diff --git a/ale/drivers/clementine_drivers.py b/ale/drivers/clementine_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..194b4e6c439a9e3ce71d5ac5427ec4ad604e4155
--- /dev/null
+++ b/ale/drivers/clementine_drivers.py
@@ -0,0 +1,111 @@
+import os
+import spiceypy as spice
+import json
+import numpy as np
+import pvl
+
+import ale
+from ale.base import Driver
+from ale.base.label_isis import IsisLabel
+from ale.base.data_naif import NaifSpice
+from ale.base.type_distortion import RadialDistortion, NoDistortion
+from ale.base.type_sensor import Framer, LineScanner
+from ale.util import generate_kernels_from_cube
+from ale.base.type_sensor import Framer
+from ale.base.type_distortion import NoDistortion
+
+from ale import util
+
+
+class ClementineUvvisIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Driver):
+ """
+ Driver for reading Ultra-violet Invisible Spectrum ISIS3 Labels
+ """
+
+ @property
+ def instrument_id(self):
+ """
+ Returns an instrument id for uniquely identifying the instrument,
+ but often also used to be piped into Spice Kernels to acquire
+ IKIDS. Therefor they are the same ID that Spice expects in bods2c
+ calls. Expect instrument_id to be defined in the IsisLabel mixin.
+ This should be a string of the form NEAR EARTH ASTEROID RENDEZVOUS
+
+ Returns
+ -------
+ : str
+ instrument id
+ """
+ lookup_table = {
+ "UVVIS": "ULTRAVIOLET/VISIBLE CAMERA"
+ }
+ return lookup_table[super().instrument_id]
+
+ @property
+ def sensor_name(self):
+ """
+ Returns the name of the instrument
+
+ Returns
+ -------
+ : str
+ instrument name
+ """
+ filter = self.label["IsisCube"]['BandBin']['FilterName']
+ return "CLEM_" + super().instrument_id + "_" + filter
+
+ @property
+ def spacecraft_name(self):
+ """
+ Returns the name of the spacecraft
+
+ Returns
+ -------
+ : str
+ spacecraft name
+ """
+ return super().spacecraft_name.replace(" ", "_")
+
+ @property
+ def sensor_model_version(self):
+ """
+ Returns ISIS sensor model version
+
+ Returns
+ -------
+ : int
+ ISIS sensor model version
+ """
+ return 1
+
+ @property
+ def ephemeris_start_time(self):
+ return spice.utc2et(self.utc_start_time.strftime("%Y-%m-%d %H:%M:%S.%f"))
+
+ @property
+ def ephemeris_stop_time(self):
+ """
+ Returns the sum of the starting ephemeris time and the exposure duration.
+ Expects ephemeris start time and exposure duration to be defined. These
+ should be double precision numbers containing the ephemeris start and
+ exposure duration of the image.
+ Returns
+ -------
+ : double
+ Ephemeris stop time for an image
+ """
+ return self.ephemeris_start_time + self.exposure_duration
+
+ @property
+ def ikid(self):
+ """
+ Overridden to grab the ikid from the Isis Cube since there is no way to
+ obtain this value with a spice bods2c call. Isis sets this value during
+ ingestion, based on the original fits file.
+
+ Returns
+ -------
+ : int
+ Naif ID used to for identifying the instrument in Spice kernels
+ """
+ return self.label["IsisCube"]["Kernels"]["NaifFrameCode"]
diff --git a/notebooks/write_MsiIsisLabelNaifSpiceDriver.ipynb b/notebooks/write_MsiIsisLabelNaifSpiceDriver.ipynb
deleted file mode 100644
index 9552ccf438aef5edf5c522b2404300a7786519f1..0000000000000000000000000000000000000000
--- a/notebooks/write_MsiIsisLabelNaifSpiceDriver.ipynb
+++ /dev/null
@@ -1,1419 +0,0 @@
-{
- "cells": [
- {
- "cell_type": "code",
- "execution_count": 1,
- "id": "e6ee49c3",
- "metadata": {},
- "outputs": [],
- "source": [
- "# You will need the ISISDATA area in your environment to get the appropriate kernel paths\n",
- "import os\n",
- "os.environ[\"ISISDATA\"] = \"/Users/ahibl/working/astro/local_isis_data/\"\n",
- "os.environ[\"ISISTESTDATA\"] = \"/Users/ahibl/astro_efs/isis_testData/\"\n",
- "os.environ[\"ISISROOT\"] = \"/Users/ahibl/working/astro/ISIS3/build/\"\n",
- "os.environ[\"ALESPICEROOT\"] = \"/Users/ahibl/astro_efs/usgs_data/\"\n",
- "\n",
- "import spiceypy as spice\n",
- "import json\n",
- "import numpy as np\n",
- "import pvl\n",
- "\n",
- "import ale\n",
- "from ale.base import Driver\n",
- "from ale.base.label_isis import IsisLabel\n",
- "from ale.base.data_naif import NaifSpice\n",
- "from ale.base.type_distortion import RadialDistortion, NoDistortion\n",
- "from ale.base.type_sensor import Framer, LineScanner\n",
- "from ale.util import generate_kernels_from_cube\n",
- "from ale.base.type_sensor import Framer\n",
- "from ale.base.type_distortion import NoDistortion\n",
- "from ale.drivers.msl_drivers import MslMastcamPds3NaifSpiceDriver\n",
- "from ale.formatters.usgscsm_formatter import to_usgscsm\n",
- "\n",
- "from ale import util\n",
- "from ale.util import generate_kernels_from_cube\n",
- "from ale.drivers import AleJsonEncoder, load, loads\n",
- "from ale.formatters.formatter import to_isd"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 2,
- "id": "6ef22a77",
- "metadata": {},
- "outputs": [
- {
- "data": {
- "text/plain": [
- "['/Users/ahibl/working/astro/local_isis_data//base/kernels/spk/de405.bsp',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/tspk/erosephem_1999004_2002181.bsp',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/spk/near_erosorbit_nav_v1.bsp',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/ck/near_2000056_v01.bc',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/fk/eros_fixed.tf',\n",
- " '/Users/ahibl/working/astro/local_isis_data//base/kernels/pck/pck00009.tpc',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/ik/msi15.ti',\n",
- " '/Users/ahibl/working/astro/local_isis_data//base/kernels/lsk/naif0012.tls',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/sclk/near_171.tsc',\n",
- " '/Users/ahibl/working/astro/local_isis_data//near/kernels/iak/msiAddendum002.ti']"
- ]
- },
- "execution_count": 2,
- "metadata": {},
- "output_type": "execute_result"
- }
- ],
- "source": [
- "# Generate kernels from an ISIS spiceinit'd label\n",
- "cube = \"/Users/ahibl/working/astro/img_data/MSI/cubes/ale/ale_spice01.cub\"\n",
- "kernels = generate_kernels_from_cube(cube, expand=True, format_as='list')\n",
- "kernels\n",
- "a\n",
- "# change to desired PDS3 image path\n",
- "#file_name = '/Users/ahibl/working/astro/img_data/0269ML0011790000106115E01_DRCX.lbl'\n",
- "\n",
- "# metakernels are furnished when entering the context (with block) with a driver instance\n",
- "# most driver constructors simply accept an image path \n",
- "#with MslMastcamPds3NaifSpiceDriver(file_name, props={'kernels': [\"/Users/ahibl/working/astro/rand/msl_2017_v01.tm\"]}) as driver:\n",
- " # pass driver instance into formatter function\n",
- " #usgscsmString = to_usgscsm(driver)"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 4,
- "id": "0721b82d",
- "metadata": {},
- "outputs": [
- {
- "ename": "NameError",
- "evalue": "name 'isis_isd' is not defined",
- "output_type": "error",
- "traceback": [
- "\u001b[0;31m---------------------------------------------------------------------------\u001b[0m",
- "\u001b[0;31mNameError\u001b[0m Traceback (most recent call last)",
- "Cell \u001b[0;32mIn [4], line 2\u001b[0m\n\u001b[1;32m 1\u001b[0m \u001b[38;5;28;01mwith\u001b[39;00m \u001b[38;5;28mopen\u001b[39m(\u001b[38;5;124m\"\u001b[39m\u001b[38;5;124m/Users/ahibl/working/astro/ISDs/msl_2.json\u001b[39m\u001b[38;5;124m\"\u001b[39m, \u001b[38;5;124m'\u001b[39m\u001b[38;5;124mw\u001b[39m\u001b[38;5;124m'\u001b[39m) \u001b[38;5;28;01mas\u001b[39;00m fp:\n\u001b[0;32m----> 2\u001b[0m json\u001b[38;5;241m.\u001b[39mdump(\u001b[43misis_isd\u001b[49m, fp, \u001b[38;5;28mcls\u001b[39m\u001b[38;5;241m=\u001b[39mAleJsonEncoder, indent\u001b[38;5;241m=\u001b[39m\u001b[38;5;241m2\u001b[39m)\n",
- "\u001b[0;31mNameError\u001b[0m: name 'isis_isd' is not defined"
- ]
- }
- ],
- "source": [
- "with open(\"/Users/ahibl/working/astro/ISDs/msl_2.json\", 'w') as fp:\n",
- " json.dump(ale_isd, fp, cls=AleJsonEncoder, indent=2)"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 4,
- "id": "2d21b857",
- "metadata": {},
- "outputs": [],
- "source": [
- "# Build new driver in this cell\n",
- "\n",
- "class MsiIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Driver):\n",
- " \n",
- " @property\n",
- " def instrument_id(self):\n",
- " \"\"\"\n",
- " Returns an instrument id for uniquely identifying the instrument,\n",
- " but often also used to be piped into Spice Kernels to acquire\n",
- " IKIDS. Therefor they are the same ID that Spice expects in bods2c\n",
- " calls. Expect instrument_id to be defined in the IsisLabel mixin.\n",
- " This should be a string of the form NEAR EARTH ASTEROID RENDEZVOUS\n",
- "\n",
- " Returns\n",
- " -------\n",
- " : str\n",
- " instrument id\n",
- " \"\"\"\n",
- " lookup_table = {\n",
- " \"MSI\": \"NEAR EARTH ASTEROID RENDEZVOUS\"\n",
- " }\n",
- " print(lookup_table[super().instrument_id])\n",
- " return lookup_table[super().instrument_id]\n",
- "\n",
- " @property\n",
- " def sensor_name(self):\n",
- " \"\"\"\n",
- " Returns the name of the instrument\n",
- "\n",
- " Returns\n",
- " -------\n",
- " : str\n",
- " instrument name\n",
- " \"\"\"\n",
- " return \"MULTI-SPECTRAL IMAGER\"\n",
- "\n",
- " @property\n",
- " def sensor_model_version(self):\n",
- " \"\"\"\n",
- " Returns ISIS sensor model version\n",
- "\n",
- " Returns\n",
- " -------\n",
- " : int\n",
- " ISIS sensor model version\n",
- " \"\"\"\n",
- " return 1\n",
- " \n",
- " # Overridden to remove decimal and 2multiply by a factor of 100 helps remove 2 fields issue cleanly\n",
- " @property\n",
- " def spacecraft_clock_start_count(self):\n",
- " \"\"\"\n",
- " The spacecraft clock start count, frequently used to determine the start time\n",
- " of the image.\n",
- "\n",
- " Returns\n",
- " -------\n",
- " : str\n",
- " spacecraft clock start count\n",
- " \"\"\"\n",
- " if 'SpacecraftClockStartCount' in self.label['IsisCube']['Instrument']:\n",
- " \n",
- " return str(self.label['IsisCube']['Instrument']['SpacecraftClockStartCount'])\n",
- " else:\n",
- " return None\n",
- "\n",
- " # Overridden to remove decimal and 2multiply by a factor of 100 helps remove 2 fields issue cleanly\n",
- " @property\n",
- " def spacecraft_clock_stop_count(self):\n",
- " \"\"\"\n",
- " The spacecraft clock stop count, frequently used to determine the stop time\n",
- " of the image.\n",
- "\n",
- " Returns\n",
- " -------\n",
- " : str\n",
- " spacecraft clock stop count\n",
- " \"\"\"\n",
- " if 'SpacecraftClockStopCount' in self.label['IsisCube']['Instrument']:\n",
- " return str(self.label['IsisCube']['Instrument']['SpacecraftClockStopCount'] * 100).replace(\".\",\"\")\n",
- " else:\n",
- " return None\n",
- "\n",
- " @property\n",
- " def ephemeris_stop_time(self):\n",
- " \"\"\"\n",
- " Returns the sum of the starting ephemeris time and the exposure duration.\n",
- " Expects ephemeris start time and exposure duration to be defined. These\n",
- " should be double precision numbers containing the ephemeris start and\n",
- " exposure duration of the image.\n",
- " Returns\n",
- " -------\n",
- " : double\n",
- " Ephemeris stop time for an image\n",
- " \"\"\"\n",
- " return self.ephemeris_start_time + self.exposure_duration\n",
- " \n",
- " @property\n",
- " def ikid(self):\n",
- " \"\"\"\n",
- " Overridden to grab the ikid from the Isis Cube since there is no way to\n",
- " obtain this value with a spice bods2c call. Isis sets this value during\n",
- " ingestion, based on the original fits file.\n",
- " \n",
- " Returns\n",
- " -------\n",
- " : int\n",
- " Naif ID used to for identifying the instrument in Spice kernels\n",
- " \"\"\"\n",
- " return self.label['IsisCube']['Kernels']['NaifFrameCode']\n",
- " "
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 7,
- "id": "27ed1125",
- "metadata": {},
- "outputs": [],
- "source": [
- "import pprint\n",
- "\n",
- "# Create ISD from ISIS label\n",
- "ale_file = \"/Users/ahibl/working/astro/img_data/MSI/cubes/ale/ale_spice01.cub\"\n",
- "#unspiced_file = \"/Users/ahibl/working/astro/img_data/MSI/ad_1.cub\"\n",
- "#isis_file = \"/Users/ahibl/working/astro/img_data/MSI/spicy_ad_1.cub\"\n",
- "\n",
- "with MsiIsisLabelNaifSpiceDriver(ale_file, props = {\"kernels\" : kernels}) as driver:\n",
- " ale_isd = to_isd(driver)\n",
- "\n",
- "#with MsiIsisLabelNaifSpiceDriver(isis_file, props = {\"kernels\" : kernels}) as driver:\n",
- " #isis_isd = to_isd(driver)\n",
- "\n",
- "#with MsiIsisLabelNaifSpiceDriver(unspiced_file, props = {\"kernels\" : kernels}) as driver:\n",
- " #unspicy_isd = to_isd(driver)\n",
- " \n",
- "#isds = [ale_isd, isis_isd, unspicy_isd]\n",
- "\n",
- "#pprint.pprint(isds[0])\n",
- "\n",
- "#print(\"\\n\\n\")\n",
- "\n",
- "#pprint.pprint(isds[1])\n",
- "\n",
- "#print(\"\\n\\n\")\n",
- "\n",
- "#pprint.pprint(isds[2])"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 12,
- "id": "24390fc9",
- "metadata": {},
- "outputs": [],
- "source": [
- "# with open(\"/Users/ahibl/working/astro/ISDs/msl_1.json\", 'w') as fp:\n",
- "# json.dump(usgscsmString, fp, cls=AleJsonEncoder, indent=2)"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": null,
- "id": "5c091e62",
- "metadata": {},
- "outputs": [],
- "source": [
- "file = \"/Users/ahibl/working/astro/ISIS3/isis/tests/data/near/msi2isis/test.cub\"\n",
- "\n",
- "with MsiIsisLabelNaifSpiceDriver(file, props = {\"kernels\" : kernels}) as driver:\n",
- " #test area"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 8,
- "id": "71e5d6cb",
- "metadata": {},
- "outputs": [],
- "source": [
- "# Write ISD to file\n",
- "with open(\"/Users/ahibl/working/astro/ISDs/msi_aled.json\", 'w') as fp:\n",
- " json.dump(ale_isd, fp, cls=AleJsonEncoder, indent=2)\n",
- "#with open(\"/Users/ahibl/working/astro/ISDs/msi_isis.json\", 'w') as fp:\n",
- "# json.dump(isis_isd, fp, cls=AleJsonEncoder, indent=2)\n",
- "#with open(\"/Users/ahibl/working/astro/ISDs/msi_unspiced.json\", 'w') as fp:\n",
- "# json.dump(unspicy_isd, fp, cls=AleJsonEncoder, indent=2)"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 3,
- "id": "85d6606d",
- "metadata": {},
- "outputs": [
- {
- "name": "stdout",
- "output_type": "stream",
- "text": [
- "Banana False False\n",
- "[<class 'ale.drivers.msi_drivers.MsiIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.osirisrex_drivers.OsirisRexCameraIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.galileo_drivers.GalileoSsiIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.clipper_drivers.ClipperEISNACFCIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.clipper_drivers.ClipperEISNACPBIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.clipper_drivers.ClipperEISWACFCIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.clipper_drivers.ClipperEISWACPBIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.dawn_drivers.DawnFcPds3NaifSpiceDriver'>, <class 'ale.drivers.co_drivers.CassiniIssIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.co_drivers.CassiniIssPds3LabelNaifSpiceDriver'>, <class 'ale.drivers.msl_drivers.MslMastcamPds3NaifSpiceDriver'>, <class 'ale.drivers.lro_drivers.LroLrocNacIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.lro_drivers.LroLrocNacPds3LabelNaifSpiceDriver'>, <class 'ale.drivers.lro_drivers.LroLrocWacIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.lro_drivers.LroMiniRfIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mex_drivers.MexHrscIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mex_drivers.MexHrscPds3NaifSpiceDriver'>, <class 'ale.drivers.mex_drivers.MexSrcPds3NaifSpiceDriver'>, <class 'ale.drivers.viking_drivers.VikingIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.chandrayaan_drivers.Chandrayaan1M3IsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mro_drivers.MroCrismIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mro_drivers.MroCtxIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mro_drivers.MroCtxPds3LabelNaifSpiceDriver'>, <class 'ale.drivers.mro_drivers.MroHiRiseIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mro_drivers.MroMarciIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.nh_drivers.NewHorizonsLeisaIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.nh_drivers.NewHorizonsLorriIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.nh_drivers.NewHorizonsMvicIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.nh_drivers.NewHorizonsMvicTdiIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.selene_drivers.KaguyaMiIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.selene_drivers.KaguyaMiPds3NaifSpiceDriver'>, <class 'ale.drivers.selene_drivers.KaguyaTcPds3NaifSpiceDriver'>, <class 'ale.drivers.mess_drivers.MessengerMdisIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.mess_drivers.MessengerMdisPds3NaifSpiceDriver'>, <class 'ale.drivers.voyager_drivers.VoyagerCameraIsisLabelNaifSpiceDriver'>, <class 'ale.drivers.co_drivers.CassiniIssIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.lro_drivers.LroLrocNacIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.lro_drivers.LroLrocWacIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.viking_drivers.VikingIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.mro_drivers.MroCtxIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.isis_ideal_drivers.IdealLsIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.selene_drivers.KaguyaTcIsisLabelIsisSpiceDriver'>, <class 'ale.drivers.mess_drivers.MessengerMdisIsisLabelIsisSpiceDriver'>]\n",
- "Attempting to pre-parse label file\n",
- "First parse attempt failed with\n",
- "(LexerError(...), 'Expecting an Aggregation Block, an Assignment Statement, or an End Statement, but found \"+\" : line 366 column 42 (char 8915) near \" = LT+S\\n \"')\n",
- "Successfully pre-parsed label file\n",
- "Trying <class 'ale.drivers.msi_drivers.MsiIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.osirisrex_drivers.OsirisRexCameraIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.galileo_drivers.GalileoSsiIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.clipper_drivers.ClipperEISNACFCIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.clipper_drivers.ClipperEISNACPBIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.clipper_drivers.ClipperEISWACFCIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.clipper_drivers.ClipperEISWACPBIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.dawn_drivers.DawnFcPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.co_drivers.CassiniIssIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.co_drivers.CassiniIssPds3LabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.msl_drivers.MslMastcamPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.lro_drivers.LroLrocNacIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.lro_drivers.LroLrocNacPds3LabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.lro_drivers.LroLrocWacIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.lro_drivers.LroMiniRfIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mex_drivers.MexHrscIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mex_drivers.MexHrscPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mex_drivers.MexSrcPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.viking_drivers.VikingIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.chandrayaan_drivers.Chandrayaan1M3IsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mro_drivers.MroCrismIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mro_drivers.MroCtxIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mro_drivers.MroCtxPds3LabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mro_drivers.MroHiRiseIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mro_drivers.MroMarciIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.nh_drivers.NewHorizonsLeisaIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.nh_drivers.NewHorizonsLorriIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.nh_drivers.NewHorizonsMvicIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.nh_drivers.NewHorizonsMvicTdiIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.selene_drivers.KaguyaMiIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.selene_drivers.KaguyaMiPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.selene_drivers.KaguyaTcPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mess_drivers.MessengerMdisIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mess_drivers.MessengerMdisPds3NaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.voyager_drivers.VoyagerCameraIsisLabelNaifSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.co_drivers.CassiniIssIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.lro_drivers.LroLrocNacIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.lro_drivers.LroLrocWacIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.viking_drivers.VikingIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mro_drivers.MroCtxIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.isis_ideal_drivers.IdealLsIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.selene_drivers.KaguyaTcIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n",
- "Trying <class 'ale.drivers.mess_drivers.MessengerMdisIsisLabelIsisSpiceDriver'>\n",
- "Failed: Expecting value: line 1 column 1 (char 0)\n",
- "\n"
- ]
- },
- {
- "name": "stderr",
- "output_type": "stream",
- "text": [
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n",
- "Traceback (most recent call last):\n",
