diff --git a/ale/drivers/juno_drivers.py b/ale/drivers/juno_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..b9bdaa889d609225ab69754f29c67ecbdacb295b
--- /dev/null
+++ b/ale/drivers/juno_drivers.py
@@ -0,0 +1,70 @@
+from ale import util
+from ale.base.data_naif import NaifSpice
+from ale.base.label_isis import IsisLabel
+from ale.base.type_sensor import Framer
+from ale.base.base import Driver
+
+class JunoJunoCamIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
+ """
+ Driver for reading Juno ISIS labels.
+ """
+
+ @property
+ def instrument_id(self):
+ """
+ Expects instrument_id to be defined in the IsisLabel mixin. This should be
+ a string of the form 'JNC'
+
+ Returns
+ -------
+ : str
+ instrument id
+ """
+ look_up = {'JNC': 'JUNO_JUNOCAM'}
+ return look_up[super().instrument_id]
+
+ @property
+ def ephemeris_start_time(self):
+ """
+ Junos camera is split into stacked frames where an image is made
+ of sets of RGBM chuncks. We need to account for these chuncks since
+ ISIS produces some number of cubes N where N = M*4.
+ Computation obtained from JunoCamera.cpp
+
+ Returns
+ -------
+ : double
+ Starting ephemeris time
+ """
+ if not hasattr(self, '_ephemeris_start_time'):
+ initial_time = super().ephemeris_start_time
+ frame_number = self.label['IsisCube']['Instrument']['FrameNumber']
+ inter_frame_delay = self.label['IsisCube']['Instrument']['InterFrameDelay'].value
+ start_time_bias = self.naif_keywords[f'INS{self.ikid}_START_TIME_BIAS']
+ inter_frame_delay_bias = self.naif_keywords[f'INS{self.ikid}_INTERFRAME_DELTA']
+ self._ephemeris_start_time = initial_time + start_time_bias + (frame_number - 1) * (inter_frame_delay + inter_frame_delay_bias)
+ return self._ephemeris_start_time
+
+ @property
+ def sensor_model_version(self):
+ """
+ Returns
+ -------
+ : int
+ ISIS sensor model version
+ """
+ return 1
+
+ @property
+ def naif_keywords(self):
+ """
+ Updated set of naif keywords containing the NaifIkCode for the specific
+ Juno filter used when taking the image.
+
+ Returns
+ -------
+ : dict
+ Dictionary of keywords and values that ISIS creates and attaches to the label
+ """
+ filter_code = self.label['IsisCube']['BandBin']['NaifIkCode']
+ return {**super().naif_keywords, **util.query_kernel_pool(f"*{filter_code}*")}
diff --git a/ale/drivers/voyager_drivers.py b/ale/drivers/voyager_drivers.py
index f771c2f0fe99ddd3e6d7ca9a788d07145442c085..c1f9c267260feb7886adbe1ed9c5bcaccc45b65f 100644
--- a/ale/drivers/voyager_drivers.py
+++ b/ale/drivers/voyager_drivers.py
@@ -6,7 +6,7 @@ from ale.base.label_isis import IsisLabel
from ale.base.type_sensor import Framer
from ale.base.base import Driver
-class VoyagerCameraLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
+class VoyagerCameraIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
@property
def instrument_id(self):
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_METHANE_0008_0.xsp b/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_METHANE_0008_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..2da61649026e829180cdd6bb82b5b6637e33a1eb
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_METHANE_0008_0.xsp
@@ -0,0 +1,278 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 72
+'JUP310 '
+'1F535FF6DA8BB1^8'
+'1F536054A0B08D^8'
+'257'
+'5'
+'1'
+'3'
+72
+'1F53948^8'
+'A8C^4'
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+'E39378A1F2DAC^-1'
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+'-11539566F110A^1'
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+'-3EE1A3E021164^0'
+'23DA47B06C976C^0'
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+'-B205CE7E23EC^-2'
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+'261733FDD8E^-3'
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+'499B464726284^2'
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+END_ARRAY 1 72
+BEGIN_ARRAY 2 30
+'MONTE Chebyshev Polynomial Table '
+'1F535FF6DA8BB1^8'
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+END_ARRAY 2 30
+BEGIN_ARRAY 3 39
+'MONTE Chebyshev Polynomial Table '
+'1F535FF6DA8BB1^8'
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+END_ARRAY 3 39
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+'MONTE Difference Line Table '
+'1F535FF6DA8BB1^8'
+'1F536054A0B08D^8'
+'-3D'
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+'D2F0B4D7ECE7F^-C'
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+'4374037FFBD844^-8'
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+'-AA564069603068^-A'
+'-BAFA248BB75B9^-A'
+'-582CA1A80D100C^-A'
+'-2345B41781F44C^-A'
+'-D6DC4978F6263^-B'
+'-53E66^-B'
+'-154F7BD165DDB9^-2'
+'-1ACC4734DA3727^-3'
+'-2BC9B768C73CA4^-4'
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+'-25DEBA17B11F4E^-6'
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+'-199C749A4B0F96^-7'
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+'-60B3B31A8EBA84^-9'
+'-19C166B479E244^-9'
+'-71B0B4FCE3B628^-A'
+'-206337D3A1CC36^-A'
+'-9F672^-B'
+'F^1'
+'E^1'
+'E^1'
+'E^1'
+'1F536EC21F3951^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/acpaquette/kernel_split/JNCR_2016240_01M06152_V01_METHANE_0008_0.bsp LOG FILE
+
+; Created 2019-10-01/10:52:26.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/acpaquette/kernel_split/JNCR_2016240_01M06152_V01_METHANE_0008_0.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/juno/kernels/spk/juno_rec_160729_160923_161027.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -61, 5, 10, 599
+ BEGIN_TIME = 2016 AUG 27 08:14:42.671
+ END_TIME = 2016 AUG 27 08:16:16.445
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_METHANE_0008_1.xsp b/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_METHANE_0008_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..aa2df1db13f70ea495f3a9034fee108de63f7137
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_METHANE_0008_1.xsp
@@ -0,0 +1,278 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 72
+'JUP310 '
+'1F536A9606D561^8'
+'1F536AF1F25A8^8'
+'257'
+'5'
+'1'
+'3'
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+'1EC0D04DB56799^-A'
+'57E06855083BFC^-B'
+'D2F0B4D7ECE7F^-C'
+'B9D924A578259^-D'
+'-A9BC8^-D'
+'-5A8A5D1952EFCC^-D'
+'335C9C9846F04E^-2'
+'248CC525D95E5^-3'
+'29D84C328F65B^-4'
+'3F63B4F0C4D084^-5'
+'737A00AE850D54^-6'
+'ED0567D1470D3^-7'
+'2033230A8468E2^-7'
+'4374037FFBD844^-8'
+'65A7BEE7946A58^-9'
+'-AA564069603068^-A'
+'-BAFA248BB75B9^-A'
+'-582CA1A80D100C^-A'
+'-2345B41781F44C^-A'
+'-D6DC4978F6263^-B'
+'-53E66^-B'
+'-154F7BD165DDB9^-2'
+'-1ACC4734DA3727^-3'
+'-2BC9B768C73CA4^-4'
+'-595782F15F1194^-5'
+'-D8F49897058278^-6'
+'-25DEBA17B11F4E^-6'
+'-76AE1E201F2788^-7'
+'-199C749A4B0F96^-7'
+'-60117C26ECC9F8^-8'
+'-17970A02B32089^-8'
+'-60B3B31A8EBA84^-9'
+'-19C166B479E244^-9'
+'-71B0B4FCE3B628^-A'
+'-206337D3A1CC36^-A'
+'-9F672^-B'
+'F^1'
+'E^1'
+'E^1'
+'E^1'
+'1F536EC21F3951^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/acpaquette/kernel_split/JNCR_2016240_01M06152_V01_METHANE_0008_1.bsp LOG FILE
+
+; Created 2019-10-01/10:52:27.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/acpaquette/kernel_split/JNCR_2016240_01M06152_V01_METHANE_0008_1.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/juno/kernels/spk/juno_rec_160729_160923_161027.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -61, 5, 10, 599
+ BEGIN_TIME = 2016 AUG 27 09:00:01.844
+ END_TIME = 2016 AUG 27 09:01:33.764
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_isis3.lbl b/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..8874f31e2305631009582da8d2bf49f6666a45c2
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/JNCR_2016240_01M06152_V01_isis3.lbl
@@ -0,0 +1,76 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 824
+ TileLines = 128
+
+ Group = Dimensions
+ Samples = 1648
+ Lines = 128
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = SignedWord
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = JUNO
+ InstrumentHostId = UNKNOWN
+ InstrumentName = "JUNO EPO CAMERA"
+ InstrumentId = JNC
+ TargetName = JUPITER
+
+ # Start time for the entire observation, i.e. start time for FrameNumber 1.
+ StartTime = 2016-08-27T09:00:04.129
+
+ # Start count for the entire observation, i.e. start count for FrameNumber 1.
+ SpacecraftClockStartCount = 525560580:87
+ ExposureDuration = 204.800000 <ms>
+ InterFrameDelay = 0.378 <s>
+ SummingMode = 1
+ NumberFramelets = 12
+ FrameNumber = 8
+ End_Group
+
+ Group = Archive
+ MissionPhase = "SCIENCE ORBITS"
+ OrbitNumber = 1
+ FocalPlaneTemperature = 273.0 <K>
+ TDICount = 64
+ CompressionType = "INTEGER COSINE TRANSFORM"
+ YearDoy = 2016240
+ SourceProductId = JNCR_2016240_01M06152_V01
+ End_Group
+
+ Group = BandBin
+ FilterName = METHANE
+ NaifIkCode = -61504
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -61500
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 487425
+ Bytes = 533
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 487958
+ Bytes = 17903
+End_Object
+End
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/jno_sclkscet_00090.tsc b/tests/pytests/data/JNCR_2016240_01M06152_V01/jno_sclkscet_00090.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..2d8b2d3714109387d8a60debe6995d50a98d6f1a
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/jno_sclkscet_00090.tsc
@@ -0,0 +1,452 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "jno_sclkscet_00090.tsc"
+MISSION_NAME = JUNO
+SPACECRAFT_NAME = JUNO
+DATA_SET_ID = "JNO-J/E/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "jno_sclkscet_00090.tsc"
+PRODUCT_CREATION_TIME = 2019-09-04T10:44:03
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = JUPITER
+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 SCLK file containing time correlation
+data for the main JUNO on-board clock, created by NAIF, JPL. The original
+name of this file was JNO_SCLKSCET.00090.tsc. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+JUNO SCLK File, for ``Standard'' and ``High Precision'' SCLK Formats
+===========================================================================
+
+ This SCLK kernel contains correlation data for the JUNO on-board
+ clock tags presented either in ``standard'' or ``high precision''
+ format.
+
+ ``Standard'' JUNO on-board clock tags are derived from 5-byte tags
+ present in majority of the spacecraft and instrument telemetry and
+ utilizing only the last of the five bytes for fractional seconds.
+ This results in one SCLK tick being equal to 1/256 of a second.
+ The ID of this clock is -61, the same as of the JUNO spacecraft.
+
+ ``High precision'' JUNO on-board clock tags are derived from
+ 6-byte tags present in some of the spacecraft and instrument
+ telemetry and utilizing the last two of the six bytes for
+ fractional seconds. This results in one SCLK tick being equal to
+ 1/65536 of a seconds. The ID of this clock is -61999.
+
+ Although SCLK parameters for these two correlations are different,
+ having them in the same file and loading them at the same time
+ does not cause any conflicts in JUNO SPICE implementation. This is
+ because: 1) different IDs are used in the names of the keywords
+ used to store these parameters in this file, 2) different IDs must
+ be provided to get access to either of the two correlations, and
+ 3) a specific ID -- normally ID of the ``standard'' clock -- is
+ associated with each of the JUNO CK-based frames via definitions
+ in the JUNO Frames Kernel.
+
+
+Production/History of This SCLK File
+--------------------------------------------------------
+
+ The data in this file was generated by the NAIF utility program
+ MAKCLK, version 4.0.0, from the most recent JUNO spacecraft
+ SCLKvSCET file (see corresponding section of the description for
+ the SCLKvSCET contents and MAKCLK setup files).
+
+
+Usage
+--------------------------------------------------------
+
+ This file must be loaded into the user's program by a call to the
+ FURNSH subroutine
+
+ CALL FURNSH( 'this_file_name' )
+
+ in order to use the SPICELIB SCLK family of subroutines to convert
+ either ``standard'' or ``high precision'' JUNO spacecraft on-board
+ clock to ET and vice versa.
+
+
+SCLK Format
+--------------------------------------------------------
+
+ As mentioned above this SCLK kernel supports conversion of the
+ JUNO on-board clock either in ``standard'' or ``high precision''
+ format.
+
+ The JUNO on-board clock tags in ``standard'' format, to be
+ converted using ID -61, have the following form:
+
+ P/SSSSSSSSSS:FFF
+
+ where:
+
+ P/ -- optional partition identifier
+
+ SSSSSSSSSS -- count of on-board seconds
+
+ FFF -- count of fractions of a second with one
+ fraction being 1/256 of a second; normally this
+ field value is within 0..255 range.
+
+ The JUNO on-board clock tags in ``high precision'' format, to be
+ converted using ID -61999, have the following form:
+
+ P/SSSSSSSSSS:FFFFF
+
+ where:
+
+ P/ -- optional partition identifier
+
+ SSSSSSSSSS -- count of on-board seconds
+
+ FFFFF -- count of fractions of a second with one
+ fraction being 1/65536 of a second; normally
+ this field value is within 0..65535 range.
+
+
+References
+--------------------------------------------------------
+
+ 1. SCLK Required Reading Document
+
+ 2. MAKCLK User's Guide Document
+
+ 3. SFOC SCLKvSCET SIS Document
+
+
+Inquiries
+--------------------------------------------------------
+
+ If you have any questions regarding this file contact NAIF at JPL
+
+ Charles H. Acton, Jr
+ (818) 354-3869
+ Chuck.Acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818) 354-8136
+ Boris.Semenov@jpl.nasa.gov
+
+
+SCLKvSCET File Contents
+--------------------------------------------------------
+
+ CCSD3ZS00001$$sclk$$NJPL3KS0L015$$scet$$
+ MISSION-NAME=JUNO;
+ SPACECRAFT-NAME=JUNO;
+ DATA-SET-ID=SCLK-SCET;
+ FILE-NAME=JNO-SCLKSCET.00090;
+ PRODUCT-CREATION-TIME=2019-08-18T17:00:00;
+ PRODUCT-VERSION-ID=90;
+ PRODUCER-ID=SCT;
+ APPLICABLE-START-TIME=2000-001T00:00:00;
+ APPLICABLE-STOP-TIME=2021-365T00:00:00;
+ MISSION-ID=34;
+ SPACECRAFT-ID=61;
+ CCSD3RE00000$$scet$$NJPL3IS00613$$data$$
+
+
+
+MAKCLK Setup Files
+--------------------------------------------------------
+
+MAKCLK Setup for ``Standard'' Format Clock
+
+ SCLKSCET_FILE = JNO_SCLKSCET.00090.clean
+ OLD_SCLK_KERNEL = /sdma/naif/ops/projects/JUNO/scet/bin/juno_template.tsc
+ FILE_NAME = JNO_SCLKSCET.00090.tsc
+ NAIF_SPACECRAFT_ID = -61
+ LEAPSECONDS_FILE = /sdma/naif/ops/projects/JUNO/lsk/juno.tls
+ PARTITION_TOLERANCE = 14
+ LOG_FILE = JNO_SCLKSCET.00090.log
+
+
+MAKCLK Setup for ``High Precision'' Format Clock
+
+ SCLKSCET_FILE = JNO_SCLKSCET.00090.clean
+ OLD_SCLK_KERNEL = /sdma/naif/ops/projects/JUNO/scet/bin/juno_template_65536.tsc
+ FILE_NAME = JNO_SCLKSCET.00090.tsc
+ NAIF_SPACECRAFT_ID = -61999
+ LEAPSECONDS_FILE = /sdma/naif/ops/projects/JUNO/lsk/juno.tls
+ PARTITION_TOLERANCE = 3584
+ LOG_FILE = JNO_SCLKSCET.00090.log
+
+
+
+Kernel DATA for ``Standard'' Format Clock
+--------------------------------------------------------
+
+\begindata
+
+
+SCLK_KERNEL_ID = ( @2019-08-18/17:03:03.00 )
+
+SCLK_DATA_TYPE_61 = ( 1 )
+SCLK01_TIME_SYSTEM_61 = ( 2 )
+SCLK01_N_FIELDS_61 = ( 2 )
+SCLK01_MODULI_61 = ( 4294967296 256 )
+SCLK01_OFFSETS_61 = ( 0 0 )
+SCLK01_OUTPUT_DELIM_61 = ( 1 )
+
+SCLK_PARTITION_START_61 = ( 0.0000000000000E+00
+ 9.3793618176000E+10
+ 1.1115002572800E+11
+ 1.1208596224000E+11
+ 1.1498689996800E+11 )
+
+SCLK_PARTITION_END_61 = ( 9.3793616905000E+10
+ 1.1115002561600E+11
+ 1.1208596226400E+11
+ 1.1498690015000E+11
+ 1.0995116277750E+12 )
+
+SCLK01_COEFFICIENTS_61 = (
+
+ 0.0000000000000E+00 6.4184000000000E+01 1.0000000000000E+00
+ 4.8472473856000E+10 1.8934566518400E+08 1.0000000000106E+00
+ 7.2714240512000E+10 2.8404006618500E+08 9.9999999998596E-01
+ 9.3793616905000E+10 3.6638138021900E+08 9.9999830502084E-01
+ 9.5755854601000E+10 3.7404635822700E+08 1.0009769999981E+00
+ 9.5756110601000E+10 3.7404735920400E+08 9.9999861571600E-01
+ 9.6339759625000E+10 3.7632723504800E+08 9.9999860983214E-01
+ 9.6715058185000E+10 3.7779324301000E+08 9.9999867672148E-01
+ 9.6891686153000E+10 3.7848319509700E+08 9.9999866448606E-01
+ 9.7557413385000E+10 3.8108368862400E+08 9.9999871140751E-01
+ 9.8076925961000E+10 3.8311303200900E+08 9.9999875092765E-01
+ 9.8658170121000E+10 3.8538351417300E+08 9.9999878280577E-01
+ 9.9961521673000E+10 3.9047472497600E+08 9.9999879327280E-01
+ 1.0095944730500E+11 3.9437286727200E+08 9.9999879311537E-01
+ 1.0213711744900E+11 3.9897313572000E+08 9.9999886086085E-01
+ 1.0292457524100E+11 4.0204913921600E+08 9.9999846554930E-01
+ 1.0302434253700E+11 4.0243885461800E+08 9.9999877775294E-01
+ 1.0444692890500E+11 4.0799582582600E+08 9.9999874887262E-01
+ 1.0517044916100E+11 4.1082207329000E+08 9.9999872396057E-01
+ 1.0718307661700E+11 4.1868388925800E+08 9.9999868519590E-01
+ 1.0766438938500E+11 4.2056401478600E+08 9.9999850961374E-01
+ 1.0816406119300E+11 4.2251585487700E+08 9.9999837597460E-01
+ 1.1115002434500E+11 4.3417975449700E+08 9.9999832720281E-01
+ 1.1208596088100E+11 4.3783575047500E+08 9.9999848532368E-01
+ 1.1233001566500E+11 4.3878908803100E+08 9.9999857803275E-01
+ 1.1249852587300E+11 4.3944733009500E+08 9.9999862950081E-01
+ 1.1288163883300E+11 4.4094386304400E+08 9.9999867732719E-01
+ 1.1327415313700E+11 4.4247712001600E+08 9.9999872144903E-01
+ 1.1380195064100E+11 4.4453882638000E+08 9.9999876230196E-01
+ 1.1498689879100E+11 4.4916752436200E+08 9.9999976768437E-01
+ 1.1527340554300E+11 4.5028669110200E+08 9.9999980316913E-01
+ 1.1560376023100E+11 4.5157713884800E+08 9.9999975773588E-01
+ 1.1637620643900E+11 4.5459450611700E+08 9.9999972223808E-01
+ 1.1703150141500E+11 4.5715425140600E+08 9.9999969168399E-01
+ 1.1822383651900E+11 4.6181180897000E+08 9.9999967239356E-01
+ 1.1946708439100E+11 4.6666824437900E+08 9.9999963973550E-01
+ 1.2363397847100E+11 4.8294516851500E+08 9.9999959524185E-01
+ 1.2517911843900E+11 4.8898086907200E+08 9.9999926219015E-01
+ 1.2521450967100E+11 4.8911911597000E+08 9.9999956075559E-01
+ 1.2592554890300E+11 4.9189661175000E+08 9.9999900867701E-01
+ 1.2616906992700E+11 4.9284786480700E+08 9.9999878685126E-01
+ 1.2722544163900E+11 4.9697431180100E+08 9.9999897334378E-01
+ 1.2793410339900E+11 4.9974251895900E+08 9.9999890872409E-01
+ 1.2885861386300E+11 5.0335388401800E+08 9.9999883179019E-01
+ 1.3102633405500E+11 5.1182153112600E+08 9.9999871955698E-01
+ 1.3126285219900E+11 5.1274542894300E+08 9.9999873424891E-01
+ 1.3149786839100E+11 5.1366345978100E+08 9.9999876447543E-01
+ 1.3360032112700E+11 5.2187615563400E+08 9.9999873337884E-01
+ 1.3424000727100E+11 5.2437492646900E+08 9.9999873799838E-01
+ 1.3461568983100E+11 5.2584243461700E+08 9.9999875275023E-01
+ 1.3492705648700E+11 5.2705870910000E+08 9.9999877250364E-01
+ 1.3493456445500E+11 5.2708803706400E+08 9.9999875462295E-01
+ 1.3574796631100E+11 5.3026538410700E+08 9.9999928991417E-01
+ 1.3590479242300E+11 5.3087798567200E+08 9.9999873941198E-01
+ 1.3691084989500E+11 5.3480789271800E+08 9.9999873182127E-01
+ 1.3734425251900E+11 5.3650086957100E+08 9.9999873587748E-01
+ 1.3762594672700E+11 5.3760123618000E+08 9.9999874719891E-01
+ 1.3820607395900E+11 5.3986735534100E+08 9.9999874246538E-01
+ 1.3888946826300E+11 5.4253686098400E+08 9.9999874455621E-01
+ 1.3924080855100E+11 5.4390928226100E+08 9.9999874396394E-01
+ 1.3990402519100E+11 5.4649996900700E+08 9.9999874246824E-01
+ 1.4039606205500E+11 5.4842198559000E+08 9.9999874728460E-01
+ 1.4101546531900E+11 5.5084152655900E+08 9.9999874386518E-01
+ 1.4116913034300E+11 5.5144177980500E+08 9.9999874431179E-01
+ 1.4128024074300E+11 5.5187580426000E+08 9.9999874717260E-01
+ 1.4160902026300E+11 5.5316009765100E+08 9.9999875414573E-01
+ 1.4218066979900E+11 5.5539310086900E+08 9.9999874959598E-01
+ 1.4274532567100E+11 5.5759878511100E+08 9.9999874609444E-01
+ 1.4335270794300E+11 5.5997136913600E+08 9.9999875456987E-01
+ 1.4409783203900E+11 5.6288200651100E+08 9.9999875372472E-01
+ 1.4476562672700E+11 5.6549057626000E+08 9.9999876249153E-01
+ 1.4551593431100E+11 5.6842146163300E+08 9.9999874981450E-01
+ 1.4573667594300E+11 5.6928373255500E+08 9.9999874603296E-01
+ 1.4626624650300E+11 5.7135236496100E+08 9.9999875347161E-01
+ 1.4691028797500E+11 5.7386814882500E+08 9.9999875544841E-01
+ 1.4755000432700E+11 5.7636703771500E+08 9.9999875348134E-01
+ 1.4796896317500E+11 5.7800359367500E+08 9.9999875594224E-01
+ 1.4859617520700E+11 5.8045363762700E+08 9.9999875394968E-01
+ 1.4914451901500E+11 5.8259560295800E+08 9.9999875464955E-01
+ 1.4980027018300E+11 5.8515712776800E+08 9.9999875434084E-01
+ 1.5044147287100E+11 5.8766182264800E+08 9.9999875442639E-01
+ 1.5097933911100E+11 5.8976286003100E+08 9.9999875281165E-01
+ 1.5153826672700E+11 5.9194616830800E+08 9.9999876516327E-01
+ 1.5210485821500E+11 5.9415941357500E+08 9.9999875149201E-01
+ 1.5281841392700E+11 5.9694673709500E+08 9.9999875571257E-01
+ 1.5328688445500E+11 5.9877669781800E+08 9.9999875535207E-01
+ 1.5386875504700E+11 6.0104962698900E+08 9.9999875421401E-01
+ 1.5445810826300E+11 6.0335178512100E+08 9.9999873876120E-01
+ 1.5504775075900E+11 6.0565507321600E+08 9.9999876079519E-01
+ 1.5562969815100E+11 6.0792830239900E+08 9.9999875277992E-01
+ 1.5622309463100E+11 6.1024625450800E+08 9.9999875813340E-01
+ 1.5679039549500E+11 6.1246227075600E+08 9.9999875353106E-01
+ 1.5732643773500E+11 6.1455618314600E+08 9.9999875679107E-01
+ 1.5799587952700E+11 6.1717118689500E+08 9.9999875800000E-01 )
+
+\begintext
+
+
+
+Kernel DATA for ``High Precision'' Format Clock
+--------------------------------------------------------
+
+\begindata
+
+
+SCLK_KERNEL_ID = ( @2019-08-18/17:03:03.00 )
+
+SCLK_DATA_TYPE_61999 = ( 1 )
+SCLK01_TIME_SYSTEM_61999 = ( 2 )
+SCLK01_N_FIELDS_61999 = ( 2 )
+SCLK01_MODULI_61999 = ( 4294967296 65536 )
+SCLK01_OFFSETS_61999 = ( 0 0 )
+SCLK01_OUTPUT_DELIM_61999 = ( 1 )
+
+SCLK_PARTITION_START_61999 = ( 0.0000000000000E+00
+ 2.4011166253056E+13
+ 2.8454406586368E+13
+ 2.8694006333440E+13
+ 2.9436646391808E+13 )
+
+SCLK_PARTITION_END_61999 = ( 2.4011165927604E+13
+ 2.8454406557677E+13
+ 2.8694006339633E+13
+ 2.9436646438492E+13
+ 2.8147497671065E+14 )
+
+SCLK01_COEFFICIENTS_61999 = (
+
+ 0.0000000000000E+00 6.4184000000000E+01 1.0000000000000E+00
+ 1.2408953307136E+13 1.8934566518400E+08 1.0000000000106E+00
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+ 3.7308589041454E+13 5.6928373255500E+08 9.9999874603296E-01
+ 3.7444159104814E+13 5.7135236496100E+08 9.9999875347161E-01
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+ 3.7772801107758E+13 5.7636703771500E+08 9.9999875348134E-01
+ 3.7880054572846E+13 5.7800359367500E+08 9.9999875594224E-01
+ 3.8040620853038E+13 5.8045363762700E+08 9.9999875394968E-01
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+ 3.8348869166894E+13 5.8515712776800E+08 9.9999875434084E-01
+ 3.8513017055022E+13 5.8766182264800E+08 9.9999875442639E-01
+ 3.8650710812462E+13 5.8976286003100E+08 9.9999875281165E-01
+ 3.8793796282158E+13 5.9194616830800E+08 9.9999876516327E-01
+ 3.8938843703086E+13 5.9415941357500E+08 9.9999875149201E-01
+ 3.9121513965358E+13 5.9694673709500E+08 9.9999875571257E-01
+ 3.9241442420526E+13 5.9877669781800E+08 9.9999875535207E-01
+ 3.9390401292078E+13 6.0104962698900E+08 9.9999875421401E-01
+ 3.9541275715374E+13 6.0335178512100E+08 9.9999873876120E-01
+ 3.9692224194350E+13 6.0565507321600E+08 9.9999876079519E-01
+ 3.9841202726702E+13 6.0792830239900E+08 9.9999875277992E-01
+ 3.9993112225582E+13 6.1024625450800E+08 9.9999875813340E-01
+ 4.0138341246766E+13 6.1246227075600E+08 9.9999875353106E-01
+ 4.0275568060206E+13 6.1455618314600E+08 9.9999875679107E-01
+ 4.0446945158958E+13 6.1717118689500E+08 9.9999875800000E-01 )
+
+\begintext
+
+
+End of SCLK file.
+
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/junoAddendum005.ti b/tests/pytests/data/JNCR_2016240_01M06152_V01/junoAddendum005.ti
new file mode 100644
index 0000000000000000000000000000000000000000..a3374f43422a7e21605db37424f42bc94532611c
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/junoAddendum005.ti
@@ -0,0 +1,71 @@
+\begintext
+The instrument addendum kernel for JUNO's JNC camera (JunoCam).
+
+history 2017-08-01 Jeannie Backer - Original version.
+ 2017-08-10 Kris Becker - Updated parameters per an email from M. Caplinger
+ received on June 20, 2017
+ 2017-08-15 Jesse Mapel - Removed duplicated keywords from juno_v12.tf and
+ juno_junocam_v02.ti
+ 2018-05-14 Jesse Mapel - Changed filter offsets to match code from M Caplinger.
+
+negate k value (per gerard post)
+\begindata
+ INS-61500_PIXEL_PITCH = 0.0074
+ INS-61500_FOCAL_LENGTH = 10.95637
+ INS-61500_BORESIGHT_LINE = 600
+ INS-61500_BORESIGHT_SAMPLE = 814.21
+ INS-61500_FILTER_OFFSET = 1
+ INS-61500_FILTER_LINES = 1200
+ INS-61500_FILTER_SAMPLES = 1648
+ INS-61500_FILTER_NAME = 'FULLCCD'
+
+\begintext
+
+Ensure this section provides all the necessary parameters
+for the PushFrameCameraCcdLayout class to provide framelet
+parameters for full ccd mapping.
