME_-130000_NAME = 'HAYABUSA_SC_BUS_PRIME' + FRAME_-130000_CLASS = 3 + FRAME_-130000_CLASS_ID = -130000 + FRAME_-130000_CENTER = -130 + CK_-130000_SCLK = -130 + CK_-130000_SPK = -130 + + \begintext + + +Hayabusa Science Instrument Frames +--------------------------------------------------------------------------- + + Hayabusa science instrument frames are defined in the IK files. + + +Hayabusa-Specific Dynamic Frames +--------------------------------------------------------------------------- + + The HAYABUSA_HP_FRAME frame, used as the reference frame in the + Hayabusa SPKs produces by JAXA, is defined as follows: + + - +Z axis is along the geometric direction from Itokawa to the + Earth + + - +X axis is as close as possible to the geometric direction + from Itokawa to the Sun + + - +Y axis completes the right-handed frame; + + This frame is defined as a two-vector style dynamic frame below. + + \begindata + + FRAME_HAYABUSA_HP = -130900 + FRAME_-130900_NAME = 'HAYABUSA_HP' + FRAME_-130900_CLASS = 5 + FRAME_-130900_CLASS_ID = -130900 + FRAME_-130900_CENTER = 2025143 + FRAME_-130900_RELATIVE = 'J2000' + FRAME_-130900_DEF_STYLE = 'PARAMETERIZED' + FRAME_-130900_FAMILY = 'TWO-VECTOR' + FRAME_-130900_PRI_AXIS = 'Z' + FRAME_-130900_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130900_PRI_OBSERVER = 2025143 + FRAME_-130900_PRI_TARGET = 'EARTH' + FRAME_-130900_PRI_ABCORR = 'NONE' + FRAME_-130900_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130900_SEC_OBSERVER = 2025143 + FRAME_-130900_SEC_TARGET = 'SUN' + FRAME_-130900_SEC_AXIS = 'X' + FRAME_-130900_SEC_ABCORR = 'NONE' + + \begintext + + + The ITOKAWA_-Z_SUN_+X frame, representing the nominal Itokawa-pointed + orientation, is defined as follows: + + - -Z axis is along the geometric direction from Hayabusa to + Itokawa + + - +X axis is as close as possible to the geometric direction from + Hayabusa to the Sun + + - +Y axis completes the right-handed frame; + + This frame is defined as a two-vector style dynamic frame below. + + \begindata + + FRAME_ITOKAWA_-Z_SUN_+X = -130910 + FRAME_-130910_NAME = 'ITOKAWA_-Z_SUN_+X' + FRAME_-130910_CLASS = 5 + FRAME_-130910_CLASS_ID = -130910 + FRAME_-130910_CENTER = -130 + FRAME_-130910_RELATIVE = 'J2000' + FRAME_-130910_DEF_STYLE = 'PARAMETERIZED' + FRAME_-130910_FAMILY = 'TWO-VECTOR' + FRAME_-130910_PRI_AXIS = '-Z' + FRAME_-130910_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130910_PRI_OBSERVER = -130 + FRAME_-130910_PRI_TARGET = 2025143 + FRAME_-130910_PRI_ABCORR = 'NONE' + FRAME_-130910_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130910_SEC_OBSERVER = -130 + FRAME_-130910_SEC_TARGET = 'SUN' + FRAME_-130910_SEC_AXIS = 'X' + FRAME_-130910_SEC_ABCORR = 'NONE' + + \begintext + + + The EARTH_ITOKAWA_P frame is defined as follows: + + - +Z axis is along the geometric direction from the Earth to + Itokawa + + - +Y axis is as close as possible to the geometric direction from + the Earth to the Sun + + - +X axis completes the right-handed frame; + + This frame is defined as a two-vector style dynamic frame below. + + \begindata + + FRAME_EARTH_ITOKAWA_P = -130920 + FRAME_-130920_NAME = 'EARTH_ITOKAWA_P' + FRAME_-130920_CLASS = 5 + FRAME_-130920_CLASS_ID = -130920 + FRAME_-130920_CENTER = 399 + FRAME_-130920_RELATIVE = 'J2000' + FRAME_-130920_DEF_STYLE = 'PARAMETERIZED' + FRAME_-130920_FAMILY = 'TWO-VECTOR' + FRAME_-130920_PRI_AXIS = 'Z' + FRAME_-130920_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130920_PRI_OBSERVER = 'EARTH' + FRAME_-130920_PRI_TARGET = 2025143 + FRAME_-130920_PRI_ABCORR = 'NONE' + FRAME_-130920_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' + FRAME_-130920_SEC_OBSERVER = 'EARTH' + FRAME_-130920_SEC_TARGET = 'SUN' + FRAME_-130920_SEC_AXIS = 'Y' + FRAME_-130920_SEC_ABCORR = 'NONE' + + \begintext + + +End of FK file. diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc new file mode 100644 index 0000000..f7b2965 --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc @@ -0,0 +1,56 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/CK ' +'2' +'6' +'HAYABUSA S/C ATTITUDE ' +BEGIN_ARRAY 1 35 +'HAYABUSA S/C ATTITUDE ' +'8EA18B4B85^A' +'8EA1B1D732^A' +'-1FBD0' +'1' +'3' +'1' +35 +'8BA142187DFB4^0' +'5094EC77B2BA54^0' +'-AB9C9B9D0EA3D8^0' +'6479EC1B2DCAB^0' +'11D7870BA38^-6' +'1B604FE2ADC806^-4' +'F53927DE6EB42^-5' +'8B9DA3138E081^0' +'509AF6BDB14E44^0' +'-AB9C01A71924B^0' +'647B22F732861C^0' +'66F5C84D53E6B4^-4' +'33935D6FF25D32^-4' +'1F60D50AAF5E1B^-4' +'8BA02C68AAAB6^0' +'50973E4BF26B14^0' +'-ABAAAAA97514B^0' +'64618AAA220764^0' +'4F6BBFBB42D5C4^-4' +'-3E92B2B1C6FD12^-4' +'-1ED85C91CE00A7^-4' +'8BA8B732ACDAD8^0' +'508974F1A13A98^0' +'-ABABB657142FC8^0' +'645EEF5A4874DC^0' +'-151CBD15BAEFC9^-4' +'-3F7E9F1B8893BC^-4' +'-24B1A7A465C88A^-4' +'8EA18B4B85^A' +'8EA197E001AF28^A' +'8EA1A7E0035DF^A' +'8EA1B1D732^A' +'8EA18B4B85^A' +'1^1' +'4^1' +END_ARRAY 1 35 +TOTAL_ARRAYS 1 + ~NAIF/SPC BEGIN COMMENTS~ +This CK is for testing with the image: ~/data/isistestdata/hayabusa/nirs/2392975548_lvl3_0.ale.cub + +This CK was generated using the following command: {} + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc new file mode 100644 index 0000000..3a581b1 --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc @@ -0,0 +1,120 @@ +DAFETF NAIF DAF ENCODED TRANSFER FILE +'DAF/CK ' +'2' +'6' +'HAYABUSA S/C ATTITUDE ' +BEGIN_ARRAY 1 99 +'HAYABUSA S/C ATTITUDE ' +'8EA1D1656C^A' +'8EA1F7BC19^A' +'-1FBD0' +'1' +'3' +'1' +99 +'8BAC935814D8A8^0' +'5083C19F10C4E^0' +'-AB9E2D3CF59A9^0' +'64754652318348^0' +'-9682518AF744A8^-5' +'1FA58BF555BE56^-4' +'1CA5922433E4AA^-4' +'8BAB729B6C3BF^0' +'5086CFBE811EC8^0' +'-AB9DCCB188C75^0' +'647509CCA04A54^0' +'-249F661FA151D2^-5' +'28EC3E88292384^-4' +'23AEDC32845414^-4' +'8BA7E8BFD965B8^0' +'50911E306560F^0' +'-ABA0598369693^0' +'646D561A806F1C^0' +'-15E52076AD6803^-4' +'3FBED909FDDE9A^-4' +'-3B6800C64BEC82^-4' +'8BA64D60463B6^0' +'50910DF79ABDC8^0' +'-ABA156AA12E5D^0' +'646DEE89199C58^0' +'66F4F4D09DC0F8^-4' +'5A4BBC498F306^-4' +'5B5CDE8EEE152C^-4' +'8BA68AFF460A78^0' +'50925206F19E^0' +'-ABA33DC0838DD^0' +'64695455D4BF1^0' +'-E132E669A2DA7^-5' +'4207DF589FEF88^-4' +'813F19E633FFB8^-5' +'8BA51EBBBBF1A^0' +'509389F8880D58^0' +'-ABA41D67C91B4^0' +'6468D650F743F^0' +'9761139106E4D8^-5' +'-73FB6A0E0D1274^-4' +'108421FC1634FC^-5' +'8BA7A7E26CF068^0' +'5091FA488DE668^0' +'-ABA23E575AEEC8^0' +'6469C31902D0A4^0' +'-F5CB1F11A2E76^-5' +'-134F53B558F9C3^-5' +'-2CC181B83629D2^-4' +'8BA6FB3F420298^0' +'5091497FB7B408^0' +'-ABA2798CCE0058^0' +'646ADBD63FB24^0' +'7B7B4881DF1D04^-5' +'103F021EBD174D^-4' +'5DF0B9C5582628^-4' +'8BA7DE51E6F11^0' +'509352A691378C^0' +'-ABA1EC23CDAC2^0' +'6468EF9081B74C^0' +'15E7BFA42574B6^-4' +'23DD3D29177CF8^-4' +'-71C6105E09417C^-5' +'8BA73ED07779C8^0' +'50933D7267763^0' +'-ABA2DF4832353^0' +'64683ED01A11C8^0' +'-2CDED1E10D9A12^-4' +'-2D1AD488D940EE^-4' +'-3248A2CC68A8D8^-4' +'8BA721F95B5FE^0' +'50926608EAE174^0' +'-ABA20C403C6FB^0' +'646A7C7ED86E08^0' +'C5AFA258A01D68^-4' +'-35A9145D304ACC^-4' +'-301C6E8ED5983E^-5' +'8BA7D06FB55D68^0' +'50917A9F782478^0' +'-ABA264C1149D78^0' +'6469AF78A4404^0' +'286EBE0B14597A^-4' +'-EB91DC08E5A418^-5' +'132100BC924F5B^-4' +'8EA1D1656C^A' +'8EA1D7E00038F^A' +'8EA1E7E001E7B^A' +'8EA1E949022BD^A' +'8EA1EB48FD42F^A' +'8EA1ED49008B4^A' +'8EA1EF4903D388^A' +'8EA1F148FEEAA8^A' +'8EA1F3490232F8^A' +'8EA1F548FD4A08^A' +'8EA1F74900925^A' +'8EA1F7BC19^A' +'8EA1D1656C^A' +'1^1' +'C^1' +END_ARRAY 