- " File \"/Users/ahibl/working/astro/ale/ale/drivers/__init__.py\", line 153, in load\n",
- " res = driver(label, props=props, parsed_label=parsed_label)\n",
- " File \"/Users/ahibl/working/astro/ale/ale/base/base.py\", line 26, in __init__\n",
- " self._props = json.loads(props)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/__init__.py\", line 346, in loads\n",
- " return _default_decoder.decode(s)\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 337, in decode\n",
- " obj, end = self.raw_decode(s, idx=_w(s, 0).end())\n",
- " File \"/Users/ahibl/homebrew/Caskroom/miniconda/base/envs/ale-dvlp/lib/python3.10/json/decoder.py\", line 355, in raw_decode\n",
- " raise JSONDecodeError(\"Expecting value\", s, err.value) from None\n",
- "json.decoder.JSONDecodeError: Expecting value: line 1 column 1 (char 0)\n"
- ]
- },
- {
- "ename": "Exception",
- "evalue": "No Such Driver for Label",
- "output_type": "error",
- "traceback": [
- "\u001b[0;31m---------------------------------------------------------------------------\u001b[0m",
- "\u001b[0;31mException\u001b[0m Traceback (most recent call last)",
- "Cell \u001b[0;32mIn [3], line 2\u001b[0m\n\u001b[1;32m 1\u001b[0m file \u001b[38;5;241m=\u001b[39m \u001b[38;5;124m'\u001b[39m\u001b[38;5;124m/Users/ahibl/working/astro/img_data/MSI/labels/ale_spice01.lbl\u001b[39m\u001b[38;5;124m'\u001b[39m\n\u001b[0;32m----> 2\u001b[0m \u001b[43male\u001b[49m\u001b[38;5;241;43m.\u001b[39;49m\u001b[43mload\u001b[49m\u001b[43m(\u001b[49m\u001b[43mfile\u001b[49m\u001b[43m,\u001b[49m\u001b[43m \u001b[49m\u001b[38;5;124;43m\"\u001b[39;49m\u001b[38;5;124;43male\u001b[39;49m\u001b[38;5;124;43m\"\u001b[39;49m\u001b[43m)\u001b[49m\n",
- "File \u001b[0;32m~/working/astro/ale/ale/drivers/__init__.py:166\u001b[0m, in \u001b[0;36mload\u001b[0;34m(label, props, formatter, verbose, only_isis_spice, only_naif_spice)\u001b[0m\n\u001b[1;32m 164\u001b[0m \u001b[38;5;28mprint\u001b[39m(\u001b[38;5;124mf\u001b[39m\u001b[38;5;124m'\u001b[39m\u001b[38;5;124mFailed: \u001b[39m\u001b[38;5;132;01m{\u001b[39;00me\u001b[38;5;132;01m}\u001b[39;00m\u001b[38;5;130;01m\\n\u001b[39;00m\u001b[38;5;124m'\u001b[39m)\n\u001b[1;32m 165\u001b[0m traceback\u001b[38;5;241m.\u001b[39mprint_exc()\n\u001b[0;32m--> 166\u001b[0m \u001b[38;5;28;01mraise\u001b[39;00m \u001b[38;5;167;01mException\u001b[39;00m(\u001b[38;5;124m'\u001b[39m\u001b[38;5;124mNo Such Driver for Label\u001b[39m\u001b[38;5;124m'\u001b[39m)\n",
- "\u001b[0;31mException\u001b[0m: No Such Driver for Label"
- ]
- }
- ],
- "source": [
- "file = '/Users/ahibl/working/astro/img_data/MSI/labels/ale_spice01.lbl'\n",
- "ale.load(file, \"ale\")"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": 9,
- "id": "a1d84d0e",
- "metadata": {},
- "outputs": [
- {
- "name": "stdout",
- "output_type": "stream",
- "text": [
- "Object = IsisCube\n",
- " Object = Core\n",
- " StartByte = 65537\n",
- " Format = Tile\n",
- " TileSamples = 179\n",
- " TileLines = 412\n",
- "\n",
- " Group = Dimensions\n",
- " Samples = 537\n",
- " Lines = 412\n",
- " Bands = 1\n",
- " End_Group\n",
- "\n",
- " Group = Pixels\n",
- " Type = Real\n",
- " ByteOrder = Lsb\n",
- " Base = 0.0\n",
- " Multiplier = 1.0\n",
- " End_Group\n",
- " End_Object\n",
- "\n",
- " Group = Instrument\n",
- " SpacecraftName = \"NEAR EARTH ASTEROID RENDEZVOUS\"\n",
- " InstrumentId = MSI\n",
- " TargetName = EROS\n",
- " StartTime = 2000-02-25T05:16:12.656\n",
- " StopTime = 2000-02-25T05:16:12.745\n",
- " SpacecraftClockStartCount = 126865998830\n",
- " SpacecraftClockStopCount = 126865998919\n",
- " ExposureDuration = 89.00 <ms>\n",
- " OriginalSpacecraftClockStartCount = 126865998.830\n",
- " OriginalSpacecraftClockStopCount = 126865998.919\n",
- " DpuDeckTemperature = 286.50 <K>\n",
- " End_Group\n",
- "\n",
- " Group = Archive\n",
- " DataSetId = NEAR-A-MSI-3-EDR-EROS/ORBIT-V1.0\n",
- " ProducerFullName = \"Scott L. Murchie\"\n",
- " ProductId = M0126865998F4_2P_IOF.FIT\n",
- " ProductVersionId = 1.0\n",
- " InstrumentHostName = \"NEAR EARTH ASTEROID RENDEZVOUS\"\n",
- " InstrumentName = \"MULTI-SPECTRAL IMAGER\"\n",
- " InstrumentId = MSI\n",
- " TargetName = EROS\n",
- " End_Group\n",
- "\n",
- " Group = BandBin\n",
- " FilterNumber = 4\n",
- " Center = 950 <nm>\n",
- " End_Group\n",
- "\n",
- " Group = Kernels\n",
- " NaifFrameCode = -93001\n",
- " LeapSecond = $base/kernels/lsk/naif0012.tls\n",
- " TargetAttitudeShape = $base/kernels/pck/pck00009.tpc\n",
- " TargetPosition = (Table, $base/kernels/spk/de405.bsp,\n",
- " $near/kernels/tspk/erosephem_1999004_2002181.-\n",
- " bsp)\n",
- " InstrumentPointing = (Table, $near/kernels/ck/near_2000056_v01.bc,\n",
- " $near/kernels/fk/eros_fixed.tf)\n",
- " Instrument = $near/kernels/ik/msi15.ti\n",
- " SpacecraftClock = $near/kernels/sclk/near_171.tsc\n",
- " InstrumentPosition = (Table,\n",
- " $near/kernels/spk/near_erosorbit_nav_v1.bsp)\n",
- " InstrumentAddendum = $near/kernels/iak/msiAddendum002.ti\n",
- " ShapeModel = Null\n",
- " InstrumentPositionQuality = Reconstructed\n",
- " InstrumentPointingQuality = Reconstructed\n",
- " CameraVersion = 2\n",
- " Source = ale\n",
- " End_Group\n",
- "End_Object\n",
- "\n",
- "Object = Label\n",
- " Bytes = 65536\n",
- "End_Object\n",
- "\n",
- "Object = Table\n",
- " Name = InstrumentPointing\n",
- " StartByte = 955907\n",
- " Bytes = 128\n",
- " Records = 2\n",
- " ByteOrder = Lsb\n",
- " TimeDependentFrames = (-93000, 1)\n",
- " ConstantFrames = (-93001, -93000)\n",
- " ConstantRotation = (-0.0014422521585656, 6.97819591591179e-07,\n",
- " 0.99999895995357, -4.83840156360023e-04,\n",
- " -0.99999988294934, 0.0, 0.99999884290304,\n",
- " -4.83839653143797e-04, 0.0014422523273822)\n",
- " CkTableStartTime = 4727836.2200713\n",
- " CkTableEndTime = 4727837.220071\n",
- " CkTableOriginalSize = 2\n",
- " FrameTypeCode = 3\n",
- " Description = \"Created by spiceinit\"\n",
- " Kernels = ($near/kernels/ck/near_2000056_v01.bc,\n",
- " $near/kernels/fk/eros_fixed.tf)\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q0\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q1\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q2\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q3\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = AV1\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = AV2\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = AV3\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = ET\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "End_Object\n",
- "\n",
- "Object = Table\n",
- " Name = InstrumentPosition\n",
- " StartByte = 956035\n",
- " Bytes = 56\n",
- " Records = 1\n",
- " ByteOrder = Lsb\n",
- " CacheType = Linear\n",
- " SpkTableStartTime = 4727836.8855711\n",
- " SpkTableEndTime = 4727836.8855711\n",
- " SpkTableOriginalSize = 1.0\n",
- " Description = \"Created by spiceinit\"\n",
- " Kernels = $near/kernels/spk/near_erosorbit_nav_v1.bsp\n",
- "\n",
- " Group = Field\n",
- " Name = J2000X\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Y\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Z\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000XV\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000YV\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000ZV\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = ET\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "End_Object\n",
- "\n",
- "Object = Table\n",
- " Name = BodyRotation\n",
- " StartByte = 956091\n",
- " Bytes = 64\n",
- " Records = 1\n",
- " ByteOrder = Lsb\n",
- " TimeDependentFrames = (2000433, 1)\n",
- " CkTableStartTime = 4727836.8855711\n",
- " CkTableEndTime = 4727836.8855711\n",
- " CkTableOriginalSize = 1\n",
- " FrameTypeCode = 3\n",
- " Description = \"Created by spiceinit\"\n",
- " Kernels = ($base/kernels/spk/de405.bsp,\n",
- " $near/kernels/tspk/erosephem_1999004_2002181.bsp,\n",
- " $base/kernels/pck/pck00009.tpc)\n",
- " SolarLongitude = 128.72797999357\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q0\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q1\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q2\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Q3\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = AV1\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = AV2\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = AV3\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = ET\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "End_Object\n",
- "\n",
- "Object = Table\n",
- " Name = SunPosition\n",
- " StartByte = 956155\n",
- " Bytes = 56\n",
- " Records = 1\n",
- " ByteOrder = Lsb\n",
- " CacheType = Linear\n",
- " SpkTableStartTime = 4727836.8855711\n",
- " SpkTableEndTime = 4727836.8855711\n",
- " SpkTableOriginalSize = 1.0\n",
- " Description = \"Created by spiceinit\"\n",
- " Kernels = ($base/kernels/spk/de405.bsp,\n",
- " $near/kernels/tspk/erosephem_1999004_2002181.bsp)\n",
- "\n",
- " Group = Field\n",
- " Name = J2000X\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Y\n",
- " Type = Double\n",
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- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000Z\n",
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- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000XV\n",
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- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000YV\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = J2000ZV\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "\n",
- " Group = Field\n",
- " Name = ET\n",
- " Type = Double\n",
- " Size = 1\n",
- " End_Group\n",
- "End_Object\n",
- "\n",
- "Object = History\n",
- " Name = IsisCube\n",
- " StartByte = 956211\n",
- " Bytes = 2503\n",
- "End_Object\n",
- "\n",
- "Object = OriginalLabel\n",
- " Name = IsisCube\n",
- " StartByte = 950513\n",
- " Bytes = 3820\n",
- "End_Object\n",
- "\n",
- "Object = NaifKeywords\n",
- " BODY2000433_LONG_AXIS = 0\n",
- " BODY2000433_PM = (326.07, 1639.38864745, 0)\n",
- " BODY2000433_POLE_DEC = (17.22, 0, 0)\n",
- " BODY2000433_POLE_RA = (11.35, 0, 0)\n",
- " BODY2000433_RADII = (17, 5.5, 5.5)\n",
- " BODY_CODE = 2000433\n",
- " BODY_FRAME_CODE = 2.00043e+06\n",
- " FRAME_-93001_CENTER = -93\n",
- " FRAME_-93001_CLASS = 4\n",
- " FRAME_-93001_CLASS_ID = -93001\n",
- " FRAME_-93001_NAME = NEAR_MSI\n",
- " FRAME_2000433_CENTER = 2.00043e+06\n",
- " FRAME_2000433_CLASS = 2\n",
- " FRAME_2000433_CLASS_ID = 2.00043e+06\n",
- " FRAME_2000433_NAME = EROS_FIXED\n",
- " INS-93001_BORESIGHT = (1, 0, 0)\n",
- " INS-93001_BORESIGHT_LINE = 206.5\n",
- " INS-93001_BORESIGHT_SAMPLE = 269\n",
- " INS-93001_FOCAL_LENGTH = 166.85\n",
- " INS-93001_FOV_BOUNDARY_CORNERS = (1, 0.01974485714, 0.02575366124, 1,\n",
- " -0.01974485714, 0.02575366124, 1,\n",
- " -0.01974485714, -0.02575366124, 1)\n",
- " INS-93001_FOV_FRAME = NEAR_MSI\n",
- " INS-93001_FOV_SHAPE = POLYGON\n",
- " INS-93001_FRAME_ID = -93001\n",
- " INS-93001_ITRANSL = (0, 0, -62.5)\n",
- " INS-93001_ITRANSS = (0, 62.5, 0)\n",
- " INS-93001_K1 = -7e-05\n",
- " INS-93001_LIGHTTIME_CORRECTION = LT+S\n",
- " INS-93001_LT_SURFACE_CORRECT = FALSE\n",
- " INS-93001_PIXEL_PITCH = 0.016\n",
- " INS-93001_PLATFORM_ID = -93000\n",
- " INS-93001_SWAP_OBSERVER_TARGET = TRUE\n",
- " INS-93001_TRANSX = (0, 0.016, 0)\n",
- " INS-93001_TRANSY = (0, 0, -0.016)\n",
- " OBJECT_2000433_FRAME = EROS_FIXED\n",
- " TKFRAME_-93001_ANGLES = (90, -179.972278, -0.082635)\n",
- " TKFRAME_-93001_AXES = (2, 1, 2)\n",
- " TKFRAME_-93001_RELATIVE = NEAR_SC_BUS_PRIME\n",
- " TKFRAME_-93001_SPEC = ANGLES\n",
- " TKFRAME_-93001_UNITS = DEGREES\n",
- " CLOCK_ET_-93_126865998830_COMPUTED = eb1bd43507095241\n",
- "End_Object\n",
- "End\n",
- "\n"
- ]
- }
- ],
- "source": [
- "with open(file) as f:\n",
- " print(f.read())"
- ]
- },
- {
- "cell_type": "code",
- "execution_count": null,
- "id": "4e8eae81",
- "metadata": {},
- "outputs": [],
- "source": []
- }
- ],
- "metadata": {
- "kernelspec": {
- "display_name": "Python 3 (ipykernel)",
- "language": "python",
- "name": "python3"
- },
- "language_info": {
- "codemirror_mode": {
- "name": "ipython",
- "version": 3
- },
- "file_extension": ".py",
- "mimetype": "text/x-python",
- "name": "python",
- "nbconvert_exporter": "python",
- "pygments_lexer": "ipython3",
- "version": "3.10.6"
- }
- },
- "nbformat": 4,
- "nbformat_minor": 5
-}
diff --git a/tests/pytests/data/LUA3107H.161/LUA3107H.161.clem_0.xsp b/tests/pytests/data/LUA3107H.161/LUA3107H.161.clem_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..0096699a1beb0d6037ece4b9320b16c2276f19ef
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/LUA3107H.161.clem_0.xsp
@@ -0,0 +1,334 @@
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+ ~NAIF/SPC BEGIN COMMENTS~
+; uvvis/LUA3107H.161.clem_0.bsp LOG FILE
+
+; Created 2023-07-28/10:00:46.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Users/ahibl/astro_efs/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = uvvis/LUA3107H.161.clem_0.bsp
+ SOURCE_SPK_KERNEL = /Users/ahibl/astro_efs/base/kernels/spk/de430.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 3, 10, 301
+ BEGIN_TIME = 1994 MAR 25 15:03:56.564
+ END_TIME = 1994 MAR 25 15:07:57.205
+SOURCE_SPK_KERNEL = /Users/ahibl/astro_efs/Clementine1/kernels/spk/SPKMERGE_940219_940504_CLEMV001b.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -40
+ BEGIN_TIME = 1994 MAR 25 15:03:56.564
+ END_TIME = 1994 MAR 25 15:07:57.205
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/LUA3107H.161/LUA3107H.161.clem_1.xsp b/tests/pytests/data/LUA3107H.161/LUA3107H.161.clem_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..7beba1b8bbe31295447fcfc38fd43e6aa6998311
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/LUA3107H.161.clem_1.xsp
@@ -0,0 +1,334 @@
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+ ~NAIF/SPC BEGIN COMMENTS~
+; uvvis/LUA3107H.161.clem_1.bsp LOG FILE
+
+; Created 2023-07-28/10:00:47.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
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+
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+ INCLUDE_COMMENTS = NO
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+ INCLUDE_COMMENTS = NO
+ BODIES = -40
+ BEGIN_TIME = 1994 MAR 25 15:12:15.347
+ END_TIME = 1994 MAR 25 15:16:15.356
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/LUA3107H.161/LUA3107H.161_isis3.lbl b/tests/pytests/data/LUA3107H.161/LUA3107H.161_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..c2f2a86b47d5c64f7e4611893d814435b227578b
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/LUA3107H.161_isis3.lbl
@@ -0,0 +1,411 @@
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+ Object = Core
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+
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+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
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+ Multiplier = 1.0
+ End_Group
+ End_Object
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+ Group = Instrument
+ SpacecraftName = "CLEMENTINE 1"
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+ TargetName = MOON
+ StartTime = 1994-03-25T15:14:15.347
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+ GainModeID = 1
+ CryocoolerDuration = N/A
+ EncodingCompressionRatio = 11.71
+ EncodingFormat = CLEM-JPEG-1
+ End_Group
+
+ Group = Archive
+ ProductID = LUA3107H.161
+ MissionPhase = "LUNAR MAPPING"
+ End_Group
+
+ Group = BandBin
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+ Width = 0.04 <micrometers>
+ End_Group
+
+ Group = Kernels
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+ TargetAttitudeShape = ($base/kernels/pck/pck00009.tpc,
+ $base/kernels/pck/lunar_de403_1950-2199_pa.bp-
+ c, $base/kernels/fk/lunarMeanEarth001.tf)
+ TargetPosition = (Table, $base/kernels/spk/de430.bsp)
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+ $Clementine1/kernels/ck/clem_5sc.bck,
+ $clementine1/kernels/fk/clem_v12.tf)
+ Instrument = $Clementine1/kernels/ik/clem_uvvis_beta_ik_v0-
+ 4.ti
+ SpacecraftClock = $Clementine1/kernels/sclk/dspse002.tsc
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+ $Clementine1/kernels/spk/SPKMERGE_940219_9405-
+ 04_CLEMV001b.bsp)
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+ ShapeModel = $base/dems/ldem_128ppd_Mar2011_clon180_radius-
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diff --git a/tests/pytests/data/LUA3107H.161/clem_5sc_0_sliced_-40000.xfr b/tests/pytests/data/LUA3107H.161/clem_5sc_0_sliced_-40000.xfr
new file mode 100644
index 0000000000000000000000000000000000000000..e51a100d565410dd9d3ee61fcbd555fcff3aad2b
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/clem_5sc_0_sliced_-40000.xfr
@@ -0,0 +1,416 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
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+'A27CE29D65^B'
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+'A27CE2B116^B'
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+'A27CE2C4C5^B'
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+'A27CE309AE^B'
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+'A27CE327368^B'
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+'A27CE344BD^B'
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+'A27CE3586E^B'
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+'A27CE389A58^B'
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+'A27CE3A72E^B'
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+'A27CE3BADD^B'
+'A27CE3C4B68^B'
+'A27CE3CE8E^B'
+'A27CE3D8658^B'
+'A27CE3E23D^B'
+'A27CE3EC168^B'
+'A27CE3F5EE8^B'
+'A27CE3FFC6^B'
+'A27CE409A1^B'
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+'A27CE41D52^B'
+'A27CE4272A^B'
+'A27CE431018^B'
+'A27CE43AD9^B'
+'A27CE444B28^B'
+'A27CE44CCA4^B'
+'A27CE276CA1^B'
+'1^1'
+'31^2'
+END_ARRAY 1 395
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/ahibl/astro_efs/test_imgs/uvvis/LUA3107H.161.clem.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/LUA3107H.161/clem_5sc_1_sliced_-40000.xfr b/tests/pytests/data/LUA3107H.161/clem_5sc_1_sliced_-40000.xfr
new file mode 100644
index 0000000000000000000000000000000000000000..f82b5ab42628838a7125b0563ef680fab4347e7b
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/clem_5sc_1_sliced_-40000.xfr
@@ -0,0 +1,416 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'CREATED USING ORIGINAL CLEM CK BY NAIF, JPL; DEC 11, 1995 '
+BEGIN_ARRAY 1 395
+'5 SEC SPACED ATT. DATA INTERVALS ONLY '
+'A27CE644F98^B'
+'A27CE819BE1^B'
+'-9C40'
+'1'
+'3'
+'1'
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+'-3DFCC58C807F02^-2'
+'-6A8A168D279478^-3'
+'B9F27CD2CF4E6^0'
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+'1EFAACE12693E5^0'
+'12DAC41F8D80BD^-2'
+'-40D05B42F9914^-2'
+'-1F3AC17CC6F4^-2'
+'A27CE644F98^B'
+'A27CE64E69^B'
+'A27CE658428^B'
+'A27CE6621A^B'
+'A27CE66BF18^B'
+'A27CE675C9^B'
+'A27CE67FA28^B'
+'A27CE6897A^B'
+'A27CE693518^B'
+'A27CE69D29^B'
+'A27CE6A7028^B'
+'A27CE6B0DA^B'
+'A27CE6BAB18^B'
+'A27CE6C489^B'
+'A27CE6CE628^B'
+'A27CE6D83A^B'
+'A27CE6E2118^B'
+'A27CE6EBE9^B'
+'A27CE6F5C28^B'
+'A27CE6FF9A^B'
+'A27CE70972^B'
+'A27CE713498^B'
+'A27CE71D21^B'
+'A27CE726FA8^B'
+'A27CE730D2^B'
+'A27CE73AA98^B'
+'A27CE74481^B'
+'A27CE74E5A8^B'
+'A27CE75832^B'
+'A27CE762098^B'
+'A27CE76BE1^B'
+'A27CE775BA8^B'
+'A27CE77F92^B'
+'A27CE789698^B'
+'A27CE79341^B'
+'A27CE79D1A8^B'
+'A27CE7A6F2^B'
+'A27CE7B0C98^B'
+'A27CE7BAA1^B'
+'A27CE7C47A8^B'
+'A27CE7CE52^B'
+'A27CE7D8298^B'
+'A27CE7E201^B'
+'A27CE7EBDA8^B'
+'A27CE7F5B2^B'
+'A27CE7FF8A^B'
+'A27CE809618^B'
+'A27CE81339^B'
+'A27CE819BE1^B'
+'A27CE644F98^B'
+'1^1'
+'31^2'
+END_ARRAY 1 395
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/ahibl/astro_efs/test_imgs/uvvis/LUA3107H.161.clem.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/LUA3107H.161/clem_uvvis_beta_ik_v04.ti b/tests/pytests/data/LUA3107H.161/clem_uvvis_beta_ik_v04.ti
new file mode 100644
index 0000000000000000000000000000000000000000..23018ba41673d69be4fe1355177a3c65f6f01e14
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/clem_uvvis_beta_ik_v04.ti
@@ -0,0 +1,530 @@
+KPL/IK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "clem_uvvis_009.ti"
+MISSION_NAME = "DEEP SPACE PROGRAM SCIENCE EXPERIMENT"
+SPACECRAFT_NAME = "CLEMENTINE 1"
+DATA_SET_ID = "CLEM1-L-SPICE-6-V1.0"
+KERNEL_TYPE_ID = IK
+PRODUCT_ID = "clem_uvvis_009.ti"
+PRODUCT_CREATION_TIME = 2017-10-01T00:00:00
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = "N/A"
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "CLEMENTINE SPACECRAFT"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MOON
+INSTRUMENT_NAME = "ULTRAVIOLET/VISIBLE CAMERA"
+NAIF_INSTRUMENT_ID = {
+ -40002,
+ -40021,
+ -40022,
+ -40023,
+ -40024,
+ -40025,
+ -40026
+ }
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = INSTRUMENT
+ DESCRIPTION = "Clementine SPICE IK file for Ultraviolet
+and Visible Imaging Camera (UVVIS) providing FOV definition and other
+geometric parameters for the instrument, created by NAIF, JPL and
+modified by ASU "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+UVVIS Instrument Kernel
+========================================================================
+
+ This Clementine instrument kernel (I-kernel) contains the
+ instrument geometric parameters for the Ultraviolet and Visible
+ Imaging Camera (UVVIS).