+
+The order of the filters on the CCD, from top to bottom is
+METHANE (-61504), BLUE (-61501), GREEN (-61502), RED (-61503)
+
+\begindata
+
+ INS-61504_FILTER_NAME = 'METHANE'
+ INS-61504_FILTER_OFFSET = 284.52
+ INS-61504_FILTER_LINES = 128
+ INS-61504_FILTER_SAMPLES = 1648
+
+ INS-61501_FILTER_NAME = 'BLUE'
+ INS-61501_FILTER_OFFSET = 441.52
+ INS-61501_FILTER_LINES = 128
+ INS-61501_FILTER_SAMPLES = 1648
+
+ INS-61502_FILTER_NAME = 'GREEN'
+ INS-61502_FILTER_OFFSET = 596.52
+ INS-61502_FILTER_LINES = 128
+ INS-61502_FILTER_SAMPLES = 1648
+
+ INS-61503_FILTER_NAME = 'RED'
+ INS-61503_FILTER_OFFSET = 751.52
+ INS-61503_FILTER_LINES = 128
+ INS-61503_FILTER_SAMPLES = 1648
+
+\begintext
+Calculated transformation and inverse transfromation vectors using pixel pitch and 1/pixel pitch
+
+\begindata
+ INS-61500_TRANSX = (0.0000, 0.0074, 0.0000)
+ INS-61500_TRANSY = (0.0000, 0.0000, 0.0074)
+ INS-61500_ITRANSS = (0.0000, 135.1351, 0.0000)
+ INS-61500_ITRANSL = (0.0000, 0.0000, 135.1351)
+
+\begintext
+
+ Turn off surface correction adjustment for now (KJB - 2017-08-10)
+
+\begindata
+
+ INS-61500_SWAP_OBSERVER_TARGET = 'TRUE'
+ INS-61500_LIGHTTIME_CORRECTION = 'NONE'
+ INS-61500_LT_SURFACE_CORRECT = 'FALSE'
+
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_junocam_v03.ti b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_junocam_v03.ti
new file mode 100644
index 0000000000000000000000000000000000000000..4ec19c8bdb8732b2d0e6d1ef79a41d4e8726be58
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_junocam_v03.ti
@@ -0,0 +1,482 @@
+KPL/IK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "juno_junocam_v03.ti"
+MISSION_NAME = JUNO
+SPACECRAFT_NAME = JUNO
+DATA_SET_ID = "JNO-J/E/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = IK
+PRODUCT_ID = "juno_junocam_v03.ti"
+PRODUCT_CREATION_TIME = 2019-09-04T10:44:03
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "JUNO SPACECRAFT"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = JUPITER
+INSTRUMENT_NAME = "JUNO EPO CAMERA"
+NAIF_INSTRUMENT_ID = {
+ -61504,
+ -61503,
+ -61502,
+ -61501,
+ -61500
+ }
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = INSTRUMENT
+ DESCRIPTION = "SPICE IK file providing FOV definitions and
+other instrument parameters for the JUNO EPO Camera (JUNOCAM) instrument,
+created by NAIF, JPL. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Juno JUNOCAM Instrument Kernel
+===============================================================================
+
+ This Instrument Kernel (IK) file contains optics and detector
+ parameters and FOV definitions for the JUNO Camera (JUNOCAM)
+ instrument.
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ Version 0.3 -- August 7, 2019 -- Boris Semenov, NAIF
+
+ Updated FOVs to use vectors computed using distortion models.
+
+ Version 0.2 -- August 3, 2017 -- Boris Semenov, NAIF
+
+ Updated most sections based on [8].
+
+ Version 0.1 -- September 29, 2016 -- Boris Semenov, NAIF
+
+ Updated based on [5].
+
+ Version 0.0 -- June 9, 2009 -- Boris Semenov, NAIF
+
+ Initial Release.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. Kernel Pool Required Reading
+
+ 2. GETFOV, getfoc_c, cspice_getfov headers
+
+ 3. JUNO FK file, latest version
+
+ 4. JUNOCAM CDR Presentations
+
+ 5. E-mail from Mike Caplinger, MSSS re actual JUNOCAM parameters,
+ 09/19/16.
+
+ 6. C.J. Hansen, et al, "Junocam: Juno~s Outreach Camera", Space Sci Rev,
+ DOI 10.1007/s11214-014-0079-x
+
+ 7. http://www.msss.com/all_projects/junocam.php, accessed 09/29/16
+
+ 8. E-mail from Mike Caplinger, MSSS re updated Junocam camera model,
+ 06/20/17
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Boris V. Semenov, NAIF/JPL, (818)-354-8136, Boris.Semenov@jpl.nasa.gov
+
+
+Implementation Notes
+-------------------------------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make
+ use of this kernel must ``load'' the kernel, normally during program
+ initialization. The SPICE routine FURNSH loads a kernel file into
+ the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name; ) -- FORTRAN
+ furnsh_c ( "frame_kernel_name" ); -- C
+ cspice_furnsh, frame_kernel_name -- IDL
+ cspice_furnsh( 'frame_kernel_name' ) -- MATLAB
+
+ Once the file has been loaded, the SPICE routine GETFOV (getfov_c in
+ C, cspice_getfov in IDL and MATLAB) can be used to retrieve FOV
+ parameters for a given instrument or structure.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Naming Conventions
+----------------------------------------------------------
+
+ All names referencing values in this IK file start with the
+ characters `INS' followed by the NAIF JUNO spacecraft ID number
+ (-61) followed by a NAIF three digit ID code for the camera or one
+ of its spectral bands. This is the full list of names and IDs for
+ the camera and spectral bands described by this IK file:
+
+ JUNO_JUNOCAM_METHANE -61504
+ JUNO_JUNOCAM_BLUE -61501
+ JUNO_JUNOCAM -61500
+ JUNO_JUNOCAM_GREEN -61502
+ JUNO_JUNOCAM_RED -61503
+
+ The remainder of the keyword name is an underscore character
+ followed by the unique name of the data item. For example, the
+ JUNOCAM "blue" band boresight direction in the JUNO_JUNOCAM frame is
+ specified by:
+
+ INS-61501_BORESIGHT
+
+ The upper bound on the length of the name of any data item is 32
+ characters.
+
+ If the same item is included in more than one file, or if the same
+ item appears more than once within a single file, the latest value
+ supersedes any earlier values.
+
+
+Instrument Description
+---------------------------------------------------------
+
+ From [7]:
+
+ Junocam will acquire 3-color (red, green, blue) images of Jupiter
+ during Juno's first seven orbits around the giant planet. The
+ data will be processed and studied by students as part of the
+ Juno Education and Public Outreach effort.
+
+ The camera, derived from the MSL MARDI instrument, is designed to
+ acquire red-, green- and blue-wavelength images of Jupiter's
+ polar regions and lower-latitude cloud tops during Juno's first
+ seven orbits around the planet. These images, of approximately 15
+ kilometers (9.3 miles) per pixel resolution, will be used by
+ students to create the first color images of the jovian poles, as
+ well as high resolution views of lower-latitude cloud belts.
+ After the required, seven orbit design life, Junocam will
+ continue to operate as long as possible in the harsh jovian
+ radiation environment.
+
+ For a detailed description see [6]
+
+
+Mounting Alignment
+--------------------------------------------------------
+
+ Refer to the latest version of the Juno Frames Definition Kernel
+ (FK) [3] for the JUNOCAM frame definitions and mounting alignment
+ information.
+
+
+Apparent FOV Layout
+--------------------------------------------------------
+
+ The diagram below illustrates the nominal JUNOCAM camera FOV/CCD
+ layout:
+
+
+ --- 0,0--------------------------------------------.
+ 5 deg | METHANE 128 pix * | --------
+ --- `-----------------------------------------1648,128 | 245 pixels
+ |
+ --- 0,0--------------------------------------------. |
+ 5 deg | BLUE 128 pix * | | ---
+ --- `-----------------------------------------1648,128 | |80 pixels
+ +Zjc x-------------> +Xjc --- ---
+ --- 0,0---------------------|----------------------. | |75 pixels
+ 5 deg | GREEN 128 pix * | | ---
+ --- `----------------------|------------------1648,128 |
+ | |
+ --- 0,0---------------------|----------------------. | 230 pixels
+ 5 deg | RED 128 pix * | --------
+ --- `----------------------|------------------1648,128
+ |
+ V +Yjc
+
+ | 58 deg | Boresight
+ |---------------------------------------------| (+Zjc axis)
+ | | is into
+ the page
+
+
+ Note 1: In addition to photoactive pixels the sensor has dark and
+ overscan columns that are present in all 1648 pixels wide Junocam
+ images. There are 23 dark pixels at the start of each line,
+ followed by 1608 photoactive pixels and additional dark, isolation,
+ and overscan/dummy pixels for a total of 1648 pixels per line.
+
+ Note 2: the angular dimensions above are nominal. The actual extents
+ of the photoactive pixel areas vary due to optical distortion and,
+ depending on a band, are between ~4.90 and ~5.05 deg in the YZ
+ direction and between ~57.5 and ~58.5 deg in the XZ direction.
+
+
+Optical and Detector Parameters
+--------------------------------------------------------
+
+ This section provides two parameters that, in combination with the
+ optical distortion and filter parameters, are needed to compute the
+ view directions of the individual CCD pixels. These parameters are
+ the focal length and pixel size, both given in millimeters.
+
+ \begindata
+
+ INS-61504_FOCAL_LENGTH = ( 10.95637 )
+ INS-61504_PIXEL_SIZE = ( 0.0074 )
+
+ INS-61501_FOCAL_LENGTH = ( 10.95637 )
+ INS-61501_PIXEL_SIZE = ( 0.0074 )
+
+ INS-61500_FOCAL_LENGTH = ( 10.95637 )
+ INS-61500_PIXEL_SIZE = ( 0.0074 )
+
+ INS-61502_FOCAL_LENGTH = ( 10.95637 )
+ INS-61502_PIXEL_SIZE = ( 0.0074 )
+
+ INS-61503_FOCAL_LENGTH = ( 10.95637 )
+ INS-61503_PIXEL_SIZE = ( 0.0074 )
+
+ \begintext
+
+
+FOV Definition
+--------------------------------------------------------
+
+ This section contains definitions of the JUNOCAM band and total
+ FOVs.
+
+ All FOVs are defined as (nearly) rectangular pyramids using boundary
+ vectors computed using the distortion model in the "Optical
+ Distortion" section below for pixels (23.5,0.5), (23.5,127.5),
+ (1630.5,127.5), and (1630.5,0.5) and using the boresight computed
+ for the pixel (827.0,64.0). They are provided for visualization
+ purposes, do not represent the geometry of the actual FOV sides, and
+ are not intended for quantitative analysis.
+
+ The total FOV (ID -61500), spanning from the METHANE top edge to the
+ RED bottom edge through all band boundary vectors, with the
+ boresight set to be exactly along the the JUNO_JUNOCAM frame +Z
+ axis, is defined as a polygon and provided solely for convenience.
+
+ \begindata
+
+ INS-61504_FOV_FRAME = 'JUNO_JUNOCAM'
+ INS-61504_FOV_SHAPE = 'RECTANGLE'
+ INS-61504_BORESIGHT = (
+ 0.00854687, -0.16805056, 0.98574133
+ )
+ INS-61504_FOV_BOUNDARY_CORNERS = (
+ -0.47351727, -0.18862601, 0.86034971
+ -0.47852984, -0.11376363, 0.87067045
+ 0.49067337, -0.11299511, 0.86398596
+ 0.48553839, -0.18735362, 0.85390345
+ )
+
+ INS-61501_FOV_FRAME = 'JUNO_JUNOCAM'
+ INS-61501_FOV_SHAPE = 'RECTANGLE'
+ INS-61501_BORESIGHT = (
+ 0.00862523, -0.06371477, 0.99793088
+ )
+ INS-61501_FOV_BOUNDARY_CORNERS = (
+ -0.47934991, -0.09577177, 0.87238262
+ -0.48125208, -0.01885545, 0.87637943
+ 0.49346247, -0.01872799, 0.86956544
+ 0.49151356, -0.09512467, 0.86565912
+ )
+
+ INS-61500_FOV_FRAME = 'JUNO_JUNOCAM'
+ INS-61500_FOV_SHAPE = 'POLYGON'
+ INS-61500_BORESIGHT = (
+ 0.00000000, 0.00000000, 1.00000000
+ )
+ INS-61500_FOV_BOUNDARY_CORNERS = (
+ -0.47351727, -0.18862601, 0.86034971
+ -0.47852984, -0.11376363, 0.87067045
+ -0.47934991, -0.09577177, 0.87238262
+ -0.48125208, -0.01885545, 0.87637943
+ -0.48132762, -0.00181401, 0.87653889
+ -0.48010800, 0.07530320, 0.87397125
+ -0.47949606, 0.09218676, 0.87268845
+ -0.47518685, 0.16768048, 0.86375964
+ 0.48724863, 0.16654879, 0.85723408
+ 0.49166330, 0.09156385, 0.86595800
+ 0.49229026, 0.07479430, 0.86721169
+ 0.49353987, -0.00180175, 0.86972131
+ 0.49346247, -0.01872799, 0.86956544
+ 0.49151356, -0.09512467, 0.86565912
+ 0.49067337, -0.11299511, 0.86398596
+ 0.48553839, -0.18735362, 0.85390345
+ )
+
+ INS-61502_FOV_FRAME = 'JUNO_JUNOCAM'
+ INS-61502_FOV_SHAPE = 'RECTANGLE'
+ INS-61502_BORESIGHT = (
+ 0.00863288, 0.04084925, 0.99912803
+ )
+ INS-61502_FOV_BOUNDARY_CORNERS = (
+ -0.48132762, -0.00181401, 0.87653889
+ -0.48010800, 0.07530320, 0.87397125
+ 0.49229026, 0.07479430, 0.86721169
+ 0.49353987, -0.00180175, 0.86972131
+ )
+
+ INS-61503_FOV_FRAME = 'JUNO_JUNOCAM'
+ INS-61503_FOV_SHAPE = 'RECTANGLE'
+ INS-61503_BORESIGHT = (
+ 0.00857099, 0.14442688, 0.98947835
+ )
+ INS-61503_FOV_BOUNDARY_CORNERS = (
+ -0.47949606, 0.09218676, 0.87268845
+ -0.47518685, 0.16768048, 0.86375964
+ 0.48724863, 0.16654879, 0.85723408
+ 0.49166330, 0.09156385, 0.86595800
+ )
+
+ \begintext
+
+
+Optical Distortion
+--------------------------------------------------------
+
+ This code recipe with fragments in Python, based on [8], maps to and
+ from pixel coordinates (for full images with 1648 samples per line)
+ and vectors in the JUNO_JUNOCAM reference frame.
+
+ The distortion parameters are set from these IK keywords assigned in
+ the data block below the recipe (# is 4 for METHANE, 1 for BLUE, 2
+ for GREEN, and 3 for RED):
+
+ cx = INS-6150#_DISTORTION_X
+ cy = INS-6150#_DISTORTION_Y
+ k1 = INS-6150#_DISTORTION_K1
+ k2 = INS-6150#_DISTORTION_K2
+ fl = INS-6150#_FOCAL_LENGTH/INS-6150#_PIXEL_SIZE
+
+ Using these "distort" and "undistort" functions:
+
+ def undistort(c):
+ xd, yd = c[0], c[1]
+ for i in range(5): # fixed number of iterations for simplicity
+ r2 = (xd**2+yd**2)
+ dr = 1+k1*r2+k2*r2*r2
+ xd = c[0]/dr
+ yd = c[1]/dr
+ return [xd, yd]
+
+ def distort(c):
+ xd, yd = c[0], c[1]
+ r2 = (xd**2+yd**2)
+ dr = 1+k1*r2+k2*r2*r2
+ xd *= dr
+ yd *= dr
+ return [xd, yd]
+
+ given a vector v in the JUNO_JUNOCAM reference frame, the following
+ computes an XY coordinate in Junocam framelet coordinates with 0,0
+ in the upper left:
+
+ alpha = v[2]/fl
+ cam = [v[0]/alpha, v[1]/alpha]
+ cam = distort(cam)
+ x = cam[0]+cx
+ y = cam[1]+cy
+
+ and the following takes an XY coordinate in Junocam framelet
+ coordinates and produces a vector in the JUNO_JUNOCAM reference
+ frame (of arbitrary length).
+
+ cam[0] = x-cx
+ cam[1] = y-cy
+ cam = undistort(cam)
+ v = [cam[0], cam[1], fl]
+
+ The K1, K2, CX, and CY values are provided in the keyword below.
+
+ \begindata
+
+ INS-61504_DISTORTION_K1 = -5.9624209455667325e-08
+ INS-61504_DISTORTION_K2 = 2.7381910042256151e-14
+ INS-61504_DISTORTION_X = 814.21
+ INS-61504_DISTORTION_Y = 315.48
+
+ INS-61501_DISTORTION_K1 = -5.9624209455667325e-08
+ INS-61501_DISTORTION_K2 = 2.7381910042256151e-14
+ INS-61501_DISTORTION_X = 814.21
+ INS-61501_DISTORTION_Y = 158.48
+
+ INS-61500_DISTORTION_K1 = -5.9624209455667325e-08
+ INS-61500_DISTORTION_K2 = 2.7381910042256151e-14
+ INS-61500_DISTORTION_X = 814.21
+ INS-61500_DISTORTION_Y = 78.48
+
+ INS-61502_DISTORTION_K1 = -5.9624209455667325e-08
+ INS-61502_DISTORTION_K2 = 2.7381910042256151e-14
+ INS-61502_DISTORTION_X = 814.21
+ INS-61502_DISTORTION_Y = 3.48
+
+ INS-61503_DISTORTION_K1 = -5.9624209455667325e-08
+ INS-61503_DISTORTION_K2 = 2.7381910042256151e-14
+ INS-61503_DISTORTION_X = 814.21
+ INS-61503_DISTORTION_Y = -151.52
+
+ \begintext
+
+
+Timing
+--------------------------------------------------------
+
+ From [8]:
+
+ Each Junocam image consists of multiple frames, each a readout of
+ a portion of the CCD containing one or more filter strips
+ ("framelets") as described in the I kernel. The timing of each
+ frame is set by a base time (the "START_TIME" keyword in the PDS
+ label of each Junocam product) and an interframe delay
+ ("INTERFRAME_DELAY"). We have found that there is a fixed bias
+ of 61.88 msec in the start time with a possible jitter of order
+ 20 msec relative to the reported value (that is, you should add
+ 61.88 msec to the value of START_TIME.) You should also add 1
+ msec to the value of INTERFRAME_DELAY.
+
+ The start time bias and additional interfame delay delta are
+ provided in the keywords below in seconds.
+
+ \begindata
+
+ INS-61504_START_TIME_BIAS = 0.06188
+ INS-61504_INTERFRAME_DELTA = 0.001
+
+ INS-61501_START_TIME_BIAS = 0.06188
+ INS-61501_INTERFRAME_DELTA = 0.001
+
+ INS-61500_START_TIME_BIAS = 0.06188
+ INS-61500_INTERFRAME_DELTA = 0.001
+
+ INS-61502_START_TIME_BIAS = 0.06188
+ INS-61502_INTERFRAME_DELTA = 0.001
+
+ INS-61503_START_TIME_BIAS = 0.06188
+ INS-61503_INTERFRAME_DELTA = 0.001
+
+ \begintext
+
+
+Filters
+--------------------------------------------------------
+
+ TBD; may be based on MRO/MARCI
+
+
+End of the IK file.
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_sc_rec_160821_160827_v01_0_sliced_-61000.xc b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_sc_rec_160821_160827_v01_0_sliced_-61000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..78ea896afb887bd6557d358565fa8662d5d11a55
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_sc_rec_160821_160827_v01_0_sliced_-61000.xc
@@ -0,0 +1,792 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'JUNO Reconstructed SC Bus CK File by NAIF/JPL '
+BEGIN_ARRAY 1 771
+'JUNO SC BUS REC ATT_RECON QUATS '
+'1F53605E48^A'
+'1F5360BC0E^A'
+'-EE48'
+'1'
+'3'
+'1'
+771
+'AFB77AC517F098^0'
+'-21948FA234DF48^0'
+'-B55F59D85CD408^0'
+'-193835C3D98722^0'
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+'-213FCCE18676EC^-1'
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+'344550FE30833C^0'
+'-213FCD530D20D8^-1'
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+'-3DCD9A3CACAEA^0'
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+'344550F9E50042^0'
+'-213FD08BAF5C6^-1'
+'-2032A8A75C2D86^-1'
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+'1F53609BD4F8F4^A'
+'1F53609CD4F8F4^A'
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+'1F53609FD4F8F4^A'
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+'1F5360A2D4F8F4^A'
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+'1F5360A4D4F8F4^A'
+'1F5360A5D4F8F4^A'
+'1F5360A6D4F8F4^A'
+'1F5360A7D4F8F4^A'
+'1F5360A8D4F8F4^A'
+'1F5360A9D4F8F4^A'
+'1F5360AAD4F8F4^A'
+'1F5360ABD4F8F4^A'
+'1F5360ACD4F8F4^A'
+'1F5360ADD4F8F4^A'
+'1F5360AED4F8F4^A'
+'1F5360AFD4F8F4^A'
+'1F5360B0D4F8F4^A'
+'1F5360B1D4F8F4^A'
+'1F5360B2D4F8F4^A'
+'1F5360B3D4F8F4^A'
+'1F5360B4D4F8F4^A'
+'1F5360B5D4F8F4^A'
+'1F5360B6D4F8F4^A'
+'1F5360B7D4F8F4^A'
+'1F5360B8D4F8F4^A'
+'1F5360B9D4F8F4^A'
+'1F5360BAD4F8F4^A'
+'1F5360BBD4F8F4^A'
+'1F5360BC0E^A'
+'1F53605E48^A'
+'1^1'
+'6^2'
+END_ARRAY 1 771
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/acpaquette/juno/JNCR_2016240_01M06152_V01_METHANE_0008.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_sc_rec_160821_160827_v01_1_sliced_-61000.xc b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_sc_rec_160821_160827_v01_1_sliced_-61000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..3377bc7e6498d4d10c9fb2f46f1ad314622abaa3
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_sc_rec_160821_160827_v01_1_sliced_-61000.xc
@@ -0,0 +1,776 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'JUNO Reconstructed SC Bus CK File by NAIF/JPL '
+BEGIN_ARRAY 1 755
+'JUNO SC BUS REC ATT_RECON QUATS '
+'1F536AFD75^A'
+'1F536B5961^A'
+'-EE48'
+'1'
+'3'
+'1'
+755
+'18CDC18467200D^0'
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+'2BABBF2D744ED4^0'
+'-B47EEF494E7D9^0'
+'-265E6EFA78706E^0'
+'-ABFB7C7820A31^0'
+'344544DCED9B12^0'
+'-213CAFCD7C63EE^-1'
+'-20328FF52B0FCE^-1'
+'19E0BAF8307535^0'
+'-B77532F270A05^0'
+'-13C19D50AAB4C1^0'
+'-AF8DDC6195465^0'
+'3445454401E284^0'
+'-213C657230DB26^-1'
+'-2032995A5992C4^-1'
+'7D0820575AD22C^-1'
+'-B880E54B516AB8^0'
+'-EFF5D7EF25F948^-2'
+'-B14ACBC4FEBBF8^0'
+'344545AB1629F4^0'
+'-213C1B16E5525E^-1'
+'-2032A30440455A^-1'
+'-A549EE8B8E691^-1'
+'-B79F39D2C5C658^0'
+'11E435F94FFC5B^0'
+'-B12DA44623837^0'
+'344546122A7166^0'
+'-213BD0BB99C996^-1'
+'-2032AC696EC84E^-1'
+'1438D680761589^0'
+'B653B021D52518^0'
+'-1C1FBA997D44D5^0'
+'B055052673C8F^0'
+'3445464A8C5EDA^0'
+'-213BA80FA07F7^-1'
+'-2032B1B29D0B3E^-1'
+'1F536AFD75^A'
+'1F536AFDD4F8F4^A'
+'1F536AFED4F8F4^A'
+'1F536AFFD4F8F4^A'
+'1F536B00D4F8F4^A'
+'1F536B01D4F8F4^A'
+'1F536B02D4F8F4^A'
+'1F536B03D4F8F4^A'
+'1F536B04D4F8F4^A'
+'1F536B05D4F8F4^A'
+'1F536B06D4F8F4^A'
+'1F536B07D4F8F4^A'
+'1F536B08D4F8F4^A'
+'1F536B09D4F8F4^A'
+'1F536B0AD4F8F4^A'
+'1F536B0BD4F8F4^A'
+'1F536B0CD4F8F4^A'
+'1F536B0DD4F8F4^A'
+'1F536B0ED4F8F4^A'
+'1F536B0FD4F8F4^A'
+'1F536B10D4F8F4^A'
+'1F536B11D4F8F4^A'
+'1F536B12D4F8F4^A'
+'1F536B13D4F8F4^A'
+'1F536B14D4F8F4^A'
+'1F536B15D4F8F4^A'
+'1F536B16D4F8F4^A'
+'1F536B17D4F8F4^A'
+'1F536B18D4F8F4^A'
+'1F536B19D4F8F4^A'
+'1F536B1AD4F8F4^A'
+'1F536B1BD4F8F4^A'
+'1F536B1CD4F8F4^A'
+'1F536B1DD4F8F4^A'
+'1F536B1ED4F8F4^A'
+'1F536B1FD4F8F4^A'
+'1F536B20D4F8F4^A'
+'1F536B21D4F8F4^A'
+'1F536B22D4F8F4^A'
+'1F536B23D4F8F4^A'
+'1F536B24D4F8F4^A'
+'1F536B25D4F8F4^A'
+'1F536B26D4F8F4^A'
+'1F536B27D4F8F4^A'
+'1F536B28D4F8F4^A'
+'1F536B29D4F8F4^A'
+'1F536B2AD4F8F4^A'
+'1F536B2BD4F8F4^A'
+'1F536B2CD4F8F4^A'
+'1F536B2DD4F8F4^A'
+'1F536B2ED4F8F4^A'
+'1F536B2FD4F8F4^A'
+'1F536B30D4F8F4^A'
+'1F536B31D4F8F4^A'
+'1F536B32D4F8F4^A'
+'1F536B33D4F8F4^A'
+'1F536B34D4F8F4^A'
+'1F536B35D4F8F4^A'
+'1F536B36D4F8F4^A'
+'1F536B37D4F8F4^A'
+'1F536B38D4F8F4^A'
+'1F536B39D4F8F4^A'
+'1F536B3AD4F8F4^A'
+'1F536B3BD4F8F4^A'
+'1F536B3CD4F8F4^A'
+'1F536B3DD4F8F4^A'
+'1F536B3ED4F8F4^A'
+'1F536B3FD4F8F4^A'
+'1F536B40D4F8F4^A'
+'1F536B41D4F8F4^A'
+'1F536B42D4F8F4^A'
+'1F536B43D4F8F4^A'
+'1F536B44D4F8F4^A'
+'1F536B45D4F8F4^A'
+'1F536B46D4F8F4^A'
+'1F536B47D4F8F4^A'
+'1F536B48D4F8F4^A'
+'1F536B49D4F8F4^A'
+'1F536B4AD4F8F4^A'
+'1F536B4BD4F8F4^A'
+'1F536B4CD4F8F4^A'
+'1F536B4DD4F8F4^A'
+'1F536B4ED4F8F4^A'
+'1F536B4FD4F8F4^A'
+'1F536B50D4F8F4^A'
+'1F536B51D4F8F4^A'
+'1F536B52D4F8F4^A'
+'1F536B53D4F8F4^A'
+'1F536B54D4F8F4^A'
+'1F536B55D4F8F4^A'
+'1F536B56D4F8F4^A'
+'1F536B57D4F8F4^A'
+'1F536B58D4F8F4^A'
+'1F536B5961^A'
+'1F536AFD75^A'
+'1^1'
+'5E^2'
+END_ARRAY 1 755
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/acpaquette/juno/JNCR_2016240_01M06152_V01_METHANE_0008.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_v12.tf b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_v12.tf
new file mode 100644
index 0000000000000000000000000000000000000000..58baa81cba461674d49c6f058a9b02375f1c9ca4
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/juno_v12.tf
@@ -0,0 +1,3695 @@
+KPL/FK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "juno_v12.tf"
+MISSION_NAME = JUNO
+SPACECRAFT_NAME = JUNO
+DATA_SET_ID = "JNO-J/E/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = FK
+PRODUCT_ID = "juno_v12.tf"
+PRODUCT_CREATION_TIME = 2017-08-25T15:25:37
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = JUPITER
+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 FK file defining reference frames the
+JUNO spacecraft, its structures, and science instruments, created by NAIF,
+JPL. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Juno Frames Kernel
+===============================================================================
+
+ This frame kernel contains complete set of frame definitions for the
+ Juno (JUNO) spacecraft, its structures and science instruments. This
+ frame kernel also contains name - to - NAIF ID mappings for JUNO
+ science instruments and s/c structures (see the last section of the
+ file.)
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ Version 1.2 -- June 24, 2017 -- Boris Semenov, NAIF
+
+ Updated the JUNO_JUNOCAM frame alignment based on [14].
+
+ Version 1.1 -- June 8, 2017 -- Boris Semenov, NAIF
+
+ Updated JUNO_JADE_* frame alignments based on [13].
+
+ Version 1.0 -- June 1, 2017 -- Boris Semenov, NAIF
+
+ Updated JUNO_UVS_BASE alignment angles per [12].
+
+ Added a warning about time-dependency of the JUNO_CHU*_TO_SC,
+ JUNO_MOB_*B_TO_SC, and JUNO_SC_TO_MOB_*B alignments to the
+ comments in their sections.
+
+ Version 0.9 -- September 8, 2016 -- Boris Semenov, NAIF
+
+ Added JUNO_MAG_VIP4, JUNO_JSS, JUNO_JSO, JUNO_JH, and
+ JUNO_SUN_EQU_RTN frames for magnetospheric studies at Jupiter
+ defined in [9].
+
+ Updated JUNO_CHU*_TO_FGM_*B and JUNO_MOB_*B_TO_FGM_*B alignments
+ based on [10].
+
+ Updated JUNO_CHU*_TO_SC, JUNO_MOB_*B_TO_SC, and JUNO_SC_TO_MOB_*B
+ alignments based on a quick comparison of CHU, MOB and S/C CKs
+ for January-March 2016 time period, then again based on
+ quick comparison for August 6-19, 2016 period.
+
+ Updated HGA alignment based on [11].
+
+ Version 0.8 -- November 5, 2014 -- Boris Semenov, NAIF
+
+ Redefined SRU frames according to [6]. Note that the updated
+ SRU frames are very different from those defined in the
+ earlier version of this kernel.