1 99 +TOTAL_ARRAYS 1 + ~NAIF/SPC BEGIN COMMENTS~ +This CK is for testing with the image: ~/data/isistestdata/hayabusa/nirs/2392975548_lvl3_0.ale.cub + +This CK was generated using the following command: {} + ~NAIF/SPC END COMMENTS~ diff --git a/tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf b/tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf new file mode 100755 index 0000000..1a6630f --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf @@ -0,0 +1,94 @@ +KPL/FK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "itokawa_fixed.tf" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = FK +PRODUCT_ID = "itokawa_fixed.tf" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:41 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = FRAMES + DESCRIPTION = "SPICE Frames Kernel (FK) file containing +the definition of the asteroid Itokawa body-fixed frame, created by the +Hayabusa Joint Science Team. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +ITOKAWA Body-Fixed Frame Definition Kernel +=========================================================================== + + This frame kernel contains asteroid ITOKAWA body-fixed frame definition. + + +Version and Date +-------------------------------------------------------- + + Version 1.0 -- May 25, 2004 -- Naru Hirata + + Initial release. + + +Implementation Notes +-------------------------------------------------------- + + This file is used by the SPICE system as follows: programs that make + use of this frame kernel must `load' the kernel, normally during program + initialization. Loading the kernel associates data items with their + names in a data structure called the `kernel pool'. The SPICELIB + routine FURNSH loads a kernel file into the pool as shown below. + + CALL FURNSH ( frame_kernel_name ) + + This file was created and may be updated with a text editor or word + processor. + + +ITOKAWA Body-Fixed Frame +-------------------------------------------------------- + + This kernel file defines asteroid ITOKAWA body-frame, ITOKAWA_FIXED, with + the frame ID code 2025143 in the same as any other PCK frame: + + * +Z along asteroid's North pole; + + * +X along asteroid's prime meridian; + + * +Y complements to the right hand frame; + + * the origin of this frame is at the center of the asteroid ellipsoid. + + As for any PCK frame orientation of this frame is computed by evaluating + corresponding rotation constants provided in a PCK file. + + \begindata + + FRAME_ITOKAWA_FIXED = 2025143 + FRAME_2025143_NAME = 'ITOKAWA_FIXED' + FRAME_2025143_CLASS = 2 + FRAME_2025143_CLASS_ID = 2025143 + FRAME_2025143_CENTER = 2025143 + + OBJECT_2025143_FRAME = 'ITOKAWA_FIXED' + + \begintext + diff --git a/tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc b/tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc new file mode 100755 index 0000000..e8abb4d --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc @@ -0,0 +1,115 @@ +KPL/PCK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "itokawa_gaskell_n3.tpc" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = PCK +PRODUCT_ID = "itokawa_gaskell_n3.tpc" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:42 +PRODUCER_ID = "R.GASKELL/PSI" +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "N/A" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "N/A" +NAIF_INSTRUMENT_ID = "N/A" +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = TARGET_CONSTANTS + DESCRIPTION = "SPICE Planetary Constants Kernel (PCK) file +containing the asteroid Itokawa radii values, body-fixed frame definition, +and rotation constants derived by Dr. Robert W. Gaskell, PSI. The original +name of this files was Itokawa_Gaskell_n3.tpc. It contains the rotation +constants consistent with the Itokawa shape models archived in the PDS data +set HAY-A-AMICA-5-ITOKAWASHAPE-V1.0. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Asteroid Itokawa P_constants (PcK) SPICE kernel file +=========================================================================== + + By Hayabusa Joint Science Team, <unknown date>; miscellaneous comments + added by Boris Semenov, NAIF/JPL, on September 24, 2009. + + +Summary +-------------------------------------------------------- + + This PCK file contains Itokawa rotation constants, radii and + the definition of the Itokawa body-fixed frame, ITOKAWA_FIXED. + + The Itokawa rotation constants provided in this PCK are + from the data set catalog file for the Itokawa shape model + data set (HAY-A-AMICA-5-ITOKAWASHAPE-V1.0) by the Dr. Robert W. + Gaskell, PSI. + + +Rotation constants for asteroid Itokawa +-------------------------------------------------------- + + Itokawa rotation constants are provided in the keywords below. + + \begindata + + BODY2025143_POLE_RA = ( 90.02564 0.0 0.0 ) + BODY2025143_POLE_DEC = (-67.02704 0.0 0.0 ) + BODY2025143_PM = (129.73000 712.14376110 0.0 ) + + \begintext + + +Radii for asteroid ITOKAWA +-------------------------------------------------------- + + The Itokawa radii are provided in the keyword below. + + \begindata + + BODY2025143_RADII = ( 0.274 0.156 0.138 ) + + \begintext + + +ITOKAWA_FIXED Frame Definition +-------------------------------------------------------- + + The ITOKAWA fixed frame is defined in the same as any other PCK + frame: + + * +Z along the North pole; + + * +X toward the prime meridian; + + * +Y completes the right hand frame; + + * the origin of this frame is at the center of the body. + + The orientation of this frame is computed by evaluating + corresponding rotation constants provided in this PCK file. + + \begindata + + FRAME_ITOKAWA_FIXED = 2025143 + FRAME_2025143_NAME = 'ITOKAWA_FIXED' + FRAME_2025143_CLASS = 2 + FRAME_2025143_CLASS_ID = 2025143 + FRAME_2025143_CENTER = 2025143 + + OBJECT_2025143_FRAME = 'ITOKAWA_FIXED' + + \begintext + + +End of PCK file. diff --git a/tests/pytests/data/2392975548_lvl3_0/naif0012.tls b/tests/pytests/data/2392975548_lvl3_0/naif0012.tls new file mode 100755 index 0000000..e1afdee --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/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/2392975548_lvl3_0/nirs10.ti b/tests/pytests/data/2392975548_lvl3_0/nirs10.ti new file mode 100755 index 0000000..0bf1a61 --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/nirs10.ti @@ -0,0 +1,184 @@ +KPL/IK + +\beginlabel +PDS_VERSION_ID = PDS3 +RECORD_TYPE = STREAM +RECORD_BYTES = "N/A" +^SPICE_KERNEL = "nirs10.ti" +MISSION_NAME = HAYABUSA +SPACECRAFT_NAME = HAYABUSA +DATA_SET_ID = "HAY-A-SPICE-6-V1.0" +KERNEL_TYPE_ID = IK +PRODUCT_ID = "nirs10.ti" +PRODUCT_CREATION_TIME = 2009-11-30T13:50:42 +PRODUCER_ID = JAXA +MISSION_PHASE_NAME = "N/A" +PRODUCT_VERSION_TYPE = ACTUAL +PLATFORM_OR_MOUNTING_NAME = "HAYABUSA SPACECRAFT BUS" +START_TIME = "N/A" +STOP_TIME = "N/A" +SPACECRAFT_CLOCK_START_COUNT = "N/A" +SPACECRAFT_CLOCK_STOP_COUNT = "N/A" +TARGET_NAME = "25143 ITOKAWA" +INSTRUMENT_NAME = "NEAR INFRARED SPECTROMETER" +NAIF_INSTRUMENT_ID = -130200 +SOURCE_PRODUCT_ID = "N/A" +NOTE = "See comments in the file for details" +OBJECT = SPICE_KERNEL + INTERCHANGE_FORMAT = ASCII + KERNEL_TYPE = INSTRUMENT + DESCRIPTION = "SPICE I-Kernel (IK) file containing FOV and +reference frame definitions for the Hayabusa Near InfraRed Spectrometer +(NIRS) instrument, created by the Hayabusa Joint Science Team. " +END_OBJECT = SPICE_KERNEL +\endlabel + + +Hayabusa NIRS Instrument and Frame Kernel Kile +=========================================================================== + + This instrument kernel (I-kernel) contains the frames and FOV + definitions for Hayabusa Near-Infrared Spectrometer (NIRS). + + +Version and Date +--------------------------------------------------------------------------- + + Version 1.0 by Boris Semenov, NAIF/JPL 23 Sep. 2009 + + Corrected _RELATIVE frame in the _NIRS_IDEAL frame definition + (HAYABUSA_SC_BUS -> HAYABUSA_SC_BUS_PRIME). Added miscellaneous + comments. File name and version were not changed. + + Version 1.0 by Shinsuke Abe, Kobe Univ. 9 Sep. 2005 + + Version 0.0 (prototype) by Masanao Abe, ISAS/JAXA, 4 June 2005 + + +Implementation Notes +--------------------------------------------------------------------------- + + Applications that need SPICE I-kernel data must ``load'' the + I-kernel file, normally during program initialization. Loading the + kernel using the SPICELIB routine FURNSH causes the data items and + their associated values present in the kernel to become associated + with a data structure called the ``kernel pool''. The application + program may then obtain the value(s) for any IK data item using the + SPICELIB routines GDPOOL, GIPOOL, GCPOOL. Routine GETFOV may be used + if the file contains instrument field-of-view (FOV) specification. + The frame definitions information is accessed via any interfaces + utilizing SPICE frames subsystem (PXFORM, etc). + + This file was created with, and can be updated with a text editor or + word processor. + + +Conventions for Specifying Data +--------------------------------------------------------------------------- + + Instrument data items are specified using ``keyword=value'' + assignments. All keywords referencing instrument values in this + I-kernel start with the characters `INS' followed by the NAIF + instrument ID code for NIRS, -130200. The remainder of the keyword + is an underscore character followed by the unique name of the data + item. For example, NIRS boresight vector is specified by + + INS-130200_BORESIGHT + + The upper bound on the length of all keywords is 32 characters. + + +Hayabusa Spacecraft Frame Definition +--------------------------------------------------------------------------- + + This HAYABUSA_SC_BUS_PRIME frame definition is a copy of the + definition provided in the main Hayabusa FK file. It is included in + this IK file for historical reasons. + +\begindata + + FRAME_HAYABUSA_SC_BUS_PRIME = -130000 + FRAME_-130000_NAME = 'HAYABUSA_SC_BUS_PRIME' + FRAME_-130000_CLASS = 3 + FRAME_-130000_CLASS_ID = -130000 + FRAME_-130000_CENTER = -130 + CK_-130000_SCLK = -130 + CK_-130000_SPK = -130 + +\begintext + + +NIRS Frame Definitions +--------------------------------------------------------------------------- + + Two frames are defined for NIRS: HAYABUSA_NIRS_IDEAL and + HAYABUSA_NIRS. + + The HAYABUSA_NIRS_IDEAL frame incorporates the ideal fixed + instrument alignment relative to the spacecraft frame, + HAYABUSA_SC_BUS_PRIME. The +Z axis of the HAYABUSA_NIRS_IDEAL frame + is along the ideally-mounted instrument boresight. + + The HAYABUSA_NIRS frame incorporates the the actual instrument + misalignment relative to its ideal orientation represented by the + HAYABUSA_NIRS_IDEAL frame. The +Z axis of this frame is along the + actual instrument boresight. + + Both frames are defined as fixed offset frames with their + orientation specified using Euler