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 9.0 -- October 01, 2017 -- Emerson Speyerer, ASU
+
+ - BETA VERSION -
+ - Still in testing -
+
+ Updated IK to include band specific optical distortion
+ parameters.
+
+ Added platform IDs
+
+ Removed Fortran code
+
+ Added documentation for loading a kernel into MICE (MATLAB SPICE
+ utility)
+
+ Version 8.0 -- June 11, 2007 -- Boris Semenov, NAIF
+
+ Updated comments. Added FOV definition. Added PLATFORM_ID.
+
+ Version 7.0 -- Feb 3, 1995
+
+
+References
+--------------------------------------------------------
+
+ 1. "Models of the Clementine Spacecraft and Remote Sensing
+ Science Instruments for Geodesy, Cartography, and Dynamical
+ Sciences", Draft version 1.0, December 1993.
+
+
+Implementation Notes
+--------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that
+ make use of this I-kernel must `load' the kernel, normally during
+ program initialization. Loading the kernel associates data items
+ with their names in a data structure called the `kernel pool'. The
+ SPICE routine FURNSH loads a kernel file into the pool as shown
+ below.
+
+ CALL FURNSH( 'this_kernel_name' ) in FORTRAN (SPICELIB)
+ furnsh_c ( "this_kernel_name" ); in C (CSPICE)
+ cspice_furnsh, "this_kernel_name" in IDL (ICY)
+ cspice_furnsh( 'this_kernel_name' ); in MATLAB (MICE)
+
+
+Naming Conventions
+--------------------------------------------------------
+
+ All keywords referencing data in this I-kernel are of the form
+
+ INS<instrument-ID>_<data_item_name>
+
+ The instrument ID is an negative integer value that uniquely
+ identifies an instrument or specific band. For Clementine Ultraviolet
+ and Visible Imaging Camera the instrument ID is -40002. In addition,
+ each band also has its own NAIF ID:
+
+ Table 1: Clementine UVVIS Instrument IDs
+ ---------------- ----------- -----------------------
+ Frame Name NAIF ID Comments
+ ---------------- ---------- -----------------------
+ CLEM_UVVIS -40002 *Deprecated*
+ CLEM_UVVIS_A -40021 Filter A: 415 nm
+ CLEM_UVVIS_B -40022 Filter B: 750 nm
+ CLEM_UVVIS_C -40023 Filter C: 900 nm
+ CLEM_UVVIS_D -40024 Filter D: 950 nm
+ CLEM_UVVIS_E -40025 Filter E: 1000 nm
+ CLEM_UVVIS_F -40026 Filter F: Broadband
+
+
+ The upper bound on the length of a name is 32 characters.
+
+UVVIS Description
+---------------------------------------------------------------------------
+-- In progress
+
+UVVIS Geometric Calibration
+---------------------------------------------------------------------------
+-- In progress
+
+Pixel Coordinate Definition:
+---------------------------------------------------------------------------
+-- In progress
+
+UVVIS First Order Optical Parameters:
+---------------------------------------------------------------------------
+
+ The following section contains the first order optical parameters for
+ the Clementine UVVIS camera. The values are derived from the sensor
+ specifications and from models derived from on-orbit observations.
+ The parameters are wavelength dependent due to chromatic aberrations
+ in the optical system.
+
+ Optical Parameter Definitions:
+
+ Effective Focal Length: Distance along the optical axis from the
+ perspective center to the detector (units of mm)
+
+ F/ratio (or f-number): Ratio of the effective focal length to the
+ dimeter of the entrance pupil (effective aperture)
+
+ Spectral Band: Wavelength range (or spectral response) of the
+ optics
+
+ Boresight Line and Sample (principal point): Point at which the
+ optical axis intersects the detector array
+
+ IFOV (Instantaneous field of view): Angle subtended by a single
+ detector element on the axis of the optical system
+
+ Table 2: Original UVVIS Optical Parameters
+ ------------------------------- -----------
+ Parameter, Unit Value
+ ------------------------------- -----------
+ Focal Length (USGS), mm 90.15
+ Focal Length (NAIF), mm 90.00
+ Pixel Pitch, mm 0.023
+ Boresight Sample, pixel 192.5
+ Boresight Line, pixel 144.5
+ Max Samples, pixels 342
+ Max Lines, pixels 288
+ Distortion (Alpha), 1/mm**2 0
+
+ Table 3: UVVIS Focal Length
+ -------- ------------ ------------------------------
+ Filter Wavelength Effective Focal Length, mm
+ -------- ------------ ------------------------------
+ A 415 nm
+ B 750 nm
+ C 900 nm
+ D 950 nm
+ E 1000 nm
+ F Broadband
+
+ Deprecated Values from the USGS IAK
+
+
+
+ INS-40002_FOCAL_LENGTH = ( 90.15 ) -- Not used
+
+ \begindata
+
+ INS-40002_PIXEL_PITCH = ( 0.023 )
+ INS-40002_BORESIGHT_SAMPLE = ( 192.5 )
+ INS-40002_BORESIGHT_LINE = ( 144.5 )
+ INS-40002_TRANSX = (0.0 0.023 0.0)
+ INS-40002_TRANSY = (0.0 0.0 0.023)
+ INS-40002_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40002_ITRANSL = (0.0 0.0 43.47826087)
+
+ \begintext
+
+ Additional values from the original NAIF IK
+
+ \begindata
+
+ INS-40002_FOCAL_LENGTH = ( 90.00 )
+ INS-40002_K = ( 43.4783 )
+ INS-40002_S0 = ( 192.5 )
+ INS-40002_L0 = ( 144.5 )
+ INS-40002_S_MAX = ( 384 )
+ INS-40002_L_MAX = ( 288 )
+ INS-40002_ALPHA0 = ( 0.0 )
+
+ \begintext
+
+ Band Spacific Parameters
+
+ \begindata
+ INS-40021_FOCAL_LENGTH = 89.874444
+ INS-40021_F/RATIO = -999.9999
+ INS-40021_BORESIGHT_SAMPLE = 192.5
+ INS-40021_BORESIGHT_LINE = 144.5
+ INS-40021_IFOV = -999.999
+ INS-40021_PIXEL_SAMPLES = 384
+ INS-40021_PIXEL_LINES = 288
+ INS-40021_PIXEL_PITCH = 0.023
+ INS-40021_PIXEL_SIZE = ( 0.023 0.023 )
+ INS-40021_CCD_CENTER = ( 512.5 512.5 )
+ INS-40021_FILTER_NAME = 'A'
+ INS-40021_FILTER_BANDCENTER = 415
+ INS-40021_FILTER_BANDWIDTH = 40
+ INS-40021_FOV_FRAME = 'CLEM_UVVIS_A'
+ INS-40021_FOV_SHAPE = 'RECTANGLE'
+ INS-40021_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40021_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40021_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40021_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40021_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40021_FOV_ANGLE_UNITS = 'DEGREES'
+ INS-40021_TRANSX = (0.0 0.023 0.0)
+ INS-40021_TRANSY = (0.0 0.0 0.023)
+ INS-40021_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40021_ITRANSL = (0.0 0.0 43.47826087)
+
+ INS-40022_FOCAL_LENGTH = 89.979236
+ INS-40022_F/RATIO = -999.9999
+ INS-40022_BORESIGHT_SAMPLE = 192.5
+ INS-40022_BORESIGHT_LINE = 144.5
+ INS-40022_IFOV = -999.999
+ INS-40022_PIXEL_SAMPLES = 384
+ INS-40022_PIXEL_LINES = 288
+ INS-40022_PIXEL_PITCH = 0.023
+ INS-40022_PIXEL_SIZE = ( 0.023 0.023 )
+ INS-40022_CCD_CENTER = ( 512.5 512.5 )
+ INS-40022_FILTER_NAME = 'B'
+ INS-40022_FILTER_BANDCENTER = 750
+ INS-40022_FILTER_BANDWIDTH = 10
+ INS-40022_FOV_FRAME = 'CLEM_UVVIS_B'
+ INS-40022_FOV_SHAPE = 'RECTANGLE'
+ INS-40022_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40022_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40022_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40022_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40022_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40022_FOV_ANGLE_UNITS = 'DEGREES'
+ INS-40022_TRANSX = (0.0 0.023 0.0)
+ INS-40022_TRANSY = (0.0 0.0 0.023)
+ INS-40022_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40022_ITRANSL = (0.0 0.0 43.47826087)
+
+ INS-40023_FOCAL_LENGTH = 89.987163
+ INS-40023_F/RATIO = -999.9999
+ INS-40023_BORESIGHT_SAMPLE = 192.5
+ INS-40023_BORESIGHT_LINE = 144.5
+ INS-40023_IFOV = -999.999
+ INS-40023_PIXEL_SAMPLES = 384
+ INS-40023_PIXEL_LINES = 288
+ INS-40023_PIXEL_PITCH = 0.023
+ INS-40023_PIXEL_SIZE = ( 0.023 0.023 )
+ INS-40023_CCD_CENTER = ( 512.5 512.5 )
+ INS-40023_FILTER_NAME = 'C'
+ INS-40023_FILTER_BANDCENTER = 900
+ INS-40023_FILTER_BANDWIDTH = 20
+ INS-40023_FOV_FRAME = 'CLEM_UVVIS_C'
+ INS-40023_FOV_SHAPE = 'RECTANGLE'
+ INS-40023_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40023_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40023_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40023_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40023_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40023_FOV_ANGLE_UNITS = 'DEGREES'
+ INS-40023_TRANSX = (0.0 0.023 0.0)
+ INS-40023_TRANSY = (0.0 0.0 0.023)
+ INS-40023_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40023_ITRANSL = (0.0 0.0 43.47826087)
+
+ INS-40024_FOCAL_LENGTH = 89.991267
+ INS-40024_F/RATIO = -999.9999
+ INS-40024_BORESIGHT_SAMPLE = 192.5
+ INS-40024_BORESIGHT_LINE = 144.5
+ INS-40024_IFOV = -999.999
+ INS-40024_PIXEL_SAMPLES = 384
+ INS-40024_PIXEL_LINES = 288
+ INS-40024_PIXEL_PITCH = 0.023
+ INS-40024_PIXEL_SIZE = ( 0.023 0.023 )
+ INS-40024_CCD_CENTER = ( 512.5 512.5 )
+ INS-40024_FILTER_NAME = 'D'
+ INS-40024_FILTER_BANDCENTER = 950
+ INS-40024_FILTER_BANDWIDTH = 30
+ INS-40024_FOV_FRAME = 'CLEM_UVVIS_D'
+ INS-40024_FOV_SHAPE = 'RECTANGLE'
+ INS-40024_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40024_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40024_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40024_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40024_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40024_FOV_ANGLE_UNITS = 'DEGREES'
+ INS-40024_TRANSX = (0.0 0.023 0.0)
+ INS-40024_TRANSY = (0.0 0.0 0.023)
+ INS-40024_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40024_ITRANSL = (0.0 0.0 43.47826087)
+
+ INS-40025_FOCAL_LENGTH = 89.994013
+ INS-40025_F/RATIO = -999.9999
+ INS-40025_BORESIGHT_SAMPLE = 192.5
+ INS-40025_BORESIGHT_LINE = 144.5
+ INS-40025_IFOV = -999.999
+ INS-40025_PIXEL_SAMPLES = 384
+ INS-40025_PIXEL_LINES = 288
+ INS-40025_PIXEL_PITCH = 0.023
+ INS-40025_PIXEL_SIZE = ( 0.023 0.023 )
+ INS-40025_CCD_CENTER = ( 512.5 512.5 )
+ INS-40025_FILTER_NAME = 'E'
+ INS-40025_FILTER_BANDCENTER = 1000
+ INS-40025_FILTER_BANDWIDTH = 30
+ INS-40025_FOV_FRAME = 'CLEM_UVVIS_E'
+ INS-40025_FOV_SHAPE = 'RECTANGLE'
+ INS-40025_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40025_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40025_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40025_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40025_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40025_FOV_ANGLE_UNITS = 'DEGREES'
+ INS-40025_TRANSX = (0.0 0.023 0.0)
+ INS-40025_TRANSY = (0.0 0.0 0.023)
+ INS-40025_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40025_ITRANSL = (0.0 0.0 43.47826087)
+
+ INS-40026_FOCAL_LENGTH = 90.00
+ INS-40026_F/RATIO = -999.9999
+ INS-40026_BORESIGHT_SAMPLE = 192.5
+ INS-40026_BORESIGHT_LINE = 144.5
+ INS-40026_IFOV = -999.999
+ INS-40026_PIXEL_SAMPLES = 384
+ INS-40026_PIXEL_LINES = 288
+ INS-40026_PIXEL_PITCH = 0.023
+ INS-40026_PIXEL_SIZE = ( 0.023 0.023 )
+ INS-40026_CCD_CENTER = ( 512.5 512.5 )
+ INS-40026_FILTER_NAME = 'F'
+ INS-40026_FILTER_BANDCENTER = 650
+ INS-40026_FILTER_BANDWIDTH = 550
+ INS-40026_FOV_FRAME = 'CLEM_UVVIS_F'
+ INS-40026_FOV_SHAPE = 'RECTANGLE'
+ INS-40026_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40026_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40026_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40026_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40026_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40026_FOV_ANGLE_UNITS = 'DEGREES'
+ INS-40026_TRANSX = (0.0 0.023 0.0)
+ INS-40026_TRANSY = (0.0 0.0 0.023)
+ INS-40026_ITRANSS = (0.0 43.47826087 0.0)
+ INS-40026_ITRANSL = (0.0 0.0 43.47826087)
+
+ \begintext
+
+
+UVVIS Camera Model
+---------------------------------------------------------------------------
+
+ (xd, yd) = distorted image point
+ (xu, yu) = undistorted image point
+ (xp, yp) = distortion center (principal point)
+ k1= 1st radial distortion coefficient
+ k2= 2nd radial distortion coefficient
+ k3= 3rd radial distortion coefficient
+ p1= 1st tangential distortion coefficient
+ p2= 2nd tangential distortion coefficient
+
+ Step 1: remove principal point offset (xp,yp)
+ x = xd - xp;
+ y = yd - yp;
+
+ Step 2: Calculate r - distance between the principal point and the
+ measured point on the image
+ rr = x * x + y * y
+
+ Step 3: Calculate dr - radial distortion contribution
+ dr = k1 + k2 * rr + k3 * rr * rr;
+
+ Step 4: Calculate tx and ty - decentering distortion contribution
+ tx = p1 * (rr + 2.0 * x * x) + 2.0 * p2 * x * y;
+ ty = 2.0 * p1 * x * y + p2 * (rr + 2 * y * y);
+
+ Step 5: Calculate xu, yu
+ xu = xd + x * dr + tx;
+ yu = yd + y * dr + ty;
+
+ UVVIS coefficients:
+
+ PP = (xp yp)
+ OD_K = (k1 k2 k3)
+ DECENTER = (p1 p2)
+
+ \begindata
+ INS-40021_PP = ( 0 0 )
+ INS-40022_PP = ( 0 0 )
+ INS-40023_PP = ( 0 0 )
+ INS-40024_PP = ( 0 0 )
+ INS-40025_PP = ( 0 0 )
+ INS-40026_PP = ( 0 0 )
+
+ INS-40021_OD_K = ( 0 -2.422842e-05 0 )
+ INS-40022_OD_K = ( 0 -3.820233e-05 0 )
+ INS-40023_OD_K = ( 0 -3.767127e-05 0 )
+ INS-40024_OD_K = ( 0 -2.398624e-05 0 )
+ INS-40025_OD_K = ( 0 -2.248022e-05 0 )
+ INS-40026_OD_K = ( 0 0 0 )
+
+ INS-40021_DECENTER = ( +2.255006e-05 +2.108941e-05 )
+ INS-40022_DECENTER = ( +3.203789e-07 +3.706078e-07 )
+ INS-40023_DECENTER = ( +4.978645e-06 -3.698737e-05 )
+ INS-40024_DECENTER = ( +1.414502e-05 -1.372645e-04 )
+ INS-40025_DECENTER = ( +2.922347e-05 -4.655129e-05 )
+ INS-40026_DECENTER = ( 0 0 )
+ \begintext
+
+
+
+
+Instrument Frame - Line/Sample Coordinates Diagram
+--------------------------------------------------------
+
+ This diagram illustrates the relationship of the instrument frame
+ axes and the sample/line coordinates:
+
+
+ sample sample
+ 1 S max
+ +-------------------------+-------------+
+ Line 1 | |
+ | |
+ | |
+ | |
+ | |
+ | +Z |
+ | (into the page) | +X
+ | x-------------------------->
+ | |(L_0,S_0) |
+ | | |
+ | | |
+ | | * + L
+ | | (L,S) |
+ | | |
+ | | |
+ Line max +-------------------|-------------------+
+ |
+ |
+ |
+ V +Y
+
+ Assuming no optical distortion the view direction in the
+ instrument frame (X,Y,Z) for a given pixel specified by its
+ line/sample coordinates (L,S) is computed as follows:
+
+ X = (S - S_0) / K
+ Y = (L - L_0) / K
+ Z = FOCAL_LENGTH
+
+
+FOV Definition
+--------------------------------------------------------
+
+ The FOV of Ultraviolet and Visible Imaging Camera is defined below
+ in the ``CLEM_UVVIS'' reference frame as a 5.623 deg by 4.217 deg
+ rectangle with the boresight along +Z axis. (The angular extents
+ were computed using the values from the section ``Camera Optics''
+ above.)