+
+ Version 0.7 -- September 16, 2014 -- Boris Semenov, NAIF
+
+ Updated JIRAM alignments based on the information provided by
+ Alessandro Mura, INAF-IAPS on September 9 and 16, 2014.
+
+ Version 0.6 -- September 17, 2013 -- Boris Semenov, NAIF
+
+ Corrected the rotation order in the JEDI_090 and JEDI_270 frame
+ definitions.
+
+ Added the JUNOCAM_CUBE frame; incorporated the JUNOCAM pre-launch
+ DCM and CCD twist into the JUNOCAM_CUBE and JUNOCAM frame
+ definitions.
+
+ Incorporated actual JIRAM alignments provided by Alberto Adriani,
+ INAF-IAPS on September 16, 2013.
+
+ Version 0.5 -- November 15, 2011 -- Boris Semenov, NAIF
+
+ Changed MAG frames:
+
+ -- added layers of "connection" fixed-offset frames
+ incorporating CHU? and MOB_?? to FGM_?? alignments
+ (CHU?_TO_FGM_??, MOB_??_TO_FGM_??, 6 frames), CHU? and
+ MOB_?? to spacecraft alignments (CHU?_TO_SC, MOB_??_TO_SC,
+ 6 frames), and spacecraft to MOB_?? alignments
+ (SC_TO_MOB_??, 2 frames)
+
+ Version 0.4 -- November 4, 2011 -- Boris Semenov, NAIF
+
+ Changed MAG frames and instrument names based on the calibration
+ reports and discussions with the MAG team as follows:
+
+ -- renamed ASC_CHU1 -> ASC_CHUD, ASC_CHU2 -> ASC_CHUC,
+ ASC_CHU3 -> ASC_CHUB, ASC_CHU4 -> ASC_CHUA
+
+ -- redefined MOB frames to have +Z between the directions of
+ CHU +Zs (s/c -Z)
+
+ -- redefined MOB_OB and CHUA/B frames to have +X along s/c -X and
+ MOB_IB and CHUC/D frames to have +X along s/c +X
+
+ -- redefined FGM_IB and FGM_OB frames to be CK-based with with
+ orientation provided by CKs relative to CHU*, MOB_*B or
+ J2000 frames
+
+ Version 0.3 -- September 1, 2010 -- Boris Semenov, NAIF
+
+ Changed MAG frames and instrument names based on review comments
+ by Jack Connerney as follows:
+
+ -- terminology change: in-bound -> inboard, out-bound ->
+ outboard
+
+ -- frame and instrument name change: ASC1 -> ASC_CHU1, ASC2 ->
+ ASC_CHU2, ASC3 -> ASC_CHU3, ASC4 -> ASC_CHU4
+
+ -- re-defined MOB_OB and MOB_IB frames to be co-aligned with
+ the FGM_OB and FGM_IB frames correspondingly
+
+ Version 0.2 -- July 13, 2009 -- Boris Semenov, NAIF
+
+ Re-defined JUNO_FGM_IB and JUNO_FGM_IB frames based on
+ the input from Jack Connerney.
+
+ Version 0.1 -- June 12, 2009 -- Boris Semenov, NAIF
+
+ Defined preliminary frames for all structures and instruments
+ based on CDR materials and draft MICDs.
+
+ Version 0.0 -- February 3, 2009 -- Boris Semenov, NAIF
+
+ Initial Release: bare-bones version with just two frames needed
+ to access JUNO nominal attitude CK file.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``C-Kernel Required Reading''
+
+ 4. JUNO Instrument ICDs and MICDs
+
+ 5. JUNO CDR Materials.
+
+ 6. JUNO-ME-11-5159_Pointing_Alignment Verification.xlsx
+
+ 7. Updated JIRAM alignment angles provided in the updated FK
+ ``juno_v02.corretto.new.2.tf'' by Alberto Adriani, INAF-IAPS on
+ September 16, 2013.
+
+ 8. E-mail ``Modifications to JUNO/JIRAM *tf and *ti kernel files.''
+ from Alessandro Mura, INAF-IAPS, September 9 and 16, 2014.
+
+ 9. ``Jupiter Coordinate Systems'', F. Bagenal & R. J. Wilson, LASP -
+ U of Colorado, TBD -- 07/15/16
+
+ 10. JN-DTU-TN-3105_v1_1_Juno_MAG_to_mASC_relative_orientation.pdf
+
+ 11. E-mail stating the measured HGA electrical boresight direction,
+ from Kristen Francis, LMCO to William Folkner, JPL, 09/07/16
+
+ 12. juno_v08rev_tkg.tf; modified FK used by the UVS team, SWRI;
+ provided by Brad Trantham on 05/31/17
+
+ 13. ANODE_LOOK_ELC_DEFL_NONE_V02.CSV and ANODE_LOOK_ION_DEFL_NONE_V02.CSV
+ from JNO-J/SW-JAD-3-CALIBRATED-V1.0, provided by Rob Wilson, LASP
+ on 05/25/17.
+
+ 14. E-mail from Mike Caplinger, MSSS re updated Junocam camera model,
+ 06/20/17
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Boris V. Semenov, NAIF/JPL, (818)-354-8136, bsemenov@spice.jpl.nasa.gov
+
+
+Implementation Notes
+-------------------------------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make
+ use of this frame kernel must ``load'' the kernel, normally during
+ program initialization. The SPICE routine FURNSH loads a kernel file
+ into the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name; ) -- FORTRAN
+ furnsh_c ( "frame_kernel_name" ); -- C
+ cspice_furnsh, frame_kernel_name -- IDL
+ cspice_furnsh( 'frame_kernel_name' ) -- MATLAB
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+JUNO Frames
+-------------------------------------------------------------------------------
+
+ The following JUNO frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== ===================== ============ =======
+
+ Frames for Magnetospheric Studies at Jupiter:
+ ---------------------------------------------
+ JUNO_MAG_VIP4 IAU_JUPITER FIXED -61952
+ JUNO_JSS J2000 DYNAMIC -61953
+ JUNO_JSO J2000 DYNAMIC -61954
+ JUNO_JH J2000 DYNAMIC -61955
+ JUNO_SUN_EQU_RTN J2000 DYNAMIC -61956
+
+ Spacecraft frame:
+ -----------------
+ JUNO_SPACECRAFT varies CK -61000
+ JUNO_SPIN_AXIS J2000 CK -61900
+
+ Magnetometer and ASC CHU frames:
+ --------------------------------
+ JUNO_ASC_CHUD J2000, SPACECRAFT CK -61111
+ JUNO_ASC_CHUC J2000, SPACECRAFT CK -61112
+ JUNO_MOB_IB J2000 CK -61113
+ JUNO_FGM_IB MOB_IB, CHUD, CHUC CK -61114
+
+ JUNO_ASC_CHUB J2000, SPACECRAFT CK -61121
+ JUNO_ASC_CHUA J2000, SPACECRAFT CK -61122
+ JUNO_MOB_OB J2000 CK -61123
+ JUNO_FGM_OB MOB_OB, CHUB, CHUA CK -61124
+
+ JUNO_CHUA_TO_FGM_OB CHUA FIXED -61131 (a)
+ JUNO_CHUB_TO_FGM_OB CHUB FIXED -61132 (b)
+ JUNO_CHUC_TO_FGM_IB CHUC FIXED -61133 (c)
+ JUNO_CHUD_TO_FGM_IB CHUD FIXED -61134 (d)
+ JUNO_MOB_OB_TO_FGM_OB MOB_OB FIXED -61135 (e)
+ JUNO_MOB_IB_TO_FGM_IB MOB_IB FIXED -61136 (f)
+
+ JUNO_CHUA_TO_SC CHUA FIXED -61141 (g)
+ JUNO_CHUB_TO_SC CHUB FIXED -61142 (h)
+ JUNO_CHUC_TO_SC CHUC FIXED -61143 (i)
+ JUNO_CHUD_TO_SC CHUD FIXED -61144 (j)
+ JUNO_MOB_OB_TO_SC MOB_OB FIXED -61145 (k)
+ JUNO_MOB_IB_TO_SC MOB_IB FIXED -61146 (l)
+
+ JUNO_SC_TO_MOB_OB SPACECRAFT FIXED -61155 (m)
+ JUNO_SC_TO_MOB_IB SPACECRAFT FIXED -61156 (n)
+
+ JADE Frames:
+ ------------
+ JUNO_JADE_E060 SPACECRAFT FIXED -61201
+ JUNO_JADE_E180 SPACECRAFT FIXED -61202
+ JUNO_JADE_E300 SPACECRAFT FIXED -61203
+ JUNO_JADE_I SPACECRAFT FIXED -61204
+
+ JEDI Frames:
+ ------------
+ JUNO_JEDI_090 SPACECRAFT FIXED -61301
+ JUNO_JEDI_A180 SPACECRAFT FIXED -61302
+ JUNO_JEDI_270 SPACECRAFT FIXED -61303
+
+ JIRAM Frames:
+ -------------
+ JUNO_JIRAM_URF SPACECRAFT FIXED -61401
+ JUNO_JIRAM_I JIRAM_URF FIXED -61410
+ JUNO_JIRAM_I_LBAND JIRAM_IMAGER FIXED -61411
+ JUNO_JIRAM_I_MBAND JIRAM_IMAGER FIXED -61412
+ JUNO_JIRAM_S JIRAM_IMAGER FIXED -61420
+
+ JUNOCAM Frames:
+ ---------------
+ JUNO_JUNOCAM_CUBE SPACECRAFT FIXED -61505
+ JUNO_JUNOCAM JUNOCAM_CUBE FIXED -61500
+
+ MWR Frames:
+ -----------
+ JUNO_MWR_A1 SPACECRAFT FIXED -61601
+ JUNO_MWR_A2 SPACECRAFT FIXED -61602
+ JUNO_MWR_A3 SPACECRAFT FIXED -61603
+ JUNO_MWR_A4 SPACECRAFT FIXED -61604
+ JUNO_MWR_A5 SPACECRAFT FIXED -61605
+ JUNO_MWR_A6 SPACECRAFT FIXED -61606
+
+ UVS Frames:
+ -----------
+ JUNO_UVS_BASE SPACECRAFT FIXED -61700
+ JUNO_UVS UVS_BASE CK -61701
+
+ WAVES Frames:
+ -----------
+ JUNO_WAVES_MSC SPACECRAFT FIXED -61810
+ JUNO_WAVES_ANTENNA SPACECRAFT FIXED -61820
+
+ Solar Array frames:
+ -------------------
+ JUNO_SA1_HINGE SPACECRAFT FIXED -61010
+ JUNO_SA1 SA1_HINGE CK -61011
+ JUNO_SA2_HINGE SPACECRAFT FIXED -61020
+ JUNO_SA2 SA2_HINGE CK -61021
+ JUNO_SA3_HINGE SPACECRAFT FIXED -61030
+ JUNO_SA3 SA3_HINGE CK -61031
+
+ Antenna frames:
+ ---------------
+ JUNO_HGA SPACECRAFT FIXED -61040
+ JUNO_MGA SPACECRAFT FIXED -61050
+ JUNO_LGA_FORWARD SPACECRAFT FIXED -61061
+ JUNO_LGA_AFT SPACECRAFT FIXED -61062
+ JUNO_LGA_TOROID SPACECRAFT FIXED -61063
+
+ ACS Sensor frames:
+ ------------------
+ JUNO_SRU1 SPACECRAFT FIXED -61071
+ JUNO_SRU2 SPACECRAFT FIXED -61072
+ JUNO_SSS1 SPACECRAFT FIXED -61073
+ JUNO_SSS2 SPACECRAFT FIXED -61074
+
+ Truster frames:
+ ---------------
+ JUNO_REM_FL1 SPACECRAFT FIXED -61081
+ JUNO_REM_FL2 SPACECRAFT FIXED -61082
+ JUNO_REM_FL3 SPACECRAFT FIXED -61083
+ JUNO_REM_FL4 SPACECRAFT FIXED -61084
+ JUNO_REM_FA1 SPACECRAFT FIXED -61085
+ JUNO_REM_FA2 SPACECRAFT FIXED -61086
+
+ JUNO_REM_RL1 SPACECRAFT FIXED -61091
+ JUNO_REM_RL2 SPACECRAFT FIXED -61092
+ JUNO_REM_RL3 SPACECRAFT FIXED -61093
+ JUNO_REM_RL4 SPACECRAFT FIXED -61094
+ JUNO_REM_RA1 SPACECRAFT FIXED -61095
+ JUNO_REM_RA2 SPACECRAFT FIXED -61096
+
+
+JUNO Frames Hierarchy
+-------------------------------------------------------------------------------
+
+ The diagram below shows the JUNO frames hierarchy:
+
+ JUNO_MAG_VIP4 JUNO_JSO JUNO_SUN_EQU_RTN
+ -------------- -------- ----------------
+ ^ ^ ^
+ |<-fxd |<-dyn dyn->|
+ | | |
+ | JUNO_JSS | JUNO_JH |
+ | -------- | ------- |
+ | ^ | ^ |
+ | |<-dyn | |<-dyn |
+ | | | | |
+ | | | "J2000" INERTIAL | |
+ +----------------------------------------------------------------+
+ | | | | | | | | | |
+ |<-pck | | | ck->| |<-ck | | | pck->|
+ | | | | | | | | | |
+ V | | | V | | | | V
+ "IAU_JUPITER" | | | "JUNO_SPIN_AXIS" | | | | "IAU_EARTH"
+ ------------- | | | ---------------- | | | | -----------
+ | | | | | | | |
+ ck->| | |<-ck ck->| | ck->| | |<-ck
+ | | | | | | | |
+ V | V | | V | V
+ "JUNO_ASC_CHUD" | "JUNO_ASC_CHUC" | | "JUNO_ASC_CHUB" | "JUNO_ASC_CHUA"
+ --------------- | --------------- | | --------------- | ---------------
+ | | | | | | | | | | | |
+ | | |<-ck | | | | | | |<-ck | |
+ | | | | | | | | | | | |
+ | | | | | | | | | | | |
+ | | | | | fxd | | fxd | | | | |
+ | | "(n)"<-----------------. | | .----------------->"(m)" | |
+ | | ----- | | | | | | | | | | ----- | |
+ | | | | | | ck | | | | ck | | | | | |
+ | | | | "(l)"-------. | | | | .-------"(k)" | | | |
+ | | | | ----- | | | | | | | | | | ----- | | | |
+ | | | | ^ | | | | | | | | | | ^ | | | |
+ | |ck>| |fx>| | | | | | | | | | | |<fx| |<ck| |
+ | | | | | | | | | | | | | | | | | | | |
+ | | V V | | | | | | | | | | V V | |
+ | | "JUNO_MOB_IB" | | | | | | | | | | "JUNO_MOB_OB" | |
+ | | ------------- | | | | | | | | | | ------------- | |
+ | | | | | | | | | | | | | | | |
+ | |<-fxd | fxd->| | | | | | | | | |<-fxd | fxd->| |
+ | | | | | | | | | | | | | | | |
+ | | fxd->| | | | | | | | | | | fxd->| | |
+ | | | | | | | | | | | | | | | |
+ | V V V | | | | | | | | V V v |
+ | "(d)" "(f)" "(c)" | | | | | | | | "(b)" "(e)" "(a)" |
+ | ----- ----- ----- | | | | | | | | ----- ----- ----- |
+ | | | | | | | | | | | | | | | |
+ | |<-ck | ck->| | | | | | | | | |<-ck | ck->| |
+ | | | | | | | | | | | | | | | |
+ | | |<-ck | | | | | | | | | | |<-ck | |
+ | | | | | | | | | | | | | | | |
+ | V V V | | | | | | | | V V V |
+ | "JUNO_FGM_IB" | | | | | | | | "JUNO_FGM_OB" |
+ | ------------- | | | | | | | | ------------- |
+ | | | | | | | | | |
+ | | | | | | | | | |
+ |<-fxd fxd->| | | | | | | |<-fxd fxd->|
+ | | | | | | | | | |
+ V V | | | | | | V V
+ "(j)" "(i)" | | | | | | "(h)" "(g)"
+ ----- ----- | | | | | | ----- -----
+ | | | | | | | | | |
+ |<-ck ck->| | | | | | | |<-ck |<-ck
+ | | | | | | | | | |
+ V V V | V V | V V V
+ "JUNO_SPACECRAFT"
+ +-----------------------------------------------------------------+
+ | | | | | | | | | | | | | |
+ fxd->| | | | | | | fxd->| | | | | | |
+ | | | | | | | | | | | | | |
+ V | | | | | | V | | | | | |
+ "JUNO_JADE_*" | | | | | | "JUNO_HGA" | | | | | |
+ ------------- | | | | | | ---------- | | | | | |
+ | | | | | | | | | | | |
+ fxd->| | | | | | fxd->| | | | | |
+ | | | | | | | | | | | |
+ V | | | | | V | | | | |
+ "JUNO_JEDI_*" | | | | | "JUNO_MGA" | | | | |
+ ------------- | | | | | ---------- | | | | |
+ | | | | | | | | | |
+ fxd->| | | | | fxd->| | | | |
+ | | | | | | | | | |
+ V | | | | V | | | |
+ "JUNO_JIRAM_URF" | | | | "JUNO_LGA_*" | | | |
+ ---------------- | | | | ------------ | | | |
+ | | | | | | | | |
+ fxd->| | | | | fxd->| | | |
+ | | | | | | | | |
+ V | | | | V | | |
+ "JUNO_JIRAM_S" | | | | "JUNO_REM_*" | | |
+ -------------- | | | | ------------ | | |
+ | | | | | | | |
+ fxd->| | | | |<-fxd fxd->| | |
+ | | | | | | | |
+ V | | | V V | |
+ "JUNO_JIRAM_I" | | | "JUNO_WAVES_*" "JUNO_SRU*" | |
+ -------------- | | | -------------- ----------- | |
+ | | | | | |
+ fxd->| | | |<-fxd fxd->| |
+ | | | | | |
+ V | | V V |
+ "JUNO_JIRAM_I_*BAND" | | "JUNO_UVS_BASE" "JUNO_SSS*" |
+ -------------------- | | --------------- ----------- |
+ | | | |
+ fxd->| | |<-ck fxd->|
+ | | | |
+ V | V V
+ "JUNO_JUNOCAM_CUBE" | "JUNO_UVS" "JUNO_SA*_HINGE"
+ ------------------- | ---------- ----------------
+ | | |
+ fxd->| | |
+ | | |
+ V | |
+ "JUNO_JUNOCAM" | |
+ -------------- | |
+ | |
+ fxd->| ck->|
+ | |
+ V V
+ "JUNO_MWR_A*" "JUNO_SA*"
+ ------------- ----------
+
+
+Spacecraft Orientation Frame Chains
+
+ Possible "J2000" -> "JUNO_SPACECRAFT" frame chains are:
+
+ -- using data from a nominal spacecraft CK:
+
+ "J2000"
+ -ck-> "JUNO_SPIN_AXIS"
+ -ck-> "JUNO_SPACECRAFT"
+
+ -- using data from a reconstructed spacecraft CK:
+
+ "J2000"
+ -ck-> "JUNO_SPACECRAFT"
+
+ -- using data from a reconstructed MOB_## CK, the MOB_##-to-S/C
+ alignment fixed-offset frame, and an alignment frame-to-s/c
+ "coverage" CK:
+
+ "J2000"
+ -ck-> "JUNO_MOB_##"
+ -fxd-> "JUNO_MOB_##_TO_SC"
+ -ck-> "JUNO_SPACECRAFT"
+
+ -- using data from a reconstructed CHU# CK, the CHU#-to-S/C
+ alignment fixed-offset frame, and an alignment frame-to-s/c
+ "coverage" CK:
+
+ "J2000"
+ -ck-> "JUNO_ASC_CHU#"
+ -fxd-> "JUNO_CHU#_TO_SC"
+ -ck-> "JUNO_SPACECRAFT"
+
+
+Magnetometer Sensor Frame Chains
+
+ Possible "J2000" -> "JUNO_FGM_IB" frame chains are (same for OB):
+
+ -- using data from a nominal spacecraft CK, the s/c-to-MOB_IB
+ alignment fixed-offset frame, an alignment frame-to-MOB_IB
+ "coverage" CK, the MOB_IB-to-FGM_IB alignment fixed-offset
+ frame, and an alignment-to-FGM_IB "coverage" CK:
+
+ "J2000"
+ -ck-> "JUNO_SPIN_AXIS"
+ -ck-> "JUNO_SPACECRAFT"
+ -fxd-> "JUNO_SC_TO_MOB_IB"
+ -ck-> "JUNO_MOB_IB"
+ -fxd-> "JUNO_MOB_IB_TO_FGM_IB"
+ -ck-> "JUNO_FGM_IB"
+
+ -- using data from a reconstructed spacecraft CK, the s/c-to-MOB_IB
+ alignment fixed-offset frame, an alignment frame-to-MOB_IB
+ "coverage" CK, the MOB_IB-to-FGM_IB alignment fixed-offset
+ frame, and an alignment-to-FGM_IB "coverage" CK:
+
+ "J2000"
+ -ck-> "JUNO_SPACECRAFT"
+ -fxd-> "JUNO_SC_TO_MOB_IB"
+ -ck-> "JUNO_MOB_IB"
+ -fxd-> "JUNO_MOB_IB_TO_FGM_IB"
+ -ck-> "JUNO_FGM_IB"
+
+ -- using data from a reconstructed MOB_IB CK, the MOB_IB-to-FGM_IB
+ alignment fixed-offset frame, and an alignment-to-FGM_IB
+ "coverage" CK:
+
+ "J2000"
+ -ck-> "JUNO_MOB_IB"
+ -fxd-> "JUNO_MOB_IB_TO_FGM_IB"
+ -ck-> "JUNO_FGM_IB"
+
+ -- using data from a reconstructed CHU# CK, the CHU#-to-FGM_IB
+ alignment fixed-offset frame, and an alignment-to-FGM_IB
+ "coverage" CK:
+
+ "J2000"
+ -ck-> "JUNO_ASC_CHU#"
+ -fxd-> "JUNO_CHU#_TO_FGM_IB"
+ -ck-> "JUNO_FGM_IB"
+
+
+Frames for Magnetospheric Studies at Jupiter
+-------------------------------------------------------------------------------
+
+ This section defines a few frames for magnetospheric studies at
+ Jupiter described in [9].
+
+
+Jupiter Magnetic VIP4 Frame
+
+ The JUNO_MAG_VIP4 frame implements the JUNO mission Jupiter
+ Magnetic VIP4 (MAG_VIP4) reference frame described in [9].
+
+ It is defined as a fixed offset frame with respect to the
+ IAU_JUPITER frame (which is equivalent to the System III right
+ handed frame when used with pck00010.tpc) as follows:
+
+ - +Z axis is along planetocentric LON=159.2 deg/LAT=80.5 deg in
+ in the IAU_JUPITER frame
+
+ - +Y axis is along planetocentric LON=249.2 deg/LAT=0 deg in
+ the IAU_JUPITER frame
+
+ - +X completes the right handed frame
+
+ - the center is at the center of Jupiter.
+
+ Two rotations are needed to align the IAU_JUPITER frame with the
+ JUNO_MAG_VIP4 frame: first by +159.2 degrees about Z, second by +9.5
+ degrees about Y.
+
+ The keywords below implement the JUNO_MAG_VIP4 frame. Since the
+ frame definition below contains the reverse transformation -- from
+ the JUNO_MAG_VIP4 frame to the IAU_JUPITER frame -- the order of
+ rotations is reversed and the signs of rotation angles are changed
+ to the opposite ones compared to the description above.
+
+ \begindata
+
+ FRAME_JUNO_MAG_VIP4 = -61952
+ FRAME_-61952_NAME = 'JUNO_MAG_VIP4'
+ FRAME_-61952_CLASS = 4
+ FRAME_-61952_CLASS_ID = -61952
+ FRAME_-61952_CENTER = 599
+ TKFRAME_-61952_SPEC = 'ANGLES'
+ TKFRAME_-61952_RELATIVE = 'IAU_JUPITER'
+ TKFRAME_-61952_ANGLES = ( 0, -159.2, -9.5 )
+ TKFRAME_-61952_AXES = ( 2, 3, 2 )
+ TKFRAME_-61952_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Jupiter-De-Spun-Sun Frame
+
+ The JUNO_JSS frame implements the JUNO mission Jupiter-De-Spun-Sun
+ (JSS) reference frame described in [9].
+
+ It is defined as a dynamic frame as follows:
+
+ - +Z axis is along the Jupiter north pole (+Z of the IAU_JUPITER
+ frame)
+
+ - +X axis is in the direction of the geometric position of the
+ Sun as seen from Jupiter
+
+ - +Y completes the right handed frame
+
+ - the center is at the center of Jupiter.
+
+ The keywords below implement the JUNO_JSS frame as a dynamic frame.
+
+ \begindata
+
+ FRAME_JUNO_JSS = -61953
+ FRAME_-61953_NAME = 'JUNO_JSS'
+ FRAME_-61953_CLASS = 5
+ FRAME_-61953_CLASS_ID = -61953
+ FRAME_-61953_CENTER = 599
+ FRAME_-61953_RELATIVE = 'J2000'
+ FRAME_-61953_DEF_STYLE = 'PARAMETERIZED'
+ FRAME_-61953_FAMILY = 'TWO-VECTOR'
+ FRAME_-61953_PRI_AXIS = 'Z'
+ FRAME_-61953_PRI_VECTOR_DEF = 'CONSTANT'
+ FRAME_-61953_PRI_FRAME = 'IAU_JUPITER'
+ FRAME_-61953_PRI_SPEC = 'RECTANGULAR'
+ FRAME_-61953_PRI_VECTOR = ( 0, 0, 1 )
+ FRAME_-61953_SEC_AXIS = 'X'
+ FRAME_-61953_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+ FRAME_-61953_SEC_OBSERVER = 'JUPITER'
+ FRAME_-61953_SEC_TARGET = 'SUN'
+ FRAME_-61953_SEC_ABCORR = 'NONE'
+
+ \begintext
+
+
+Jupiter-Sun-Orbit Frame
+
+ The JUNO_JSO frame implements the JUNO mission Jupiter-Sun-Orbit
+ (JSO) reference frame described in [9].
+
+ It is defined as a dynamic frame as follows:
+
+ - +X axis is along the geometric position of the Sun as seen
+ from Jupiter
+
+ - +Y axis is in the direction of the inertial geometric velocity
+ of the Sun as seen from Jupiter
+
+ - +Z completes the right handed frame
+
+ - the center is at the center of Jupiter.
+
+ The keywords below implement the JUNO_JSO frame as a dynamic frame.
+
+ \begindata
+
+ FRAME_JUNO_JSO = -61954
+ FRAME_-61954_NAME = 'JUNO_JSO'
+ FRAME_-61954_CLASS = 5
+ FRAME_-61954_CLASS_ID = -61954
+ FRAME_-61954_CENTER = 599
+ FRAME_-61954_RELATIVE = 'J2000'
+ FRAME_-61954_DEF_STYLE = 'PARAMETERIZED'
+ FRAME_-61954_FAMILY = 'TWO-VECTOR'
+ FRAME_-61954_PRI_AXIS = 'X'
+ FRAME_-61954_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+ FRAME_-61954_PRI_OBSERVER = 'JUPITER'
+ FRAME_-61954_PRI_TARGET = 'SUN'
+ FRAME_-61954_PRI_ABCORR = 'NONE'
+ FRAME_-61954_SEC_AXIS = 'Y'
+ FRAME_-61954_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY'
+ FRAME_-61954_SEC_OBSERVER = 'JUPITER'
+ FRAME_-61954_SEC_TARGET = 'SUN'
+ FRAME_-61954_SEC_ABCORR = 'NONE'
+ FRAME_-61954_SEC_FRAME = 'J2000'
+
+ \begintext
+
+
+Jupiter Heliospheric Frame
+
+ The JUNO_JH frame implements the JUNO mission Jupiter Heliospheric
+ (JH) reference frame described in [9].
+
+ It is defined as a dynamic frame as follows:
+
+ - +X axis is along the geometric position of the Sun as seen
+ from Jupiter
+
+ - +Z axis is in the direction of the Sun north pole.
+
+ - +Y completes the right handed frame
+
+ - the center is at the center of Jupiter.
+
+ The keywords below implement the JUNO_JH frame as a dynamic frame.
+
+ \begindata
+
+ FRAME_JUNO_JH = -61955
+ FRAME_-61955_NAME = 'JUNO_JH'
+ FRAME_-61955_CLASS = 5
+ FRAME_-61955_CLASS_ID = -61955
+ FRAME_-61955_CENTER = 599
+ FRAME_-61955_RELATIVE = 'J2000'
+ FRAME_-61955_DEF_STYLE = 'PARAMETERIZED'
+ FRAME_-61955_FAMILY = 'TWO-VECTOR'
+ FRAME_-61955_PRI_AXIS = 'X'
+ FRAME_-61955_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+ FRAME_-61955_PRI_OBSERVER = 'JUPITER'
+ FRAME_-61955_PRI_TARGET = 'SUN'
+ FRAME_-61955_PRI_ABCORR = 'NONE'
+ FRAME_-61955_SEC_AXIS = 'Z'
+ FRAME_-61955_SEC_VECTOR_DEF = 'CONSTANT'
+ FRAME_-61955_SEC_FRAME = 'IAU_SUN'
+ FRAME_-61955_SEC_SPEC = 'RECTANGULAR'
+ FRAME_-61955_SEC_VECTOR = ( 0, 0, 1 )
+
+ \begintext
+
+
+Juno Solar Equatorial RTN Frame
+
+ The JUNO_SUN_EQU_RTN frame implements the JUNO mission JUNO RTN
+ reference frame described in [9].
+
+ It is defined as a dynamic frame as follows:
+
+ - +X axis is along the geometric position of Juno as seen
+ from the Sun
+
+ - +Z axis is in the direction of the Sun north pole.
+
+ - +Y completes the right handed frame
+
+ - the center is at the JUNO spacecraft.
+
+ The keywords below implement the JUNO_SUN_EQU_RTN frame as a dynamic
+ frame.