angles. + + Note that angles in the frame definitions are specified for "from + instrument to base (relative to) frame" transformation. + +\begindata + + FRAME_HAYABUSA_NIRS = -130200 + FRAME_-130200_NAME = 'HAYABUSA_NIRS' + FRAME_-130200_CLASS = 4 + FRAME_-130200_CLASS_ID = -130200 + FRAME_-130200_CENTER = -130 + TKFRAME_-130200_SPEC = 'ANGLES' + TKFRAME_-130200_RELATIVE = 'HAYABUSA_NIRS_IDEAL' + TKFRAME_-130200_ANGLES = ( -0.1140, -0.0012, 0.0 ) + TKFRAME_-130200_AXES = ( 1, 2, 3 ) + TKFRAME_-130200_UNITS = 'DEGREES' + + FRAME_HAYABUSA_NIRS_IDEAL = -130201 + FRAME_-130201_NAME = 'HAYABUSA_NIRS_IDEAL' + FRAME_-130201_CLASS = 4 + FRAME_-130201_CLASS_ID = -130201 + FRAME_-130201_CENTER = -130 + TKFRAME_-130201_SPEC = 'ANGLES' + TKFRAME_-130201_RELATIVE = 'HAYABUSA_SC_BUS_PRIME' + TKFRAME_-130201_ANGLES = ( 0.0, 180.0, -90.0 ) + TKFRAME_-130201_AXES = ( 1, 2, 3 ) + TKFRAME_-130201_UNITS = 'DEGREES' + +\begintext + + +NIRS Field-Of-View Definition +--------------------------------------------------------------------------- + + The NIRS FOV is defined using a corner-style definition as a 0.1 by + 0.1 degree square pyramid centered around the boresight that points + along the +Z axis of the HAYABUSA_NIRS frame. The FOV shape is set + to 'POLYGON'; it could also have been set to 'RECTANGLE'. The + corner direction vectors are given counterclockwise as seen from + boresight. + +\begindata + + INS-130200_FOV_FRAME = 'HAYABUSA_NIRS' + INS-130200_FOV_SHAPE = 'POLYGON' + INS-130200_BORESIGHT = ( 0.0 0.0 1.0 ) + INS-130200_FOV_BOUNDARY_CORNERS = ( + 0.000872664 0.000872664 1.0 + -0.000872664 0.000872664 1.0 + -0.000872664 -0.000872664 1.0 + 0.000872664 -0.000872664 1.0 + ) + +\begintext + +End of IK file. diff --git a/tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti b/tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti new file mode 100755 index 0000000..0426f06 --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti @@ -0,0 +1,34 @@ +\begintext +The focal length was calculated from f# = 1 and aperture = 27.2 mm +See: http://sbn.psi.edu/pds/asteroid/HAY_A_NIRS_3_NIRSCAL_V1_0/document/nirscalpaper.pdf +The units for focal length are meters and the units for pixel pitch are mm. + +\begindata + INS-130200_FOCAL_LENGTH = 0.0272 + + INS-130200_PIXEL_PITCH = 0.047472922 + INS-130200_BORESIGHT_SAMPLE = 0.0 + INS-130200_BORESIGHT_LINE = 0.0 + +\begintext + The NIRS orientientiation in ISIS camera model implemenation is + +Y = +SAMPLE, +X = -LINE, Z = +Z + + ITRANSS and ITRANSL were calculated using the camcoeffs application. + +\begindata + + INS-130200_TRANSX = (0.0, 0.0, -0.047472922) + INS-130200_TRANSY = (0.0, 0.047472922, 0.0) + INS-130200_ITRANSS = (0.0, 0.0, 21.064639754005) + INS-130200_ITRANSL = (0.0, -21.064639754005, 0.0) + +\begintext +NIRS is very close to Itokawa so light time correction +and target/observer perspective are set as follows. + +\begindata + +INS-130200_SWAP_OBSERVER_TARGET = 'TRUE' +INS-130200_LIGHTTIME_CORRECTION = 'NONE' +INS-130200_LT_SURFACE_CORRECT = 'FALSE' diff --git a/tests/pytests/data/2392975548_lvl3_0/pck00009.tpc b/tests/pytests/data/2392975548_lvl3_0/pck00009.tpc new file mode 100755 index 0000000..bfadaab --- /dev/null +++ b/tests/pytests/data/2392975548_lvl3_0/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/hayabusanirs_isd.json b/tests/pytests/data/isds/hayabusanirs_isd.json new file mode 100644 index 0000000..2d80c5f --- /dev/null +++ b/tests/pytests/data/isds/hayabusanirs_isd.json @@ -0,0 +1,260 @@ +{ + "isis_camera_version": 1, + "image_lines": 1, + "image_samples": 1, + "name_platform": "HAYABUSA", + "name_sensor": "HAYABUSA_NIRS", + "reference_height": { + "maxheight": 