+
+ \begindata
+
+ INS-40002_FOV_FRAME = 'CLEM_UVVIS'
+ INS-40002_FOV_SHAPE = 'RECTANGLE'
+ INS-40002_BORESIGHT = ( 0.0 0.0 1.0 )
+ INS-40002_FOV_CLASS_SPEC = 'ANGLES'
+ INS-40002_FOV_REF_VECTOR = ( 1.0 0.0 0.0 )
+ INS-40002_FOV_REF_ANGLE = ( 2.8115 )
+ INS-40002_FOV_CROSS_ANGLE = ( 2.1085 )
+ INS-40002_FOV_ANGLE_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Platform ID
+--------------------------------------------------------
+
+ This number is the NAIF instrument ID of the platform on which the
+ instrument is mounted -- the spacecraft bus.
+
+ \begindata
+
+ INS-40002_PLATFORM_ID = ( -40000 )
+ INS-40021_PLATFORM_ID = ( -40002 )
+ INS-40022_PLATFORM_ID = ( -40002 )
+ INS-40023_PLATFORM_ID = ( -40002 )
+ INS-40024_PLATFORM_ID = ( -40002 )
+ INS-40025_PLATFORM_ID = ( -40002 )
+ INS-40026_PLATFORM_ID = ( -40002 )
+
+ \begintext
+
+
diff --git a/tests/pytests/data/LUA3107H.161/clem_v12.tf b/tests/pytests/data/LUA3107H.161/clem_v12.tf
new file mode 100644
index 0000000000000000000000000000000000000000..1b8aa6483dd65066174359a2e4748676be2b9798
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/clem_v12.tf
@@ -0,0 +1,662 @@
+KPL/FK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "clem_v21.tf"
+MISSION_NAME = "DEEP SPACE PROGRAM SCIENCE EXPERIMENT"
+SPACECRAFT_NAME = "CLEMENTINE 1"
+DATA_SET_ID = "CLEM1-L-SPICE-6-V1.0"
+KERNEL_TYPE_ID = FK
+PRODUCT_ID = "clem_v21.tf"
+PRODUCT_CREATION_TIME = 2017-10-01T00:00:00
+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 = MOON
+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 = "Clementine SPICE FK file providing the
+complete set of frame definitions for the Clementine spacecraft and its
+science instruments, including band specific frames for the UVVIS
+camera. Created by NAIF with additions by ASU."
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Clementine Frame Definitions Kernel
+==============================================================================
+
+ This frame kernel (FK) contains the Clementine spacecraft and
+ science instrument frame definitions. It also contains name -
+ to - NAIF ID mappings for the Clementine science instruments (see
+ the last section of the file.)
+
+ Additional frames for each UVVIS camera filter have been added to
+ handle band specific optical distortion parameters.
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 2.1 -- October 01, 2017 -- Emerson Speyerer, ASU
+
+ Added descriptions and new frames for each UVVIS filter.
+
+ Version 2.0 -- June 11, 2007 -- Boris Semenov
+
+ Added descriptions. Added name-ID mapping keywords.
+
+ Version 1.0 -- September 29, 2000 -- Boris Semenov
+
+ Initial Release. Contains Euler angles from Clementine I-Kernel
+ files. Does not contain a description for any of the frames.
+
+
+References
+--------------------------------------------------------
+
+ 1. C-kernel Required Reading
+
+ 2. Kernel Pool Required Reading
+
+ 3. Frames Required Reading
+
+ 4. High-Resolution Imager (HIRES) I-Kernel File "clem_hires_008.ti"
+
+ 5. Ultraviolet and Visible Imaging Camera (UVVIS) I-Kernel File
+ "clem_uvvis_008.ti"
+
+ 6. Near Infrared Mapping Spectrometer (NIR) I-Kernel File
+ "clem_nir_009.ti"
+
+ 7. Long Wavelength Infrared Mapping Spectrometer (LWIR) I-Kernel
+ File "clem_lwir_008.ti"
+
+ 8. Laser Ranger (LIDAR) I-Kernel File "clem_lidar_005.ti"
+
+ 9. Star Tracker A (ASTAR) I-Kernel File "clem_astar_006.ti"
+
+ 10. Star Tracker B (BSTAR) I-Kernel File "clem_bstar_006.ti"
+
+ 11. Charged Particle Telescope (CPT) I-Kernel File "clem_cpt_002.ti"
+
+ 12. "Post Launch Alignment and Geometric Calibration of the
+ Clementine Spacecraft and Remote Sensing Science Instruments",
+ T. Duxbury, Rough Draft, no date
+
+ 13. "Models of the Clementine Spacecraft and Remote Sensing Science
+ Instruments for Geodesy, Cartography, and Dynamical Sciences",
+ Draft version 1.0, December 1993.
+
+
+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 frame kernel must ``load'' the kernel, normally during
+ program initialization (see [2]). The SPICELIB routine FURNSH
+ (furnsh_c in CSPICE, cspice_furnsh in ICY) loads a kernel file into
+ the pool as follows:
+
+ CALL FURNSH ( 'frame_kernel_name' )
+ furnsh_c ( "frame_kernel_name" );
+ cspice_furnsh, "frame_kernel_name"
+
+ This file was created and may be updated with a text editor or word
+ processor. Should you need to update this kernel in any way,
+ please, modify the "Version and Date" section above to reflect the
+ changes.
+
+
+Clementine Frames
+--------------------------------------------------------
+
+ The following Clementine frames are defined in this kernel file:
+
+ Frame Name Relative to Type NAIF ID
+ ===================== ================== ======= =======
+
+ Spacecraft Bus Frame:
+ ---------------------
+ CLEM_SC_BUS rel.to J2000 CK -40000
+
+ Instrument Frames:
+ ------------------
+ CLEM_HIRES rel.to SC_BUS FIXED -40001
+ CLEM_UVVIS rel.to SC_BUS FIXED -40002
+ CLEM_NIR rel.to SC_BUS FIXED -40003
+ CLEM_LWIR rel.to SC_BUS FIXED -40004
+ CLEM_LIDAR rel.to SC_BUS FIXED -40005
+ CLEM_ASTAR rel.to SC_BUS FIXED -40006
+ CLEM_BSTAR rel.to SC_BUS FIXED -40007
+ CLEM_CPT rel.to SC_BUS FIXED -40008
+
+ UVVIS Specific Frames:
+ ----------------------
+ CLEM_UVVIS_A rel.to CLEM_UVVIS FIXED -40021
+ CLEM_UVVIS_B rel.to CLEM_UVVIS FIXED -40022
+ CLEM_UVVIS_C rel.to CLEM_UVVIS FIXED -40023
+ CLEM_UVVIS_D rel.to CLEM_UVVIS FIXED -40024
+ CLEM_UVVIS_E rel.to CLEM_UVVIS FIXED -40025
+ CLEM_UVVIS_F rel.to CLEM_UVVIS FIXED -40026
+
+
+Clementine Frames Hierarchy
+--------------------------------------------------------
+
+ The diagram below shows Clementine frames hierarchy:
+
+
+ "J2000" INERTIAL
+ +--------------------------------------------+
+ | |
+ | <--ck | <--pck
+ | |
+ | V
+ | "IAU_EARTH"
+ | EARTH BFR(*)
+ | ------------
+ |
+ |
+ | "CLEM_ASTAR" "CLEM_BSTAR"
+ | ------------ ------------
+ | ^ ^
+ | | |
+ V |<--fixed |<--fixed
+ "CLEM_SC_BUS" | |
+ +----------------------------------------------------------+
+ | | | | | |
+ |<--fixed |<--fixed |<-fixed |<--fixed |<--fixed |<--fixed
+ | | | | | |
+ V V V V V V
+ "CLEM_HIRES" "CLEM_UVVIS" "CLEM_NIR" "CLEM_LWIR" "CLEM_LIDAR" "CLEM_CPT"
+ ------------ ------------ ---------- ----------- ------------ ----------
+ |
+ |---> CLEM_UVVIS_A (fixed)
+ |
+ |---> CLEM_UVVIS_B (fixed)
+ |
+ |---> CLEM_UVVIS_C (fixed)
+ |
+ |---> CLEM_UVVIS_D (fixed)
+ |
+ |---> CLEM_UVVIS_E (fixed)
+ |
+ |---> CLEM_UVVIS_F (fixed)
+
+
+Spacecraft Bus Frame
+--------------------------------------------------------
+
+ The Clementine spacecraft bus frame is defined by the spacecraft
+ design as follows ([12]):
+
+ * +Z axis is in the direction of the nominal remote sensing
+ science instrument boresight vectors;
+
+ * +X axis is in the direction of the main rocket engine;
+
+ * +Y axis completes the right handed frame and is in the plane
+ of the solar arrays;
+
+ * the origin of this frame is at the geometric center of the
+ spacecraft's octagonal prizm shaped body.
+
+ This diagram illustrates the spacecraft frame:
+
+ ________________
+ `. .'
+ _______ _______ ------------------- _______ _______
+ | | | | | | | | | |
+ | | | | | Science | | | | |
+ | | | | | Deck | | | | |
+ | | | | | | | | | |
+ | | | |+Ysc| +Zsc| | | | |
+ | | |=| <------o | |=| | |
+ | | | | | | | | | | |
+ | | | | | | | | | | |
+ | | | | | | | | | | |
+ | | | | | V | | | | |
+ | | | | | +Xsc| | | | |
+ ------- ------- ------------------- ------- -------
+ |_|
+ / \
+ . .
+ ._____.
+
+ The spacecraft bus attitude with respect to an inertial frame is
+ provided by CK kernels. Therefore the spacecraft frame is defined as
+ a CK-based frame.
+
+ \begindata
+
+ FRAME_CLEM_SC_BUS = -40000
+ FRAME_-40000_NAME = 'CLEM_SC_BUS'
+ FRAME_-40000_CLASS = 3
+ FRAME_-40000_CLASS_ID = -40000
+ FRAME_-40000_CENTER = -40
+ CK_-40000_SCLK = -40
+ CK_-40000_SPK = -40
+
+ \begintext
+
+
+Science Instrument Frames
+--------------------------------------------------------
+
+ All Clementine instrument frames are defined in the same way as
+ follows ([12,13]):
+
+ * +Z axis is along the instrument boresight vector;
+
+ * +X axis is in the image plane and in the direction of
+ increasing pixels;
+
+ * +Y axis is in the image plane and in the direction of
+ increasing lines;
+
+ Since all insruments are rigidly mounted on the spacecraft, the
+ orientation of their frames is constant with respect to the
+ spacecraft frame. Therefore, all instrument frames are defined as
+ fixed offset frames with respect to the spacecraft frame.
+
+ Originally mounting alignment of the instruments was included in
+ the IK files by providing the orientation of the instrument frame
+ relative to the spacecraft frame as three angles: thetaX, thetaY,
+ and thetaZ. The spacecraft-to-instrument frame transformation,
+ TXYZxyz, could derived from these angles as follows:
+
+ TXYZxyz = R (thetaZ) R (thetaY) R (thetaX)
+ Z Y X
+
+ where R (theta) represents a 3x3 rotation matrix of angle theta
+ i
+ about the i axis.
+
+ The instrument frame definitions below incorporate the rotation
+ angles from the latest versions of the IKs available at the time
+ when this FK was created.
+
+
+High-Resolution Imager (HIRES) Frame
+
+ The rotation angles provided in the HIRES frame definition below are
+ from [4].
+
+ \begindata
+
+ FRAME_CLEM_HIRES = -40001
+ FRAME_-40001_NAME = 'CLEM_HIRES'
+ FRAME_-40001_CLASS = 4
+ FRAME_-40001_CLASS_ID = -40001
+ FRAME_-40001_CENTER = -40
+ TKFRAME_-40001_SPEC = 'ANGLES'
+ TKFRAME_-40001_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40001_ANGLES = ( -0.00504400153826,
+ -0.00125663706144,
+ -3.14333798284179 )
+ TKFRAME_-40001_AXES = ( 1, 2, 3 )
+ TKFRAME_-40001_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Ultraviolet and Visible Imaging Camera (UVVIS) Frame
+
+ The rotation angles provided in the UVVIS frame definition below are
+ from [5]. Band specific frames are included to handle the different
+ optical distortion parameters
+
+ \begindata
+
+ FRAME_CLEM_UVVIS = -40002
+ FRAME_-40002_NAME = 'CLEM_UVVIS'
+ FRAME_-40002_CLASS = 4
+ FRAME_-40002_CLASS_ID = -40002
+ FRAME_-40002_CENTER = -40
+ TKFRAME_-40002_SPEC = 'ANGLES'
+ TKFRAME_-40002_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40002_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-40002_AXES = ( 1, 2, 3 )
+ TKFRAME_-40002_UNITS = 'RADIANS'
+
+ FRAME_CLEM_UVVIS_A = -40021
+ FRAME_-40021_NAME = 'CLEM_UVVIS_A'
+ FRAME_-40021_CLASS = 4
+ FRAME_-40021_CLASS_ID = -40021
+ FRAME_-40021_CENTER = -40
+ TKFRAME_-40021_SPEC = 'ANGLES'
+ TKFRAME_-40021_RELATIVE = 'CLEM_UVVIS'
+ TKFRAME_-40021_ANGLES = ( -0.00553269372882, -0.00104719755120, 1.57690497917688 )
+ TKFRAME_-40021_AXES = ( 1, 2, 3 )
+ TKFRAME_-40021_UNITS = 'RADIANS'
+
+ FRAME_CLEM_UVVIS_B = -40022
+ FRAME_-40022_NAME = 'CLEM_UVVIS_B'
+ FRAME_-40022_CLASS = 4
+ FRAME_-40022_CLASS_ID = -40022
+ FRAME_-40022_CENTER = -40
+ TKFRAME_-40022_SPEC = 'ANGLES'
+ TKFRAME_-40022_RELATIVE = 'CLEM_UVVIS'
+ TKFRAME_-40022_ANGLES = ( -0.00553269372882, -0.00104719755120, 1.57690497917688 )
+ TKFRAME_-40022_AXES = ( 1, 2, 3 )
+ TKFRAME_-40022_UNITS = 'RADIANS'
+
+ FRAME_CLEM_UVVIS_C = -40023
+ FRAME_-40023_NAME = 'CLEM_UVVIS_C'
+ FRAME_-40023_CLASS = 4
+ FRAME_-40023_CLASS_ID = -40023
+ FRAME_-40023_CENTER = -40
+ TKFRAME_-40023_SPEC = 'ANGLES'
+ TKFRAME_-40023_RELATIVE = 'CLEM_UVVIS'
+ TKFRAME_-40023_ANGLES = ( -0.00553269372882, -0.00104719755120, 1.57690497917688 )
+ TKFRAME_-40023_AXES = ( 1, 2, 3 )
+ TKFRAME_-40023_UNITS = 'RADIANS'
+
+ FRAME_CLEM_UVVIS_D = -40024
+ FRAME_-40024_NAME = 'CLEM_UVVIS_D'
+ FRAME_-40024_CLASS = 4
+ FRAME_-40024_CLASS_ID = -40024
+ FRAME_-40024_CENTER = -40
+ TKFRAME_-40024_SPEC = 'ANGLES'
+ TKFRAME_-40024_RELATIVE = 'CLEM_UVVIS'
+ TKFRAME_-40024_ANGLES = ( -0.00553269372882, -0.00104719755120, 1.57690497917688 )
+ TKFRAME_-40024_AXES = ( 1, 2, 3 )
+ TKFRAME_-40024_UNITS = 'RADIANS'
+
+ FRAME_CLEM_UVVIS_E = -40025
+ FRAME_-40025_NAME = 'CLEM_UVVIS_E'
+ FRAME_-40025_CLASS = 4
+ FRAME_-40025_CLASS_ID = -40025
+ FRAME_-40025_CENTER = -40
+ TKFRAME_-40025_SPEC = 'ANGLES'
+ TKFRAME_-40025_RELATIVE = 'CLEM_UVVIS'
+ TKFRAME_-40025_ANGLES = ( -0.00553269372882, -0.00104719755120, 1.57690497917688 )
+ TKFRAME_-40025_AXES = ( 1, 2, 3 )
+ TKFRAME_-40025_UNITS = 'RADIANS'
+
+ FRAME_CLEM_UVVIS_F = -40026
+ FRAME_-40026_NAME = 'CLEM_UVVIS_F'
+ FRAME_-40026_CLASS = 4
+ FRAME_-40026_CLASS_ID = -40026
+ FRAME_-40026_CENTER = -40
+ TKFRAME_-40026_SPEC = 'ANGLES'
+ TKFRAME_-40026_RELATIVE = 'CLEM_UVVIS'
+ TKFRAME_-40026_ANGLES = ( -0.00553269372882, -0.00104719755120, 1.57690497917688 )
+ TKFRAME_-40026_AXES = ( 1, 2, 3 )
+ TKFRAME_-40026_UNITS = 'RADIANS'
+
+
+ \begintext
+
+
+Near Infrared Mapping Spectrometer (NIR) Frame
+
+ The rotation angles provided in the frame NIT definition below are
+ from [6].
+
+ \begindata
+
+ FRAME_CLEM_NIR = -40003
+ FRAME_-40003_NAME = 'CLEM_NIR'
+ FRAME_-40003_CLASS = 4
+ FRAME_-40003_CLASS_ID = -40003
+ FRAME_-40003_CENTER = -40
+ TKFRAME_-40003_SPEC = 'ANGLES'
+ TKFRAME_-40003_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40003_ANGLES = ( -0.005525711614,
+ -0.001685987814,
+ -0.023816759530 )
+ TKFRAME_-40003_AXES = ( 1, 2, 3 )
+ TKFRAME_-40003_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Long Wavelength Infrared Mapping Spectrometer (LWIR) Frame
+
+ The rotation angles provided in the frame LWIR definition below are
+ from [7].
+
+ \begindata
+
+ FRAME_CLEM_LWIR = -40004
+ FRAME_-40004_NAME = 'CLEM_LWIR'
+ FRAME_-40004_CLASS = 4
+ FRAME_-40004_CLASS_ID = -40004
+ FRAME_-40004_CENTER = -40
+ TKFRAME_-40004_SPEC = 'ANGLES'
+ TKFRAME_-40004_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40004_ANGLES = ( -0.00053581608036,
+ -0.00019722220548,
+ -3.14159265358979 )
+ TKFRAME_-40004_AXES = ( 1, 2, 3 )
+ TKFRAME_-40004_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Laser Ranger (LIDAR) Frame
+
+ The rotation angles provided in the frame LIDAR definition below are
+ from [8].
+
+ \begindata
+
+ FRAME_CLEM_LIDAR = -40005
+ FRAME_-40005_NAME = 'CLEM_LIDAR'
+ FRAME_-40005_CLASS = 4
+ FRAME_-40005_CLASS_ID = -40005
+ FRAME_-40005_CENTER = -40
+ TKFRAME_-40005_SPEC = 'ANGLES'
+ TKFRAME_-40005_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40005_ANGLES = ( -0.00504400153826,
+ -0.00125663706144,
+ 0.0 )
+ TKFRAME_-40005_AXES = ( 1, 2, 3 )
+ TKFRAME_-40005_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Star Tracker A (ASTAR) Frame
+
+ The rotation angles provided in the ASTAR frame definition below are
+ from [9].
+
+ \begindata
+
+ FRAME_CLEM_ASTAR = -40006
+ FRAME_-40006_NAME = 'CLEM_ASTAR'
+ FRAME_-40006_CLASS = 4
+ FRAME_-40006_CLASS_ID = -40006
+ FRAME_-40006_CENTER = -40
+ TKFRAME_-40006_SPEC = 'ANGLES'
+ TKFRAME_-40006_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40006_ANGLES = ( 2.04022706372830,
+ -0.52166146012859,
+ -3.06113297507285 )
+ TKFRAME_-40006_AXES = ( 1, 2, 3 )
+ TKFRAME_-40006_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Star Tracker B (BSTAR) Frame
+
+ The rotation angles provided in the frame BSTAR definition below are
+ from [10].
+
+ \begindata
+
+ FRAME_CLEM_BSTAR = -40007
+ FRAME_-40007_NAME = 'CLEM_BSTAR'
+ FRAME_-40007_CLASS = 4
+ FRAME_-40007_CLASS_ID = -40007
+ FRAME_-40007_CENTER = -40
+ TKFRAME_-40007_SPEC = 'ANGLES'
+ TKFRAME_-40007_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40007_ANGLES = ( -2.05078106971511,
+ -0.51341128875441,
+ -0.08063421144214 )
+ TKFRAME_-40007_AXES = ( 1, 2, 3 )
+ TKFRAME_-40007_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Charged Particle Telescope (CPT) Frame
+
+
+ The rotation angles provided in the frame definition below are
+ from [11].