+
+ \begindata
+
+ FRAME_JUNO_SUN_EQU_RTN = -61956
+ FRAME_-61956_NAME = 'JUNO_SUN_EQU_RTN'
+ FRAME_-61956_CLASS = 5
+ FRAME_-61956_CLASS_ID = -61956
+ FRAME_-61956_CENTER = -61
+ FRAME_-61956_RELATIVE = 'J2000'
+ FRAME_-61956_DEF_STYLE = 'PARAMETERIZED'
+ FRAME_-61956_FAMILY = 'TWO-VECTOR'
+ FRAME_-61956_PRI_AXIS = 'X'
+ FRAME_-61956_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+ FRAME_-61956_PRI_OBSERVER = 'SUN'
+ FRAME_-61956_PRI_TARGET = 'JUNO'
+ FRAME_-61956_PRI_ABCORR = 'NONE'
+ FRAME_-61956_SEC_AXIS = 'Z'
+ FRAME_-61956_SEC_VECTOR_DEF = 'CONSTANT'
+ FRAME_-61956_SEC_FRAME = 'IAU_SUN'
+ FRAME_-61956_SEC_SPEC = 'RECTANGULAR'
+ FRAME_-61956_SEC_VECTOR = ( 0, 0, 1 )
+
+ \begintext
+
+
+Spacecraft Bus Frame
+-------------------------------------------------------------------------------
+
+ The spacecraft frame (or AACS control frame) is defined by the s/c design
+ as follows [from 5]:
+
+ - +Z axis is along the nominal spin axis and points in the
+ direction of the nominal HGA boresight
+
+ - +X axis is along the solar array 1 symmetry axis and points
+ towards the magnetometer boom
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is centered on the launch vehicle
+ separation plane.
+
+ These diagrams illustrates the s/c frame:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ .-\
+ .-' \
+ .-' \ Solar Array 3
+ .-' \
+ \ .-'\
+ \ .-' \
+ \ ,-' \
+ \-' .-'\
+ \ .-' \
+ \ .-' \
+ \-' .-'\ <-. Spin Direction
+ \ .-' \ `.
+ \ .-' \.
+ \-' .-' `-.
+ \ .-' `-.
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | / | \ | | | |``--..
+ | ' | +Xsc | | | | `--..
+ | | o------> | | | | | |
+ | . +Zsc , | | | | ..--''
+ | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. .-'
+ / `-. .-'
+ /`-. /'
+ / `-. /
+ / `-. /
+ /`-. `-/
+ / `-. /
+ / `-. /
+ /`-. `-/
+ / `-. /
+ / `-. /
+ /. `-/
+ `-. / Solar Array 2 +Zsc is out of
+ `-. / the page.
+ `-. /
+ `
+
+
+ Spacecraft -Y side view:
+ ------------------------
+ o
+ / \
+ .-----------------, HGA
+ \ /
+ `. .'
+ `-------'
+ | | Magnetometer
+ | | Boom
+ ================o==o==o==o-----------o======o======o======o===========*
+ Solar | | | Solar Array 1
+ Array 2 | | |
+ | |
+ | |
+ | +Zsc ^ |
+ | | |
+ | | |
+ | | | +Ysc is into
+ `----- +Ysc x------> -' the page.
+ /_____\ +Xsc
+
+
+ Since the S/C bus attitude with respect to an inertial frame is provided
+ by a C kernel (see [3] for more information), this frame is defined as
+ a CK-based frame.
+
+ \begindata
+
+ FRAME_JUNO_SPACECRAFT = -61000
+ FRAME_-61000_NAME = 'JUNO_SPACECRAFT'
+ FRAME_-61000_CLASS = 3
+ FRAME_-61000_CLASS_ID = -61000
+ FRAME_-61000_CENTER = -61
+ CK_-61000_SCLK = -61
+ CK_-61000_SPK = -61
+
+ \begintext
+
+
+Spin Axis Frame
+-------------------------------------------------------------------------------
+
+
+ The JUNO_SPIN_AXIS frame is a special frame used in the nominal
+ orientation CK files. In these files the JUNO_SPACECRAFT frame
+ orientation is not stored relative to the J2000 frame. Instead it is
+ "decomposed" into two orientations: the nominal spin axis
+ orientation captured in the segments providing the orientation of
+ the JUNO_SPIN_AXIS frame relative to the J2000 frame and the nominal
+ rotation about the spin axis captured in the segments providing the
+ orientation of the JUNO_SPACECRAFT frame relative to the
+ JUNO_SPIN_AXIS frame.
+
+ JUNO_SPIN_AXIS is defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_JUNO_SPIN_AXIS = -61900
+ FRAME_-61900_NAME = 'JUNO_SPIN_AXIS'
+ FRAME_-61900_CLASS = 3
+ FRAME_-61900_CLASS_ID = -61900
+ FRAME_-61900_CENTER = -61
+ CK_-61900_SCLK = -61
+ CK_-61900_SPK = -61
+
+ \begintext
+
+
+Magnetometer Frames
+-------------------------------------------------------------------------------
+
+ The set of frames for the Magnetometer experiment includes
+
+ - two fluxgate magnetometer (FGM) frames (JUNO_FGM_IB and
+ JUNO_FGM_OB)
+
+ - two magnetometer optical bench (MOB) frames (JUNO_MOB_IB and
+ JUNO_MOB_OB)
+
+ - four Advanced Stellar Compass (ASC) Camera Head Unit (CHU)
+ frames (JUNO_ASC_CHUA, JUNO_ASC_CHUB, JUNO_ASC_CHUC, and
+ JUNO_ASC_CHUD.
+
+ The set also includes an additional set of fixed-offset frames
+ incorporating relative alignment data for
+
+ - FGM_## relative to CHU# (JUNO_CHU#_TO_FGM_##)
+
+ - FGM_## relative to MOB_## (JUNO_MOB_##_TO_FGM_##)
+
+ - spacecraft relative to CHU# (JUNO_CHU#_TO_SC)
+
+ - spacecraft relative to MOB_## (JUNO_MOB_##_TO_SC)
+
+ - MOB_## relative to spacecraft (JUNO_SC_TO_MOB_##)
+
+ The "alignment" frames facilitate the ability to easily change the
+ values of alignments and to switch different alignment sets by
+ storing alignments directly in the FK (instead of CKs) while using
+ "coverage" CKs to store zero-offset rotations from these alignment
+ frames to the desired structure frames by simply constraining
+ coverages available to SPICE.
+
+
+FGM Frames
+
+ The FGM frames -- JUNO_FGM_IB and JUNO_FGM_OB -- are the frames with
+ respect to which the FGM sensors were calibrated. These frames are
+ defined by the orthogonal faces of the alignment cubes mounted on
+ the optical benches as follows:
+
+ - +Z axis is the normal to the top side of the alignment cube
+ (the side parallel to the optical bench plane) and pointing
+ away from the bench; nominally points in the same direction as
+ the s/c +Z axis.
+
+ - +X axis is the normal to the side of the cube facing the FGM
+ sensor mounted on the bench; for OB FGM nominally points in
+ the same direction as the s/c +X axis, for IB FGM nominally
+ points in the same direction as the s/c -X axis
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is in the geometric center of the FGM
+ enclosures
+
+ The OB FGM frame is nominally co-aligned with the spacecraft frame.
+
+ The IB FGM frame is nominally rotated from the spacecraft frame by
+ 180 degrees about Z.
+
+ This diagram illustrates the FGM frames:
+
+ Spacecraft -Z side view:
+ ------------------------
+
+
+ Magnetometer Boom
+
+ /```---...
+ | ```---.. +Yfgm_ib
+ | ^ .
+ | | ```---...
+ | | CHUD CHUB...
+ +Zsc +Xsc | .-|--@. .@----.| +Xfgm_ob
+ x------> | <------x @ | | @ x------>
+ | | +Xfgm_ib `----@' `@--|-'|
+ | | CHUC CHUA'''|
+ | | ...---''' |
+ v | /''' V
+ +Ysc | ...---'''\ / +Yfgm_ob
+ \...---''' ---
+
+
+ +Zsc, +Zfgm_ib, +Zfgm_ob,
+ are into the page.
+
+
+ The FGM frames are defined as CK-based frames because their
+ orientation can be provided with respect to either one of the CHU
+ frames (of the two CHUs mounted on the bench) or with respect to the
+ bench's MOB frame.
+
+ \begindata
+
+ FRAME_JUNO_FGM_IB = -61114
+ FRAME_-61114_NAME = 'JUNO_FGM_IB'
+ FRAME_-61114_CLASS = 3
+ FRAME_-61114_CLASS_ID = -61114
+ FRAME_-61114_CENTER = -61
+ CK_-61114_SCLK = -61
+ CK_-61114_SPK = -61
+
+ FRAME_JUNO_FGM_OB = -61124
+ FRAME_-61124_NAME = 'JUNO_FGM_OB'
+ FRAME_-61124_CLASS = 3
+ FRAME_-61124_CLASS_ID = -61124
+ FRAME_-61124_CENTER = -61
+ CK_-61124_SCLK = -61
+ CK_-61124_SPK = -61
+
+ \begintext
+
+
+MOB Frames
+
+ The MOB frames -- JUNO_MOB_IB and JUNO_MOB_OB -- are the principal
+ optical bench orientation frames. These frames are not tied to a
+ particular physical feature but are instead defined by two vectors
+ that are the sum and the difference of the boresight directions of
+ the two CHUs mounted on each bench:
+
+ - +Z axis is along the vector that is the sum of the CHU
+ boresight directions (CHUA + CHUB for OB, CHUD + CHUC for IB)
+
+ - +Y axis is along the vector that is the difference of the
+ boresight directions (CHUA - CHUB for OB, CHUD - CHUC for IB)
+
+ - +X axis completes the right-handed frame
+
+ - the origin of the frame is between the focal points of the two
+ CHUs whose boresights define the frame.
+
+ The OB MOB frame is nominally rotated from the s/c frame by 180
+ degrees about X, then by 180 degrees about Z.
+
+ The IB MOB nominally rotated from the s/c frame by 180 degrees about
+ X.
+
+ This diagram illustrates the MOB frames:
+
+ Spacecraft -Z side view:
+ ------------------------
+
+
+ Magnetometer Boom
+
+ /```---... ___
+ | ```---.../ \ +Ymob_ib
+ | \..^
+ | |```---...
+ | | CHUD CHUB...
+ +Zsc +Xsc | .---|@. +X .@----..
+ x------> | FGM_IB | @ o-----> <-----o @ ||FGM_OB
+ | | `----@' +X `@|---''
+ | | CHUC CHUA'|'
+ | | ...---''' |
+ v | /''' V
+ +Ysc | ...---'''\ / +Ymob_ob
+ \...---''' ---
+
+ +Zsc is into the page.
+
+ +Zmob_ib, and +Zmob_ob
+ are out of the page.
+
+
+ The MOB frames are defined as CK-based frames because their
+ orientation is provided in CKs with respect to the J2000 frame.
+
+ \begindata
+
+ FRAME_JUNO_MOB_IB = -61113
+ FRAME_-61113_NAME = 'JUNO_MOB_IB'
+ FRAME_-61113_CLASS = 3
+ FRAME_-61113_CLASS_ID = -61113
+ FRAME_-61113_CENTER = -61
+ CK_-61113_SCLK = -61
+ CK_-61113_SPK = -61
+
+ FRAME_JUNO_MOB_OB = -61123
+ FRAME_-61123_NAME = 'JUNO_MOB_OB'
+ FRAME_-61123_CLASS = 3
+ FRAME_-61123_CLASS_ID = -61123
+ FRAME_-61123_CENTER = -61
+ CK_-61123_SCLK = -61
+ CK_-61123_SPK = -61
+
+ \begintext
+
+
+CHU frames
+
+ The ASC CHU frames -- JUNO_ASC_CHUA, JUNO_ASC_CHUB, JUNO_ASC_CHUC,
+ and JUNO_ASC_CHUD -- are defined as follows:
+
+ - +Z axis is along the boresight
+
+ - +X axis is along the sensor side roughly aligned with the cable
+ direction, pointing away from the cable side.
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the CHU's focal point
+
+ The mapping between CHUs and their telemetry designations (0-3) is
+ as follows:
+
+ CHUA (-61122) -> TLM "0"
+ CHUB (-61121) -> TLM "1"
+ CHUC (-61112) -> TLM "2"
+ CHUD (-61111) -> TLM "3"
+
+ These diagrams illustrate the ASC CHU frames:
+
+ Spacecraft -Z side view:
+ ------------------------
+
+
+ Magnetometer Boom
+ /```---... ___
+ | ```---.../ \ ^ +YchuD
+ | \...|
+ | ^ +YchuC
+ | CHUD | ```- CHUB
+ +Zsc +Xsc | .--- o----> <----o----..
+ x------> | FGM_IB| @ @|| +X +X ||@ @ ||FGM_OB
+ | | `--- o----> <----o----''
+ | | CHUC ...| CHUA
+ | | ...- +YchuB V
+ v | /''' |
+ +Ysc | ...---'''\ / +YchuA V
+ \...---''' ---
+
+ +Zsc is into the page.
+
+ +Zchu1, +Zchu2, +Zchu3, and +Zchu4
+ are out of the page, inclined at
+ ~13 degrees.
+
+ This diagram illustrates all magnetometer frames together.
+
+ Spacecraft +X side view:
+ ------------------------
+
+
+ Outboard Bench Inboard Bench
+ -------------- -------------
+
+ +Z +Z +Z
+ ^ ^ ^
+ | | |
+ | FGM_OB | S/C FGM_IB |
+ +X +Y | | | +Y +X
+ x------> o------> o------> <------x <------o
+ | +X +Y +X +Y +Y +X |
+ | MOB_OB MOB_IB |
+ | |
+ v v
+ +Z +Z
+ .> +Y +Y <.
+ +X .-' `-. +X
+ +X x x' CHUA `o o +X
+ / `-. \ / .-' \
+ / `> \ CHUD / <' \
+ / CHUB +Y \ / +Y CHUC \
+ v v v v
+ +Z +Z +Z +Z
+
+ /<--------|-------->\ /<--------|-------->\
+ 13 deg | 13 deg 13 deg | 13 deg
+
+
+
+ +Xs of s/c, FGM_OB, MOB_IB, CHUC, and CHUD are out of the page.
+ +Xs of FGM_IB, MOB_OB, CHUA, and CHUB are into the page.
+
+
+ The ASC CHU frames are defined as CK-based frames because their
+ orientation is provided either with respect to the J2000 frame,
+ based on the CHU's attitude solution, or with respect to the
+ spacecraft frame, based on the in-flight relative alignment
+ calibration.
+
+ \begindata
+
+ FRAME_JUNO_ASC_CHUD = -61111
+ FRAME_-61111_NAME = 'JUNO_ASC_CHUD'
+ FRAME_-61111_CLASS = 3
+ FRAME_-61111_CLASS_ID = -61111
+ FRAME_-61111_CENTER = -61
+ CK_-61111_SCLK = -61
+ CK_-61111_SPK = -61
+
+ FRAME_JUNO_ASC_CHUC = -61112
+ FRAME_-61112_NAME = 'JUNO_ASC_CHUC'
+ FRAME_-61112_CLASS = 3
+ FRAME_-61112_CLASS_ID = -61112
+ FRAME_-61112_CENTER = -61
+ CK_-61112_SCLK = -61
+ CK_-61112_SPK = -61
+
+ FRAME_JUNO_ASC_CHUB = -61121
+ FRAME_-61121_NAME = 'JUNO_ASC_CHUB'
+ FRAME_-61121_CLASS = 3
+ FRAME_-61121_CLASS_ID = -61121
+ FRAME_-61121_CENTER = -61
+ CK_-61121_SCLK = -61
+ CK_-61121_SPK = -61
+
+ FRAME_JUNO_ASC_CHUA = -61122
+ FRAME_-61122_NAME = 'JUNO_ASC_CHUA'
+ FRAME_-61122_CLASS = 3
+ FRAME_-61122_CLASS_ID = -61122
+ FRAME_-61122_CENTER = -61
+ CK_-61122_SCLK = -61
+ CK_-61122_SPK = -61
+
+ \begintext
+
+
+Alignment Frames
+
+ In the FK versions 0.5 (November 2011) to 0.8 (up to April 2016)
+ the JUNO_CHU#_TO_FGM_## frames below incorporated the following CHU#
+ to FGM_## alignments based on the "Micro Advanced Stellar Compass
+ JUNO Reference Cube Calibration Test Report"
+ (JN-DTU-TR-3008_v1_0_ref_cube_calibration_report-2.pdf):
+
+ --------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ --------------------------------------------------------
+ FGM_OB -> CHUA 166.98004591 0.83914744 -179.77479685
+ FGM_OB -> CHUB -167.65012849 0.22864645 -179.36168926
+ FGM_IB -> CHUC -166.89008185 0.16658654 179.10988258
+ FGM_IB -> CHUD 166.92526364 0.41005034 178.56549108
+ --------------------------------------------------------
+
+ These alignments were derived by creating the transformation
+ matrices from the CHU# frames to the FGM frames that have their +X
+ axes (primary axes) along the vectors that are the negative of the
+ measured optical cube X side normals given in the CHU# frames and
+ their +Y axes (plane defining axes) along the vectors that are the
+ measured optical cube Y side normals given in the CHU# frames.
+
+ These angles were provided in the frame definitions using the
+ following keywords:
+
+ tkframe_-61131_angles = ( 166.98004591, 0.83914744, -179.77479685 )
+ tkframe_-61132_angles = ( -167.65012849, 0.22864645, -179.36168926 )
+ tkframe_-61133_angles = ( -166.89008185, 0.16658654, 179.10988258 )
+ tkframe_-61134_angles = ( 166.92526364, 0.41005034, 178.56549108 )
+
+
+ Starting with the FK version 0.9 (April 2016)
+ the JUNO_CHU#_TO_FGM_## frames below incorporate the following CHU#
+ to FGM_## alignments from [10] table 4:
+
+ --------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ --------------------------------------------------------
+ FGM_OB -> CHUA 166.981554 0.867687 -179.789384
+ FGM_OB -> CHUB -167.680175 0.231891 -179.384575
+ FGM_IB -> CHUC -166.964941 0.211558 179.078816
+ FGM_IB -> CHUD 166.887958 0.457271 178.543535
+ --------------------------------------------------------
+
+ \begindata
+
+ FRAME_JUNO_CHUA_TO_FGM_OB = -61131
+ FRAME_-61131_NAME = 'JUNO_CHUA_TO_FGM_OB'
+ FRAME_-61131_CLASS = 4
+ FRAME_-61131_CLASS_ID = -61131
+ FRAME_-61131_CENTER = -61
+ TKFRAME_-61131_SPEC = 'ANGLES'
+ TKFRAME_-61131_RELATIVE = 'JUNO_ASC_CHUA'
+ TKFRAME_-61131_ANGLES = ( 166.981554, 0.867687, -179.789384 )
+ TKFRAME_-61131_AXES = ( 1, 2, 3 )
+ TKFRAME_-61131_UNITS = 'DEGREES'
+
+ FRAME_JUNO_CHUB_TO_FGM_OB = -61132
+ FRAME_-61132_NAME = 'JUNO_CHUB_TO_FGM_OB'
+ FRAME_-61132_CLASS = 4
+ FRAME_-61132_CLASS_ID = -61132
+ FRAME_-61132_CENTER = -61
+ TKFRAME_-61132_SPEC = 'ANGLES'
+ TKFRAME_-61132_RELATIVE = 'JUNO_ASC_CHUB'
+ TKFRAME_-61132_ANGLES = ( -167.680175, 0.231891, -179.384575 )
+ TKFRAME_-61132_AXES = ( 1, 2, 3 )
+ TKFRAME_-61132_UNITS = 'DEGREES'
+
+ FRAME_JUNO_CHUC_TO_FGM_IB = -61133
+ FRAME_-61133_NAME = 'JUNO_CHUC_TO_FGM_IB'
+ FRAME_-61133_CLASS = 4
+ FRAME_-61133_CLASS_ID = -61133
+ FRAME_-61133_CENTER = -61
+ TKFRAME_-61133_SPEC = 'ANGLES'
+ TKFRAME_-61133_RELATIVE = 'JUNO_ASC_CHUC'
+ TKFRAME_-61133_ANGLES = ( -166.964941, 0.211558, 179.078816 )
+ TKFRAME_-61133_AXES = ( 1, 2, 3 )
+ TKFRAME_-61133_UNITS = 'DEGREES'
+
+ FRAME_JUNO_CHUD_TO_FGM_IB = -61134
+ FRAME_-61134_NAME = 'JUNO_CHUD_TO_FGM_IB'
+ FRAME_-61134_CLASS = 4
+ FRAME_-61134_CLASS_ID = -61134
+ FRAME_-61134_CENTER = -61
+ TKFRAME_-61134_SPEC = 'ANGLES'
+ TKFRAME_-61134_RELATIVE = 'JUNO_ASC_CHUD'
+ TKFRAME_-61134_ANGLES = ( 166.887958, 0.457271, 178.543535 )
+ TKFRAME_-61134_AXES = ( 1, 2, 3 )
+ TKFRAME_-61134_UNITS = 'DEGREES'
+
+ \begintext
+
+ In the FK versions 0.5 (November 2011) to 0.8 (up to April 2016)
+ the JUNO_MOB_##_TO_FGM_## frames below incorporated the following
+ MOB_## to FGM_## alignments based on the "Micro Advanced Stellar
+ Compass JUNO Reference Cube Calibration Test Report"
+ (JN-DTU-TR-3008_v1_0_ref_cube_calibration_report-2.pdf):
+
+ -----------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ -----------------------------------------------------------
+ FGM_OB -> MOB_OB 179.65236785 0.57188198 179.06999179
+ FGM_IB -> MOB_IB -179.98504194 0.35177733 178.31458807
+ -----------------------------------------------------------
+
+ These angles were provided in the frame definitions using the
+ following keywords:
+
+ tkframe_-61135_angles = ( 179.65236785, 0.57188198, 179.06999179 )
+ tkframe_-61136_angles = ( -179.98504194, 0.35177733, 178.31458807 )
+
+
+ Starting with the FK version 0.9 (April 2016)
+ the JUNO_CHU#_TO_FGM_## frames below incorporate the following CHU#
+ to FGM_## alignments based on [10]:
+
+ -----------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ -----------------------------------------------------------
+ FGM_OB -> MOB_OB 179.63717677 0.58603721 178.99314287
+ FGM_IB -> MOB_IB 179.95841684 0.39617415 178.28125011
+ -----------------------------------------------------------
+
+ These alignments were derived by creating the transformation
+ matrices from the FGM_## frames to the MOB_## frames that have their
+ +Z axes (primary axes) along the sums of a particular MOB's CHU#
+ boresight vectors and their +Y axes (plane defining axes) along the
+ differences of a particular MOB's CHU# boresight vectors.
+
+ \begindata
+
+ FRAME_JUNO_MOB_OB_TO_FGM_OB = -61135
+ FRAME_-61135_NAME = 'JUNO_MOB_OB_TO_FGM_OB'
+ FRAME_-61135_CLASS = 4
+ FRAME_-61135_CLASS_ID = -61135
+ FRAME_-61135_CENTER = -61
+ TKFRAME_-61135_SPEC = 'ANGLES'
+ TKFRAME_-61135_RELATIVE = 'JUNO_MOB_OB'
+ TKFRAME_-61135_ANGLES = ( 179.63717677, 0.58603721, 178.99314287 )
+ TKFRAME_-61135_AXES = ( 1, 2, 3 )
+ TKFRAME_-61135_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MOB_IB_TO_FGM_IB = -61136
+ FRAME_-61136_NAME = 'JUNO_MOB_IB_TO_FGM_IB'
+ FRAME_-61136_CLASS = 4
+ FRAME_-61136_CLASS_ID = -61136
+ FRAME_-61136_CENTER = -61
+ TKFRAME_-61136_SPEC = 'ANGLES'
+ TKFRAME_-61136_RELATIVE = 'JUNO_MOB_IB'
+ TKFRAME_-61136_ANGLES = ( 179.95841684, 0.39617415, 178.28125011 )
+ TKFRAME_-61136_AXES = ( 1, 2, 3 )
+ TKFRAME_-61136_UNITS = 'DEGREES'
+
+ \begintext
+
+ In the FK versions 0.5 (November 2011) to 0.8 (up to April 2016)
+ the JUNO_CHU#_TO_SC frames below incorporated the following CHU# to
+ SC alignments based on a quick comparison of the CHU and s/c
+ orientations during the ASC turn-on activity on August 25, 2011:
+
+ -------------------------------------------------------
+ Rot3 Z Rot2 Y Rot1 X
+ -------------------------------------------------------
+ S/C->CHUA 179.215 0.207 -167.634
+ S/C->CHUB 178.862 -0.010 167.032
+ S/C->CHUC -0.724 -0.633 -166.482
+ S/C->CHUD -0.460 -0.608 167.377
+ -------------------------------------------------------
+
+ These angles were provided in the frame definitions using the
+ following keywords:
+
+ tkframe_-61141_angles = ( 179.215, 0.207, -167.634 )
+ tkframe_-61142_angles = ( 178.862, -0.010, 167.032 )
+ tkframe_-61143_angles = ( -0.724, -0.633, -166.482 )
+ tkframe_-61144_angles = ( -0.460, -0.608, 167.377 )
+
+
+ Starting with the FK version 0.9, draft 2 (April 2016)
+ the JUNO_CHU#_TO_SC frames below incorporate the following CHU# to
+ SC alignments based on a quick comparison of the CHU and s/c
+ orientations during January-March 2016:
+
+ -------------------------------------------------------
+ Rot3 Z Rot2 Y Rot1 X
+ -------------------------------------------------------
+ S/C->CHUA 178.970 1.290 -167.630
+ S/C->CHUB 179.100 1.065 167.035
+ S/C->CHUC -0.980 0.375 -166.475
+ S/C->CHUD -0.240 0.400 167.385
+ -------------------------------------------------------
+
+ These angles were provided in the frame definitions using the
+ following keywords:
+
+ tkframe_-61141_angles = ( 178.970, 1.290, -167.630 )
+ tkframe_-61142_angles = ( 179.100, 1.065, 167.035 )
+ tkframe_-61143_angles = ( -0.980, 0.375, -166.475 )
+ tkframe_-61144_angles = ( -0.240, 0.400, 167.385 )
+
+ Starting with the FK version 0.9, draft 5 (August 2016)
+ the JUNO_CHU#_TO_SC frames below incorporate the following CHU# to
+ SC alignments based on a quick comparison of the CHU and s/c
+ orientations for August 6-19, 2016:
+
+ -------------------------------------------------------
+ Rot3 Z Rot2 Y Rot1 X
+ -------------------------------------------------------
+ S/C->CHUA 178.950 1.370 -167.635
+ S/C->CHUB 179.125 1.150 167.035
+ S/C->CHUC -1.000 0.480 -166.480
+ S/C->CHUD -0.220 0.510 167.380
+ -------------------------------------------------------
+
+ WARNING: the fixed alignments below are just a snapshot of the actual
+ alignments at a particular point in time. The actual alignments proved
+ to be significantly varying due a temperature-dependent solar array
+ flexing, both during cruise and during orbital operations, with the
+ Y rotation changing back and forth by as much as 0.08 deg during each
+ peri-jove pass. Because of this variability the frames below and any
+ frame chains containing them should NOT be used in science data
+ analysis.