1000, + "minheight": -1000, + "unit": "m" + }, + "name_model": "USGS_ASTRO_FRAME_SENSOR_MODEL", + "center_ephemeris_time": 180486501.50056908, + "radii": { + "semimajor": 0.274, + "semiminor": 0.138, + "unit": "km" + }, + "body_rotation": { + "time_dependent_frames": [ + 2025143, + 1 + ], + "ck_table_start_time": 180486501.50056908, + "ck_table_end_time": 180486501.50056908, + "ck_table_original_size": 1, + "ephemeris_times": [ + 180486501.50056908 + ], + "quaternions": [ + [ + -0.16055829299369445, + -0.7903828492935261, + 0.57934404912348, + 0.11779838215701044 + ] + ], + "angular_velocities": [ + [ + -2.512589340257489e-08, + 5.614694041984393e-05, + -0.00013244767067246738 + ] + ], + "reference_frame": 1 + }, + "instrument_pointing": { + "time_dependent_frames": [ + -130000, + 1 + ], + "ck_table_start_time": 180486501.50056908, + "ck_table_end_time": 180486501.50056908, + "ck_table_original_size": 1, + "ephemeris_times": [ + 180486501.50056908 + ], + "quaternions": [ + [ + -0.5455420110134627, + -0.314681795394347, + 0.6704074453706204, + -0.3923176507097482 + ] + ], + "angular_velocities": [ + [ + -1.0633204332538909e-06, + 3.518145848279672e-06, + -2.36852765977406e-06 + ] + ], + "reference_frame": 1, + "constant_frames": [ + -130200, + -130201, + -130000 + ], + "constant_rotation": [ + 4.167163544668958e-08, + 0.9999999997806756, + 2.0943909565874054e-05, + 0.9999980205966593, + 8.20744220945079e-17, + -0.0019896740344834754, + -0.001989674034047091, + 2.0943951022400417e-05, + -0.9999980203773353 + ] + }, + "naif_keywords": { + "BODY2025143_RADII": [ + 0.274, + 0.156, + 0.138 + ], + "BODY_FRAME_CODE": 2025143, + "BODY_CODE": 2025143, + "INS-130200_SWAP_OBSERVER_TARGET": "TRUE", + "FRAME_-130200_CLASS": 4.0, + "INS-130200_LT_SURFACE_CORRECT": "FALSE", + "INS-130200_LIGHTTIME_CORRECTION": "NONE", + "INS-130200_FOV_BOUNDARY_CORNERS": [ + 0.000872664, + 0.000872664, + 1.0, + -0.000872664, + 0.000872664, + 1.0, + -0.000872664, + -0.000872664, + 1.0, + 0.000872664 + ], + "INS-130200_BORESIGHT_SAMPLE": 0.0, + "INS-130200_ITRANSL": [ + 0.0, + -21.064639754005, + 0.0 + ], + "INS-130200_ITRANSS": [ + 0.0, + 0.0, + 21.064639754005 + ], + "TKFRAME_-130200_RELATIVE": "HAYABUSA_NIRS_IDEAL", + "TKFRAME_-130200_UNITS": "DEGREES", + "FRAME_-130200_CLASS_ID": -130200.0, + "INS-130200_TRANSX": [ + 0.0, + 0.0, + -0.047472922 + ], + "INS-130200_TRANSY": [ + 0.0, + 0.047472922, + 0.0 + ], + "INS-130200_PIXEL_PITCH": 0.047472922, + "INS-130200_BORESIGHT": [ + 0.0, + 0.0, + 1.0 + ], + "TKFRAME_-130200_ANGLES": [ + -0.114, + -0.0012, + 0.0 + ], + "FRAME_-130200_CENTER": -130.0, + "INS-130200_FOV_SHAPE": "POLYGON", + "INS-130200_FOCAL_LENGTH": 0.0272, + "TKFRAME_-130200_AXES": [ + 1.0, + 2.0, + 3.0 + ], + "TKFRAME_-130200_SPEC": "ANGLES", + "FRAME_-130200_NAME": "HAYABUSA_NIRS", + "INS-130200_FOV_FRAME": "HAYABUSA_NIRS", + "INS-130200_BORESIGHT_LINE": 0.0, + "OBJECT_2025143_FRAME": "ITOKAWA_FIXED", + "FRAME_2025143_CLASS": 2.0, + "BODY2025143_PM": [ + 129.73, + 712.1437611, + 0.0 + ], + "BODY2025143_POLE_RA": [ + 90.02564, + 0.0, + 0.0 + ], + "FRAME_2025143_CLASS_ID": 2025143.0, + "BODY2025143_POLE_DEC": [ + -67.02704, + 0.0, + 0.0 + ], + "FRAME_2025143_CENTER": 2025143.0, + "BODY2025143_LONG_AXIS": 0.0, + "FRAME_2025143_NAME": "ITOKAWA_FIXED" + }, + "detector_sample_summing": 1, + "detector_line_summing": 1, + "focal_length_model": { + "focal_length": 0.0272 + }, + "detector_center": { + "line": 0.0, + "sample": 0.0 + }, + "focal2pixel_lines": [ + 0.0, + -21.064639754005, + 0.0 + ], + "focal2pixel_samples": [ + 0.0, + 0.0, + 21.064639754005 + ], + "optical_distortion": { + "radial": { + "coefficients": [ + 0.0, + 0.0, + 0.0 + ] + } + }, + "starting_detector_line": 0, + "starting_detector_sample": 0, + "instrument_position": { + "spk_table_start_time": 180486501.50056908, + "spk_table_end_time": 180486501.50056908, + "spk_table_original_size": 1, + "ephemeris_times": [ + 180486501.50056908 + ], + "positions": [ + [ + 16.755715427571857, + -3.217421876546119, + -1.8170226741623652 + ] + ], + "velocities": [ + [ + 2.1028869650818293e-05, + -3.528483828922901e-07, + -4.334941153621985e-07 + ] + ], + "reference_frame": 1 + }, + "sun_position": { + "spk_table_start_time": 180486501.50056908, + "spk_table_end_time": 180486501.50056908, + "spk_table_original_size": 1, + "ephemeris_times": [ + 180486501.50056908 + ], + "positions": [ + [ + 157546274.8360496, + -51773929.736718364, + -27634141.47982414 + ] + ], + "velocities": [ + [ + 3.4484780727773905, + 27.389486836276948, + 12.105185350948945 + ] + ], + "reference_frame": 1 + } +} \ No newline at end of file diff --git a/tests/pytests/test_hayabusa_drivers.py b/tests/pytests/test_hayabusa_drivers.py index 2da7df8..f36384c 100644 --- a/tests/pytests/test_hayabusa_drivers.py +++ b/tests/pytests/test_hayabusa_drivers.py @@ -8,10 +8,11 @@ import json from conftest import get_image, get_image_label, get_isd, get_image_kernels, convert_kernels, compare_dicts import ale -from ale.drivers.hayabusa_drivers import HayabusaAmicaIsisLabelNaifSpiceDriver +from ale.drivers.hayabusa_drivers import HayabusaAmicaIsisLabelNaifSpiceDriver, HayabusaNirsIsisLabelNaifSpiceDriver from ale import util +# AMICA Tests @pytest.fixture(scope='module') def test_amica_kernels(): kernels = get_image_kernels('st_2458542208_v') @@ -29,7 +30,7 @@ def test_amica_load(test_amica_kernels): assert compare_dicts(isd_obj, compare_dict) == [] -class test_nac_isis_naif(unittest.TestCase): +class test_amica_isis_naif(unittest.TestCase): def setUp(self): label = get_image_label("st_2458542208_v", "isis") self.driver = HayabusaAmicaIsisLabelNaifSpiceDriver(label) @@ -42,3 +43,46 @@ class test_nac_isis_naif(unittest.TestCase): def test_sensor_name(self): assert self.driver.sensor_name == "HAYABUSA_AMICA" + + +# NIRS Tests +@pytest.fixture(scope='module') +def test_nirs_kernels(): + kernels = get_image_kernels('2392975548_lvl3_0') + updated_kernels, binary_kernels = convert_kernels(kernels) + yield updated_kernels + for kern in binary_kernels: + os.remove(kern) + +def test_nirs_load(test_nirs_kernels): + label_file = get_image_label('2392975548_lvl3_0', 'isis') + compare_dict = get_isd("hayabusanirs") + + isd_str = ale.loads(label_file, props={'kernels': test_nirs_kernels}, verbose=True) + isd_obj = json.loads(isd_str) + assert compare_dicts(isd_obj, compare_dict) == [] + + +class test_nirs_isis_naif(unittest.TestCase): + def setUp(self): + label = get_image_label("2392975548_lvl3_0", "isis") + self.driver = HayabusaNirsIsisLabelNaifSpiceDriver(label) + + def test_instrument_id(self): + assert self.driver.instrument_id == "HAYABUSA_NIRS" + + def test_sensor_model_version(self): + assert self.driver.sensor_model_version == 1 + + def test_sensor_name(self): + assert self.driver.sensor_name == "HAYABUSA_NIRS" + + def test_exposure_duration(self): + with patch('ale.drivers.hayabusa_drivers.spice.scs2e', return_value=12345) as scs2e: + assert self.driver.exposure_duration == 0 + scs2e.assert_called_with(-130, '1/2392973413.133') + + def test_ephemeris_stop_time(self): + with patch('ale.drivers.hayabusa_drivers.spice.scs2e', return_value=12345) as scs2e: + assert self.driver.ephemeris_stop_time == 12345 + scs2e.assert_called_with(-130, '1/2392975548.000') -- GitLab