+
+ \begindata
+
+ FRAME_CLEM_CPT = -40008
+ FRAME_-40008_NAME = 'CLEM_CPT'
+ FRAME_-40008_CLASS = 4
+ FRAME_-40008_CLASS_ID = -40008
+ FRAME_-40008_CENTER = -40
+ TKFRAME_-40008_SPEC = 'ANGLES'
+ TKFRAME_-40008_RELATIVE = 'CLEM_SC_BUS'
+ TKFRAME_-40008_ANGLES = ( 0.0,
+ -3.141592654,
+ 0.0 )
+ TKFRAME_-40008_AXES = ( 1, 2, 3 )
+ TKFRAME_-40008_UNITS = 'RADIANS'
+
+ \begintext
+
+
+Clementine NAIF ID Codes Definitions
+--------------------------------------------------------
+
+ This section contains name - to - NAIF ID mappings for the Clementine
+ mission. Once the contents of this file is loaded into the KERNEL
+ POOL, these mappings become available within SPICE, making it
+ possible to use these names in the high level SPICE routine calls.
+
+ Spacecraft:
+ -----------
+
+ DSPSE -40
+ CLEM -40
+ CLEMENTINE_1 -40
+ CLEMENTINE -40
+
+ CLEM_SPACECRAFT -40000
+ CLEM_SPACECRAFT_BUS -40000
+ CLEM_SC_BUS -40000
+
+ Science Instruments:
+ --------------------
+
+ CLEM_HIRES -40001
+ CLEM_UVVIS -40002
+ CLEM_NIR -40003
+ CLEM_LWIR -40004
+ CLEM_LIDAR -40005
+ CLEM_ASTAR -40006
+ CLEM_BSTAR -40007
+ CLEM_CPT -40008
+
+ UVVIS Specific Frames:
+ ----------------------
+
+ CLEM_UVVIS_A -40021
+ CLEM_UVVIS_B -40022
+ CLEM_UVVIS_C -40023
+ CLEM_UVVIS_D -40024
+ CLEM_UVVIS_E -40025
+ CLEM_UVVIS_F -40026
+
+
+ The mappings summarized in this table are implemented by the keywords
+ below.
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'DSPSE' )
+ NAIF_BODY_CODE += ( -40 )
+
+ NAIF_BODY_NAME += ( 'CLEM' )
+ NAIF_BODY_CODE += ( -40 )
+
+ NAIF_BODY_NAME += ( 'CLEMENTINE_1' )
+ NAIF_BODY_CODE += ( -40 )
+
+ NAIF_BODY_NAME += ( 'CLEMENTINE' )
+ NAIF_BODY_CODE += ( -40 )
+
+ NAIF_BODY_NAME += ( 'CLEM_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -40000 )
+
+ NAIF_BODY_NAME += ( 'CLEM_SPACECRAFT_BUS' )
+ NAIF_BODY_CODE += ( -40000 )
+
+ NAIF_BODY_NAME += ( 'CLEM_SC_BUS' )
+ NAIF_BODY_CODE += ( -40000 )
+
+ NAIF_BODY_NAME += ( 'CLEM_HIRES' )
+ NAIF_BODY_CODE += ( -40001 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS' )
+ NAIF_BODY_CODE += ( -40002 )
+
+ NAIF_BODY_NAME += ( 'CLEM_NIR' )
+ NAIF_BODY_CODE += ( -40003 )
+
+ NAIF_BODY_NAME += ( 'CLEM_LWIR' )
+ NAIF_BODY_CODE += ( -40004 )
+
+ NAIF_BODY_NAME += ( 'CLEM_LIDAR' )
+ NAIF_BODY_CODE += ( -40005 )
+
+ NAIF_BODY_NAME += ( 'CLEM_ASTAR' )
+ NAIF_BODY_CODE += ( -40006 )
+
+ NAIF_BODY_NAME += ( 'CLEM_BSTAR' )
+ NAIF_BODY_CODE += ( -40007 )
+
+ NAIF_BODY_NAME += ( 'CLEM_CPT' )
+ NAIF_BODY_CODE += ( -40008 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS_A' )
+ NAIF_BODY_CODE += ( -40021 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS_B' )
+ NAIF_BODY_CODE += ( -40022 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS_C' )
+ NAIF_BODY_CODE += ( -40023 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS_D' )
+ NAIF_BODY_CODE += ( -40024 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS_E' )
+ NAIF_BODY_CODE += ( -40025 )
+
+ NAIF_BODY_NAME += ( 'CLEM_UVVIS_F' )
+ NAIF_BODY_CODE += ( -40026 )
+
+ \begintext
+
diff --git a/tests/pytests/data/LUA3107H.161/dspse002.tsc b/tests/pytests/data/LUA3107H.161/dspse002.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..daa3c09496405fb84f75e7be1496c3b7172e612b
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/dspse002.tsc
@@ -0,0 +1,73 @@
+DSPSE SPICE SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between DSPSE
+ spacecraft clock time (SCLK) and ephemeris time.
+
+ NAIF suggests that you do not modify this file. If you do modify it,
+ be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ This file is DSPSE version 1, released 18-JAN-1994.
+
+
+Implementation notes
+--------------------------------------------------------
+
+ You must load this file into the kernel pool before using any of the
+ SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also need
+ to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names of
+ the files used on your system as arguments to LDPOOL. Because the file
+ names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading files.
+ The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+The DSPSE clock zero count occurs at 1-JAN-1950/00:00:00 UTC. Nominally,
+the clock will advance at UTC time. When a leapsecond occurs, the clock
+will be adjusted accordingly. When this event occurs, a new partition
+must be added to this file. To account for leapseconds prior to the
+launch of the spacecraft, the begin time below is
+1-JAN-1950/00:00:19.000.
+
+
+\begindata
+
+SCLK_KERNEL_ID = ( @1994-01-18 )
+
+SCLK_DATA_TYPE_40 = ( 1 )
+SCLK01_TIME_SYSTEM_40 = ( 2 )
+SCLK01_N_FIELDS_40 = ( 3 )
+SCLK01_MODULI_40 = ( 65536 10546.875 65536 )
+SCLK01_OFFSETS_40 = ( 0 0 0 )
+SCLK01_OUTPUT_DELIM_40 = ( 1 )
+
+SCLK_PARTITION_START_40 = ( 0.0000000000000E+00 )
+
+SCLK_PARTITION_END_40 = ( 4.5298483199999E+13 )
+
+SCLK01_COEFFICIENTS_40 = (
+
+ 0.0000000000000E+00 -1.5778799398160E+09 8.6400000000000E+04 )
+
+\begintext
+
diff --git a/tests/pytests/data/LUA3107H.161/lunarMeanEarth001.tf b/tests/pytests/data/LUA3107H.161/lunarMeanEarth001.tf
new file mode 100644
index 0000000000000000000000000000000000000000..a11b4a97a651ca2dfe5d8fe362f7d49531dd8a21
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/lunarMeanEarth001.tf
@@ -0,0 +1,370 @@
+
+KPL/FK
+
+
+ SPICE Generic Lunar Reference Frame Specification Kernel
+ =====================================================================
+
+ Original file name: lunar_060616.tf
+ Creation date: 2006 June 16 18:54
+ Created by: Nat Bachman (NAIF/JPL)
+
+ Modified: 2007 July 10 15:02
+ Modified By: Jeff Anderson
+ Note: Define lunar frame to default
+ to mean-earth
+
+
+ Introduction
+ =====================================================================
+
+ This kernel specifies lunar body-fixed reference frames for use by
+ SPICE-based application software. These reference frames are
+ associated with high-accuracy lunar orientation data provided by the
+ JPL Solar System Dynamics Group's planetary ephemerides (both
+ trajectory and lunar orientation data are stored in these ephemeris
+ files). These ephemerides have names of the form DE-nnn (DE stands
+ for "developmental ephemeris").
+
+ The frames specified by this kernel are realizations of two different
+ lunar reference systems:
+
+ Principal axes (PA) system
+ --------------------------
+ The axes of this system are defined by the principal axes of the
+ Moon. Note that, due to the nature of the Moon's orbit and
+ rotation, the Z axis of this system does not coincide with the
+ Moon's mean spin axis, nor does the X axis coincide with the mean
+ direction to the center of the Earth.
+
+ Lunar principal axes frames realizing the lunar PA system and
+ specified by this kernel are associated with JPL planetary
+ ephemerides. Each new JPL planetary ephemeris can (but does not
+ necessarily) define a new realization of the lunar principal axes
+ system. Coordinates of lunar surface features expressed in lunar
+ PA frames can change slightly from one lunar ephemeris version to
+ the next.
+
+
+ Mean Earth/polar axis (ME) system
+ ---------------------------------
+ The Lunar mean Earth/axis system is a lunar body-fixed reference
+ system used in the IAU/IAG Working Group Report [2] to describe
+ the orientation of the Moon relative to the ICRF frame. The +Z
+ axis of this system is aligned with the mean lunar north pole,
+ while the prime meridian contains the the mean Earth direction.
+
+ The mean directions used to define the axes of a mean Earth/polar
+ axis reference frame realizing the lunar ME system and specified
+ by this kernel are associated with a given JPL planetary
+ ephemeris version. The rotation between the mean Earth frame for
+ a given ephemeris version and the associated principal axes frame
+ is given by a constant matrix (see [1]).
+
+
+ For each JPL planetary ephemeris (DE), this kernel includes
+ specifications of the corresponding principal axes and mean Earth/
+ polar axis frames. The names of these frames have the form
+
+ LUNAR_DE-nnn_PR_AXES
+
+ and
+
+ LUNAR_DE-nn_MEAN_EARTH
+
+ respectively. This set of DE-dependent frame specifications will
+ grow over time; frame specifications pertaining to older DEs will
+ be retained in later versions of this frame kernel.
+
+ For each type of reference frame, there are two "generic"
+ frame specifications: these frames are simply aliases for the
+ two lunar body-fixed frames associated with the latest DE. The
+ generic frame names are
+
+ LUNAR_PR_AXES
+ LUNAR_MEAN_EARTH
+
+ SPICE users may, if they wish, modify this kernel to assign these
+ frame aliases to older DE-based frames. NAIF recommends that, if
+ this file is modified, the name of this file also be changed to
+ avoid confusion.
+
+
+ Comparison of PA and ME frames
+ ------------------------------
+
+ The rotation between the mean Earth frame for a given DE and the
+ associated principal axes frame for the same DE is given by a constant
+ matrix (see [1]). For DE-403, the rotation angle of this matrix is
+ approximately 0.028241 degrees; this is equivalent to approximately 860 m
+ when expressed as a displacement along a great circle on the Moon's
+ surface.
+
+
+ Comparison of DE-based and IAU/IAG report rotation data
+ -------------------------------------------------------
+
+ Within the SPICE system, the lunar ME frame specified by the
+ rotational elements from the IAU/IAG Working Group report [2] is
+ given the name IAU_MOON; the data defining this frame are provided
+ in a generic text PCK.
+
+ The orientation of the lunar ME frame obtained from the DE-based
+ lunar libration data and application of the DE-based PA-to-ME
+ rotation described above does not agree closely with the lunar ME
+ frame orientation given by the rotational elements from the IAU/IAG
+ Working Group report (that is, the IAU_MOON frame). The difference
+ is due to truncation of the libration series used in the report's
+ formula for lunar orientation (see [1]).
+
+ In the case of DE-403, for the time period ~2000-2020, this
+ time-dependent difference has an amplitude of approximately 0.005
+ degrees, which is equivalent to approximately 150 m, measured along
+ a great circle on the Moon's surface, while the average value is
+ approximately 0.0025 degrees, or 75 m.
+
+
+ Using this Kernel
+ =====================================================================
+
+ In order for a SPICE-based application to use reference frames
+ specified by this kernel, the application must load both this kernel
+ and a binary lunar PCK containing lunar orientation data for the
+ time of interest. Normally the kernels need be loaded only once
+ during program initialization.
+
+ SPICE users may find it convenient to use a meta-kernel (also called
+ a "FURNSH kernel") to name the kernels to be loaded. Below, we show
+ an example of such a meta-kernel, as well as the source code of a
+ small Fortran program that uses lunar body fixed frames. The
+ program's output is included as well.
+
+ The kernel names shown here are simply used as examples; users must
+ select the kernels appropriate for their applications.
+
+ Numeric results shown below may differ from those obtained on users'
+ computer systems.
+
+
+ Meta-kernel
+ -----------
+
+ Example meta-kernel showing use of
+
+ - binary lunar PCK
+ - generic lunar frame kernel (FK)
+ - leapseconds kernel (LSK)
+ - planetary SPK
+
+ 16-JUN-2006 (NJB)
+
+ Note: to actually use this kernel, replace the @
+ characters below with backslashes (\). The
+ backslash character cannot be used here because these
+ comments would be interpreted as actual load commands.
+
+ @begindata
+
+ KERNELS_TO_LOAD = ( 'de403_2000-2020_pa.bpc'
+ 'lunar_060616.tf'
+ '/kernels/gen/lsk/leapseconds.ker'
+ '/kernels/gen/spk/de405.bsp' )
+
+ @begintext
+
+
+ Example program
+ ---------------
+
+ PROGRAM EX1
+ IMPLICIT NONE
+
+ INTEGER FILSIZ
+ PARAMETER ( FILSIZ = 255 )
+
+ CHARACTER*(FILSIZ) META
+
+ DOUBLE PRECISION ET
+ DOUBLE PRECISION LT
+ DOUBLE PRECISION STME ( 6 )
+ DOUBLE PRECISION STPA ( 6 )
+
+ C
+ C Prompt user for meta-kernel name.
+ C
+ CALL PROMPT ( 'Enter name of meta-kernel > ', META )
+
+ C
+ C Load lunar PCK, generic lunar frame kernel,
+ C leapseconds kernel, and planetary ephemeris
+ C via metakernel.
+ C
+ CALL FURNSH ( META )
+
+ C
+ C Convert a time of interest from UTC to ET.
+ C
+ CALL STR2ET ( '2006 jun 8 06:50:00', ET )
+
+ WRITE (*,*) 'ET (sec past J2000 TDB): ', ET
+ WRITE (*,*) ' State of Earth relative to Moon'
+
+ C
+ C Find the geometric state of the Earth relative to the
+ C Moon at ET, expressed relative to the generic ME frame.
+ C
+ CALL SPKEZR ( 'Earth', ET, 'LUNAR_MEAN_EARTH',
+ . 'NONE', 'Moon', STME, LT )
+
+ WRITE (*,*) ' In ME frame:'
+ WRITE (*,*) STME
+
+ C
+ C Find the geometric state of the Earth relative to the
+ C Moon at ET, expressed relative to the generic PA frame.
+ C
+ CALL SPKEZR ( 'Earth', ET, 'LUNAR_PR_AXES',
+ . 'NONE', 'Moon', STPA, LT )
+
+ WRITE (*,*) ' In PA frame:'
+ WRITE (*,*) STPA
+
+ END
+
+
+ Program output
+ --------------
+
+ Enter name of meta-kernel > meta
+ ET (sec past J2000 TDB): 203021465.
+ State of Earth relative to Moon
+ In ME frame:
+ 391739.183 -33210.254 25299.0887 -0.0592286405 -0.048721834 0.0917188552
+ In PA frame:
+ 391719.148 -33331.588 25449.2934 -0.0592788895 -0.0487034073 0.0916961762
+
+
+
+ References
+ =====================================================================
+
+ [1] A.S. Konopliv, S.W. Asmar, E. Carranza, W.L. Sjogren, and D.N.
+ Yuan (2001). "Recent Gravity Models as a Result of the Lunar
+ Prospector Mission," Icarus 150, pp. 1-18.
+
+ [2] Seidelmann, P.K., Abalakin, V.K., Bursa, M., Davies, M.E.,
+ Bergh, C. de, Lieske, J.H., Oberst, J., Simon, J.L., Standish,
+ E.M., Stooke, P., and Thomas, P.C. (2002). "Report of the
+ IAU/IAG Working Group on Cartographic Coordinates and Rotational
+ Elements of the Planets and Satellites: 2000," Celestial
+ Mechanics and Dynamical Astronomy, v.82, Issue 1, pp. 83-111.
+
+ [3] Roncoli, R. (2005). "Lunar Constants and Models Document,"
+ JPL D-32296.
+
+
+ Frame Specifications
+ =====================================================================
+
+ LUNAR_PR_AXES is the name of the generic lunar principal axes
+ reference frame. This frame is an alias for the principal axes
+ frame defined by the latest version of the JPL Solar System Dynamics
+ Group's planetary ephemeris.
+
+ Currently LUNAR_PR_AXES is an alias for the lunar principal axes
+ frame associated with the planetary ephemeris DE-403.
+
+ \begindata
+
+ FRAME_LUNAR_PR_AXES = 310000
+ FRAME_310000_NAME = 'LUNAR_PR_AXES'
+ FRAME_310000_CLASS = 4
+ FRAME_310000_CLASS_ID = 310000
+ FRAME_310000_CENTER = 301
+
+ TKFRAME_310000_SPEC = 'MATRIX'
+ TKFRAME_310000_RELATIVE = 'LUNAR_DE-403_PR_AXES'
+ TKFRAME_310000_MATRIX = ( 1 0 0
+ 0 1 0
+ 0 0 1 )
+
+ \begintext
+
+ LUNAR_MEAN_EARTH is the name of the generic lunar mean Earth/ polar
+ axis reference frame. This frame is an alias for the mean
+ Earth/polar axis frame defined by the latest version of the JPL
+ Solar System Dynamics Group's planetary ephemeris.
+
+ Currently LUNAR_MEAN_EARTH is an alias for the lunar mean Earth/
+ polar axis frame associated with the planetary ephemeris DE-403.
+
+ \begindata
+
+ FRAME_LUNAR_MEAN_EARTH = 310001
+ FRAME_310001_NAME = 'LUNAR_MEAN_EARTH'
+ FRAME_310001_CLASS = 4
+ FRAME_310001_CLASS_ID = 310001
+ FRAME_310001_CENTER = 301
+
+ TKFRAME_310001_SPEC = 'MATRIX'
+ TKFRAME_310001_RELATIVE = 'LUNAR_DE-403_MEAN_EARTH'
+ TKFRAME_310001_MATRIX = ( 1 0 0
+ 0 1 0
+ 0 0 1 )
+
+ \begintext
+
+
+ LUNAR_DE-403_PR_AXES is the name of the lunar principal axes
+ reference frame defined by JPL's DE-403 planetary ephemeris.
+
+ \begindata
+
+ FRAME_LUNAR_DE-403_PR_AXES = 310002
+ FRAME_310002_NAME = 'LUNAR_DE-403_PR_AXES'
+ FRAME_310002_CLASS = 2
+ FRAME_310002_CLASS_ID = 31000
+ FRAME_310002_CENTER = 301
+
+ \begintext
+
+
+
+ LUNAR_DE-403_MEAN_EARTH is the name of the lunar mean Earth/polar
+ axis reference frame defined by JPL's DE-403 planetary ephemeris.
+
+ Rotation angles are from reference [1].
+
+ \begindata
+
+ FRAME_LUNAR_DE-403_MEAN_EARTH = 310003
+ FRAME_310003_NAME = 'LUNAR_DE-403_MEAN_EARTH'
+ FRAME_310003_CLASS = 4
+ FRAME_310003_CLASS_ID = 310003
+ FRAME_310003_CENTER = 301
+
+ TKFRAME_310003_SPEC = 'ANGLES'
+ TKFRAME_310003_RELATIVE = 'LUNAR_PR_AXES'
+ TKFRAME_310003_ANGLES = ( 63.8986 79.0768 0.1462 )
+ TKFRAME_310003_AXES = ( 3, 2, 1 )
+ TKFRAME_310003_UNITS = 'ARCSECONDS'
+
+ \begintext
+
+ Set to Mean Earth Lunar frame, dcook July 2007
+
+ \begindata
+ OBJECT_MOON_FRAME = 'LUNAR_MEAN_EARTH'
+ OBJECT_301_FRAME = 'LUNAR_MEAN_EARTH'
+
+ \begintext
+ End of kernel
+
+
+
+
+
+
+
+
+
diff --git a/tests/pytests/data/LUA3107H.161/lunar_de403_1950-2199_pa.bpc b/tests/pytests/data/LUA3107H.161/lunar_de403_1950-2199_pa.bpc
new file mode 100644
index 0000000000000000000000000000000000000000..40930fe3ec1d2dcbd5967f46346ceb4794d05521
Binary files /dev/null and b/tests/pytests/data/LUA3107H.161/lunar_de403_1950-2199_pa.bpc differ
diff --git a/tests/pytests/data/LUA3107H.161/naif0012.tls b/tests/pytests/data/LUA3107H.161/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/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/LUA3107H.161/pck00009.tpc b/tests/pytests/data/LUA3107H.161/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+Purpose
+--------------------------------------------------------
+
+ This file makes available for use in SPICE-based application
+ software orientation and size/shape data for natural bodies. The
+ principal source of the data is a published report by the IAU/IAG
+ Working Group on Cartographic Coordinates and Rotational Elements [1].