+
+ \begindata
+
+ FRAME_JUNO_CHUA_TO_SC = -61141
+ FRAME_-61141_NAME = 'JUNO_CHUA_TO_SC'
+ FRAME_-61141_CLASS = 4
+ FRAME_-61141_CLASS_ID = -61141
+ FRAME_-61141_CENTER = -61
+ TKFRAME_-61141_SPEC = 'ANGLES'
+ TKFRAME_-61141_RELATIVE = 'JUNO_ASC_CHUA'
+ TKFRAME_-61141_ANGLES = ( 178.950, 1.370, -167.635 )
+ TKFRAME_-61141_AXES = ( 3, 2, 1 )
+ TKFRAME_-61141_UNITS = 'DEGREES'
+
+ FRAME_JUNO_CHUB_TO_SC = -61142
+ FRAME_-61142_NAME = 'JUNO_CHUB_TO_SC'
+ FRAME_-61142_CLASS = 4
+ FRAME_-61142_CLASS_ID = -61142
+ FRAME_-61142_CENTER = -61
+ TKFRAME_-61142_SPEC = 'ANGLES'
+ TKFRAME_-61142_RELATIVE = 'JUNO_ASC_CHUB'
+ TKFRAME_-61142_ANGLES = ( 179.125, 1.150, 167.035 )
+ TKFRAME_-61142_AXES = ( 3, 2, 1 )
+ TKFRAME_-61142_UNITS = 'DEGREES'
+
+ FRAME_JUNO_CHUC_TO_SC = -61143
+ FRAME_-61143_NAME = 'JUNO_CHUC_TO_SC'
+ FRAME_-61143_CLASS = 4
+ FRAME_-61143_CLASS_ID = -61143
+ FRAME_-61143_CENTER = -61
+ TKFRAME_-61143_SPEC = 'ANGLES'
+ TKFRAME_-61143_RELATIVE = 'JUNO_ASC_CHUC'
+ TKFRAME_-61143_ANGLES = ( -1.000, 0.480, -166.480 )
+ TKFRAME_-61143_AXES = ( 3, 2, 1 )
+ TKFRAME_-61143_UNITS = 'DEGREES'
+
+ FRAME_JUNO_CHUD_TO_SC = -61144
+ FRAME_-61144_NAME = 'JUNO_CHUD_TO_SC'
+ FRAME_-61144_CLASS = 4
+ FRAME_-61144_CLASS_ID = -61144
+ FRAME_-61144_CENTER = -61
+ TKFRAME_-61144_SPEC = 'ANGLES'
+ TKFRAME_-61144_RELATIVE = 'JUNO_ASC_CHUD'
+ TKFRAME_-61144_ANGLES = ( -0.220, 0.510, 167.380 )
+ TKFRAME_-61144_AXES = ( 3, 2, 1 )
+ TKFRAME_-61144_UNITS = 'DEGREES'
+
+ \begintext
+
+ In the FK versions 0.5 (November 2011) to 0.8 (up to April 2016)
+ the JUNO_MOB_##_TO_SC and JUNO_SC_TO_MOB_## frames below incorporated
+ the following MOB_## to SC alignments based on a quick comparison of
+ the CHU and s/c orientations during the ASC turn-on activity on
+ August 25, 2011:
+
+ -------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ -------------------------------------------------------
+ SC -> MOB_OB -179.69984062 0.10355166 179.50575594
+ SC -> MOB_IB -179.55188944 0.63655035 0.06025323
+ -------------------------------------------------------
+
+ -------------------------------------------------------
+ Rot3 Z Rot2 Y Rot1 X
+ -------------------------------------------------------
+ MOB_OB -> SC -179.50575594 -0.10355166 179.69984062
+ MOB_IB -> SC -0.06025323 -0.63655035 179.55188944
+ -------------------------------------------------------
+
+ These angles were provided in the frame definitions using the
+ following keywords:
+
+ tkframe_-61145_angles = ( -179.69984062, 0.10355166, 179.50575594 )
+ tkframe_-61146_angles = ( -179.55188944, 0.63655035, 0.06025323 )
+ tkframe_-61155_angles = ( -179.50575594, -0.10355166, 179.69984062 )
+ tkframe_-61156_angles = ( -0.06025323, -0.63655035, 179.55188944 )
+
+
+ Starting with the FK version 0.9, draft 2 (April 2016)
+ the JUNO_MOB_##_TO_SC and JUNO_SC_TO_MOB_## frames below incorporate
+ the following MOB_## to SC alignments based on a quick comparison of
+ the CHU and s/c orientations during January-March 2016:
+
+ -------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ -------------------------------------------------------
+ SC -> MOB_OB -179.71273540 1.20947262 179.49305746
+ SC -> MOB_IB -179.54535339 -0.39823128 0.05211686
+ -------------------------------------------------------
+
+ -------------------------------------------------------
+ Rot3 Z Rot2 Y Rot1 X
+ -------------------------------------------------------
+ MOB_OB -> SC -179.49305746 -1.20947262 179.71273540
+ MOB_IB -> SC -0.05211686 0.39823128 179.54535339
+ -------------------------------------------------------
+
+ These angles were provided in the frame definitions using the
+ following keywords:
+
+ tkframe_-61145_angles = ( -179.71273540, 1.20947262, 179.49305746 )
+ tkframe_-61146_angles = ( -179.54535339, -0.39823128, 0.05211686 )
+ tkframe_-61155_angles = ( -179.49305746, -1.20947262, 179.71273540 )
+ tkframe_-61156_angles = ( -0.05211686, 0.39823128, 179.54535339 )
+
+
+ Starting with the FK version 0.9, draft 5 (August 2016)
+ the JUNO_MOB_##_TO_SC and JUNO_SC_TO_MOB_## frames below incorporate
+ the following MOB_## to SC alignments based on a quick comparison of
+ the CHU and s/c orientations for August 6-19, 2016:
+
+ -------------------------------------------------------
+ Rot3 X Rot2 Y Rot1 Z
+ -------------------------------------------------------
+ SC -> MOB_OB -179.71070379 1.29397715 179.50482902
+ SC -> MOB_IB -179.55054081 -0.50866857 0.06234192
+ -------------------------------------------------------
+
+ -------------------------------------------------------
+ Rot3 Z Rot2 Y Rot1 X
+ -------------------------------------------------------
+ MOB_OB -> SC -179.50482902 -1.29397715 179.71070379
+ MOB_IB -> SC -0.06234192 0.50866857 179.55054081
+ -------------------------------------------------------
+
+ These alignments were derived by creating the transformation
+ matrices from the SC frame to the MOB_## frames that have their +Z
+ axes (primary axes) along the sums of a particular MOB's CHU#
+ boresight vectors and their +Y axes (plane defining axes) along the
+ differences of a particular MOB's CHU# boresight vectors.
+
+ WARNING: the fixed alignments below are just a snapshot of the actual
+ alignments at a particular point in time. The actual alignments proved
+ to be significantly varying due a temperature-dependent solar array
+ flexing, both during cruise and during orbital operations, with the
+ Y rotation changing back and forth by as much as 0.08 deg during each
+ peri-jove pass. Because of this variability the frames below and any
+ frame chains containing them should NOT be used in science data
+ analysis.
+
+ \begindata
+
+ FRAME_JUNO_MOB_OB_TO_SC = -61145
+ FRAME_-61145_NAME = 'JUNO_MOB_OB_TO_SC'
+ FRAME_-61145_CLASS = 4
+ FRAME_-61145_CLASS_ID = -61145
+ FRAME_-61145_CENTER = -61
+ TKFRAME_-61145_SPEC = 'ANGLES'
+ TKFRAME_-61145_RELATIVE = 'JUNO_MOB_OB'
+ TKFRAME_-61145_ANGLES = ( -179.71070379, 1.29397715, 179.50482902 )
+ TKFRAME_-61145_AXES = ( 1, 2, 3 )
+ TKFRAME_-61145_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MOB_IB_TO_SC = -61146
+ FRAME_-61146_NAME = 'JUNO_MOB_IB_TO_SC'
+ FRAME_-61146_CLASS = 4
+ FRAME_-61146_CLASS_ID = -61146
+ FRAME_-61146_CENTER = -61
+ TKFRAME_-61146_SPEC = 'ANGLES'
+ TKFRAME_-61146_RELATIVE = 'JUNO_MOB_IB'
+ TKFRAME_-61146_ANGLES = ( -179.55054081, -0.50866857, 0.06234192 )
+ TKFRAME_-61146_AXES = ( 1, 2, 3 )
+ TKFRAME_-61146_UNITS = 'DEGREES'
+
+ FRAME_JUNO_SC_TO_MOB_OB = -61155
+ FRAME_-61155_NAME = 'JUNO_SC_TO_MOB_OB'
+ FRAME_-61155_CLASS = 4
+ FRAME_-61155_CLASS_ID = -61155
+ FRAME_-61155_CENTER = -61
+ TKFRAME_-61155_SPEC = 'ANGLES'
+ TKFRAME_-61155_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61155_ANGLES = ( -179.50482902, -1.29397715, 179.71070379 )
+ TKFRAME_-61155_AXES = ( 3, 2, 1 )
+ TKFRAME_-61155_UNITS = 'DEGREES'
+
+ FRAME_JUNO_SC_TO_MOB_IB = -61156
+ FRAME_-61156_NAME = 'JUNO_SC_TO_MOB_IB'
+ FRAME_-61156_CLASS = 4
+ FRAME_-61156_CLASS_ID = -61156
+ FRAME_-61156_CENTER = -61
+ TKFRAME_-61156_SPEC = 'ANGLES'
+ TKFRAME_-61156_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61156_ANGLES = ( -0.06234192, 0.50866857, 179.55054081 )
+ TKFRAME_-61156_AXES = ( 3, 2, 1 )
+ TKFRAME_-61156_UNITS = 'DEGREES'
+
+ \begintext
+
+
+JADE Frames
+-------------------------------------------------------------------------------
+
+ The set of frames for the JADE experiment includes three Electron
+ Sensor frames -- JUNO_JADE_E060, JUNO_JADE_E180, and JUNO_JADE_E300
+ -- and one Ion Sensor frame -- JUNO_JADE_I.
+
+ The JADE Elector Sensor frames -- JUNO_JADE_E060, JUNO_JADE_E180, and
+ JUNO_JADE_E300 -- are fixed w.r.t. to the spacecraft and defined as
+ follows:
+
+ - +Z axis is normal to the plane between upper and lower
+ entrance deflectors ("principal" plane) and points away from
+ the sensor base
+
+ - +X axis is in the "principal" plane nominally points towards the
+ center of the sensor FOV
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the intersection of the "principal"
+ plane and the sensor symmetry axis.
+
+ This diagram illustrates the JADE Electron sensor frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3
+ ~ ~ ~ ~ ~ ~ ~ ~
+ \ .-' \ +Xe060
+ \-' .-'\ ^ <-. Spin Direction
+ \ .-' / `.
+ \ .-' <. /
+ \-' +Ye060 `-. /
+ \ .-' `o.+Ze060
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | \ | | | |``--..
+ +Xe180 +Ze180 | +Xsc | | | | `--..
+ <------o o------> | | | | | |
+ | . +Zsc , | | | | ..--''
+ | \ / | | | |..--'
+ | \ HGA / | | | Magnetometer
+ V . `. .' .> -------------------' Boom
+ +Ye180 `-. ` ----- ' .-' +Ye300
+ / `- +Ze300 o'
+ / `-. .-' \
+ /`-. /' \
+ / `-. / \
+ / `-. / v
+ /`-. `-/ +Xe300
+ /~ ~ ~ ~ ~ ~ ~ ~ +Zsc, +Zje060, +Zje180,
+ Solar Array 2 +Zje300 are out of
+ the page.
+
+ As seen on the diagram the JUNO_JADE_E060, JUNO_JADE_E180, and
+ JUNO_JADE_E300 frames are nominally rotated from the spacecraft
+ frame by +60, 180 and -60 degrees about +Z axis correspondingly.
+ These nominal rotations were provided in the FK versions 0.0-1.0
+ as
+
+ tkframe_-61201_angles = ( -60.0, 0.0, 0.0 )
+ tkframe_-61201_axes = ( 3, 2, 1 )
+
+ tkframe_-61202_angles = ( 180.0, 0.0, 0.0 )
+ tkframe_-61202_axes = ( 3, 2, 1 )
+
+ tkframe_-61203_angles = ( 60.0, 0.0, 0.0 )
+ tkframe_-61203_axes = ( 3, 2, 1 )
+
+ Based on the JADE_E* anode look directions from [13], the
+ JUNO_JADE_E060 frame is rotated from the spacecraft frame first by
+ +60 deg about Z then by +0.35 deg about Y, JUNO_JADE_E180 -- first
+ by 180 deg about Z then by +0.48 deg about Y, and JUNO_JADE_E300 --
+ first by -60 degrees about Z then by +0.34 deg about Y.
+
+ Since the frame definitions below contains the reverse
+ transformations -- from the JADE Electron Sensor frames to the
+ spacecraft frame -- the order of rotations is reversed and the signs
+ of rotation angles are changed to the opposite ones compared to the
+ description above.
+
+ \begindata
+
+ FRAME_JUNO_JADE_E060 = -61201
+ FRAME_-61201_NAME = 'JUNO_JADE_E060'
+ FRAME_-61201_CLASS = 4
+ FRAME_-61201_CLASS_ID = -61201
+ FRAME_-61201_CENTER = -61
+ TKFRAME_-61201_SPEC = 'ANGLES'
+ TKFRAME_-61201_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61201_ANGLES = ( -60.0, -0.35, 0.0 )
+ TKFRAME_-61201_AXES = ( 3, 2, 1 )
+ TKFRAME_-61201_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JADE_E180 = -61202
+ FRAME_-61202_NAME = 'JUNO_JADE_E180'
+ FRAME_-61202_CLASS = 4
+ FRAME_-61202_CLASS_ID = -61202
+ FRAME_-61202_CENTER = -61
+ TKFRAME_-61202_SPEC = 'ANGLES'
+ TKFRAME_-61202_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61202_ANGLES = ( 180.0, -0.48, 0.0 )
+ TKFRAME_-61202_AXES = ( 3, 2, 1 )
+ TKFRAME_-61202_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JADE_E300 = -61203
+ FRAME_-61203_NAME = 'JUNO_JADE_E300'
+ FRAME_-61203_CLASS = 4
+ FRAME_-61203_CLASS_ID = -61203
+ FRAME_-61203_CENTER = -61
+ TKFRAME_-61203_SPEC = 'ANGLES'
+ TKFRAME_-61203_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61203_ANGLES = ( 60.0, -0.34, 0.0 )
+ TKFRAME_-61203_AXES = ( 3, 2, 1 )
+ TKFRAME_-61203_UNITS = 'DEGREES'
+
+ \begintext
+
+ The JADE Ion Sensor frame -- JUNO_JADE_I -- is fixed w.r.t. to the
+ spacecraft and defined as follows:
+
+ - +Z axis is normal to the plane between upper and lower
+ entrance deflectors ("principal" plane) and points away from
+ the anode
+
+ - +X axis is in the "principal" plane nominally points towards the
+ center of the sensor FOV
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the intersection of the "principal"
+ plane and the sensor symmetry axis.
+
+ This diagram illustrates the JADE Ion sensor frame:
+
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ ~ `.
+ \ .-' \.
+ \-' .-' `-.
+ \ .-' `-.
+ (45 deg above \ .-' ----- . `-. Solar Array 1
+ the page) .-' +Ysc ^ `. `-.--------------------.
+ +Xi ..@ / | \ | | | |
+ <-'' |\ | \ | | | |``--..
+ +Yi | \ | +Xsc | | | | `--..
+ (45 deg below |15\ o------> | | | | | |
+ the page) | v +Zsc , | | | | ..--''
+ | +Zi / | | | |..--'
+ | HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. .-'
+ / `-. .-'
+ /`-. /'
+ ~ ~ ~ ~ ~ ~ ~ ~ +Zsc is out of
+ Solar Array 2 the page.
+
+
+ As seen on the diagram the JUNO_JADE_I frame is nominally rotated
+ from the spacecraft first by -75 degrees about +Z, then by +90
+ degrees about +Y, then by -135 degrees about +Z.
+
+ Based on the JADE_I* anode look directions from [13], the nominal
+ orientation described above has been used for JADE_I observation
+ geometry computations.
+
+ Since the frame definitions below contains the reverse
+ transformation -- from the JADE Ion Sensor frame to the spacecraft
+ frame -- the order of rotations is reversed and the signs of
+ rotation angles are changed to the opposite ones compared to the
+ description above.
+
+ \begindata
+
+ FRAME_JUNO_JADE_I = -61204
+ FRAME_-61204_NAME = 'JUNO_JADE_I'
+ FRAME_-61204_CLASS = 4
+ FRAME_-61204_CLASS_ID = -61204
+ FRAME_-61204_CENTER = -61
+ TKFRAME_-61204_SPEC = 'ANGLES'
+ TKFRAME_-61204_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61204_ANGLES = ( 75.0, -90.0, 135.0 )
+ TKFRAME_-61204_AXES = ( 3, 2, 3 )
+ TKFRAME_-61204_UNITS = 'DEGREES'
+
+ \begintext
+
+
+JEDI Frames
+-------------------------------------------------------------------------------
+
+ The set of frames for the JEDI experiment includes three JEDI Sensor
+ frames -- JUNO_JEDI_090, JUNO_JEDI_A180, and JUNO_JEDI_270, -- fixed
+ w.r.t. to the spacecraft and defined as follows:
+
+ - +Z axis is along the sensor head symmetry axis, pointing away
+ from the sensor electronics box
+
+ - +X axis is in the FOV center plane, nominally pointing towards
+ the center of the full (160 x 12) sensor FOV
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the intersection of the FOV
+ center plane and the sensor head symmetry axis.
+
+ Note that for the JEDI/090 and JEDI/270 sensors the frame is as
+ defined in the JEDI MICD. For the JEDI/A180 sensor the frame is not
+ as defined in the JEDI MICD: it is rotated by -90 degrees about +X
+ to align the +Z axis with the sensor's symmetry axis.
+
+ This diagram illustrates the JEDI sensor frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3
+ ~ ~ ~ ~ ~ ~ ~ ~
+ \ .-' \ +X090
+ \ .-' \ ^
+ \-' .-'\ | <-. Spin Direction
+ \ \ | `.
+ \ . +Y090 \ |
+ \-' <------o +Z090
+ \ .- `-.
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | / | \ | | | |``--..
+ | ' | +Xsc | | | | `--..
+ o------> | | | | | |
+ +Xa180 +Ya180 +Zsc , | | | | ..--''
+ <------x / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ | . `. .' .-'--------------------' Boom
+ | `-. ` ----- ' .-'
+ V +Z270 .-'
+ +Za180 -. o------> +X090 and +X270 are out
+ / | +Y270 of the page, ~10 degrees
+ / `-. / | above the s/c XY plane.
+ / `-. / |
+ /`-. `-/ V +Z090 and +Z270 are out
+ / `-. / +X270 of the page, tilted by ~13
+ ~ ~ ~ ~ ~ ~ ~ ~ degrees towards the s/c +Z axis.
+ Solar Array 2
+ +Y090 is out of the page,
+ ~8 deg above the s/c XY plane.
+
+ +Y270 is into the page,
+ ~8 deg below the s/c XY plane.
+
+ +Yja180 is into the page.
+
+ +Zsc is out of the page.
+
+ The JUNO_JEDI_090 frame is nominally rotated from the spacecraft
+ frame first by +90 degrees about +Z, then by +8 degrees about +X,
+ then by -10 degrees about +Y.
+
+ The JUNO_JEDI_A180 frame is nominally rotated from the spacecraft
+ frame first by 180 degrees about +Z, then by -90 degrees about +X.
+
+ The JUNO_JEDI_270 frame is nominally rotated from the spacecraft
+ frame first by -90 degrees about +Z, then by -8 degrees about +X,
+ then by -10 degrees about +Y.
+
+ Since the frame definitions below contains the reverse
+ transformations -- from the JEDI Sensor frames to the spacecraft
+ frame -- the order of rotations is reversed and the signs of
+ rotation angles are changed to the opposite ones compared to the
+ description above.
+
+ \begindata
+
+ FRAME_JUNO_JEDI_090 = -61301
+ FRAME_-61301_NAME = 'JUNO_JEDI_090'
+ FRAME_-61301_CLASS = 4
+ FRAME_-61301_CLASS_ID = -61301
+ FRAME_-61301_CENTER = -61
+ TKFRAME_-61301_SPEC = 'ANGLES'
+ TKFRAME_-61301_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61301_ANGLES = ( -90.0, -8.0, 10.0 )
+ TKFRAME_-61301_AXES = ( 3, 1, 2 )
+ TKFRAME_-61301_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JEDI_A180 = -61302
+ FRAME_-61302_NAME = 'JUNO_JEDI_A180'
+ FRAME_-61302_CLASS = 4
+ FRAME_-61302_CLASS_ID = -61302
+ FRAME_-61302_CENTER = -61
+ TKFRAME_-61302_SPEC = 'ANGLES'
+ TKFRAME_-61302_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61302_ANGLES = ( 180.0, 0.0, 90.0 )
+ TKFRAME_-61302_AXES = ( 3, 2, 1 )
+ TKFRAME_-61302_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JEDI_270 = -61303
+ FRAME_-61303_NAME = 'JUNO_JEDI_270'
+ FRAME_-61303_CLASS = 4
+ FRAME_-61303_CLASS_ID = -61303
+ FRAME_-61303_CENTER = -61
+ TKFRAME_-61303_SPEC = 'ANGLES'
+ TKFRAME_-61303_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61303_ANGLES = ( 90.0, 8.0, 10.0 )
+ TKFRAME_-61303_AXES = ( 3, 1, 2 )
+ TKFRAME_-61303_UNITS = 'DEGREES'
+
+ \begintext
+
+
+JIRAM Frames:
+-------------------------------------------------------------------------------
+
+ The set of frames for the JIRAM experiment includes the unit
+ reference frame (URF) -- JUNO_JIRAM_URF, -- the imager and
+ spectrometer frames -- JUNO_JIRAM_I and JUNO_JIRAM_S, -- and the
+ imager L-band and M-band channel frames -- JUNO_JIRAM_I_LBAND and
+ JUNO_JIRAM_I_MBAND. This set of frames does not attempt to account
+ for the de-spinning mirror motion and assumes that the de-spinning
+ compensation results in effectively inertially fixed instrument
+ pointing for a given observation.
+
+ The JIRAM unit reference frame -- JUNO_JIRAM_URF -- is the JIRAM
+ "hardware" frame. It is fixed w.r.t. to the spacecraft and is
+ defined as follows:
+
+ - +Z axis is normal to the JIRAM optical head base, points from
+ the base towards the spacecraft, and is nominally co-aligned
+ with the spacecraft +Z axis;
+
+ - +X axis is along the nominal FOV center axis
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at center of the JIRAM optical
+ head reference mounting hole.
+
+ This diagram illustrates the JIRAM unit reference frame:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ ~ `.
+ \ .-' \.
+ -. \-' .-' `-.
+ ` +Xurf \ .-' `-.
+ 22 <-. \ .-' ----- . `-. Solar Array 1
+ deg `-. .-' +Ysc ^ `. `-.--------------------.
+ --- `o / | \ | | | |
+ /|+Zurf | \ | | | |``--..
+ / | ' | +Xsc | | | | `--..
+ / | | o------> | | | | | |
+ V | . +Zsc , | | | | ..--''
+ +Yurf | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. .-'
+ / `-. .-'
+ /`-. /'
+ ~ ~ ~ ~ ~ ~ ~ ~
+ Solar Array 2 +Zurf and +Zsc are out of
+ the page.
+
+ As seen on the diagram the JUNO_JIRAM_URF frame is nominally rotated
+ from the spacecraft frame by +158 degrees about +Z.
+
+ Since the frame definition below contain the reverse transformation
+ -- from the JIRAM unit reference frame to the spacecraft frame --
+ the order of rotations is reversed and the signs of rotation angles
+ are changed to the opposite ones compared to the description above.
+
+ \begindata
+
+ FRAME_JUNO_JIRAM_URF = -61401
+ FRAME_-61401_NAME = 'JUNO_JIRAM_URF'
+ FRAME_-61401_CLASS = 4
+ FRAME_-61401_CLASS_ID = -61401
+ FRAME_-61401_CENTER = -61
+ TKFRAME_-61401_SPEC = 'ANGLES'
+ TKFRAME_-61401_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61401_ANGLES = ( -158.0, 0.0, 0.0 )
+ TKFRAME_-61401_AXES = ( 3, 2, 1 )
+ TKFRAME_-61401_UNITS = 'DEGREES'
+
+ \begintext
+
+ The JIRAM imager and spectrometer frames -- JUNO_JIRAM_I and
+ JUNO_JIRAM_S, -- and the imager L-band and M-band channel frames --
+ JUNO_JIRAM_I_LBAND and JUNO_JIRAM_I_MBAND -- are the "image" frames
+ defined as follows:
+
+ - +Z axis is along the boresight (view direction of the center
+ pixel of the spectrometer line, combined imager CCD or individual
+ L-band and M-band CCDs);
+
+ - +X axis is along the CCD columns (spectral direction of the
+ spectrometer), pointing in the "along-track" direction resulting
+ from the spacecraft rotation
+
+ - +Y axis completes the right-handed frame, pointing along the
+ spatial spectrometer direction.
+
+ - the origin of the frame is the instrument's focal point.
+
+ This diagram illustrates the spectrometer and imager frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ ~ `.
+ \ .-' \.
+ ' .-' `-.
+ +Zs/i/m/l .-' `-.
+ <-. .-' ----- . `-. Solar Array 1
+ `-. .-' +Ysc ^ `. `-.--------------------.
+ `o / | \ | | | |
+ /|+Ys/i/m/l | \ | | | |``--..
+ / | ' | +Xsc | | | | `--..
+ / | | o------> | | | | | |
+ V | . +Zsc , | | | | ..--''
+ +Xs/i/m/l | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. .-'
+ / `-. .-'
+ /`-. /'
+ ~ ~ ~ ~ ~ ~ ~ ~
+ Solar Array 2 +Ys/i/m/l and +Zsc are out of
+ the page.
+
+ The spectrometer frame is defined w.r.t. to the unit reference
+ frame; the imager frame is defined w.r.t. to the spectrometer frame;
+ the imager L-band and M-band channel frames are defined w.r.t. to
+ the imager frame.
+
+ Based on [7] the JIRAM spectrometer frame is rotated from the unit
+ reference frame first by +90 degrees about +Y, then by +90 degrees
+ about +Z, then by +6.125 degrees about +Y.
+
+ The JIRAM imager frame is rotated from the spectrometer frame by
+ +0.22689 degrees about +Y.
+
+ The JIRAM imager L-band frame is rotated from the imager frame by
+ +0.96257 degrees (1/2 of L-band CCD) about +Y.
+
+ The JIRAM imager M-band frame is rotated from the imager frame by
+ -0.93507 degrees (1/2 of M-band CCD) about +Y.
+
+ The rotation angles above were used in the FK version 0.6 and were
+ incorporated into the frame definitions using the following
+ keywords:
+
+ TKFRAME_-61420_ANGLES = ( -90.0, -90.0, -6.125 )
+ TKFRAME_-61410_ANGLES = ( 0.0, -0.22689, 0.0 )
+ TKFRAME_-61411_ANGLES = ( 0.0, -0.96257, 0.0 )
+ TKFRAME_-61412_ANGLES = ( 0.0, +0.93507, 0.0 )
+
+
+ Based on [8], which provided a summary of alignment changes that
+ resulted from star and Moon calibrations and from correcting pixel
+ offsets between detector and band centers, the JIRAM spectrometer
+ frame is rotated from the unit reference frame first by +90.063
+ degrees about +Y, then by +90 degrees about +Z, then by +6.2765
+ degrees about +Y.
+
+ The JIRAM imager frame is rotated from the spectrometer frame by
+ +0.23844 degrees about +Y due to 17.5 pixel offset between the
+ center of spectrometer and imager.
+
+ The JIRAM imager L-band frame is rotated from the imager frame by
+ +0.94012 degrees (1/2 of L-band CCD) about +Y due to 69 pixel offset
+ between L center and I center.
+
+ The JIRAM imager M-band frame is rotated from the imager frame by
+ -0.94012 degrees (1/2 of M-band CCD) about +Y due to 69 pixel offset
+ between M center and I center.
+
+ Since the frame definitions below contain the reverse
+ transformations, the order of rotations is reversed and the signs of
+ rotation angles are changed to the opposite ones compared to the
+ description above.
+
+ \begindata
+
+ FRAME_JUNO_JIRAM_S = -61420
+ FRAME_-61420_NAME = 'JUNO_JIRAM_S'
+ FRAME_-61420_CLASS = 4
+ FRAME_-61420_CLASS_ID = -61420
+ FRAME_-61420_CENTER = -61
+ TKFRAME_-61420_SPEC = 'ANGLES'
+ TKFRAME_-61420_RELATIVE = 'JUNO_JIRAM_URF'
+ TKFRAME_-61420_ANGLES = ( -90.063, -90.0, -6.2765 )
+ TKFRAME_-61420_AXES = ( 2, 3, 2 )
+ TKFRAME_-61420_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JIRAM_I = -61410
+ FRAME_-61410_NAME = 'JUNO_JIRAM_I'
+ FRAME_-61410_CLASS = 4
+ FRAME_-61410_CLASS_ID = -61410
+ FRAME_-61410_CENTER = -61
+ TKFRAME_-61410_SPEC = 'ANGLES'
+ TKFRAME_-61410_RELATIVE = 'JUNO_JIRAM_S'
+ TKFRAME_-61410_ANGLES = ( 0.0, -0.23844, 0.0 )
+ TKFRAME_-61410_AXES = ( 3, 2, 1 )
+ TKFRAME_-61410_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JIRAM_I_LBAND = -61411
+ FRAME_-61411_NAME = 'JUNO_JIRAM_I_LBAND'
+ FRAME_-61411_CLASS = 4
+ FRAME_-61411_CLASS_ID = -61411
+ FRAME_-61411_CENTER = -61
+ TKFRAME_-61411_SPEC = 'ANGLES'
+ TKFRAME_-61411_RELATIVE = 'JUNO_JIRAM_I'
+ TKFRAME_-61411_ANGLES = ( 0.0, -0.94012, 0.0 )
+ TKFRAME_-61411_AXES = ( 3, 2, 1 )
+ TKFRAME_-61411_UNITS = 'DEGREES'
+
+ FRAME_JUNO_JIRAM_I_MBAND = -61412
+ FRAME_-61412_NAME = 'JUNO_JIRAM_I_MBAND'
+ FRAME_-61412_CLASS = 4
+ FRAME_-61412_CLASS_ID = -61412
+ FRAME_-61412_CENTER = -61
+ TKFRAME_-61412_SPEC = 'ANGLES'
+ TKFRAME_-61412_RELATIVE = 'JUNO_JIRAM_I'
+ TKFRAME_-61412_ANGLES = ( 0.0, +0.94012, 0.0 )
+ TKFRAME_-61412_AXES = ( 3, 2, 1 )
+ TKFRAME_-61412_UNITS = 'DEGREES'
+
+ \begintext
+
+
+JUNOCAM Frames
+-------------------------------------------------------------------------------
+
+ The JUNOCAM frame -- JUNO_JUNOCAM -- is fixed w.r.t. to the
+ spacecraft and defined as follows:
+
+ - +Z axis is along the camera boresight;
+
+ - +X axis is along the CCD lines, pointing in the increasing
+ pixel direction
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the camera focal point.
+
+ This diagram illustrates the JUNOCAM frame:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ ~ `.
+ \ .-' \.
+ \-' .-' `-.
+ \ .-' `-.
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | / | \ | | | |``--..
+ ' | +Xsc | | | | `--..
+ +Xjc | o------> | | | | | |
+ <------x . +Zsc , | | | | ..--''
+ +Zjc | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ | . `. .' .-'--------------------' Boom
+ V `-. ` ----- ' .-'
+ / +Yjc `-. .-'
+ / `-. .-' +Xjc is into
+ /`-. /' the page.
+ ~ ~ ~ ~ ~ ~ ~ ~
+ Solar Array 2 +Zsc is out of
+ the page.
+
+ As seen on the diagram the JUNO_JUNOCAM frame is nominally rotated
+ from the spacecraft frame first by 180 degrees about +Z, then by +90
+ degrees about +Y.
+
+ In order to incorporate the pre-launch calibrated misalignment
+ between the spacecraft frame and JUNOCAM optical cube, specified in
+ [6] as
+
+ DCM - SMRF to JUNOCam (*)
+
+ -0.0059163 -0.0142817 -0.9998805
+ 0.0023828 -0.9998954 0.0142678
+ -0.9999797 -0.0022981 0.0059497
+
+ (*) Measured from the instrument alignment cube.
+ No correction from cube axes to instrument axes
+
+ and the pre-launch calibrated misalignment between optical cube and
+ the CCD specified in [6] as CW rotation by 0.69 degrees about +Z
+ axis of the camera frame as two separate rotations, an additional
+ frame -- JUNO_JUNOCAM_CUBE -- was added between the JUNO_SPACECRAFT
+ frame and the JUNO_JUNOCAM frame in the FK ver. 0.6. The rotation
+ between these two frames was implemented in FKs up to ver. 1.1 using
+ these keywords:
+
+ tkframe_-61500_axes = ( 3, 2, 1 )
+ tkframe_-61500_angles = ( 0.69, 0.0, 0.0 )
+
+ Based on the initial reanalysis of Junocam cruise star imaging (per
+ [14]) the angles aligning the JUNO_JUNOCAM_CUBE frame with the
+ JUNO_JUNOCAM frame were changed to: the first rotation by -0.69
+ degrees about Z, the second rotation by +0.469 degrees about Y, and
+ the third rotation by -0.583 degrees about X.