+
+ Orientation and size/shape data not provided by this file may be
+ available in mission-specific PCK files. Such PCKs may be the preferred
+ data source for mission-related applications. Mission-specific PCKs can
+ be found in PDS archives or on the NAIF web site at URL:
+
+ http://naif.jpl.nasa.gov
+
+
+File Organization
+--------------------------------------------------------
+
+ The contents of this file are as follows.
+
+ Introductory Information:
+
+ -- Purpose
+
+ -- File Organization
+
+ -- Version description
+
+ -- Disclaimer
+
+ -- Sources
+
+ -- Explanatory notes
+
+ -- Body numbers and names
+
+
+ PcK Data:
+
+
+ Orientation Data
+ ----------------
+
+ -- Orientation constants for the Sun and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+Disclaimer
+--------------------------------------------------------
+
+Applicability of Data
+
+ This P_constants file may not contain the parameter values that
+ you prefer. NAIF suggests that you inspect this file visually
+ before proceeding with any critical or extended data processing.
+
+File Modifications by Users
+
+ Note that this file may be readily modified by you to change
+ values or add/delete parameters. NAIF requests that you update the
+ "by line," date, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG Working Group Report [1] to be accurate to 0.1 degree
+ ([1], p.158). However, NAIF notes that orientation models for
+ natural satellites and asteroids have in some cases changed
+ substantially with the availability of new observational data, so
+ users are urged to investigate the suitability for their
+ applications of the models presented here.
+
+ Earth orientation
+ -----------------
+
+ NAIF strongly cautions against using the earth rotation model
+ (from [1]) for work demanding high accuracy. This model has been
+ determined by NAIF to have an error in the prime meridian location
+ of magnitude at least 150 arcseconds, with a local minimum
+ occurring during the year 1999. Regarding availability of better
+ earth orientation data for use with the SPICE system:
+
+ Earth orientation data are available from NAIF in the form of
+ binary earth PCK files. NAIF employs an automated process to
+ create these files; each time JPL's Tracking Systems and
+ Applications Section produces a new earth orientation parameter
+ (EOP) file, a new PCK is produced. These PCKs cover a roughly
+ 10 year time span starting at Jan. 1, 2000. In these PCK files,
+ the following effects are accounted for in modeling the earth's
+ rotation:
+
+ - Precession: 1976 IAU model
+
+ - Nutation: 1980 IAU model, plus interpolated
+ EOP nutation corrections
+
+ - Polar motion: interpolated from EOP file
+
+ - True sidereal time:
+
+ UT1 - UT1R (if needed): given by analytic formula
+ + TAI - UT1 (or UT1R): interpolated from EOP file
+ + UT1 - GMST: given by analytic formula
+ + equation of equinoxes: given by analytic formula
+
+ where
+
+ TAI = International Atomic Time
+ UT1 = Greenwich hour angle of computed mean sun - 12h
+ UT1R = Regularized UT1
+ GMST = Greenwich mean sidereal time
+
+ These kernels are available from the NAIF web site
+
+ http://naif.jpl.nasa.gov
+
+ (follow the links to Data, generic_kernels, and PCK data) or
+
+ ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck
+
+ or via anonymous ftp from the server
+
+ naif.jpl.nasa.gov
+
+ The kernels are in the path
+
+ pub/naif/generic_kernels/pck
+
+ At this time, these kernels have file names of the form
+
+ earth_000101_yymmdd_yymmdd.bpc
+
+ The second and third dates are, respectively, the file's
+ coverage end time and the epoch of the last datum.
+
+ These binary PCK files are very accurate (error < 0.1
+ microradian) for epochs preceding the epoch of the last datum.
+ For later epochs, the error rises to several microradians.
+
+ Binary PCK files giving accurate earth orientation from 1972 to
+ 2007 and *low accuracy* predicted earth orientation from
+ 2007 to 2037 are also available in the same location. See the
+ aareadme.txt file at the "pck" URL above for details.
+
+ Characteristics and names of the binary kernels described here
+ are subject to change. See the "pck" URL above for information
+ on current binary earth PCKs.
+
+
+ Lunar orientation
+ -----------------
+
+ The lunar orientation formula provided by this file is a
+ trigonometric polynomial approximation yielding the orientation of
+ the lunar "Mean Earth/Polar Axis" (ME) reference frame. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which are available on the NAIF web site (see URLS above)
+ and in the NAIF server's ftp area. The lunar frame kernel
+ is located in the path
+
+ pub/naif/generic_kernels/fk/satellites
+
+ and has a name of the form
+
+ moon_yymmdd.tf
+
+ The binary lunar PCK is in the path
+
+ pub/naif/generic_kernels/pck
+
+ and has a name of the form
+
+ moon_pa_dennn_yyyy-yyyy.bpc
+
+ See the "aareadme.txt" files in the paths shown above for details
+ on file contents and versions. We also suggest you refer to the
+ SPICE tutorial named "lunar_earth_pck-fk," which is available from
+ the NAIF web site.
+
+
+ Earth geomagnetic dipole
+ ------------------------
+
+ The SPICE Toolkit doesn't currently contain software to model the
+ earth's north geomagnetic centered dipole as a function of time.
+ As a convenience for users, the north dipole location from the
+ J2000 epoch was selected as a representative datum, and the
+ planetocentric longitude and latitude of this location have been
+ associated with the keywords
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT
+
+ Values for the earth's north geomagnetic centered dipole are
+ presented in comments as a discrete time series for the time range
+ 1945-2000. For details concerning the geomagnetic field model from
+ which these values were derived, including a discussion of the
+ model's accuracy, see [9].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value is provided for informational
+ purposes only.
+
+
+ Software limitations
+ --------------------
+
+ SPICE Toolkits prior to version N0057 cannot make use of
+ trigonometric polynomial terms in the formulas for orientation of
+ the planets. The only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ The second nutation precession angle (M2) for Mars is represented
+ by a quadratic polynomial in the 2006 IAU report. The SPICELIB
+ subroutine BODEUL can not handle this term (which is extremely
+ small), so we truncate the polynomial to a linear one. The
+ resulting orientation error has a maximum magnitude of less
+ than 0.0032 degrees over the time span 1996-2015 and less than
+ 0.0082 degrees over the time span 1986-2025.
+
+
+Sources
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Conrad, A., Consolmagno, G.J., Hestroffer, D.,
+ Hilton, J.L., Krasinsky, G.A., Neumann, G.,
+ Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J.,
+ and Thomas, P.C. "Report of the IAU/IAG Working Group
+ on cartographic coordinates and rotational elements: 2006."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] Nautical Almanac Office, United States Naval Observatory
+ and H.M. Nautical Almanac Office, Rutherford Appleton
+ Laboratory (2010). "The Astronomical Almanac for
+ the Year 2010," U.S. Government Printing Office,
+ Washington, D.C.: and The Stationary Office, London.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [5] Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+ Conventions," presentation to the Mars Express Data
+ Archive Working Group, Dec. 14, 2001.
+
+ [6] Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic
+ Field and Magnetosphere." <http://www-ssc.igpp.ucla.
+ edu/personnel/russell/papers/earth_mag>. Originally
+ published in "Encyclopedia of Planetary Sciences," J.H.
+ Shirley and R.W. Fainbridge, eds. Chapman and Hall,
+ New York, pp 208-211.
+
+ [7] Russell, C.T. (1971). "Geophysical Coordinate
+ Transformations," Cosmic Electrodynamics 2 184-186.
+ NAIF document 181.0.
+
+ [8] ESA/ESTEC Space Environment Information System (SPENVIS)
+ (2003). Web page: "Dipole approximations of the
+ geomagnetic field." <http://www.spenvis.oma.be/spenvis/
+ help/background/magfield/cd.html>.
+
+ [9] International Association of Geomagnetism and Aeronomy
+ and International Union of Geodesy and Geophysics (2004).
+ Web page: "The 9th Generation International Geomagnetic
+ Reference Field." <http://www.ngdc.noaa.gov/
+ IAGA/vmod/igrf.html>.
+
+ [10] Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
+ and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
+ Working Group on Cartographic Coordinates and Rotational
+ Elements of the Planets and Satellites: 1988," Celestial
+ Mechanics and Dynamical Astronomy, v.46, no.2, pp.
+ 187-204.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- The second nutation precession angle (M2) for Mars is
+ represented by a quadratic polynomial in the 2000
+ IAU report. The SPICELIB subroutine BODEUL can not
+ handle this term (which is extremely small), so we
+ truncate the polynomial to a linear one.
+
+ -- Earth north geomagnetic centered dipole values are from
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+Explanatory Notes
+--------------------------------------------------------
+
+ This file, which is logically part of the SPICE P-kernel, contains
+ constants used to model the orientation, size and shape of the
+ Sun, planets, natural satellites, and selected comets and
+ asteroids. The orientation models express the direction of the
+ pole and location of the prime meridian of a body as a function of
+ time. The size/shape models ("shape models" for short) represent
+ all bodies as ellipsoids, using two equatorial radii and a polar
+ radius. Spheroids and spheres are obtained when two or all three
+ radii are equal.
+
+ The SPICE Toolkit routines that use this file are documented in
+ the SPICE "Required Reading" file pck.req. They are also
+ documented in the "PCK" SPICE tutorial, which is available on
+ the NAIF web site.
+
+File Format
+
+ A terse description of the PCK file format is given here. See the
+ SPICE "Required Reading" files pck.req and kernel.req for a
+ detailed explanation of the SPICE text kernel file format. The
+ files pck.req and kernel.req are included in the documentation
+ provided with the SPICE Toolkit.
+
+ The file starts out with the ``ID word'' string
+
+ KPL/PCK
+
+ This string identifies the file as a text kernel containing PCK
+ data.
+
+ This file consists of a series of comment blocks and data blocks.
+ Comment blocks, which contain free-form descriptive or explanatory
+ text, are preceded by a \begintext token. Data blocks follow a
+ \begindata token. In order to be recognized, each of these tokens
+ must be placed on a line by itself.
+
+ The portion of the file preceding the first data block is treated
+ as a comment block; it doesn't require an initial \begintext
+ token.
+
+ This file identifies data using a series of
+
+ KEYWORD = VALUE
+
+ assignments. The left hand side of each assignment is a
+ "kernel variable" name; the right hand side is an associated value
+ or list of values. The SPICE subroutine API allows SPICE routines
+ and user applications to retrieve the set of values associated
+ with each kernel variable name.
+
+ Kernel variable names are case-sensitive and are limited to
+ 32 characters in length.
+
+ Numeric values may be integer or floating point. String values
+ are normally limited to 80 characters in length; however, SPICE
+ provides a mechanism for identifying longer, "continued" strings.
+ See the SPICE routine STPOOL for details.
+
+ String values are single quoted.
+
+ When the right hand side of an assignment is a list of values,
+ the list items may be separated by commas or simply by blanks.
+ The list must be bracketed by parentheses. Example:
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ This file may contain blank lines anywhere. Non-printing
+ characters including TAB should not be present in the file: the
+ presence of such characters may cause formatting errors when the
+ file is viewed.
+
+Time systems and reference frames
+
+ The 2006 IAU/IAG Working Group Report [1] states the time scale
+ used as the independent variable for the rotation formulas is
+ Barycentric Dynamical Time (TDB) and that the epoch of variable
+ quantities is J2000 TDB (2000 Jan 1 12:00 TDB). Throughout SPICE
+ documentation and in this file, we use the names "J2000 TDB" and
+ "J2000" for this epoch. The name "J2000.0" is equivalent.
+
+ SPICE documentation refers to the time system used in this file
+ as either "ET" or "TDB." SPICE software makes no distinction
+ between TDB and the time system associated with the independent
+ variable of the JPL planetary ephemerides T_eph.
+
+ The inertial reference frame used for the rotational elements in
+ this file is identified by [1] as the ICRF (International
+ Celestial Reference Frame).
+
+ The SPICE PCK software that reads this file uses the label "J2000"
+ to refer to the ICRF; this is actually a mislabeling which has
+ been retained in the interest of backward compatibility. Using
+ data from this file, by means of calls to the SPICE frame
+ transformation routines, will actually compute orientation
+ relative to the ICRF.
+
+ The difference between the J2000 frame and the ICRF is
+ on the order of tens of milliarcseconds and is well below the
+ accuracy level of the formulas in this file.
+
+Orientation models
+
+ All of the orientation models use three Euler angles to describe
+ the orientation of the coordinate axes of the "Body Equator and
+ Prime Meridian" system with respect to an inertial system. By
+ default, the inertial system is the ICRF (labeled as "J2000"), but
+ other frames can be specified in the file. See the PCK Required
+ Reading for details.
+
+ The first two angles, in order, are the ICRF right ascension and
+ declination (henceforth RA and DEC) of the north pole of a body as
+ a function of time. The third angle is the prime meridian location
+ (represented by "W"), which is expressed as a rotation about the
+ north pole, and is also a function of time.
+
+ For each body, the expressions for the north pole's right
+ ascension and declination, as well as prime meridian location, are
+ sums (as far as the models that appear in this file are concerned)
+ of quadratic polynomials and trigonometric polynomials, where the
+ independent variable is time.
+
+ In this file, the time arguments in expressions always refer to
+ Barycentric Dynamical Time (TDB), measured in centuries or days
+ past a reference epoch. By default, the reference epoch is the
+ J2000 epoch, which is Julian ephemeris date 2451545.0, but other
+ epochs can be specified in the file. See the PCK Required Reading
+ for details.
+
+ Orientation models for satellites and some planets (including
+ Jupiter) involve both polynomial terms and trigonometric terms.
+ The arguments of the trigonometric terms are linear polynomials.
+ In this file, we call the arguments of these trigonometric terms
+ "nutation precession angles."
+
+ Example: 2006 IAU Model for orientation of Jupiter. Note that
+ these values are used as an example only; see the data area below
+ for current values.
+
+ Right ascension
+ ---------------
+
+ alpha = 268.056595 - 0.006499 T + 0.000117 sin(Ja)
+ 0 + 0.000938 sin(Jb) + 0.001432 sin(Jc)
+ + 0.000030 sin(Jd) + 0.002150 sin(Je)
+
+ Declination
+ -----------
+
+ delta = 64.495303 + 0.002413 T + 0.000050 cos(Ja)
+ 0 + 0.000404 cos(Jb) + 0.000617 cos(Jc)
+ - 0.000013 cos(Jd) + 0.000926 cos(Je)
+
+ Prime meridian
+ --------------
+
+ W = 284.95 + 870.5366420 d
+
+
+ Here
+
+ T represents centuries past J2000 ( TDB ),
+
+ d represents days past J2000 ( TDB ).
+
+ Ja-Je are nutation precession angles.
+
+ In this file, the polynomials' coefficients above are assigned
+ to kernel variable names (left-hand-side symbols) as follows
+
+ BODY599_POLE_RA = ( 268.056595 -0.006499 0. )
+ BODY599_POLE_DEC = ( 64.495303 0.002413 0. )
+ BODY599_PM = ( 284.95 870.5366420 0. )
+
+ and the trigonometric polynomials' coefficients are assigned
+ as follows
+
+ BODY599_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117
+ 0.000938
+ 0.001432
+ 0.000030
+ 0.002150 )
+
+ BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050
+ 0.000404
+ 0.000617
+ -0.000013
+ 0.000926 )
+
+ BODY599_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0 )
+
+ Note the number "599"; this is the NAIF ID code for Jupiter.
+
+ In this file, the polynomial expressions for the nutation
+ precession angles are listed along with the planet's RA, DEC, and
+ prime meridian terms. Below are the 2006 IAU nutation precession
+ angles for the Jupiter system.
+
+ J1 = 73.32 + 91472.9 T
+ J2 = 24.62 + 45137.2 T
+ J3 = 283.90 + 4850.7 T
+ J4 = 355.80 + 1191.3 T
+ J5 = 119.90 + 262.1 T
+ J6 = 229.80 + 64.3 T
+ J7 = 352.25 + 2382.6 T
+ J8 = 113.35 + 6070.0 T
+
+ J9 = 146.64 + 182945.8 T
+ J10 = 49.24 + 90274.4 T
+
+ Ja = 99.360714 + 4850.4046 T
+ Jb = 175.895369 + 1191.9605 T
+ Jc = 300.323162 + 262.5475 T
+ Jd = 114.012305 + 6070.2476 T
+ Je = 49.511251 + 64.3000 T
+
+ Here
+
+ T represents centuries past J2000 ( TDB )
+
+ J1-J10 and Ja-Je are the nutation precession angles. The angles
+ J9 and J10 are equal to 2*J1 and 2*J2, respectively.
+
+ Angles J9 and J10 are not present in [1]; they have been added
+ to fit the terms 2*J1 and 2*J2, which appear in the orientation
+ models of several satellites, into a form that can be accepted
+ by the PCK system.
+
+ The assignment of the nutation precession angles for the
+ Jupiter system is as follows:
+
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.25 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4
+ 99.360714 4850.4046
+ 175.895369 1191.9605
+ 300.323162 262.5475
+ 114.012305 6070.2476
+ 49.511251 64.3000 )
+
+ You'll see an additional symbol grouped with the ones listed
+ above; it is
+
+ BODY599_LONG_AXIS
+
+ This term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ The pattern of the formulas for satellite orientation is similar
+ to that for Jupiter. Example: 2006 IAU values for Io. Again, these
+ values are used as an example only; see the data area below for
+ current values.
+
+ Right ascension
+ ---------------
+
+ alpha = 268.05 - 0.009 T + 0.094 sin(J3) + 0.024 sin(J4)
+ 0
+
+ Declination
+ -----------
+
+ delta = 64.50 + 0.003 T + 0.040 cos(J3) + 0.011 cos(J4)
+ 0
+
+ Prime meridian
+ --------------
+
+ W = 200.39 + 203.4889538 d - 0.085 sin(J3) - 0.022 sin(J4)
+
+
+ d represents days past J2000.
+
+ J3 and J4 are nutation precession angles.
+
+ The polynomial terms are assigned to symbols by the statements
+
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( 64.50 0.003 0. )
+ BODY501_PM = ( 200.39 203.4889538 0. )
+
+ The coefficients of the trigonometric terms are assigned to symbols by
+ the statements
+
+ BODY501_NUT_PREC_RA = ( 0. 0. 0.094 0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. 0.040 0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+
+ 501 is the NAIF ID code for Io.
+
+ SPICE software expects the models for satellite orientation to
+ follow the form of the model shown here: the polynomial portions of the
+ RA, DEC, and W expressions are expected to be quadratic, the
+ trigonometric terms for RA and W (satellite prime meridian) are expected
+ to be linear combinations of sines of nutation precession angles, the
+ trigonometric terms for DEC are expected to be linear combinations of
+ cosines of nutation precession angles, and the polynomials for the
+ nutation precession angles themselves are expected to be linear.
+
+ Eventually, the software will handle more complex expressions, we
+ expect.
+
+
+Shape models
+
+ There is only one kind of shape model supported by the SPICE Toolkit
+ software at present: the triaxial ellipsoid. The 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ For each body, three radii are listed: The first number is
+ the largest equatorial radius (the length of the semi-axis
+ containing the prime meridian), the second number is the smaller
+ equatorial radius, and the third is the polar radius.
+
+ Example: Radii of the Earth.
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers and Names
+--------------------------------------------------------
+
+
+ 1 Mercury barycenter
+ 2 Venus barycenter
+ 3 Earth barycenter
+ 4 Mars barycenter
+ 5 Jupiter barycenter
+ 6 Saturn barycenter
+ 7 Uranus barycenter
+ 8 Neptune barycenter
+ 9 Pluto barycenter
+ 10 Sun
+
+
+ 199 Mercury
+
+
+ 299 Venus
+
+
+ 399 Earth
+
+ 301 Moon
+
+
+ 499 Mars
+
+ 401 Phobos 402 Deimos
+
+
+ 599 Jupiter
+
+ 501 Io 502 Europa 503 Ganymede 504 Callisto
+ 505 Amalthea 506 Himalia 507 Elara 508 Pasiphae
+ 509 Sinope 510 Lysithea 511 Carme 512 Ananke
+ 513 Leda 514 Thebe 515 Adrastea 516 Metis
+
+
+ 699 Saturn
+
+ 601 Mimas 602 Enceladus 603 Tethys 604 Dione
+ 605 Rhea 606 Titan 607 Hyperion 608 Iapetus
+ 609 Phoebe 610 Janus 611 Epimetheus 612 Helene
+ 613 Telesto 614 Calypso 615 Atlas 616 Prometheus
+ 617 Pandora 618 Pan
+
+
+ 799 Uranus
+
+ 701 Ariel 702 Umbriel 703 Titania 704 Oberon
+ 705 Miranda 706 Cordelia 707 Ophelia 708 Bianca
+ 709 Cressida 710 Desdemona 711 Juliet 712 Portia
+ 713 Rosalind 714 Belinda 715 Puck
+
+
+ 899 Neptune
+
+ 801 Triton 802 Nereid 803 Naiad 804 Thalassa
+ 805 Despina 806 Galatea 807 Larissa 808 Proteus
+
+
+ 999 Pluto
+
+ 901 Charon
+
+
+ 1000005 Comet 19P/Borrelly
+ 1000036 Comet Halley
+ 1000093 Comet 9P/Tempel 1
+ 1000107 Comet 81P/Wild 2
+
+ 2000001 Asteroid Ceres
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body10_pole_ra = ( 286.13 0. 0. )
+ body10_pole_dec = ( 63.87 0. 0. )
+ body10_pm = ( 84.10 14.18440 0. )
+ body10_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY10_POLE_RA = ( 286.13 0. 0. )
+ BODY10_POLE_DEC = ( 63.87 0. 0. )
+ BODY10_PM = ( 84.176 14.18440 0. )
+ BODY10_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_POLE_RA = ( 272.76 0. 0. )
+ BODY299_POLE_DEC = ( 67.16 0. 0. )
+ BODY299_PM = ( 160.20 -1.4813688 0. )
+
+ BODY299_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY399_POLE_RA = ( 0. -0.641 0. )
+ BODY399_POLE_DEC = ( 90. -0.557 0. )
+ BODY399_PM = ( 190.147 360.9856235 0. )
+ BODY399_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Nutation precession angles for the Earth-Moon system:
+
+ The linear coefficients have been scaled up from degrees/day
+ to degrees/century, because the SPICELIB PCK reader expects
+ these units. The original constants were:
+
+ 125.045D0 -0.0529921D0
+ 250.089D0 -0.1059842D0
+ 260.008D0 13.0120009D0
+ 176.625D0 13.3407154D0
+ 357.529D0 0.9856003D0
+ 311.589D0 26.4057084D0
+ 134.963D0 13.0649930D0
+ 276.617D0 0.3287146D0
+ 34.226D0 1.7484877D0
+ 15.134D0 -0.1589763D0
+ 119.743D0 0.0036096D0
+ 239.961D0 0.1643573D0
+ 25.053D0 12.9590088D0
+
+
+ \begindata
+
+
+ BODY3_NUT_PREC_ANGLES = ( 125.045 -1935.5364525000
+ 250.089 -3871.0729050000
+ 260.008 475263.3328725000
+ 176.625 487269.6299850000
+ 357.529 35999.0509575000
+ 311.589 964468.4993100000
+ 134.963 477198.8693250000
+ 276.617 12006.3007650000
+ 34.226 63863.5132425000
+ 15.134 -5806.6093575000
+ 119.743 131.8406400000
+ 239.961 6003.1503825000
+ 25.053 473327.7964200000 )
+
+
+ \begintext
+
+
+ Earth north geomagnetic centered dipole:
+
+ Old values:
+
+ Values are from [7]. Note the year of publication was 1971.
+
+ body399_mag_north_pole_lon = ( -69.761 )
+ body399_mag_north_pole_lat = ( 78.565 )
+
+
+ Current values:
+
+ The north dipole location is time-varying. The values shown
+ below, taken from [8], represent a discrete sampling of the
+ north dipole location from 1945 to 2000. The terms DGRF and
+ IGRF refer to, respectively, "Definitive Geomagnetic
+ Reference Field" and "International Geomagnetic Reference
+ Field." See references [6], [8], and [9] for details.
+
+ Coordinates are planetocentric.
+
+ Data source Lat Lon
+ ----------- ----- ------
+ DGRF 1945 78.47 291.47
+ DGRF 1950 78.47 291.15
+ DGRF 1955 78.46 290.84
+ DGRF 1960 78.51 290.53
+ DGRF 1965 78.53 290.15
+ DGRF 1970 78.59 289.82
+ DGRF 1975 78.69 289.53
+ DGRF 1980 78.81 289.24
+ DGRF 1985 78.97 289.10
+ DGRF 1990 79.13 288.89
+ IGRF 1995 79.30 288.59
+ IGRF 2000 79.54 288.43
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY499_POLE_RA = ( 317.68143 -0.1061 0. )
+ BODY499_POLE_DEC = ( 52.88650 -0.0609 0. )
+ BODY499_PM = ( 176.630 350.89198226 0. )
+
+ \begintext
+
+ Source [5] specifies the following value for the lambda_a term
+ (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
+ LONGITUDE, measured from the prime meridian, of the meridian
+ containing the longest axis of the reference ellipsoid.
+ (CAUTION: previous values were POSITIVE WEST.)
+
+ body499_long_axis = ( 252. )
+
+ We list this lambda_a value for completeness. The IAU report
+ [1] gives equal values for both equatorial radii, so the
+ lambda_a offset does not apply to the IAU model.
+
+ The 2003 IAU report defines M2, the second nutation precession angle,
+ by:
+
+ 2
+ 192.93 + 1128.4096700 d + 8.864 T
+
+ We truncate the M2 series to a linear expression, because the PCK
+ software cannot handle the quadratic term.
+
+ Again, the linear terms are scaled by 36525.0:
+
+ -0.4357640000000000 --> -15916.28010000000
+ 1128.409670000000 --> 41215163.19675000
+ -1.8151000000000000E-02 --> -662.9652750000000
+
+ We also introduce a fourth nutation precession angle, which
+ is the pi/2-complement of the third angle. This angle is used
+ in computing the prime meridian location for Deimos. See the
+ discussion of this angle below in the section containing orientation
+ constants for Deimos.
+
+ \begindata
+
+ BODY4_NUT_PREC_ANGLES = ( 169.51 -15916.2801
+ 192.93 41215163.19675
+ 53.47 -662.965275
+ 36.53 662.965275 )
+
+ \begintext
+
+
+Jupiter
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body599_pole_ra = ( 268.05 -0.009 0. )
+ body599_pole_dec = ( 64.49 0.003 0. )
+ body599_pm = ( 284.95 870.5366420 0. )
+ body599_long_axis = ( 0. )
+
+ body5_nut_prec_angles = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.35 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4 )
+
+
+
+ Current values:
+
+ The number of nutation precession angles is 15. The ninth and
+ tenth are twice the first and second, respectively. The
+ eleventh through fifteenth correspond to angles JA-JE in
+ the 2006 IAU report; angles JA-JE were not used prior to that
+ report.
+
+ \begindata
+
+
+ BODY599_POLE_RA = ( 268.056595 -0.006499 0. )
+ BODY599_POLE_DEC = ( 64.495303 0.002413 0. )
+ BODY599_PM = ( 284.95 870.5366420 0. )
+ BODY599_LONG_AXIS = ( 0. )
+
+ BODY599_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117
+ 0.000938
+ 0.001432
+ 0.000030
+ 0.002150 )
+
+ BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050
+ 0.000404
+ 0.000617
+ -0.000013
+ 0.000926 )
+
+ BODY599_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0
+ 0.0
+ 0.0
+ 0.0
+ 0.0 )
+
+
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.25 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4
+ 99.360714 4850.4046
+ 175.895369 1191.9605
+ 300.323162 262.5475
+ 114.012305 6070.2476
+ 49.511251 64.3000 )
+ \begintext
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_POLE_RA = ( 40.589 -0.036 0. )
+ BODY699_POLE_DEC = ( 83.537 -0.004 0. )
+ BODY699_PM = ( 38.90 810.7939024 0. )
+ BODY699_LONG_AXIS = ( 0. )
+
+ \begintext
+
+ The first seven angles given here are the angles S1
+ through S7 from the 2000 report; the eighth and
+ ninth angles are 2*S1 and 2*S2, respectively.
+
+
+ \begindata
+
+ BODY6_NUT_PREC_ANGLES = ( 353.32 75706.7
+ 28.72 75706.7
+ 177.40 -36505.5
+ 300.00 -7225.9
+ 316.45 506.2
+ 345.20 -1016.3
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_POLE_RA = ( 257.311 0. 0. )
+ BODY799_POLE_DEC = ( -15.175 0. 0. )
+ BODY799_PM = ( 203.81 -501.1600928 0. )
+ BODY799_LONG_AXIS = ( 0. )
+
+ \begintext
+
+ The first 16 angles given here are the angles U1
+ through U16 from the 2000 report; the 17th and
+ 18th angles are 2*U11 and 2*U12, respectively.
+
+ \begindata
+
+ BODY7_NUT_PREC_ANGLES = ( 115.75 54991.87
+ 141.69 41887.66
+ 135.03 29927.35
+ 61.77 25733.59
+ 249.32 24471.46
+ 43.86 22278.41
+ 77.66 20289.42
+ 157.36 16652.76
+ 101.81 12872.63
+ 138.64 8061.81
+ 102.23 -2024.22
+ 316.41 2863.96
+ 304.01 -51.94
+ 308.71 -93.17
+ 340.82 -75.32
+ 259.14 -504.81
+ 204.46 -4048.44
+ 632.82 5727.92 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY899_POLE_RA = ( 299.36 0. 0. )
+ BODY899_POLE_DEC = ( 43.46 0. 0. )
+ BODY899_PM = ( 253.18 536.3128492 0. )
+ BODY899_LONG_AXIS = ( 0. )
+
+
+ BODY899_NUT_PREC_RA = ( 0.70 0. 0. 0. 0. 0. 0. 0. )
+ BODY899_NUT_PREC_DEC = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
+ BODY899_NUT_PREC_PM = ( -0.48 0. 0. 0. 0. 0. 0. 0. )
+
+ \begintext
+
+ The 2000 report defines the nutation precession angles
+
+ N, N1, N2, ... , N7
+
+ and also uses the multiples of N1 and N7
+
+ 2*N1
+
+ and
+
+ 2*N7, 3*N7, ..., 9*N7
+
+ In this file, we treat the angles and their multiples as
+ separate angles. In the kernel variable
+
+ BODY8_NUT_PREC_ANGLES
+
+ the order of the angles is
+
+ N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
+
+ Each angle is defined by a linear polynomial, so two
+ consecutive array elements are allocated for each
+ angle. The first term of each pair is the constant term,
+ the second is the linear term.
+
+ \begindata
+
+ BODY8_NUT_PREC_ANGLES = ( 357.85 52.316
+ 323.92 62606.6
+ 220.51 55064.2
+ 354.27 46564.5
+ 75.31 26109.4
+ 35.36 14325.4
+ 142.61 2824.6
+ 177.85 52.316
+ 647.840 125213.200
+ 355.700 104.632
+ 533.550 156.948
+ 711.400 209.264
+ 889.250 261.580
+ 1067.100 313.896
+ 1244.950 366.212
+ 1422.800 418.528
+ 1600.650 470.844 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ BODY999_POLE_RA = ( 312.993 0. 0. )
+ BODY999_POLE_DEC = ( 6.163 0. 0. )
+ BODY999_PM = ( 237.305 -56.3625225 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ New values:
+
+ \begindata
+
+
+
+
+
+ BODY301_POLE_RA = ( 269.9949 0.0031 0. )
+ BODY301_POLE_DEC = ( 66.5392 0.0130 0. )
+ BODY301_PM = ( 38.3213 13.17635815 -1.4D-12 )
+ BODY301_LONG_AXIS = ( 0. )
+
+ BODY301_NUT_PREC_RA = ( -3.8787 -0.1204 0.0700 -0.0172
+ 0.0 0.0072 0.0 0.0
+ 0.0 -0.0052 0.0 0.0
+ 0.0043 )
+
+ BODY301_NUT_PREC_DEC = ( 1.5419 0.0239 -0.0278 0.0068
+ 0.0 -0.0029 0.0009 0.0
+ 0.0 0.0008 0.0 0.0
+ -0.0009 )
+
+ BODY301_NUT_PREC_PM = ( 3.5610 0.1208 -0.0642 0.0158
+ 0.0252 -0.0066 -0.0047 -0.0046
+ 0.0028 0.0052 0.0040 0.0019
+ -0.0044 )
+ \begintext
+
+
+
+Satellites of Mars
+
+
+ Phobos
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ The quadratic prime meridian term is scaled by 1/36525**2:
+
+ 8.864000000000000 ---> 6.6443009930565219E-09
+
+ \begindata
+
+ BODY401_POLE_RA = ( 317.68 -0.108 0. )
+ BODY401_POLE_DEC = ( 52.90 -0.061 0. )
+ BODY401_PM = ( 35.06 1128.8445850 6.6443009930565219E-09 )
+
+ BODY401_LONG_AXIS = ( 0. )
+
+ BODY401_NUT_PREC_RA = ( 1.79 0. 0. 0. )
+ BODY401_NUT_PREC_DEC = ( -1.08 0. 0. 0. )
+ BODY401_NUT_PREC_PM = ( -1.42 -0.78 0. 0. )
+
+
+ \begintext
+
+
+ Deimos
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ New values:
+
+ The Deimos prime meridian expression is:
+
+
+ 2
+ W = 79.41 + 285.1618970 d - 0.520 T - 2.58 sin M
+ 3
+
+ + 0.19 cos M .
+ 3
+
+
+ At the present time, the PCK kernel software (the routine
+ BODEUL in particular) cannot handle the cosine term directly,
+ but we can represent it as
+
+ 0.19 sin M
+ 4
+
+ where
+
+ M = 90.D0 - M
+ 4 3
+
+ Therefore, the nutation precession angle assignments for Phobos
+ and Deimos contain four coefficients rather than three.
+
+ The quadratic prime meridian term is scaled by 1/36525**2:
+
+ -0.5200000000000000 ---> -3.8978300049519307E-10
+
+ \begindata
+
+ BODY402_POLE_RA = ( 316.65 -0.108 0. )
+ BODY402_POLE_DEC = ( 53.52 -0.061 0. )
+ BODY402_PM = ( 79.41 285.1618970 -3.897830D-10 )
+ BODY402_LONG_AXIS = ( 0. )
+
+ BODY402_NUT_PREC_RA = ( 0. 0. 2.98 0. )
+ BODY402_NUT_PREC_DEC = ( 0. 0. -1.78 0. )
+ BODY402_NUT_PREC_PM = ( 0. 0. -2.58 0.19 )
+
+ \begintext
+
+
+
+
+Satellites of Jupiter
+
+
+ Io
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( 64.50 0.003 0. )
+ BODY501_PM = ( 200.39 203.4889538 0. )
+ BODY501_LONG_AXIS = ( 0. )
+
+ BODY501_NUT_PREC_RA = ( 0. 0. 0.094 0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. 0.040 0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+
+ \begintext
+
+
+
+ Europa
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 0. )
+ body502_long_axis = ( 0. )
+
+ body502_nut_prec_ra = ( 0. 0. 0. 1.086 0.060 0.015 0.009 )
+ body502_nut_prec_dec = ( 0. 0. 0. 0.468 0.026 0.007 0.002 )
+ body502_nut_prec_pm = ( 0. 0. 0. -0.980 -0.054 -0.014 -0.008 )
+
+
+ Current values:
+
+ \begindata
+
+ BODY502_POLE_RA = ( 268.08 -0.009 0. )
+ BODY502_POLE_DEC = ( 64.51 0.003 0. )
+ BODY502_PM = ( 36.022 101.3747235 0. )
+ BODY502_LONG_AXIS = ( 0. )
+
+ BODY502_NUT_PREC_RA = ( 0. 0. 0. 1.086 0.060 0.015 0.009 )
+ BODY502_NUT_PREC_DEC = ( 0. 0. 0. 0.468 0.026 0.007 0.002 )
+ BODY502_NUT_PREC_PM = ( 0. 0. 0. -0.980 -0.054 -0.014 -0.008 )
+
+ \begintext
+
+
+ Ganymede
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY503_POLE_RA = ( 268.20 -0.009 0. )
+ BODY503_POLE_DEC = ( 64.57 0.003 0. )
+ BODY503_PM = ( 44.064 50.3176081 0. )
+ BODY503_LONG_AXIS = ( 0. )
+
+ BODY503_NUT_PREC_RA = ( 0. 0. 0. -0.037 0.431 0.091 )
+ BODY503_NUT_PREC_DEC = ( 0. 0. 0. -0.016 0.186 0.039 )
+ BODY503_NUT_PREC_PM = ( 0. 0. 0. 0.033 -0.389 -0.082 )
+
+ \begintext
+
+
+ Callisto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY504_POLE_RA = ( 268.72 -0.009 0. )
+ BODY504_POLE_DEC = ( 64.83 0.003 0. )
+ BODY504_PM = ( 259.51 21.5710715 0. )
+ BODY504_LONG_AXIS = ( 0. )
+
+ BODY504_NUT_PREC_RA = ( 0. 0. 0. 0. -0.068 0.590 0. 0.010 )
+ BODY504_NUT_PREC_DEC = ( 0. 0. 0. 0. -0.029 0.254 0. -0.004 )
+ BODY504_NUT_PREC_PM = ( 0. 0. 0. 0. 0.061 -0.533 0. -0.009 )
+
+ \begintext
+
+
+ Amalthea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY505_POLE_RA = ( 268.05 -0.009 0. )
+ BODY505_POLE_DEC = ( 64.49 0.003 0. )
+ BODY505_PM = ( 231.67 722.6314560 0. )
+ BODY505_LONG_AXIS = ( 0. )
+
+ BODY505_NUT_PREC_RA = ( -0.84 0. 0. 0. 0. 0. 0. 0. 0.01 0. )
+ BODY505_NUT_PREC_DEC = ( -0.36 0. 0. 0. 0. 0. 0. 0. 0. 0. )
+ BODY505_NUT_PREC_PM = ( 0.76 0. 0. 0. 0. 0. 0. 0. -0.01 0. )
+
+ \begintext
+
+
+ Thebe
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY514_POLE_RA = ( 268.05 -0.009 0. )
+ BODY514_POLE_DEC = ( 64.49 0.003 0. )
+ BODY514_PM = ( 8.56 533.7004100 0. )
+ BODY514_LONG_AXIS = ( 0. )
+
+ BODY514_NUT_PREC_RA = ( 0. -2.11 0. 0. 0. 0. 0. 0. 0. 0.04 )
+ BODY514_NUT_PREC_DEC = ( 0. -0.91 0. 0. 0. 0. 0. 0. 0. 0.01 )
+ BODY514_NUT_PREC_PM = ( 0. 1.91 0. 0. 0. 0. 0. 0. 0. -0.04 )
+
+ \begintext
+
+
+ Adrastea
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+
+ BODY515_POLE_RA = ( 268.05 -0.009 0. )
+ BODY515_POLE_DEC = ( 64.49 0.003 0. )
+ BODY515_PM = ( 33.29 1206.9986602 0. )
+ BODY515_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Metis
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY516_POLE_RA = ( 268.05 -0.009 0. )
+ BODY516_POLE_DEC = ( 64.49 0.003 0. )
+ BODY516_PM = ( 346.09 1221.2547301 0. )
+ BODY516_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Mimas
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY601_POLE_RA = ( 40.66 -0.036 0. )
+ BODY601_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY601_PM = ( 337.46 381.9945550 0. )
+ BODY601_LONG_AXIS = ( 0. )
+
+ BODY601_NUT_PREC_RA = ( 0. 0. 13.56 0. 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_DEC = ( 0. 0. -1.53 0. 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_PM = ( 0. 0. -13.48 0. -44.85 0. 0. 0. 0. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY602_POLE_RA = ( 40.66 -0.036 0. )
+ BODY602_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY602_PM = ( 2.82 262.7318996 0. )
+ BODY602_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY603_POLE_RA = ( 40.66 -0.036 0. )
+ BODY603_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY603_PM = ( 10.45 190.6979085 0. )
+ BODY603_LONG_AXIS = ( 0. )
+
+ BODY603_NUT_PREC_RA = ( 0. 0. 0. 9.66 0. 0. 0. 0. 0. )
+ BODY603_NUT_PREC_DEC = ( 0. 0. 0. -1.09 0. 0. 0. 0. 0. )
+ BODY603_NUT_PREC_PM = ( 0. 0. 0. -9.60 2.23 0. 0. 0. 0. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY604_POLE_RA = ( 40.66 -0.036 0. )
+ BODY604_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY604_PM = ( 357.00 131.5349316 0. )
+ BODY604_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY605_POLE_RA = ( 40.38 -0.036 0. )
+ BODY605_POLE_DEC = ( 83.55 -0.004 0. )
+ BODY605_PM = ( 235.16 79.6900478 0. )
+ BODY605_LONG_AXIS = ( 0. )
+
+ BODY605_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 3.10 0. 0. 0. )
+ BODY605_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. -0.35 0. 0. 0. )
+ BODY605_NUT_PREC_PM = ( 0. 0. 0. 0. 0. -3.08 0. 0. 0. )
+
+ \begintext
+
+
+
+ Titan
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY606_POLE_RA = ( 36.41 -0.036 0. )
+ BODY606_POLE_DEC = ( 83.94 -0.004 0. )
+ BODY606_PM = ( 189.64 22.5769768 0. )
+ BODY606_LONG_AXIS = ( 0. )
+
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 2.66 0. 0 )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. -0.30 0. 0 )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. -2.64 0. 0 )
+
+ \begintext
+
+
+
+ Hyperion
+
+ The IAU report does not give an orientation model for Hyperion.
+ Hyperion's rotation is in chaotic and is not predictable for
+ long periods.