+
+ The JUNO_JUNOCAM_CUBE misalignment from [6] and the JUNO_JUNOCAM
+ from [14] are incorporated in the two frame definitions below.
+
+ \begindata
+
+ FRAME_JUNO_JUNOCAM_CUBE = -61505
+ FRAME_-61505_NAME = 'JUNO_JUNOCAM_CUBE'
+ FRAME_-61505_CLASS = 4
+ FRAME_-61505_CLASS_ID = -61505
+ FRAME_-61505_CENTER = -61
+ TKFRAME_-61505_SPEC = 'MATRIX'
+ TKFRAME_-61505_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61505_MATRIX = (
+ -0.0059163 -0.0142817 -0.9998805
+ 0.0023828 -0.9998954 0.0142678
+ -0.9999797 -0.0022981 0.0059497
+ )
+
+ FRAME_JUNO_JUNOCAM = -61500
+ FRAME_-61500_NAME = 'JUNO_JUNOCAM'
+ FRAME_-61500_CLASS = 4
+ FRAME_-61500_CLASS_ID = -61500
+ FRAME_-61500_CENTER = -61
+ TKFRAME_-61500_SPEC = 'ANGLES'
+ TKFRAME_-61500_RELATIVE = 'JUNO_JUNOCAM_CUBE'
+ TKFRAME_-61500_ANGLES = ( 0.69, -0.469, 0.583 )
+ TKFRAME_-61500_AXES = ( 3, 2, 1 )
+ TKFRAME_-61500_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MWR Frames:
+-------------------------------------------------------------------------------
+
+ The set of frames for the MWR experiment includes six MWR antenna
+ frames -- JUNO_MWR_A1, JUNO_MWR_A2, JUNO_MWR_A3, JUNO_MWR_A4,
+ JUNO_MWR_A5, and JUNO_MWR_A6, -- fixed w.r.t. to the spacecraft and
+ defined as follows:
+
+ - +Z axis is along the antenna boresight
+
+ - +Y axis is nominally along the spacecraft +Z axis
+
+ - +X axis completes the right-handed frame
+
+ - the origin of the frame is at the geometric center of the
+ antenna patch or outer rim.
+
+ This diagram illustrates the MWR antenna frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 ^ <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ +Xa1 / +Za1 `.
+ \ .-' <. /
+ \-' . `-. /
+ \ .-' `-o +Ya1
+ \ .-' ----- . -. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | / | \ | | | |``--..
+ | ' | +Xsc | | | | `--..
+ | | o------> | | | | | |
+ | . +Zsc , | | | | ..--''
+ | \ / | |..--'
+ | \ HGA / +Xa2/3/4/5/6 | | Magnetometer
+ `-. `. .' .-> -----------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. o +Ya2/3/4/5/6
+ / `-. .-' \
+ /`-. /' \
+ ~ ~ ~ ~ ~ ~ ~ ~ \ +Za2/3/4/5/6
+ Solar Array 2 V
+ +Ya* and +Zsc are
+ out of the page.
+
+
+ The JUNO_MWR_A1 frame is nominally rotated from the spacecraft frame
+ first by +150 degrees about +Z, then by +90 degrees about +X.
+
+ The JUNO_MWR_A2..A6 frames are nominally rotated from the spacecraft
+ frame first by +30 degrees about +Z, then by +90 degrees about +X.
+
+ Since the frame definitions below contain the reverse
+ transformations, the order of rotations is reversed and the signs of
+ rotation angles are changed to the opposite ones compared to the
+ description above.
+
+ \begindata
+
+ FRAME_JUNO_MWR_A1 = -61601
+ FRAME_-61601_NAME = 'JUNO_MWR_A1'
+ FRAME_-61601_CLASS = 4
+ FRAME_-61601_CLASS_ID = -61601
+ FRAME_-61601_CENTER = -61
+ TKFRAME_-61601_SPEC = 'ANGLES'
+ TKFRAME_-61601_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61601_ANGLES = ( -150.0, 0.0, -90.0 )
+ TKFRAME_-61601_AXES = ( 3, 2, 1 )
+ TKFRAME_-61601_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MWR_A2 = -61602
+ FRAME_-61602_NAME = 'JUNO_MWR_A2'
+ FRAME_-61602_CLASS = 4
+ FRAME_-61602_CLASS_ID = -61602
+ FRAME_-61602_CENTER = -61
+ TKFRAME_-61602_SPEC = 'ANGLES'
+ TKFRAME_-61602_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61602_ANGLES = ( -30.0, 0.0, -90.0 )
+ TKFRAME_-61602_AXES = ( 3, 2, 1 )
+ TKFRAME_-61602_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MWR_A3 = -61603
+ FRAME_-61603_NAME = 'JUNO_MWR_A3'
+ FRAME_-61603_CLASS = 4
+ FRAME_-61603_CLASS_ID = -61603
+ FRAME_-61603_CENTER = -61
+ TKFRAME_-61603_SPEC = 'ANGLES'
+ TKFRAME_-61603_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61603_ANGLES = ( -30.0, 0.0, -90.0 )
+ TKFRAME_-61603_AXES = ( 3, 2, 1 )
+ TKFRAME_-61603_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MWR_A4 = -61604
+ FRAME_-61604_NAME = 'JUNO_MWR_A4'
+ FRAME_-61604_CLASS = 4
+ FRAME_-61604_CLASS_ID = -61604
+ FRAME_-61604_CENTER = -61
+ TKFRAME_-61604_SPEC = 'ANGLES'
+ TKFRAME_-61604_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61604_ANGLES = ( -30.0, 0.0, -90.0 )
+ TKFRAME_-61604_AXES = ( 3, 2, 1 )
+ TKFRAME_-61604_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MWR_A5 = -61605
+ FRAME_-61605_NAME = 'JUNO_MWR_A5'
+ FRAME_-61605_CLASS = 4
+ FRAME_-61605_CLASS_ID = -61605
+ FRAME_-61605_CENTER = -61
+ TKFRAME_-61605_SPEC = 'ANGLES'
+ TKFRAME_-61605_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61605_ANGLES = ( -30.0, 0.0, -90.0 )
+ TKFRAME_-61605_AXES = ( 3, 2, 1 )
+ TKFRAME_-61605_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MWR_A6 = -61606
+ FRAME_-61606_NAME = 'JUNO_MWR_A6'
+ FRAME_-61606_CLASS = 4
+ FRAME_-61606_CLASS_ID = -61606
+ FRAME_-61606_CENTER = -61
+ TKFRAME_-61606_SPEC = 'ANGLES'
+ TKFRAME_-61606_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61606_ANGLES = ( -30.0, 0.0, -90.0 )
+ TKFRAME_-61606_AXES = ( 3, 2, 1 )
+ TKFRAME_-61606_UNITS = 'DEGREES'
+
+ \begintext
+
+
+
+UVS Frames
+-------------------------------------------------------------------------------
+
+ The set of frames for the UVS experiment includes two frames
+ -- JUNO_UVS_BASE and JUNO_UVS.
+
+ The UVS "hardware" frame, JUNO_UVS_BASE, is fixed w.r.t. to the
+ spacecraft and defined as follows:
+
+ - +Z axis is normal to the sensor mounting plane and points
+ into the sensor; it is nominally along the slit
+
+ - +X axis is parallel to the scan mirror rotation axis and points
+ from the sensor electronics towards the entrance baffle
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the center of the reference
+ mounting hole.
+
+ The UVS "observation" frame, JUNO_UVS, is a CK-based frame defined
+ as follows:
+
+ - +X axis is the instrument boresight
+
+ - +Z axis is along the slit and for the "zero" scan mirror position
+ points in the same direction as the +Z axis of the JUNO_UVS_BASE
+ frame
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the intersection of the
+ reflected boresight and the scan mirror axis.
+
+ This diagram illustrates the UVS frames (the JUNO_UVS frame is shown
+ in the "zero" scan mirror position):
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ ~ `.
+ \ .-' \.
+ \-' .-' `-.
+ \ .-' `-.
+ .-' ----- . `-. Solar Array 1
+ +Yu ' +Ysc ^ `. `-.--------------------.
+ ^ / | \ | | | |
+ | +Xub | \ | | | |``--..
+ |^ | +Xsc | | | | `--..
+ +Xu || | o------> | | | | | |
+ <------x| . +Zsc , | | | | ..--''
+ +Zu | \ / | | | |..--'
+ x------> / | | | | Magnetometer
+ +Zub +Yub HGA .' .-'--------------------' Boom
+ / `-. ----- ' .-'
+ / `-. .-'
+ / `-. .-' +Zub and +Zu are
+ /`-. /' into the page.
+ ~ ~ ~ ~ ~ ~ ~ ~
+ Solar Array 2 +Zsc is out of
+ the page.
+
+
+ Scan Mirror Plane and Axis (Spacecraft +Z side view:):
+ ------------------------------------------------------
+
+ |
+ | Scan Mirror Axis
+ |
+
+ ^ +Yu
+ . |
+ `. |
+ +Xu `.|
+ <------x.
+ Reflected +Zu `. Scan Mirror plane
+ boresight ` in "zero" position
+
+ ^ +Xub ^ +Ysc
+ | |
+ | |
+ | |
+ x------> Yub o------>
+ +Zub +Zsc +Xsc
+
+
+ As seen on the diagram the JUNO_UVS_BASE frame is nominally rotated
+ from the spacecraft frame first by +90 degrees about +Z, then by 180
+ degrees about +X. This nominal alignment was provided in FK versions
+ 0.0-0.9 as
+
+ tkframe_-61700_angles = ( -90.0, 0.0, 180.0 )
+
+ The calibrated rotations that align the spacecraft frame with the
+ JUNO_UVS_BASE frame, provided in [12], are first by +89.855 deg
+ about Z, then by -0.625 deg about Y, then by 180 degrees about X.
+ These angles are incorporated into the JUNO_UVS_BASE frame
+ definition below.
+
+ For a perfect nominal alignment of the boresight and scan mirror
+ axis and a perfect nominal 45 degrees position of the mirror plane,
+ at the "zero" mirror position the JUNO_UVS frame is simply rotated
+ by -90 degrees about +Z of the JUNO_UVS_BASE frame. For any other
+ mirror position within the +30/-30 degrees range the two additional
+ rotations are needed: first by the "scan angle" about +Y, then by
+ the "scan angle" about +X. These rotations will be stored in CK files.
+
+ Since the frame JUNO_UVS_BASE definition below contain the reverse
+ transformation -- from the UVS_BASE frame to the spacecraft frame --
+ the order of rotations is reversed and the signs of rotation angles
+ are changed to the opposite ones compared to the description above.
+
+ \begindata
+
+ FRAME_JUNO_UVS_BASE = -61700
+ FRAME_-61700_NAME = 'JUNO_UVS_BASE'
+ FRAME_-61700_CLASS = 4
+ FRAME_-61700_CLASS_ID = -61700
+ FRAME_-61700_CENTER = -61
+ TKFRAME_-61700_SPEC = 'ANGLES'
+ TKFRAME_-61700_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61700_ANGLES = ( -89.855, 0.625, 180.0 )
+ TKFRAME_-61700_AXES = ( 3, 2, 1 )
+ TKFRAME_-61700_UNITS = 'DEGREES'
+
+ FRAME_JUNO_UVS = -61701
+ FRAME_-61701_NAME = 'JUNO_UVS'
+ FRAME_-61701_CLASS = 3
+ FRAME_-61701_CLASS_ID = -61701
+ FRAME_-61701_CENTER = -61
+ CK_-61701_SCLK = -61
+ CK_-61701_SPK = -61
+
+ \begintext
+
+
+WAVES Frames
+-------------------------------------------------------------------------------
+
+ The set of frames for the WAVES experiment includes two frames
+ -- JUNO_WAVES_MSC and JUNO_WAVES_ANTENNA.
+
+ The WAVES MSC frame, JUNO_WAVES_MSC, is fixed w.r.t. to the
+ spacecraft and defined as follows:
+
+ - +Z axis is along the MSC center axis and points in the same
+ direction as the spacecraft +Z axis
+
+ - +Y axis is in the mounting plate plane and points away from
+ the spacecraft
+
+ - +X axis completes the right-handed frame
+
+ - the origin of the frame is at the geometric center of the MSC
+ center axis.
+
+ The WAVES electrical antenna frame, JUNO_WAVES_ANTENNA, is fixed
+ w.r.t. to the spacecraft and defined as follows:
+
+ - +Z axis is normal to the antenna mounting plane and points
+ away from the spacecraft; it is nominally co-aligned with the
+ spacecraft -Z axis
+
+ - +Y axis is in the mounting plate plane and points between the
+ two antennas is stowed position
+
+ - +X axis completes the right-handed frame
+
+ - the origin of the frame is at the geometric center of the
+ antenna mounting plate.
+
+ This diagram illustrates the WAVES frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ~ ~ ~ ~ ~ ~ ~ ~ `.
+ \ .-' \.
+ \-' .-' `-.
+ \ .-' `-.
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | / | | | | |``--..
+ | ' | +Yant | | `--..
+ | | o----> <----x +Zant | | |
+ | . +Zsc +Xsc , | | | ..--''
+ | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' . V -------------------' Boom
+ / `-. ` ----- ' .-' +Xant
+ Solar / `-. '
+ Array 2 / ` .o +Zmsc
+ /`-. .-' \
+ ~ ~ ~ ~ <-' \
+ +Xmsc \ +Zsc is out of
+ V +Ymsc the page.
+
+ The JUNO_WAVES_MSC frame is nominally rotated from the spacecraft
+ frame by -150 degrees about +Z.
+
+ The JUNO_WAVES_ANTENNA frame is nominally rotated from the spacecraft
+ frame first by -90 degrees about +Z, then by 180 degrees about +X.
+
+ Since the frame definitions below contain the reverse
+ transformations, the order of rotations is reversed and the signs of
+ rotation angles are changed to the opposite ones compared to the
+ description above.
+
+ \begindata
+
+ FRAME_JUNO_WAVES_MSC = -61810
+ FRAME_-61810_NAME = 'JUNO_WAVES_MSC'
+ FRAME_-61810_CLASS = 4
+ FRAME_-61810_CLASS_ID = -61810
+ FRAME_-61810_CENTER = -61
+ TKFRAME_-61810_SPEC = 'ANGLES'
+ TKFRAME_-61810_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61810_ANGLES = ( 150.0, 0.0, 0.0 )
+ TKFRAME_-61810_AXES = ( 3, 2, 1 )
+ TKFRAME_-61810_UNITS = 'DEGREES'
+
+ FRAME_JUNO_WAVES_ANTENNA = -61820
+ FRAME_-61820_NAME = 'JUNO_WAVES_ANTENNA'
+ FRAME_-61820_CLASS = 4
+ FRAME_-61820_CLASS_ID = -61820
+ FRAME_-61820_CENTER = -61
+ TKFRAME_-61820_SPEC = 'ANGLES'
+ TKFRAME_-61820_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61820_ANGLES = ( 90.0, 0.0, 180.0 )
+ TKFRAME_-61820_AXES = ( 3, 2, 1 )
+ TKFRAME_-61820_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Solar Array Frames
+-------------------------------------------------------------------------------
+
+ Two frames are defined for each of the three solar arrays.
+
+ The first frame -- a fixed-offset frame named JUNO_SA#_HINGE (where
+ # is 1, 2, or 3) -- is fixed w.r.t. to the spacecraft and is defined
+ as follows:
+
+ - +Z axis is co-aligned with the s/c +Z axis
+
+ - +X axis is along the solar array symmetry axis and points
+ from the hinge to the outer side of the array
+
+ - +Y axis is along the hinge axis and points to complete the
+ right-handed frame
+
+ - the origin of the frame is in the middle of the hinge axis
+
+ The second frame -- a CK-based frame named JUNO_SA# (where # is 1,
+ 2, or 3) -- rotates about the hinge (+Y) with respect to the
+ corresponding JUNO_SA#_HINGE frame and is defined as follows:
+
+ - +Z axis is along the normal to the array surface on the solar
+ cell side
+
+ - +X axis is along the solar array symmetry axis and points
+ from the hinge towards the outer side of the array
+
+ - +Y axis is along the hinge axis and points to complete the
+ right-handed frame
+
+ - the origin of the frame is in the middle of between two center
+ sections of the array
+
+ In the non-articulated ("zero") position the two frames for each of the
+ arrays are co-aligned, as shown on this diagram:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ .-\
+ .-' \
+ .-' \ Solar Array 3
+ .-' \
+ \ .-'\
+ \ ^ +Xsa3
+ \ , \ \
+ \-' \ .-'\
+ \ o +Zsa3 \
+ +Ysa3 .-' \
+ <-' .-'\ <-. Spin Direction
+ ^ +Xsa3h `.
+ \ . \ \.
+ \-' \ .-' `-.
+ \ o +Zsa3h `-.
+ +Ysa3h .-' ----- . `-. +Ysa1h +Ysa1 Solar Array 1
+ <.-' +Ysc ^ `. ` ^ --------- ^ ----.
+ / | \ | | | |
+ | / | \ | | | |``--..
+ | ' | +Xsc | +Xsa1h | +Xsa1 `--..
+ | | o------> | o-----> o-----> |
+ | . +Zsc , +Zsa1h +Zsa1 | ..--''
+ | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / +Zsa2h ----- ' .-'
+ / o`-. .-'
+ / / `->
+ +Xsa2h / +Ysa2h
+ / V /
+ / -. /
+ /`-. +Zsa2 `-/
+ / o /
+ / / `-.
+ +Xsa2 / `-> +Ysa2
+ / V
+ / -. /
+ /. `-/
+ `-. / Solar Array 2 All +Z axes are out of
+ `-. / the page.
+ `-. /
+ `
+
+
+ The keywords below define the solar array frames.
+
+ \begindata
+
+ FRAME_JUNO_SA1_HINGE = -61010
+ FRAME_-61010_NAME = 'JUNO_SA1_HINGE'
+ FRAME_-61010_CLASS = 4
+ FRAME_-61010_CLASS_ID = -61010
+ FRAME_-61010_CENTER = -61
+ TKFRAME_-61010_SPEC = 'ANGLES'
+ TKFRAME_-61010_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61010_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-61010_AXES = ( 1, 2, 3 )
+ TKFRAME_-61010_UNITS = 'DEGREES'
+
+ FRAME_JUNO_SA1 = -61011
+ FRAME_-61011_NAME = 'JUNO_SA1'
+ FRAME_-61011_CLASS = 3
+ FRAME_-61011_CLASS_ID = -61011
+ FRAME_-61011_CENTER = -61
+ CK_-61011_SCLK = -61
+ CK_-61011_SPK = -61
+
+ FRAME_JUNO_SA2_HINGE = -61020
+ FRAME_-61020_NAME = 'JUNO_SA2_HINGE'
+ FRAME_-61020_CLASS = 4
+ FRAME_-61020_CLASS_ID = -61020
+ FRAME_-61020_CENTER = -61
+ TKFRAME_-61020_SPEC = 'ANGLES'
+ TKFRAME_-61020_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61020_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-61020_AXES = ( 1, 2, 3 )
+ TKFRAME_-61020_UNITS = 'DEGREES'
+
+ FRAME_JUNO_SA2 = -61021
+ FRAME_-61021_NAME = 'JUNO_SA2'
+ FRAME_-61021_CLASS = 3
+ FRAME_-61021_CLASS_ID = -61021
+ FRAME_-61021_CENTER = -61
+ CK_-61021_SCLK = -61
+ CK_-61021_SPK = -61
+
+ FRAME_JUNO_SA3_HINGE = -61030
+ FRAME_-61030_NAME = 'JUNO_SA3_HINGE'
+ FRAME_-61030_CLASS = 4
+ FRAME_-61030_CLASS_ID = -61030
+ FRAME_-61030_CENTER = -61
+ TKFRAME_-61030_SPEC = 'ANGLES'
+ TKFRAME_-61030_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61030_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-61030_AXES = ( 1, 2, 3 )
+ TKFRAME_-61030_UNITS = 'DEGREES'
+
+ FRAME_JUNO_SA3 = -61031
+ FRAME_-61031_NAME = 'JUNO_SA3'
+ FRAME_-61031_CLASS = 3
+ FRAME_-61031_CLASS_ID = -61031
+ FRAME_-61031_CENTER = -61
+ CK_-61031_SCLK = -61
+ CK_-61031_SPK = -61
+
+ \begintext
+
+
+Antenna Frames
+-------------------------------------------------------------------------------
+
+ The JUNO HGA, MGA, and "forward" and "aft" LGA antenna frames --
+ JUNO_HGA, JUNO_MGA, JUNO_LGA_FORWARD, and JUNO_LGA_AFT -- are
+ defined as follows:
+
+ - +Z axis is along the antenna boresight
+
+ - +X axis is along the clock reference direction of the antenna
+ pattern
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is in the geometric center of the
+ antenna's outer rim or patch
+
+ The JUNO "toroid" LGA frame -- JUNO_LGA_TOROID -- is defined to be
+ co-aligned with the spacecraft frame.
+
+ All antenna frames are defined as fixed-offset frames with respect
+ to the spacecraft frame.
+
+ Nominally all antenna frames (except for JUNO_LGA_AFT) are
+ co-aligned with the spacecraft frame. The JUNO_LGA_AFT frame is
+ rotated from the spacecraft frame by 180 degrees about +X.
+
+ This diagram illustrates the antenna frames:
+
+ Spacecraft -Y side view:
+ ------------------------
+
+ +Zhga
+ ^
+ | +Zmga,+Zlgaf
+ | ^ ^
+ | | |
+ +Yhga x------> +Xhga
+ / \ | |
+ HGA .-------------x-x---->-> +Xmga,+Xlgaf
+ \ +Ymga,+Ylgaf
+ `. .'
+ `-------'
+ | | Magnetometer
+ | | Boom
+ ================o==o==o==o-----------o======o======o======o===========*
+ Solar | | | Solar Array 1
+ Array 2 | | |
+ | |
+ | |
+ | +Zsc ^ |
+ | +Zlgat | |
+ | | |
+ | | | +Ysc, +Yhga, Ylgaf,
+ `----- +Ysc x------> -' and +Ylgat are into
+ +Ylgaa o------> /_____\ +Xsc the page.
+ | +Xlgaa +Xlgat
+ | +Ylgaa is out of
+ | the page.
+ V +Zlgaa
+
+
+ According to [11] the measured HGA electrical boresight [in the
+ spacecraft frame, BVS] is:
+
+ [-3.022155372263570e-04 5.638899817258940e-04 0.999999795346908]
+
+ Three rotations are needed to align the HGA +Z axis with this
+ direction while keeping the HGA +X axis close to the spacecraft +X
+ axis: first by +118.1889804 degrees about Z, second by +0.03665615
+ degrees about Y and third by -118.1889804 degrees about Z. These
+ rotations are incorporated in reverse order with opposite signs in
+ the HGA frame definition below.
+
+ All other antenna frame definitions are nominal as described above.
+
+ The keywords below define the antenna frames.
+
+ \begindata
+
+ FRAME_JUNO_HGA = -61040
+ FRAME_-61040_NAME = 'JUNO_HGA'
+ FRAME_-61040_CLASS = 4
+ FRAME_-61040_CLASS_ID = -61040
+ FRAME_-61040_CENTER = -61
+ TKFRAME_-61040_SPEC = 'ANGLES'
+ TKFRAME_-61040_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61040_ANGLES = ( -118.1889804, -0.03665615, 118.1889804 )
+ TKFRAME_-61040_AXES = ( 3, 2, 3 )
+ TKFRAME_-61040_UNITS = 'DEGREES'
+
+ FRAME_JUNO_MGA = -61050
+ FRAME_-61050_NAME = 'JUNO_MGA'
+ FRAME_-61050_CLASS = 4
+ FRAME_-61050_CLASS_ID = -61050
+ FRAME_-61050_CENTER = -61
+ TKFRAME_-61050_SPEC = 'ANGLES'
+ TKFRAME_-61050_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61050_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-61050_AXES = ( 1, 2, 3 )
+ TKFRAME_-61050_UNITS = 'DEGREES'
+
+ FRAME_JUNO_LGA_FORWARD = -61061
+ FRAME_-61061_NAME = 'JUNO_LGA_FORWARD'
+ FRAME_-61061_CLASS = 4
+ FRAME_-61061_CLASS_ID = -61061
+ FRAME_-61061_CENTER = -61
+ TKFRAME_-61061_SPEC = 'ANGLES'
+ TKFRAME_-61061_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61061_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-61061_AXES = ( 1, 2, 3 )
+ TKFRAME_-61061_UNITS = 'DEGREES'
+
+ FRAME_JUNO_LGA_AFT = -61062
+ FRAME_-61062_NAME = 'JUNO_LGA_AFT'
+ FRAME_-61062_CLASS = 4
+ FRAME_-61062_CLASS_ID = -61062
+ FRAME_-61062_CENTER = -61
+ TKFRAME_-61062_SPEC = 'ANGLES'
+ TKFRAME_-61062_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61062_ANGLES = ( 180.0, 0.0, 0.0 )
+ TKFRAME_-61062_AXES = ( 1, 2, 3 )
+ TKFRAME_-61062_UNITS = 'DEGREES'
+
+ FRAME_JUNO_LGA_TOROID = -61063
+ FRAME_-61063_NAME = 'JUNO_LGA_TOROID'
+ FRAME_-61063_CLASS = 4
+ FRAME_-61063_CLASS_ID = -61063
+ FRAME_-61063_CENTER = -61
+ TKFRAME_-61063_SPEC = 'ANGLES'
+ TKFRAME_-61063_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61063_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-61063_AXES = ( 1, 2, 3 )
+ TKFRAME_-61063_UNITS = 'DEGREES'
+
+ \begintext
+
+
+ACS Sensor Frames
+-------------------------------------------------------------------------------
+
+ This section defined frames for ACS sensors -- SRUs and SSSs.
+
+
+SRU Frames
+
+ The JUNO SRU frames -- JUNO_SRU1 and JUNO_SRU2 -- are defined as
+ follows:
+
+ - +X axis is along the SRU boresight
+
+ - +Y axis is nominally along the spacecraft +Z axis
+
+ - +Z axis completes the right-handed frame
+
+ - the origin of the frame is at the SRU focal point
+
+ Nominally the SRU1 frame is rotated from the spacecraft frame first
+ by +90 degrees about X, then by +65 degrees about Y.
+
+ Nominally the SRU2 frame is rotated from the spacecraft frame first
+ by +90 degrees about X, then by +55 degrees about X.
+
+ This diagram illustrates the SRU frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+ +Xsru1
+ Solar Array 3 ^ <-. Spin Direction
+ / 10 deg `.
+ ~ ~ ~ ~ ~ ~ ~ ~\ /
+ \-' .-' / .> +Xsru2
+ \ .-' +Ysru1 o. .-'
+ \ .-' --- +Ysru2`o' Solar Array 1
+ .-' +Ysc ^ `.`> +Zsru1 ---------.
+ | / | \ `. | |
+ | / | \ | > +Zsru2 | |``--..
+ | ' | +Xsc | | | `--..
+ | | o------> | | | | | |
+ | . +Zsc , | | | | ..--''
+ | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. .-'
+ / `-. .-' +Xsru1 and +Xsru2 are
+ ~ ~ ~ ~ ~ ~ ~ ~ ' into the page.
+
+ Solar Array 2 +Zsc is out of
+ the page.
+
+ The following pre-launch calibrated misalignments between the
+ spacecraft frame and the SRU frames were provided in [6]:
+
+ DCM - SMRF to SRU1 (*)
+
+ 0.4204194 0.9073288 0.0013891
+ -0.0007953 -0.0011625 0.9999990
+ 0.9073296 -0.4204200 0.0002328
+
+ DCM - SMRF to SRU2 (*)
+
+ 0.5720852 0.8201927 -0.0015696
+ 0.0015127 0.0008586 0.9999985
+ 0.8201928 -0.5720867 -0.0007496
+
+ (*) Measured from the SRU alignment cube. Correction from
+ cube axes (ARF) to instrument axes (BRF) applied via
+ vendor data
+
+ The misalignments from [6] are incorporated in the two frame
+ definitions below.
+
+ \begindata
+
+ FRAME_JUNO_SRU1 = -61071
+ FRAME_-61071_NAME = 'JUNO_SRU1'
+ FRAME_-61071_CLASS = 4
+ FRAME_-61071_CLASS_ID = -61071
+ FRAME_-61071_CENTER = -61
+ TKFRAME_-61071_SPEC = 'MATRIX'
+ TKFRAME_-61071_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61071_MATRIX = (
+ 0.4204194 0.9073288 0.0013891
+ -0.0007953 -0.0011625 0.9999990
+ 0.9073296 -0.4204200 0.0002328
+ )
+
+ FRAME_JUNO_SRU2 = -61072
+ FRAME_-61072_NAME = 'JUNO_SRU2'
+ FRAME_-61072_CLASS = 4
+ FRAME_-61072_CLASS_ID = -61072
+ FRAME_-61072_CENTER = -61
+ TKFRAME_-61072_SPEC = 'MATRIX'
+ TKFRAME_-61072_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61072_MATRIX = (
+ 0.5720852 0.8201927 -0.0015696
+ 0.0015127 0.0008586 0.9999985
+ 0.8201928 -0.5720867 -0.0007496
+ )
+
+ \begintext
+
+
+SSS Frames
+
+ The JUNO SSS frames -- JUNO_SSS1 and JUNO_SSS2 -- are defined as
+ follows:
+
+ - +Z axis is along the SSS boresight and is nominally along the
+ spacecraft -X axis.
+
+ - +X axis is nominally along the spacecraft -Z axis
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is at the SSS geometric center
+
+ Nominally the SSS frames are rotated from the spacecraft frame first
+ by +90 degrees about Y, then by 180 degrees about X.
+
+ This diagram illustrates the SSS frames:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ `.
+ ~ ~ ~ ~ ~ ~ ~ ~\.
+ \-' .-' `-.
+ \ .-' `-.
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ +Zss1 | \ | | | |
+ <------x +Xsss1 | \ | | | |``--..
+ <------x +Xsss2 | +Xsc | | | | `--..
+ +Zsss2 | o------> | | | | | |
+ || . +Zsc , | | | | ..--''
+ +Ysss1 V| \ / | | | |..--'
+ +Ysss2 V| \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / `-. .-'
+ / `-. .-' +Xsss1 and +Xsss2 are
+ ~ ~ ~ ~ ~ ~ ~ ~/' into the page.
+
+ Solar Array 2 +Zsc is out of
+ the page.
+
+ Since the frame definitions below contains the reverse
+ transformations -- from the SSS frames to the spacecraft frame --
+ the order of rotations is reversed and the signs of rotation angles
+ are changed to the opposite ones compared to the description above.
+
+ \begindata
+
+ FRAME_JUNO_SSS1 = -61073
+ FRAME_-61073_NAME = 'JUNO_SSS1'
+ FRAME_-61073_CLASS = 4
+ FRAME_-61073_CLASS_ID = -61073
+ FRAME_-61073_CENTER = -61
+ TKFRAME_-61073_SPEC = 'ANGLES'
+ TKFRAME_-61073_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61073_ANGLES = ( 0.0, -90.0, 180.0 )
+ TKFRAME_-61073_AXES = ( 3, 2, 1 )
+ TKFRAME_-61073_UNITS = 'DEGREES'
+
+ FRAME_JUNO_SSS2 = -61074
+ FRAME_-61074_NAME = 'JUNO_SSS2'
+ FRAME_-61074_CLASS = 4
+ FRAME_-61074_CLASS_ID = -61074
+ FRAME_-61074_CENTER = -61
+ TKFRAME_-61074_SPEC = 'ANGLES'
+ TKFRAME_-61074_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61074_ANGLES = ( 0.0, -90.0, 180.0 )
+ TKFRAME_-61074_AXES = ( 3, 2, 1 )
+ TKFRAME_-61074_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Truster Frames
+-------------------------------------------------------------------------------
+
+ The JUNO REM thruster frames -- JUNO_REM_[FL1,2,3,4] [FA1,2]
+ [RL1,2,3,4] [RA1,2] -- are defined as follows:
+
+ - +Z axis is along the thrust vector.
+
+ - +X axis is in the plane containing the thrust vector and the
+ spacecraft +Z axis and points in the direction of the
+ spacecraft +Z axis
+
+ - +Y axis completes the right-handed frame
+
+ - the origin of the frame is center of the nozzle outer edge.
+
+ These diagrams approximately illustrate the REM thruster vector
+ directions -- +Z axes of the REM frames, -- other axes are not
+ shown:
+
+ Spacecraft +Z side view:
+ ------------------------
+
+ Solar Array 3 <-. Spin Direction
+ ^ +Zfa1 `.
+ ~ ~ ~ ~ ~ ~ ~ ~\|
+ +Zfl4 <------@@@------> +Zfl1
+ \ FL4 FA1 FL1
+ \ .-' ----- . `-. Solar Array 1
+ .-' +Ysc ^ `. `-.--------------------.
+ | / | \ | | | |
+ | / | \ | | | |``--..
+ | ' | +Xsc | | | | `--..
+ | | o------> | | | | | |
+ | . +Zsc , | | | | ..--''
+ | \ / | | | |..--'
+ | \ HGA / | | | | Magnetometer
+ `-. `. .' .-'--------------------' Boom
+ / `-. ` ----- ' .-'
+ / FL3 FA2 FL2
+ /+Zfl3 <------@@@------> +Zfl2
+ ~ ~ ~ ~ ~ ~ ~ ~/|
+ v +Zfa2
+ Solar Array 2 +Zsc is out of
+ the page.
+
+ Spacecraft -Z side view:
+ ------------------------
+
+ Solar Array 2 -. Spin Direction
+ ^ +Zra2 `.
+ ~ ~ ~ ~ ~ ~ ~ ~\| v
+ +Zrl3 <------@@@------> +Zrl2
+ \ RL3 RA2 RL2
+ \ .-' `-. Solar Array 1
+ .-' `-.--------------------.
+ | | | | |
+ | | | | |``--..
+ | +Zsc +Xsc | | | | `--..
+ | o------> | | | | |
+ | | | | | | ..--''
+ | | | | | |..--'
+ | | | | | | Magnetometer
+ `-. +Ysc V .-'--------------------' Boom
+ / `-. .-'
+ / RL4 RA1 RL1
+ +Zrl4 <------@@@------> +Zrl1
+ ~ ~ ~ ~ ~ ~ ~ ~/|
+ v +Zra1
+ Solar Array 3 +Zsc is into
+ the page.
+
+ The angles in the REM frame definitions below are based the
+ information from [4].
+
+ \begindata
+
+ FRAME_JUNO_REM_FL1 = -61081
+ FRAME_-61081_NAME = 'JUNO_REM_FL1'
+ FRAME_-61081_CLASS = 4
+ FRAME_-61081_CLASS_ID = -61081
+ FRAME_-61081_CENTER = -61
+ TKFRAME_-61081_SPEC = 'ANGLES'
+ TKFRAME_-61081_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61081_ANGLES = ( 22.009651, -76.551858, 157.431346 )
+ TKFRAME_-61081_AXES = ( 1, 2, 3 )
+ TKFRAME_-61081_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_FL2 = -61082
+ FRAME_-61082_NAME = 'JUNO_REM_FL2'
+ FRAME_-61082_CLASS = 4
+ FRAME_-61082_CLASS_ID = -61082
+ FRAME_-61082_CENTER = -61
+ TKFRAME_-61082_SPEC = 'ANGLES'
+ TKFRAME_-61082_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61082_ANGLES = ( -22.009640, -76.551859, -157.431357 )
+ TKFRAME_-61082_AXES = ( 1, 2, 3 )
+ TKFRAME_-61082_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_FL3 = -61083
+ FRAME_-61083_NAME = 'JUNO_REM_FL3'
+ FRAME_-61083_CLASS = 4
+ FRAME_-61083_CLASS_ID = -61083
+ FRAME_-61083_CENTER = -61
+ TKFRAME_-61083_SPEC = 'ANGLES'
+ TKFRAME_-61083_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61083_ANGLES = ( -22.009651, 76.551858, -22.568654 )
+ TKFRAME_-61083_AXES = ( 1, 2, 3 )
+ TKFRAME_-61083_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_FL4 = -61084
+ FRAME_-61084_NAME = 'JUNO_REM_FL4'
+ FRAME_-61084_CLASS = 4
+ FRAME_-61084_CLASS_ID = -61084
+ FRAME_-61084_CENTER = -61
+ TKFRAME_-61084_SPEC = 'ANGLES'
+ TKFRAME_-61084_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61084_ANGLES = ( 22.009640, 76.551859, 22.568643 )
+ TKFRAME_-61084_AXES = ( 1, 2, 3 )
+ TKFRAME_-61084_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_FA1 = -61085
+ FRAME_-61085_NAME = 'JUNO_REM_FA1'
+ FRAME_-61085_CLASS = 4
+ FRAME_-61085_CLASS_ID = -61085
+ FRAME_-61085_CENTER = -61
+ TKFRAME_-61085_SPEC = 'ANGLES'
+ TKFRAME_-61085_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61085_ANGLES = ( 10.000059, 0.000000, 90.000000 )
+ TKFRAME_-61085_AXES = ( 1, 2, 3 )
+ TKFRAME_-61085_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_FA2 = -61086
+ FRAME_-61086_NAME = 'JUNO_REM_FA2'
+ FRAME_-61086_CLASS = 4
+ FRAME_-61086_CLASS_ID = -61086
+ FRAME_-61086_CENTER = -61
+ TKFRAME_-61086_SPEC = 'ANGLES'
+ TKFRAME_-61086_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61086_ANGLES = ( -10.000059, 0.000000, -90.000000 )
+ TKFRAME_-61086_AXES = ( 1, 2, 3 )
+ TKFRAME_-61086_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_RL1 = -61091
+ FRAME_-61091_NAME = 'JUNO_REM_RL1'
+ FRAME_-61091_CLASS = 4
+ FRAME_-61091_CLASS_ID = -61091
+ FRAME_-61091_CENTER = -61
+ TKFRAME_-61091_SPEC = 'ANGLES'
+ TKFRAME_-61091_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61091_ANGLES = ( 157.990360, -76.551859, 22.568643 )
+ TKFRAME_-61091_AXES = ( 1, 2, 3 )
+ TKFRAME_-61091_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_RL2 = -61092
+ FRAME_-61092_NAME = 'JUNO_REM_RL2'
+ FRAME_-61092_CLASS = 4
+ FRAME_-61092_CLASS_ID = -61092
+ FRAME_-61092_CENTER = -61
+ TKFRAME_-61092_SPEC = 'ANGLES'
+ TKFRAME_-61092_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61092_ANGLES = ( -157.990349, -76.551858, -22.568654 )
+ TKFRAME_-61092_AXES = ( 1, 2, 3 )
+ TKFRAME_-61092_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_RL3 = -61093
+ FRAME_-61093_NAME = 'JUNO_REM_RL3'
+ FRAME_-61093_CLASS = 4
+ FRAME_-61093_CLASS_ID = -61093
+ FRAME_-61093_CENTER = -61
+ TKFRAME_-61093_SPEC = 'ANGLES'
+ TKFRAME_-61093_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61093_ANGLES = ( -157.990360, 76.551859, -157.431357 )
+ TKFRAME_-61093_AXES = ( 1, 2, 3 )
+ TKFRAME_-61093_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_RL4 = -61094
+ FRAME_-61094_NAME = 'JUNO_REM_RL4'
+ FRAME_-61094_CLASS = 4
+ FRAME_-61094_CLASS_ID = -61094
+ FRAME_-61094_CENTER = -61
+ TKFRAME_-61094_SPEC = 'ANGLES'
+ TKFRAME_-61094_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61094_ANGLES = ( 157.990349, 76.551858, 157.431346 )
+ TKFRAME_-61094_AXES = ( 1, 2, 3 )
+ TKFRAME_-61094_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_RA1 = -61095
+ FRAME_-61095_NAME = 'JUNO_REM_RA1'
+ FRAME_-61095_CLASS = 4
+ FRAME_-61095_CLASS_ID = -61095
+ FRAME_-61095_CENTER = -61
+ TKFRAME_-61095_SPEC = 'ANGLES'
+ TKFRAME_-61095_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61095_ANGLES = ( 169.999941, 0.000000, 90.000000 )
+ TKFRAME_-61095_AXES = ( 1, 2, 3 )
+ TKFRAME_-61095_UNITS = 'DEGREES'
+
+ FRAME_JUNO_REM_RA2 = -61096
+ FRAME_-61096_NAME = 'JUNO_REM_RA2'
+ FRAME_-61096_CLASS = 4
+ FRAME_-61096_CLASS_ID = -61096
+ FRAME_-61096_CENTER = -61
+ TKFRAME_-61096_SPEC = 'ANGLES'
+ TKFRAME_-61096_RELATIVE = 'JUNO_SPACECRAFT'
+ TKFRAME_-61096_ANGLES = ( -169.999941, 0.000000, -90.000000 )
+ TKFRAME_-61096_AXES = ( 1, 2, 3 )
+ TKFRAME_-61096_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Juno NAIF ID Codes -- Definitions
+========================================================================
+
+ This section contains name to NAIF ID mappings for the JUNO mission.
+ Once the contents of this file is loaded into the KERNEL POOL, these
+ mappings become available within SPICE, making it possible to use
+ names instead of ID code in the high level SPICE routine calls.
+
+ Spacecraft:
+ -----------
+
+ JUNO -61
+ JUNO -61
+ JUNO_SPACECRAFT -61000
+ JUNO_SPACECRAFT_BUS -61000
+ JUNO_SC_BUS -61000
+
+ Magnetometers and CHUs:
+ -----------------------
+
+ JUNO_ASC_CHUD -61111
+ JUNO_ASC_CHUC -61112
+ JUNO_FGM_IB -61114
+ JUNO_ASC_CHUB -61121
+ JUNO_ASC_CHUA -61122
+ JUNO_FGM_OB -61124
+
+ JADE:
+ -----
+
+ JUNO_JADE_E060 -61201
+ JUNO_JADE_E180 -61202
+ JUNO_JADE_E300 -61203
+ JUNO_JADE_I -61204
+
+ JEDI:
+ -----
+
+ JUNO_JEDI_090 -61301
+ JUNO_JEDI_A180 -61302
+ JUNO_JEDI_270 -61303
+
+ JIRAM:
+ ------
+
+ JUNO_JIRAM_I -61410
+ JUNO_JIRAM_I_LBAND -61411
+ JUNO_JIRAM_I_MBAND -61412
+ JUNO_JIRAM_S -61420
+
+ JUNOCAM:
+ --------
+
+ JUNO_JUNOCAM -61500
+ JUNO_JUNOCAM_BLUE -61501
+ JUNO_JUNOCAM_GREEN -61502
+ JUNO_JUNOCAM_RED -61503
+ JUNO_JUNOCAM_METHANE -61504
+
+ MWR:
+ ----
+
+ JUNO_MWR_A1 -61601
+ JUNO_MWR_A2 -61602
+ JUNO_MWR_A3 -61603
+ JUNO_MWR_A4 -61604
+ JUNO_MWR_A5 -61605
+ JUNO_MWR_A6 -61606
+
+ UVS:
+ ----
+
+ JUNO_UVS_BASE -61700
+ JUNO_UVS -61701
+
+ WAVES:
+ ------
+
+ JUNO_WAVES_MSC -61810
+ JUNO_WAVES_ANTENNA -61820
+
+ Solar Arrays:
+ -------------
+
+ JUNO_SA1_HINGE -61010
+ JUNO_SA1 -61011
+ JUNO_SA2_HINGE -61020
+ JUNO_SA2 -61021
+ JUNO_SA3_HINGE -61030
+ JUNO_SA3 -61031
+
+ Antennas:
+ ---------
+
+ JUNO_HGA -61040
+ JUNO_MGA -61050
+ JUNO_LGA_FORWARD -61061
+ JUNO_LGA_AFT -61062
+ JUNO_LGA_TOROID -61063
+
+ ACS Sensors:
+ ------------
+
+ JUNO_SRU1 -61071
+ JUNO_SRU2 -61072
+
+ JUNO_SSS1 -61073
+ JUNO_SSS2 -61074
+
+ Thrusters:
+ ----------
+
+ JUNO_REM_FL1 -61081
+ JUNO_REM_FL2 -61082
+ JUNO_REM_FL3 -61083
+ JUNO_REM_FL4 -61084
+ JUNO_REM_FA1 -61085
+ JUNO_REM_FA2 -61086
+
+ JUNO_REM_RL1 -61091
+ JUNO_REM_RL2 -61092
+ JUNO_REM_RL3 -61093
+ JUNO_REM_RL4 -61094
+ JUNO_REM_RA1 -61095
+ JUNO_REM_RA2 -61096
+
+ The mappings summarized in this table are implemented by the keywords
+ below.
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'JUNO' )
+ NAIF_BODY_CODE += ( -61 )
+
+ NAIF_BODY_NAME += ( 'JUNO' )
+ NAIF_BODY_CODE += ( -61 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -61000 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SPACECRAFT_BUS' )
+ NAIF_BODY_CODE += ( -61000 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SC_BUS' )
+ NAIF_BODY_CODE += ( -61000 )
+
+ NAIF_BODY_NAME += ( 'JUNO_ASC_CHUD' )
+ NAIF_BODY_CODE += ( -61111 )
+
+ NAIF_BODY_NAME += ( 'JUNO_ASC_CHUC' )
+ NAIF_BODY_CODE += ( -61112 )
+
+ NAIF_BODY_NAME += ( 'JUNO_FGM_IB' )
+ NAIF_BODY_CODE += ( -61114 )
+
+ NAIF_BODY_NAME += ( 'JUNO_ASC_CHUB' )
+ NAIF_BODY_CODE += ( -61121 )
+
+ NAIF_BODY_NAME += ( 'JUNO_ASC_CHUA' )
+ NAIF_BODY_CODE += ( -61122 )
+
+ NAIF_BODY_NAME += ( 'JUNO_FGM_OB' )
+ NAIF_BODY_CODE += ( -61124 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JADE_E060' )
+ NAIF_BODY_CODE += ( -61201 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JADE_E180' )
+ NAIF_BODY_CODE += ( -61202 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JADE_E300' )
+ NAIF_BODY_CODE += ( -61203 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JADE_I' )
+ NAIF_BODY_CODE += ( -61204 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JEDI_090' )
+ NAIF_BODY_CODE += ( -61301 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JEDI_A180' )
+ NAIF_BODY_CODE += ( -61302 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JEDI_270' )
+ NAIF_BODY_CODE += ( -61303 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JIRAM_I' )
+ NAIF_BODY_CODE += ( -61410 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JIRAM_I_LBAND' )
+ NAIF_BODY_CODE += ( -61411 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JIRAM_I_MBAND' )
+ NAIF_BODY_CODE += ( -61412 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JIRAM_S' )
+ NAIF_BODY_CODE += ( -61420 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JUNOCAM' )
+ NAIF_BODY_CODE += ( -61500 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JUNOCAM_BLUE' )
+ NAIF_BODY_CODE += ( -61501 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JUNOCAM_GREEN' )
+ NAIF_BODY_CODE += ( -61502 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JUNOCAM_RED' )
+ NAIF_BODY_CODE += ( -61503 )
+
+ NAIF_BODY_NAME += ( 'JUNO_JUNOCAM_METHANE' )
+ NAIF_BODY_CODE += ( -61504 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MWR_A1' )
+ NAIF_BODY_CODE += ( -61601 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MWR_A2' )
+ NAIF_BODY_CODE += ( -61602 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MWR_A3' )
+ NAIF_BODY_CODE += ( -61603 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MWR_A4' )
+ NAIF_BODY_CODE += ( -61604 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MWR_A5' )
+ NAIF_BODY_CODE += ( -61605 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MWR_A6' )
+ NAIF_BODY_CODE += ( -61606 )
+
+ NAIF_BODY_NAME += ( 'JUNO_UVS_BASE' )
+ NAIF_BODY_CODE += ( -61700 )
+
+ NAIF_BODY_NAME += ( 'JUNO_UVS' )
+ NAIF_BODY_CODE += ( -61701 )
+
+ NAIF_BODY_NAME += ( 'JUNO_WAVES_MSC' )
+ NAIF_BODY_CODE += ( -61810 )
+
+ NAIF_BODY_NAME += ( 'JUNO_WAVES_ANTENNA' )
+ NAIF_BODY_CODE += ( -61820 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SA1_HINGE' )
+ NAIF_BODY_CODE += ( -61010 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SA1' )
+ NAIF_BODY_CODE += ( -61011 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SA2_HINGE' )
+ NAIF_BODY_CODE += ( -61020 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SA2' )
+ NAIF_BODY_CODE += ( -61021 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SA3_HINGE' )
+ NAIF_BODY_CODE += ( -61030 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SA3' )
+ NAIF_BODY_CODE += ( -61031 )
+
+ NAIF_BODY_NAME += ( 'JUNO_HGA' )
+ NAIF_BODY_CODE += ( -61040 )
+
+ NAIF_BODY_NAME += ( 'JUNO_MGA' )
+ NAIF_BODY_CODE += ( -61050 )
+
+ NAIF_BODY_NAME += ( 'JUNO_LGA_FORWARD' )
+ NAIF_BODY_CODE += ( -61061 )
+
+ NAIF_BODY_NAME += ( 'JUNO_LGA_AFT' )
+ NAIF_BODY_CODE += ( -61062 )
+
+ NAIF_BODY_NAME += ( 'JUNO_LGA_TOROID' )
+ NAIF_BODY_CODE += ( -61063 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SRU1' )
+ NAIF_BODY_CODE += ( -61071 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SRU2' )
+ NAIF_BODY_CODE += ( -61072 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SSS1' )
+ NAIF_BODY_CODE += ( -61073 )
+
+ NAIF_BODY_NAME += ( 'JUNO_SSS2' )
+ NAIF_BODY_CODE += ( -61074 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_FL1' )
+ NAIF_BODY_CODE += ( -61081 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_FL2' )
+ NAIF_BODY_CODE += ( -61082 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_FL3' )
+ NAIF_BODY_CODE += ( -61083 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_FL4' )
+ NAIF_BODY_CODE += ( -61084 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_FA1' )
+ NAIF_BODY_CODE += ( -61085 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_FA2' )
+ NAIF_BODY_CODE += ( -61086 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_RL1' )
+ NAIF_BODY_CODE += ( -61091 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_RL2' )
+ NAIF_BODY_CODE += ( -61092 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_RL3' )
+ NAIF_BODY_CODE += ( -61093 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_RL4' )
+ NAIF_BODY_CODE += ( -61094 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_RA1' )
+ NAIF_BODY_CODE += ( -61095 )
+
+ NAIF_BODY_NAME += ( 'JUNO_REM_RA2' )
+ NAIF_BODY_CODE += ( -61096 )
+
+ \begintext
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/mgs_sc_ab1_0_sliced_-94000.xc b/tests/pytests/data/JNCR_2016240_01M06152_V01/mgs_sc_ab1_0_sliced_-94000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..c94621b4cb7a3d6605872ac1ce60b0f2da5af256
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/mgs_sc_ab1_0_sliced_-94000.xc
@@ -0,0 +1,128 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' < DAFCAT: CK CONCATENATION > '
+BEGIN_ARRAY 1 107
+'Partly corrected data: -1.414s; 98-11-29'
+'1D954003D^9'
+'1D9542BF^9'
+'-16F30'
+'1'
+'3'
+'1'
+107
+'1D790EA81EA016^0'
+'-918F0350C74828^-1'
+'-F536ADEFD16728^0'
+'-42BEB1626C7088^0'
+'-9C88FED3D85C68^-4'
+'-48E153B50983B^-2'
+'-2AD64DD1290CAC^-2'
+'1DDEECA8BF3D81^0'
+'-935854FCD9821^-1'
+'-F52A6A6B12E828^0'
+'-42BA89CD332A74^0'
+'-B4D20610ED2DE^-4'
+'-4901B2A8F29568^-2'
+'-2AE9C52CD37386^-2'
+'1E82D451C09AE5^0'
+'-95FCFBA5E059E8^-1'
+'-F5160AEEF0F52^0'
+'-42B554A5E6A2C^0'
+'-D0F19E27498D4^-4'
+'-493264A30D8644^-2'
+'-2B2C6603FBB93C^-2'
+'1F242BDA767821^0'
+'-98DC760A8D903^-1'
+'-F501D92780DD8^0'
+'-42AE6EF59E358C^0'
+'-B2D0556F0B9D4^-4'
+'-48FA33A3B36CA4^-2'
+'-2AEEA895C2581E^-2'
+'1FC6C9B34004A4^0'
+'-9B84FBFA0800F8^-1'
+'-F4ECF753141178^0'
+'-42A847DD2E469^0'
+'-9F3DDF0AF0A8E^-4'
+'-493FE2B39CA158^-2'
+'-2AFEA7D19146A2^-2'
+'206A55E36E3E24^0'
+'-9E517CED214C4^-1'
+'-F4D76645E42B3^0'
+'-42A22C1AA278B4^0'
+'-CD57A77FD3674^-4'
+'-49361589848274^-2'
+'-2B2E0E48B03EB8^-2'
+'210C2D3FE95776^0'
+'-A114D05BEE0C28^-1'
+'-F4C1CFA637BA68^0'
+'-429B5C8CEFB0EC^0'
+'-C400A5AD939B6^-4'
+'-493BAD1F2F6E98^-2'
+'-2B24B697ED3A54^-2'
+'21AE71D2E43518^0'
+'-A3E53A4E8AF69^-1'
+'-F4ABBCF5E555F8^0'
+'-42944F01FD64E^0'
+'-B434680938FEA^-4'
+'-495C1059666548^-2'
+'-2B15649A28AB6C^-2'
+'2252114BDA3AF^0'
+'-A695CE51767A9^-1'
+'-F4957FAFF9CF6^0'
+'-428BC89C91262C^0'
+'-B5085079B86EE^-4'
+'-493F19DC73777C^-2'
+'-2B2EE70CE2327^-2'
+'22F5DC45B65A1C^0'
+'-A96E842462F54^-1'
+'-F47E29E4914C98^0'
+'-4285156C0B55F^0'
+'-CA1CD01BC8FF8^-4'
+'-4995FCA91B5048^-2'
+'-2B77BFFE43A76C^-2'
+'23989FECEEA27C^0'
+'-AC22C35B6898B^-1'
+'-F466AE54FBABA^0'
+'-427E1CEC3E667C^0'
+'-B5067A01B4BBE^-4'
+'-49AC3DFD7A471^-2'
+'-2B5250124FDFCC^-2'
+'243AA6E7FC22DA^0'
+'-AEF2026FA830C^-1'
+'-F44EEAA41C9648^0'
+'-42769993672234^0'
+'-8F78169F9F462^-4'
+'-49B56A9779D06^-2'
+'-2B7A7F7CBEDB6C^-2'
+'246AC56B5D6A18^0'
+'-AFC27F630D76F^-1'
+'-F447B5DBAAA06^0'
+'-4274A3FB71B3AC^0'
+'-9663589DA9FEA^-4'
+'-49CD946BC2576^-2'
+'-2B7D1854574A64^-2'
+'1D954003D^9'
+'1D95402C5^9'
+'1D95406C5^9'
+'1D9540AC5^9'
+'1D9540EC5^9'
+'1D95412C5^9'
+'1D95416C5^9'
+'1D9541AC5^9'
+'1D9541EC5^9'
+'1D95422C5^9'
+'1D95426C5^9'
+'1D9542AC5^9'
+'1D9542BF^9'
+'1D954003D^9'
+'1^1'
+'D^1'
+END_ARRAY 1 107
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/acpaquette/lroc_nac/ab103105.spice.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/mgs_sc_ab1_1_sliced_-94000.xc b/tests/pytests/data/JNCR_2016240_01M06152_V01/mgs_sc_ab1_1_sliced_-94000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..5fb2e2dda0bb6ee68d8427ea43c8a1837268fd23
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/mgs_sc_ab1_1_sliced_-94000.xc
@@ -0,0 +1,120 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' < DAFCAT: CK CONCATENATION > '
+BEGIN_ARRAY 1 99
+'Partly corrected data: -1.414s; 98-11-29'
+'1D956C1AD^9'
+'1D956EA05^9'
+'-16F30'
+'1'
+'3'
+'1'
+99
+'84B90D871F54D8^0'
+'-25100A513E235A^0'
+'-D04ADA0ED06DB8^0'
+'-3839AB9839EBE8^0'
+'-97513BE4D06F08^-4'
+'-3E5B58EC61176C^-2'
+'-249C7B7EB50B86^-2'
+'84D96AF490FE78^0'
+'-2518604B9C87C4^0'
+'-D0364B3DDBC888^0'
+'-3833E15E72974E^0'
+'-9B711108B0905^-4'
+'-3E6A69988A7198^-2'
+'-249A8B0AB7C118^-2'
+'854D44FB261A6^0'
+'-25386E30CAAE76^0'
+'-CFEBEE81DE31E^0'
+'-381FA856DAAF78^0'
+'-78E11491D5BFE^-4'
+'-3E0F8E934C067A^-2'
+'-246866B58971^-2'
+'85C2825C3F77E8^0'
+'-25587FBCED256^0'
+'-CFA0AD2FB56618^0'
+'-3809FFD5D42A8A^0'
+'-7B49782E59EC5^-4'
+'-3E04987E5FF724^-2'
+'-245B7829015B8^-2'
+'86350495A0515^0'
+'-2578148E459B6A^0'
+'-CF56A8B3656AB^0'
+'-37F52C346974F^0'
+'-AE5781B859EED^-4'
+'-3D0BBE446B31F4^-2'
+'-24187E0B6D3068^-2'
+'86A84D939B39E8^0'
+'-2595629109AB5C^0'
+'-CF0BE215B26828^0'
+'-37E16AA03DC706^0'
+'-9F8D4E6B9FFA5^-4'
+'-3D2D25129A8594^-2'
+'-241F0F6418B59E^-2'
+'871A7E9F6C5E7^0'
+'-25B4E0B58BB7E6^0'
+'-CEC15E24309968^0'
+'-37CC7497F48D2C^0'
+'-8BFB399E127AF^-4'
+'-3D35528B677E7A^-2'
+'-24291D706693F6^-2'
+'878D8817FA2C2^0'
+'-25D4B4613F59B6^0'
+'-CE75BFDCB19DC^0'
+'-37B7E4CACAC73^0'
+'-98B066C759711^-4'
+'-3CE6AF25021256^-2'
+'-23C1FF80639FF^-2'
+'880040A9168E18^0'
+'-25F272C5FE33B8^0'
+'-CE2A61A77E5358^0'
+'-37A32AA94F9A26^0'
+'-C81380186130B^-4'
+'-3D364EF4F5F096^-2'
+'-23C01310AB1992^-2'
+'8871066C9B6AF^0'
+'-2610D9B9AF56EA^0'
+'-CDDFD5D19FBC38^0'
+'-378E4FBB138DDE^0'
+'-81980F4F53C11^-4'
+'-3CD871C936227A^-2'
+'-23AB3983C1B468^-2'
+'88E1931E8F8C68^0'
+'-262FC96791E354^0'
+'-CD9530EF3A8F1^0'
+'-37789E64AAE1A2^0'
+'-81E6D25A3C246^-4'
+'-3C71C490EF17DA^-2'
+'-23C3C77719A19A^-2'
+'893E671FE72B28^0'
+'-2647D8C5A727F^0'
+'-CD5760017204A^0'
+'-37679F1E2E83CA^0'
+'-A42413ABEA34B8^-4'
+'-3CEBC1714CA468^-2'
+'-240783A603330C^-2'
+'1D956C1AD^9'
+'1D956C2C5^9'
+'1D956C6C5^9'
+'1D956CAC5^9'
+'1D956CEC5^9'
+'1D956D2C5^9'
+'1D956D6C5^9'
+'1D956DAC5^9'
+'1D956DEC5^9'
+'1D956E2C5^9'
+'1D956E6C5^9'
+'1D956EA05^9'
+'1D956C1AD^9'
+'1^1'
+'C^1'
+END_ARRAY 1 99
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/acpaquette/lroc_nac/ab103105.spice.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/JNCR_2016240_01M06152_V01/naif0012.tls b/tests/pytests/data/JNCR_2016240_01M06152_V01/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/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/JNCR_2016240_01M06152_V01/pck00010.tpc b/tests/pytests/data/JNCR_2016240_01M06152_V01/pck00010.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..afbf0455544331d33763b83ae01a54369c579700
--- /dev/null
+++ b/tests/pytests/data/JNCR_2016240_01M06152_V01/pck00010.tpc
@@ -0,0 +1,4093 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "pck00010.tpc"
+MISSION_NAME = JUNO
+SPACECRAFT_NAME = JUNO
+DATA_SET_ID = "JNO-J/E/SS-SPICE-6-V1.0"
+KERNEL_TYPE_ID = PCK
+PRODUCT_ID = "pck00010.tpc"
+PRODUCT_CREATION_TIME = 2017-06-06T18:23:16
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = JUPITER
+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 text PCK file containing constants
+from the IAU 2009 report, created by NAIF, JPL. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2011 October 21
+
+
+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
+ 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/naif/data
+
+
+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, planets, and
+ Pluto. Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole value
+ for the epochs 2012
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids
+
+ Davida
+ Eros
+ Gaspra
+ Ida
+ Itokawa
+ Lutetia
+ Pallas
+ Steins
+ Vesta
+
+ -- Orientation constants for comets
+
+ 19P/Borrelly
+ 9P/Tempel 1
+
+
+ Orientation data provided in this file are used
+ by the SPICE Toolkit to evaluate the orientation
+ of body-fixed, body-centered reference frames
+ with respect to the ICRF frame ("J2000" in
+ SPICE documentation). These body-fixed frames
+ have names of the form
+
+ IAU_<body name>
+
+ for example
+
+ IAU_JUPITER
+
+ See the PCK Required Reading file pck.req for details.
+
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun, planets, and Pluto
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids
+
+ Ceres
+ Davida
+ Eros
+ Gaspra
+ Ida
+ Itokawa
+ Lutetia
+ Mathilde
+ Steins
+ Toutatis
+ Vesta
+
+ -- Radii of comets
+
+ 19P/Borrelly
+ 81P/Wild 2
+ 9P/Tempel 1
+ Halley
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on October 21, 2011 at NASA's Navigation and
+ Ancillary Information Facility (NAIF), located at the Jet
+ Propulsion Laboratory, Pasadena, CA.
+
+ The previous version of the file was
+
+ pck00009.tpc
+
+ That file was published March 3 2010.
+
+ This version incorporates data from reference [1]. This file
+ contains size, shape, and orientation data for all objects covered
+ by the previous version of the file.
+
+ New objects covered by this file but not the previous
+ version are:
+
+ Anthe
+ Daphnis
+ Davida
+ Lutetia
+ Methone
+ Pallas
+ Pallene
+ Polydeuces
+ Steins
+
+
+
+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, version description section, and file name
+ if you modify this file.
+
+ A user-modified file should be thoroughly tested before
+ being published or otherwise distributed.
+
+ P_constants files must conform to the standards described
+ in the two SPICE technical reference documents:
+
+ PCK Required Reading
+ Kernel Required Reading
+
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU 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]), corresponding to the SPICE reference frame name
+ IAU_EARTH, 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. These files provide orientation data
+ for the ITRF93 (terrestrial) reference frame relative to the
+ ICRF.
+
+ 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 first date in the file name, meaning 2000 January 1, is the
+ file's coverage begin time. 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. The
+ SPICE reference frame name corresponding to this model is
+ IAU_MOON.
+
+ A more accurate approximation can be obtained by using both the
+ NAIF lunar frame kernel and the binary lunar orientation PCK file.
+ These files provide orientation data for the both the Mean
+ Earth/Polar Axis frame, which has the SPICE name MOON_ME, and the
+ Lunar Principal Axes frame, which has the SPICE name MOON_PA.
+
+ These files 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
+ epoch 2012.0 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] and [11].
+
+
+ Prime meridian offsets
+ ----------------------
+
+ Prime meridian offset kernel variables, which have names
+ of the form
+
+ BODYnnn_LONG_AXIS
+
+ are not used by SPICE geometry software. These variables should be
+ considered deprecated; however, they will be retained for
+ backwards compatibility.
+
+ Users wishing to specify an offset reflecting the orientation of a
+ reference ellipsoid relative to a body-fixed reference frame
+ specified here should do so by creating a constant-offset frame
+ (also called a "TK" frame) specification. See the Frames Required
+ Reading frames.req for details.
+
+ The Mars prime meridian offset given by [5] 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 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 and References
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] Archinal, B.A., A'Hearn, M.F., Bowell, E., Conrad, A.,
+ Consolmagno, G.J., Courtin, R., Fukushima, T.,
+ Hestroffer, D., Hilton, J.L., Krasinsky, G.A.,
+ Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P.,
+ Tholen, D.J., Thomas, P.C., and Williams, I.P.
+ "Report of the IAU Working Group on Cartographic Coordinates
+ and Rotational Elements: 2009."
+
+ [2] Archinal, B.A., A'Hearn, M.F., Conrad, A.,
+ Consolmagno, G.J., Courtin, R., Fukushima, T.,
+ Hestroffer, D., Hilton, J.L., Krasinsky, G.A.,
+ Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P.,
+ Tholen, D.J., Thomas, P.C., and Williams, I.P.
+ "Erratum to: Reports of the IAU Working Group on
+ Cartographic Coordinates and Rotational Elements: 2006 &
+ 2009."
+
+ [3] 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."
+
+ [4] 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.
+
+ [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.
+
+ [11] International Association of Geomagnetism and Aeronomy
+ Web page: "International Geomagnetic Reference Field."
+ Discussion URL:
+
+ http://www.ngdc.noaa.gov/IAGA/vmod/igrf.html
+
+ Coefficients URL:
+
+ http://www.ngdc.noaa.gov/IAGA/vmod/igrf11coeffs.txt
+
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [4].
+
+ -- Prime meridian constant (W0) terms for Pluto, Charon,
+ and Ida are from [2].
+
+ -- 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
+ [11]. The values were also computed from the 11th
+ generation IGRF by Nat Bachman.
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00009.tpc dated March 3, 2010. Most of these values came
+ from the 2006 IAU report [3].
+
+
+
+
+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 = ( 6378.1366 6378.1366 6356.7519 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.1366
+ 6378.1366
+ 6356.7519 )
+
+ 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 2009 IAU 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 12:00:00 TDB, Julian ephemeris
+ date 2451545.0 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 inertial 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 (2000 Jan 1
+ 12:00:00 TDB), 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: 2009 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 = ( 284.95 870.5360000 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 is a deprecated feature; see the note on "Prime meridian
+ offsets" under "Known Limitations and Caveats" above.
+
+ 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 2009 IAU
+ report [1] does not use any other models, except in the case of
+ Mars, where separate values are given for the north and south
+ polar radii. In this file, we provide as a datum the mean Mars
+ polar radius provided by [1]. The North and South values are
+ included as comments.
+
+ 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 = ( 6378.1366 6378.1366 6356.7519 )
+
+
+
+Body Numbers and Names
+--------------------------------------------------------
+
+
+ The following NAIF body ID codes and body names appear in this
+ file. See the NAIF IDs Required Reading file naif_ids.req for
+ a detailed discussion and a complete list of ID codes 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 632 Methone 633 Pallene
+ 634 Polydeuces 635 Daphnis 649 Anthe
+
+
+ 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
+ 2000002 Asteroid Pallas
+ 2000004 Asteroid Vesta
+ 2000021 Asteroid Lutetia
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2000511 Asteroid Davida
+ 2002867 Asteroid Steins
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ 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 from the 2006 IAU report.
+
+ body199_pole_ra = ( 281.01 -0.033 0. )
+ body199_pole_dec = ( 61.45 -0.005 0. )
+ body199_pm = ( 329.548 6.1385025 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.0097 -0.0328 0. )
+ BODY199_POLE_DEC = ( 61.4143 -0.0049 0. )
+ BODY199_PM = ( 329.5469 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ BODY199_NUT_PREC_RA = ( 0. 0. 0. 0. 0. )
+
+ BODY199_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. )
+
+ BODY199_NUT_PREC_PM = ( 0.00993822
+ -0.00104581
+ -0.00010280
+ -0.00002364
+ -0.00000532 )
+ \begintext
+
+ 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:
+
+ 174.791086 4.092335
+ 349.582171 8.184670
+ 164.373257 12.277005
+ 339.164343 16.369340
+ 153.955429 20.461675
+
+
+ \begindata
+
+ BODY1_NUT_PREC_ANGLES = ( 174.791086 0.14947253587500003E+06
+ 349.582171 0.29894507175000006E+06
+ 164.373257 0.44841760762500006E+06
+ 339.164343 0.59789014350000012E+06
+ 153.955429 0.74736267937499995E+06 )
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2009 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 2009 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:
+
+ 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
+
+ Original 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 )
+
+ Previous values:
+
+ body399_n_geomag_ctr_dipole_lon = ( 288.43 )
+ body399_n_geomag_ctr_dipole_lat = ( 79.54 )
+
+
+ Current values:
+
+ Values are given for the epoch 2012.0 and were derived
+ by Nat Bachman from constants provided by [11].
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 287.62 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 80.13 )
+
+ \begintext
+
+
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2009 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:
+
+ The rotation rate is from the 2006 IAU report; all other
+ values are unchanged in the 2009 report.
+
+ body599_pm = ( 284.95 870.5366420 0. )
+
+
+ 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 = ( 284.95 870.5360000 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 from the 2006 IAU report.
+
+
+ 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. )
+
+
+ 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.
+
+
+ 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 )
+
+
+ Current values:
+
+
+ The change from the previous set of values is the
+ removal of S7. This causes BODY6_NUT_PREC_ANGLES
+ elements that formerly corresponded to 2*S1 and 2*S1
+ to be shifted toward the start of the array.
+
+ \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 six angles given here are the angles S1
+ through S6 from the 2009 report; the seventh and
+ eigth 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
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2009 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 2009 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
+
+
+
+
+Orientation Constants for the Dwarf Planet Pluto
+--------------------------------------------------------
+
+Pluto
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ Due to the new definition of planetocentric coordinates
+ for small bodies, and to the reclassification of Pluto
+ as a dwarf planet, Pluto's north pole direction has been
+ inverted.
+
+ The PM constant W0 is from [2].
+
+ \begindata
+
+ BODY999_POLE_RA = ( 132.993 0. 0. )
+ BODY999_POLE_DEC = ( -6.163 0. 0. )
+ BODY999_PM = ( 302.695 56.3625225 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2009 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 2009 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 2009 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 2009 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 unchanged in the 2009 IAU report.
+
+
+ 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 from the 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY601_POLE_RA = ( 40.66 -0.036 0. )
+ BODY601_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY601_PM = ( 333.46 381.9945550 0. )
+ BODY601_LONG_AXIS = ( 0. )
+
+ BODY601_NUT_PREC_RA = ( 0. 0. 13.56 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_DEC = ( 0. 0. -1.53 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_PM = ( 0. 0. -13.48 0. -44.85 0. 0. 0. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY602_POLE_RA = ( 40.66 -0.036 0. )
+ BODY602_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY602_PM = ( 6.32 262.7318996 0. )
+ BODY602_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY603_POLE_RA = ( 40.66 -0.036 0. )
+ BODY603_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY603_PM = ( 8.95 190.6979085 0. )
+ BODY603_LONG_AXIS = ( 0. )
+
+ BODY603_NUT_PREC_RA = ( 0. 0. 0. 9.66 0. 0. 0. 0. )
+ BODY603_NUT_PREC_DEC = ( 0. 0. 0. -1.09 0. 0. 0. 0. )
+ BODY603_NUT_PREC_PM = ( 0. 0. 0. -9.60 2.23 0. 0. 0. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY604_POLE_RA = ( 40.66 -0.036 0. )
+ BODY604_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY604_PM = ( 357.6 131.5349316 0. )
+ BODY604_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are from the 2009 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ Data values are unchanged in the 2009 IAU report. However
+ the kernel variable contents have changed due to removal of
+ the angle S7.
+
+ \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. )
+ BODY605_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. -0.35 0. 0. )
+ BODY605_NUT_PREC_PM = ( 0. 0. 0. 0. 0. -3.08 0. 0. )
+
+ \begintext
+
+
+
+ Titan
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ 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 )
+
+
+ Current values:
+
+ Note removal of dependence on the nutation precession
+ angles.
+
+ \begindata
+
+ BODY606_POLE_RA = ( 39.4827 0. 0. )
+ BODY606_POLE_DEC = ( 83.4279 0. 0. )
+ BODY606_PM = ( 186.5855 22.5769768 0. )
+ BODY606_LONG_AXIS = ( 0. )
+
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 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 from the 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY608_POLE_RA = ( 318.16 -3.949 0. )
+ BODY608_POLE_DEC = ( 75.03 -1.143 0. )
+ BODY608_PM = ( 355.2 4.5379572 0. )
+ BODY608_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ 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 2009 IAU report.
+
+
+ Current values:
+
+ Data values are unchanged in the 2009 IAU report. However
+ the kernel variable contents have changed due to removal of
+ the angle S7.
+
+ \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. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ Data values are unchanged in the 2009 IAU report. However
+ the kernel variable contents have changed due to removal of
+ the angle S7.
+
+ \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. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2009 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (notes following table 2).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2009 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 2009 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 2009 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 2009 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 2009 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 2009 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 2006 IAU report.
+
+ 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. )
+
+
+ Current values:
+
+ Due to the new definition of planetocentric coordinates
+ for small bodies, and to the reclassification of Pluto
+ as a dwarf planet, Charon's north pole direction has been
+ inverted.
+
+ The PM constant W0 is from [2].
+
+ \begindata
+
+ BODY901_POLE_RA = ( 132.993 0. 0. )
+ BODY901_POLE_DEC = ( -6.163 0. 0. )
+ BODY901_PM = ( 122.695 56.3625225 0. )
+ BODY901_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+Ceres
+
+ Current values:
+
+ \begindata
+
+ BODY2000001_POLE_RA = ( 291. 0. 0. )
+ BODY2000001_POLE_DEC = ( 59. 0. 0. )
+ BODY2000001_PM = ( 170.90 952.1532 0. )
+ BODY2000001_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Pallas
+
+ Current values:
+
+ \begindata
+
+ BODY2000002_POLE_RA = ( 33. 0. 0. )
+ BODY2000002_POLE_DEC = ( -3. 0. 0. )
+ BODY2000002_PM = ( 38. 1105.8036 0. )
+ BODY2000002_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Vesta
+
+ Old values:
+
+ Values are from the 2009 IAU report.
+
+ body2000004_pole_ra = ( 301. 0. 0. )
+ body2000004_pole_dec = ( 41. 0. 0. )
+ body2000004_pm = ( 292. 1617.332776 0. )
+ body2000004_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 305.8 0. 0. )
+ BODY2000004_POLE_DEC = ( 41.4 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Lutetia
+
+ Current values:
+
+ \begindata
+
+ BODY2000021_POLE_RA = ( 52. 0. 0. )
+ BODY2000021_POLE_DEC = ( 12. 0. 0. )
+ BODY2000021_PM = ( 94. 1057.7515 0. )
+ BODY2000021_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Ida
+
+ Old values:
+
+ 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. )
+
+ Current values:
+
+ The PM constant W0 is from [2].
+
+ \begindata
+
+ BODY2431010_POLE_RA = ( 168.76 0. 0. )
+ BODY2431010_POLE_DEC = ( -2.88 0. 0. )
+ BODY2431010_PM = ( 274.05 +1864.6280070 0. )
+ BODY2431010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2009 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
+
+
+
+Davida
+
+ Current values:
+
+ \begindata
+
+ BODY2000511_POLE_RA = ( 297. 0. 0. )
+ BODY2000511_POLE_DEC = ( 5. 0. 0. )
+ BODY2000511_PM = ( 268.1 1684.4193549 0. )
+ BODY2000511_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2009 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
+
+
+
+Steins
+
+ Current values:
+
+ \begindata
+
+ BODY2002867_POLE_RA = ( 90. 0. 0. )
+ BODY2002867_POLE_DEC = ( -62. 0. 0. )
+ BODY2002867_PM = ( 93.94 1428.852332 0. )
+ BODY2002867_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Itokawa
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ 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
+
+
+
+9P/Tempel 1
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ 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
+
+
+
+19P/Borrelly
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ 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
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body399_radii = ( 6378.14 6378.14 6356.75 )
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.1366 6378.1366 6356.7519 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+
+ Current values:
+
+ The 2009 IAU report gives separate values for the north and
+ south polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ The report provides the average of these values as well,
+ which we use 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 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Radii of the Dwarf Planet Pluto
+--------------------------------------------------------
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ body401_radii = ( 13.4 11.2 9.2 )
+ body402_radii = ( 7.5 6.1 5.2 )
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.0 11.4 9.1 )
+ BODY402_RADII = ( 7.8 6.0 5.1 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report,
+ except for those of Europa, Ganymede, Callisto,
+ and Metis. For Metis, now all three radii are
+ provided.
+
+ body502_radii = ( 1564.13 1561.23 1560.93 )
+ body503_radii = ( 2632.4 2632.29 2632.35 )
+ body504_radii = ( 2409.4 2409.2 2409.3 )
+
+ 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.
+
+ body516_radii = ( 21.5 21.5 21.5 )
+
+
+
+
+ Current values:
+
+ Note that for Ganymede and Callisto only mean radii
+ are provided.
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.4 1815.7 )
+ BODY502_RADII = ( 1562.6 1560.3 1559.5 )
+ BODY503_RADII = ( 2631.2 2631.2 2631.2 )
+ BODY504_RADII = ( 2410.3 2410.3 2410.3 )
+ 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 )
+ BODY516_RADII = ( 30 20 17 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2006 IAU report.
+
+ 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 )
+
+
+ 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.
+
+ 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 )
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ body618_radii = ( 10 10 10 )
+
+
+
+ Current values:
+
+ \begindata
+
+ BODY601_RADII = ( 207.8 196.7 190.6 )
+ BODY602_RADII = ( 256.6 251.4 248.3 )
+ BODY603_RADII = ( 538.4 528.3 526.3 )
+ BODY604_RADII = ( 563.4 561.3 559.6 )
+ BODY605_RADII = ( 765.0 763.1 762.4 )
+ BODY606_RADII = ( 2575.15 2574.78 2574.47 )
+ BODY607_RADII = ( 180.1 133.0 102.7 )
+ BODY608_RADII = ( 745.7 745.7 712.1 )
+ BODY609_RADII = ( 109.4 108.5 101.8 )
+ BODY610_RADII = ( 101.5 92.5 76.3 )
+ BODY611_RADII = ( 64.9 57.0 53.1 )
+ BODY612_RADII = ( 21.7 19.1 13.0 )
+ BODY613_RADII = ( 16.3 11.8 10.0 )
+ BODY614_RADII = ( 15.1 11.5 7.0 )
+ BODY615_RADII = ( 20.4 17.7 9.4 )
+ BODY616_RADII = ( 67.8 39.7 29.7 )
+ BODY617_RADII = ( 52.0 40.5 32.0 )
+ BODY618_RADII = ( 17.2 15.7 10.4 )
+
+ BODY632_RADII = ( 1.6 1.6 1.6 )
+ BODY633_RADII = ( 2.9 2.8 2.0 )
+ BODY634_RADII = ( 1.5 1.2 1.0 )
+ BODY635_RADII = ( 4.3 4.1 3.2 )
+ BODY649_RADII = ( 1 1 1 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2009 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 2009 IAU report.
+
+ Current values:
+
+ The 2009 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 2009
+ report. The available values are:
+
+ BODY807_RADII = ( 104 --- 89 )
+
+ For use within the SPICE system, we use only the mean radius.
+
+ \begindata
+
+ BODY807_RADII = ( 96 96 96 )
+ BODY808_RADII = ( 218 208 201 )
+
+ \begintext
+
+
+
+
+Satellites of Pluto
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+
+
+Ceres
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+
+Vesta
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+
+Lutetia
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000021_RADII = ( 62.0 50.5 46.5 )
+
+ \begintext
+
+
+
+Ida
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+Mathilde
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+
+
+Eros
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+
+Davida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000511_RADII = ( 180. 147. 127. )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+Steins
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2002867_RADII = ( 3.24 2.73 2.04 )
+
+ \begintext
+
+
+
+Toutatis
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \begintext
+
+
+
+Itokawa
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \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 2009 report.
+
+
+
+
+
+Halley
+
+
+ Old values:
+
+ Values are unchanged in the 2009 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Old values:
+
+ The effective radius is unchanged in the 2009 IAU report.
+
+ 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
+
+
+19P/Borrelly
+
+
+ Old values:
+
+ Values are unchanged in the 2009 report.
+
+ 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
+
+
+
+81P/Wild 2
+
+
+ Old values:
+
+ Values are unchanged in the 2009 report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00010.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/test_juno_drivers.py b/tests/pytests/test_juno_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..e2700ee11769bb8b82e96688446a2cf88b61ba9d
--- /dev/null
+++ b/tests/pytests/test_juno_drivers.py
@@ -0,0 +1,154 @@
+import os
+import json
+import unittest
+from unittest.mock import patch, PropertyMock
+
+import pytest
+import numpy as np
+import spiceypy as spice
+
+import ale
+from ale.drivers.juno_drivers import JunoJunoCamIsisLabelNaifSpiceDriver
+from ale.base.data_naif import NaifSpice
+
+from conftest import get_image_kernels, convert_kernels, get_image_label, compare_dicts
+
+@pytest.fixture()
+def isis_compare_dict():
+ return {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY599_RADII': np.array([71492., 71492., 66854.]),
+ 'BODY_FRAME_CODE': 10015,
+ 'BODY_CODE': 599,
+ 'INS-61500_ITRANSS': np.array([ 0. , 135.1351, 0. ]),
+ 'INS-61500_DISTORTION_K1': -5.962420945566733e-08,
+ 'INS-61500_DISTORTION_K2': 2.738191004225615e-14,
+ 'FRAME_-61500_CLASS_ID': -61500.0,
+ 'INS-61500_BORESIGHT': np.array([0., 0., 1.]),
+ 'TKFRAME_-61500_RELATIVE': 'JUNO_JUNOCAM_CUBE',
+ 'INS-61500_BORESIGHT_SAMPLE': 814.21,
+ 'INS-61500_FOV_SHAPE': 'POLYGON',
+ 'INS-61500_FILTER_OFFSET': 1.0,
+ 'INS-61500_SWAP_OBSERVER_TARGET': 'TRUE',
+ 'INS-61500_LIGHTTIME_CORRECTION': 'NONE',
+ 'INS-61500_FOV_BOUNDARY_CORNERS': np.array([-0.47351727, -0.18862601, 0.86034971, -0.47852984, -0.11376363,
+ 0.87067045, -0.47934991, -0.09577177, 0.87238262, -0.48125208]),
+ 'INS-61500_PIXEL_PITCH': 0.0074,
+ 'INS-61500_FOV_FRAME': 'JUNO_JUNOCAM',
+ 'TKFRAME_-61500_ANGLES': np.array([ 0.69 , -0.469, 0.583]),
+ 'FRAME_-61500_CENTER': -61.0,
+ 'FRAME_-61500_CLASS': 4.0,
+ 'FRAME_-61500_NAME': 'JUNO_JUNOCAM',
+ 'INS-61500_LT_SURFACE_CORRECT': 'FALSE',
+ 'TKFRAME_-61500_AXES': np.array([3., 2., 1.]),
+ 'INS-61500_PIXEL_SIZE': 0.0074,
+ 'TKFRAME_-61500_SPEC': 'ANGLES',
+ 'INS-61500_DISTORTION_X': 814.21,
+ 'INS-61500_DISTORTION_Y': 78.48,
+ 'INS-61500_BORESIGHT_LINE': 600.0,
+ 'INS-61500_FILTER_LINES': 1200.0,
+ 'INS-61500_INTERFRAME_DELTA': 0.001,
+ 'INS-61500_FILTER_NAME': 'FULLCCD',
+ 'INS-61500_TRANSX': np.array([0. , 0.0074, 0. ]),
+ 'INS-61500_TRANSY': np.array([0. , 0. , 0.0074]),
+ 'TKFRAME_-61500_UNITS': 'DEGREES',
+ 'INS-61500_ITRANSL': np.array([ 0. , 0. , 135.1351]),
+ 'INS-61500_START_TIME_BIAS': 0.06188,
+ 'INS-61500_FOCAL_LENGTH': 10.95637,
+ 'INS-61500_FILTER_SAMPLES': 1648.0,
+ 'BODY599_PM': np.array([284.95 , 870.536, 0. ]),
+ 'BODY599_LONG_AXIS': 0.0,
+ 'BODY599_NUT_PREC_DEC': np.array([0., 0., 0., 0., 0., 0., 0., 0., 0., 0.]),
+ 'BODY599_NUT_PREC_PM': np.array([0., 0., 0., 0., 0., 0., 0., 0., 0., 0.]),
+ 'BODY599_POLE_RA': np.array([ 2.68056595e+02, -6.49900000e-03, 0.00000000e+00]),
+ 'BODY599_POLE_DEC': np.array([6.4495303e+01, 2.4130000e-03, 0.0000000e+00]),
+ 'BODY599_NUT_PREC_RA': np.array([0., 0., 0., 0., 0., 0., 0., 0., 0., 0.]),
+ 'INS-61504_DISTORTION_K1': -5.962420945566733e-08,
+ 'INS-61504_DISTORTION_K2': 2.738191004225615e-14,
+ 'INS-61504_START_TIME_BIAS': 0.06188,
+ 'INS-61504_FOV_FRAME': 'JUNO_JUNOCAM',
+ 'INS-61504_FILTER_OFFSET': 284.52,
+ 'INS-61504_FILTER_NAME': 'METHANE',
+ 'INS-61504_FOV_BOUNDARY_CORNERS': np.array([-0.47351727, -0.18862601, 0.86034971, -0.47852984, -0.11376363,
+ 0.87067045, 0.49067337, -0.11299511, 0.86398596, 0.48553839]),
+ 'INS-61504_INTERFRAME_DELTA': 0.001,
+ 'INS-61504_FILTER_SAMPLES': 1648.0,
+ 'INS-61504_DISTORTION_X': 814.21,
+ 'INS-61504_DISTORTION_Y': 315.48,
+ 'INS-61504_PIXEL_SIZE': 0.0074,
+ 'INS-61504_FILTER_LINES': 128.0,
+ 'INS-61504_BORESIGHT': np.array([ 0.00854687, -0.16805056, 0.98574133]),
+ 'INS-61504_FOCAL_LENGTH': 10.95637,
+ 'INS-61504_FOV_SHAPE': 'RECTANGLE'},
+ 'InstrumentPointing': {'TimeDependentFrames': [-61000, 1],
+ 'CkTableStartTime': 525560475.1286545,
+ 'CkTableEndTime': 525560475.1286545,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': np.array([5.25560475e+08]),
+ 'Quaternions': np.array([[-0.42623555, -0.55051779, 0.46456631, -0.5472034 ]]),
+ 'AngularVelocity': np.array([[ 0.204182 , -0.00811453, -0.00786116]]),
+ 'ConstantFrames': [-61500, -61505, -61000],
+ 'ConstantRotation': np.array([ 0.0022409695777088, -0.002220557600931,
+ -0.99999502357726, 0.012486301868467,
+ -0.99991951530675, 0.0022483714915059,
+ -0.99991953192294, -0.012491278263463,
+ -0.0022130626614382])},
+ 'BodyRotation': {'TimeDependentFrames': [10015, 1],
+ 'CkTableStartTime': 525560475.1286545,
+ 'CkTableEndTime': 525560475.1286545,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': np.array([5.25560475e+08]),
+ 'Quaternions': np.array([[-0.89966963, 0.20059167, -0.09209383, 0.37666467]]),
+ 'AngularVelocity': np.array([[-2.56683271e-06, -7.56713067e-05, 1.58718697e-04]])},
+ 'InstrumentPosition': {'SpkTableStartTime': 525560475.1286545,
+ 'SpkTableEndTime': 525560475.1286545,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [525560475.1286545],
+ 'Positions': np.array([[ -7197.04131196, -382913.71404775, 145608.88474678]]),
+ 'Velocities': np.array([[ 0.39087306, 24.13639337, 2.15702628]])},
+ 'SunPosition': {'SpkTableStartTime': 525560475.0262545,
+ 'SpkTableEndTime': 525560475.0262545,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': np.array([5.25560475e+08]),
+ 'Positions': np.array([[814823700.57661,22018509.45354,-10399060.67075]]),
+ 'Velocities': np.array([[-0.10070347311145,11.449085311077,4.9098525890309]])}}
+
+@pytest.fixture(scope='module')
+def test_kernels():
+ kernels = get_image_kernels('JNCR_2016240_01M06152_V01')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+@pytest.mark.parametrize("label_type", ['isis3'])
+@pytest.mark.parametrize("formatter", ['isis'])
+def test_mro_load(test_kernels, label_type, formatter, isis_compare_dict):
+ label_file = get_image_label('JNCR_2016240_01M06152_V01', label_type)
+
+ usgscsm_isd_str = ale.loads(label_file, props={'kernels': test_kernels}, formatter=formatter)
+ usgscsm_isd_obj = json.loads(usgscsm_isd_str)
+ print(json.dumps(usgscsm_isd_obj, indent=4))
+
+ assert compare_dicts(usgscsm_isd_obj, isis_compare_dict) == []
+
+# ========= Test isislabel and naifspice driver =========
+class test_isis_naif(unittest.TestCase):
+
+ def setUp(self):
+ label = get_image_label("JNCR_2016240_01M06152_V01", "isis3")
+ self.driver = JunoJunoCamIsisLabelNaifSpiceDriver(label)
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "JUNO_JUNOCAM"
+
+ def test_ephemeris_start_time(self):
+ with patch('ale.base.data_naif.spice.scs2e', return_value=12345) as scs2e, \
+ patch('ale.drivers.juno_drivers.JunoJunoCamIsisLabelNaifSpiceDriver.naif_keywords', new_callable=PropertyMock) as naif_keywords, \
+ patch('ale.base.data_naif.spice.bods2c', return_value=-61500) as bods2c:
+ naif_keywords.return_value = {'INS-61500_INTERFRAME_DELTA': .1, 'INS-61500_START_TIME_BIAS': .1}
+ assert self.driver.ephemeris_start_time == 12348.446
+ scs2e.assert_called_with(-61500, '525560580:87')
+
+ def test_sensor_model_version(self):
+ assert self.driver.sensor_model_version == 1