+
+
+ Iapetus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY608_POLE_RA = ( 318.16 -3.949 0. )
+ BODY608_POLE_DEC = ( 75.03 -1.143 0. )
+ BODY608_PM = ( 350.20 4.5379572 0. )
+ BODY608_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY609_POLE_RA = ( 356.90 0. 0. )
+ BODY609_POLE_DEC = ( 77.80 0. 0. )
+ BODY609_PM = ( 178.58 931.639 0. )
+ BODY609_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+ Janus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY610_POLE_RA = ( 40.58 -0.036 0. )
+ BODY610_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY610_PM = ( 58.83 518.2359876 0. )
+ BODY610_LONG_AXIS = ( 0. )
+
+ BODY610_NUT_PREC_RA = ( 0. -1.623 0. 0. 0. 0. 0. 0. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY611_POLE_RA = ( 40.58 -0.036 0. )
+ BODY611_POLE_DEC = ( 83.52 -0.004 0. )
+ BODY611_PM = ( 293.87 518.4907239 0. )
+ BODY611_LONG_AXIS = ( 0. )
+
+ BODY611_NUT_PREC_RA = ( -3.153 0. 0. 0. 0. 0. 0. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY612_POLE_RA = ( 40.85 -0.036 0. )
+ BODY612_POLE_DEC = ( 83.34 -0.004 0. )
+ BODY612_PM = ( 245.12 131.6174056 0. )
+ BODY612_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Telesto
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY613_POLE_RA = ( 50.51 -0.036 0. )
+ BODY613_POLE_DEC = ( 84.06 -0.004 0. )
+ BODY613_PM = ( 56.88 190.6979332 0. )
+ BODY613_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Calypso
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY614_POLE_RA = ( 36.41 -0.036 0. )
+ BODY614_POLE_DEC = ( 85.04 -0.004 0. )
+ BODY614_PM = ( 153.51 190.6742373 0. )
+ BODY614_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Atlas
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY615_POLE_RA = ( 40.58 -0.036 0. )
+ BODY615_POLE_DEC = ( 83.53 -0.004 0. )
+ BODY615_PM = ( 137.88 598.3060000 0. )
+ BODY615_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Prometheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY616_POLE_RA = ( 40.58 -0.036 )
+ BODY616_POLE_DEC = ( 83.53 -0.004 )
+ BODY616_PM = ( 296.14 587.289000 )
+ BODY616_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Pandora
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY617_POLE_RA = ( 40.58 -0.036 0. )
+ BODY617_POLE_DEC = ( 83.53 -0.004 0. )
+ BODY617_PM = ( 162.92 572.7891000 0. )
+ BODY617_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+ Pan
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY618_POLE_RA = ( 40.6 -0.036 0. )
+ BODY618_POLE_DEC = ( 83.5 -0.004 0. )
+ BODY618_PM = ( 48.8 626.0440000 0. )
+ BODY618_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+
+Satellites of Uranus
+
+
+
+ Ariel
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY701_POLE_RA = ( 257.43 0. 0. )
+ BODY701_POLE_DEC = ( -15.10 0. 0. )
+ BODY701_PM = ( 156.22 -142.8356681 0. )
+ BODY701_LONG_AXIS = ( 0. )
+
+ BODY701_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0.29 )
+
+ BODY701_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0.28 )
+
+ BODY701_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0.05 0.08 )
+ \begintext
+
+
+
+ Umbriel
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY702_POLE_RA = ( 257.43 0. 0. )
+ BODY702_POLE_DEC = ( -15.10 0. 0. )
+ BODY702_PM = ( 108.05 -86.8688923 0. )
+ BODY702_LONG_AXIS = ( 0. )
+
+ BODY702_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0.21 )
+
+ BODY702_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0.20 )
+
+ BODY702_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. -0.09 0. 0.06 )
+
+ \begintext
+
+
+
+ Titania
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY703_POLE_RA = ( 257.43 0. 0. )
+ BODY703_POLE_DEC = ( -15.10 0. 0. )
+ BODY703_PM = ( 77.74 -41.3514316 0. )
+ BODY703_LONG_AXIS = ( 0. )
+
+ BODY703_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.29 )
+
+ BODY703_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.28 )
+
+ BODY703_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.08 )
+ \begintext
+
+
+
+ Oberon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY704_POLE_RA = ( 257.43 0. 0. )
+ BODY704_POLE_DEC = ( -15.10 0. 0. )
+ BODY704_PM = ( 6.77 -26.7394932 0. )
+ BODY704_LONG_AXIS = ( 0. )
+
+
+ BODY704_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.16 )
+
+ BODY704_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.16 )
+
+ BODY704_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0. 0.04 )
+ \begintext
+
+
+
+ Miranda
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+ BODY705_POLE_RA = ( 257.43 0. 0. )
+ BODY705_POLE_DEC = ( -15.08 0. 0. )
+ BODY705_PM = ( 30.70 -254.6906892 0. )
+ BODY705_LONG_AXIS = ( 0. )
+
+ BODY705_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 4.41 0. 0. 0. 0.
+ 0. -0.04 0. )
+
+ BODY705_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 4.25 0. 0. 0. 0.
+ 0. -0.02 0. )
+
+ BODY705_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 1.15 -1.27 0. 0. 0.
+ 0. -0.09 0.15 )
+ \begintext
+
+
+
+ Cordelia
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY706_POLE_RA = ( 257.31 0. 0. )
+ BODY706_POLE_DEC = ( -15.18 0. 0. )
+ BODY706_PM = ( 127.69 -1074.5205730 0. )
+ BODY706_LONG_AXIS = ( 0. )
+
+ BODY706_NUT_PREC_RA = ( -0.15 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY706_NUT_PREC_DEC = ( 0.14 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY706_NUT_PREC_PM = ( -0.04 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Ophelia
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY707_POLE_RA = ( 257.31 0. 0. )
+ BODY707_POLE_DEC = ( -15.18 0. 0. )
+ BODY707_PM = ( 130.35 -956.4068150 0. )
+ BODY707_LONG_AXIS = ( 0. )
+
+ BODY707_NUT_PREC_RA = ( 0. -0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY707_NUT_PREC_DEC = ( 0. 0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY707_NUT_PREC_PM = ( 0. -0.03 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Bianca
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY708_POLE_RA = ( 257.31 0. 0. )
+ BODY708_POLE_DEC = ( -15.18 0. 0. )
+ BODY708_PM = ( 105.46 -828.3914760 0. )
+ BODY708_LONG_AXIS = ( 0. )
+
+ BODY708_NUT_PREC_RA = ( 0. 0. -0.16 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY708_NUT_PREC_DEC = ( 0. 0. 0.16 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY708_NUT_PREC_PM = ( 0. 0. -0.04 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Cressida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+
+ BODY709_POLE_RA = ( 257.31 0. 0. )
+ BODY709_POLE_DEC = ( -15.18 0. 0. )
+ BODY709_PM = ( 59.16 -776.5816320 0. )
+ BODY709_LONG_AXIS = ( 0. )
+
+
+ BODY709_NUT_PREC_RA = ( 0. 0. 0. -0.04 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ BODY709_NUT_PREC_DEC = ( 0. 0. 0. 0.04 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ BODY709_NUT_PREC_PM = ( 0. 0. 0. -0.01 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+
+ \begintext
+
+
+
+ Desdemona
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY710_POLE_RA = ( 257.31 0. 0. )
+ BODY710_POLE_DEC = ( -15.18 0. 0. )
+ BODY710_PM = ( 95.08 -760.0531690 0. )
+ BODY710_LONG_AXIS = ( 0. )
+
+ BODY710_NUT_PREC_RA = ( 0. 0. 0. 0. -0.17
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY710_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.16
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY710_NUT_PREC_PM = ( 0. 0. 0. 0. -0.04
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Juliet
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY711_POLE_RA = ( 257.31 0. 0. )
+ BODY711_POLE_DEC = ( -15.18 0. 0. )
+ BODY711_PM = ( 302.56 -730.1253660 0. )
+ BODY711_LONG_AXIS = ( 0. )
+
+ BODY711_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ -0.06 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY711_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0.06 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY711_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ -0.02 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Portia
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY712_POLE_RA = ( 257.31 0. 0. )
+ BODY712_POLE_DEC = ( -15.18 0. 0. )
+ BODY712_PM = ( 25.03 -701.4865870 0. )
+ BODY712_LONG_AXIS = ( 0. )
+
+ BODY712_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. -0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY712_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0.09 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY712_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. -0.02 0. 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Rosalind
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY713_POLE_RA = ( 257.31 0. 0. )
+ BODY713_POLE_DEC = ( -15.18 0. 0. )
+ BODY713_PM = ( 314.90 -644.6311260 0. )
+ BODY713_LONG_AXIS = ( 0. )
+
+ BODY713_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. -0.29 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY713_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0.28 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY713_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. -0.08 0. 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+ Belinda
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY714_POLE_RA = ( 257.31 0. 0. )
+ BODY714_POLE_DEC = ( -15.18 0. 0. )
+ BODY714_PM = ( 297.46 -577.3628170 0. )
+ BODY714_LONG_AXIS = ( 0. )
+
+ BODY714_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. -0.03 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY714_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0.03 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY714_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. -0.01 0.
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+ \begintext
+
+
+
+ Puck
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY715_POLE_RA = ( 257.31 0. 0. )
+ BODY715_POLE_DEC = ( -15.18 0. 0. )
+ BODY715_PM = ( 91.24 -472.5450690 0. )
+ BODY715_LONG_AXIS = ( 0. )
+
+ BODY715_NUT_PREC_RA = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. -0.33
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY715_NUT_PREC_DEC = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. 0.31
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ BODY715_NUT_PREC_PM = ( 0. 0. 0. 0. 0.
+ 0. 0. 0. 0. -0.09
+ 0. 0. 0. 0. 0.
+ 0. 0. 0. )
+
+ \begintext
+
+
+
+
+Satellites of Neptune
+
+
+ Triton
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY801_POLE_RA = ( 299.36 0. 0. )
+ BODY801_POLE_DEC = ( 41.17 0. 0. )
+ BODY801_PM = ( 296.53 -61.2572637 0. )
+ BODY801_LONG_AXIS = ( 0. )
+
+
+ BODY801_NUT_PREC_RA = ( 0. 0. 0. 0.
+ 0. 0. 0. -32.35
+ 0. -6.28 -2.08 -0.74
+ -0.28 -0.11 -0.07 -0.02
+ -0.01 )
+
+
+ BODY801_NUT_PREC_DEC = ( 0. 0. 0. 0.
+ 0. 0. 0. 22.55
+ 0. 2.10 0.55 0.16
+ 0.05 0.02 0.01 0.
+ 0. )
+
+
+ BODY801_NUT_PREC_PM = ( 0. 0. 0. 0.
+ 0. 0. 0. 22.25
+ 0. 6.73 2.05 0.74
+ 0.28 0.11 0.05 0.02
+ 0.01 )
+
+ \begintext
+
+
+
+
+ Nereid
+
+ Old values:
+
+ Values are from the 1988 IAU report [10]. Note that this
+ rotation model pre-dated the 1989 Voyager 2 Neptune
+ encounter.
+
+
+ body802_pole_ra = ( 273.48 0. 0. )
+ body802_pole_dec = ( 67.22 0. 0. )
+ body802_pm = ( 237.22 0.9996465 0. )
+ body802_long_axis = ( 0. )
+
+
+ The report seems to have a typo: in the nut_prec_ra expression,
+ where the report gives -0.51 sin 3N3, we use -0.51 3N2.
+
+ body802_nut_prec_ra = ( 0. -17.81
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ 2.56 -0.51 0.11 -0.03 )
+
+ body802_nut_prec_dec = ( 0. -6.67
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ 0.47 -0.07 0.01 )
+
+ body802_nut_prec_pm = ( 0. 16.48
+ 0. 0. 0. 0.
+ 0. 0. 0.
+ -2.57 0.51 -0.11 0.02 )
+
+
+
+ Current values:
+
+ The 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY803_POLE_RA = ( 299.36 0. 0. )
+ BODY803_POLE_DEC = ( 43.36 0. 0. )
+ BODY803_PM = ( 254.06 +1222.8441209 0. )
+ BODY803_LONG_AXIS = ( 0. )
+
+
+ BODY803_NUT_PREC_RA = ( 0.70 -6.49 0. 0.
+ 0. 0. 0. 0.
+ 0.25 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY803_NUT_PREC_DEC = ( -0.51 -4.75 0. 0.
+ 0. 0. 0. 0.
+ 0.09 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY803_NUT_PREC_PM = ( -0.48 4.40 0. 0.
+ 0. 0. 0. 0.
+ -0.27 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+
+ Thalassa
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY804_POLE_RA = ( 299.36 0. 0. )
+ BODY804_POLE_DEC = ( 43.45 0. 0. )
+ BODY804_PM = ( 102.06 1155.7555612 0. )
+ BODY804_LONG_AXIS = ( 0. )
+
+
+ BODY804_NUT_PREC_RA = ( 0.70 0. -0.28 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+
+ BODY804_NUT_PREC_DEC = ( -0.51 0. -0.21 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY804_NUT_PREC_PM = ( -0.48 0. 0.19 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+ Despina
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY805_POLE_RA = ( 299.36 0. 0. )
+ BODY805_POLE_DEC = ( 43.45 0. 0. )
+ BODY805_PM = ( 306.51 +1075.7341562 0. )
+ BODY805_LONG_AXIS = ( 0. )
+
+
+ BODY805_NUT_PREC_RA = ( 0.70 0. 0. -0.09
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY805_NUT_PREC_DEC = ( -0.51 0. 0. -0.07
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY805_NUT_PREC_PM = ( -0.49 0. 0. 0.06
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+
+ Galatea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY806_POLE_RA = ( 299.36 0. 0. )
+ BODY806_POLE_DEC = ( 43.43 0. 0. )
+ BODY806_PM = ( 258.09 839.6597686 0. )
+ BODY806_LONG_AXIS = ( 0. )
+
+
+ BODY806_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ -0.07 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY806_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ -0.05 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY806_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0.05 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+ Larissa
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY807_POLE_RA = ( 299.36 0. 0. )
+ BODY807_POLE_DEC = ( 43.41 0. 0. )
+ BODY807_PM = ( 179.41 +649.0534470 0. )
+ BODY807_LONG_AXIS = ( 0. )
+
+
+ BODY807_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ 0. -0.27 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY807_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ 0. -0.20 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY807_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0. 0.19 0. 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+ \begintext
+
+
+
+ Proteus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY808_POLE_RA = ( 299.27 0. 0. )
+ BODY808_POLE_DEC = ( 42.91 0. 0. )
+ BODY808_PM = ( 93.38 +320.7654228 0. )
+ BODY808_LONG_AXIS = ( 0. )
+
+
+ BODY808_NUT_PREC_RA = ( 0.70 0. 0. 0.
+ 0. 0. -0.05 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY808_NUT_PREC_DEC = ( -0.51 0. 0. 0.
+ 0. 0. -0.04 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ BODY808_NUT_PREC_PM = ( -0.48 0. 0. 0.
+ 0. 0. 0.04 0.
+ 0. 0. 0. 0.
+ 0. 0. 0. 0.
+ 0. )
+
+ \begintext
+
+
+
+
+
+Satellites of Pluto
+
+ Charon
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ BODY901_POLE_RA = ( 312.993 0. 0. )
+ BODY901_POLE_DEC = ( 6.163 0. 0. )
+ BODY901_PM = ( 57.305 -56.3625225 0. )
+ BODY901_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000005_POLE_RA = ( 218.5 0. 0. )
+ BODY1000005_POLE_DEC = ( -12.5 0. 0. )
+ BODY1000005_PM = ( 000. 390.0 0. )
+ BODY1000005_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000093_POLE_RA = ( 294. 0. 0. )
+ BODY1000093_POLE_DEC = ( 73. 0. 0. )
+ BODY1000093_PM = ( 252.63 212.064 0. )
+ BODY1000093_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000433_POLE_RA = ( 11.35 0. 0. )
+ BODY2000433_POLE_DEC = ( 17.22 0. 0. )
+ BODY2000433_PM = ( 326.07 1639.38864745 0. )
+ BODY2000433_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+ \begindata
+
+ BODY2025143_POLE_RA = ( 90.53 0. 0. )
+ BODY2025143_POLE_DEC = ( -66.30 0. 0. )
+ BODY2025143_PM = ( 000.0 712.143 0. )
+ BODY2025143_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2431010_POLE_RA = ( 168.76 0. 0. )
+ BODY2431010_POLE_DEC = ( -2.88 0. 0. )
+ BODY2431010_PM = ( 265.95 +1864.6280070 0. )
+ BODY2431010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY9511010_POLE_RA = ( 9.47 0. 0. )
+ BODY9511010_POLE_DEC = ( 26.70 0. 0. )
+ BODY9511010_PM = ( 83.67 1226.9114850 0. )
+ BODY9511010_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values as the polar radius for
+ the triaxial model.
+
+ \begindata
+
+ BODY499_RADII = ( 3396.19 3396.19 3376.20 )
+
+ \begintext
+
+
+
+Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ BODY505_RADII = ( 125 73 64 )
+
+ \begintext
+
+ Only mean radii are available in the 2003 IAU report for bodies
+ 506-513.
+
+ \begindata
+
+ BODY506_RADII = ( 85 85 85 )
+ BODY507_RADII = ( 40 40 40 )
+ BODY508_RADII = ( 18 18 18 )
+ BODY509_RADII = ( 14 14 14 )
+ BODY510_RADII = ( 12 12 12 )
+ BODY511_RADII = ( 15 15 15 )
+ BODY512_RADII = ( 10 10 10 )
+ BODY513_RADII = ( 5 5 5 )
+ BODY514_RADII = ( 58 49 42 )
+ BODY515_RADII = ( 10 8 7 )
+
+ \begintext
+
+ The value for the second radius for body 516 is not given in
+ 2003 IAU report. The values given are:
+
+ BODY516_RADII = ( 30 --- 20 )
+
+ For use within the SPICE system, we use only the mean radius.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ body610_radii = ( 97.0 95.0 77.0 )
+ body611_radii = ( 69.0 55.0 55.0 )
+
+
+ Only the first equatorial radius for Helene (body 612) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ body613_radii = ( 15 12.5 7.5 )
+ body614_radii = ( 15.0 8.0 8.0 )
+ body615_radii = ( 18.5 17.2 13.5 )
+ body616_radii = ( 74.0 50.0 34.0 )
+ body617_radii = ( 55.0 44.0 31.0 )
+
+
+
+ Current values:
+
+ \begindata
+
+ BODY601_RADII = ( 207.4 196.8 190.6 )
+ BODY602_RADII = ( 256.6 251.4 248.3 )
+ BODY603_RADII = ( 540.4 531.1 527.5 )
+ BODY604_RADII = ( 563.8 561.0 560.3 )
+ BODY605_RADII = ( 767.2 762.5 763.1 )
+ BODY606_RADII = ( 2575 2575 2575 )
+ BODY607_RADII = ( 164 130 107 )
+ BODY608_RADII = ( 747.4 747.4 712.4 )
+ BODY609_RADII = ( 108.6 107.7 101.5 )
+ BODY610_RADII = ( 97.0 95.0 77.0 )
+ BODY611_RADII = ( 69.0 55.0 55.0 )
+
+ \begintext
+
+ Only the first equatorial radius for Helene (body 612) is given in the
+ 2006 IAU report:
+
+ BODY612_RADII = ( 17.5 --- --- )
+
+ The mean radius is 16km; we use this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ \begindata
+
+ BODY612_RADII = ( 17.5 17.5 17.5 )
+ BODY613_RADII = ( 15 12.5 7.5 )
+ BODY614_RADII = ( 15.0 8.0 8.0 )
+ BODY615_RADII = ( 18.5 17.2 13.5 )
+ BODY616_RADII = ( 74.0 50.0 34.0 )
+ BODY617_RADII = ( 55.0 44.0 31.0 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY701_RADII = ( 581.1 577.9 577.7 )
+ BODY702_RADII = ( 584.7 584.7 584.7 )
+ BODY703_RADII = ( 788.9 788.9 788.9 )
+ BODY704_RADII = ( 761.4 761.4 761.4 )
+ BODY705_RADII = ( 240.4 234.2 232.9 )
+
+ \begintext
+
+ The 2000 report gives only mean radii for satellites 706--715.
+
+ \begindata
+
+ BODY706_RADII = ( 13 13 13 )
+ BODY707_RADII = ( 15 15 15 )
+ BODY708_RADII = ( 21 21 21 )
+ BODY709_RADII = ( 31 31 31 )
+ BODY710_RADII = ( 27 27 27 )
+ BODY711_RADII = ( 42 42 42 )
+ BODY712_RADII = ( 54 54 54 )
+ BODY713_RADII = ( 27 27 27 )
+ BODY714_RADII = ( 33 33 33 )
+ BODY715_RADII = ( 77 77 77 )
+
+ \begintext
+
+
+
+
+Satellites of Neptune
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ The 2000 report gives mean radii only for bodies 801-806.
+
+ \begindata
+
+ BODY801_RADII = ( 1352.6 1352.6 1352.6 )
+ BODY802_RADII = ( 170 170 170 )
+ BODY803_RADII = ( 29 29 29 )
+ BODY804_RADII = ( 40 40 40 )
+ BODY805_RADII = ( 74 74 74 )
+ BODY806_RADII = ( 79 79 79 )
+
+ \begintext
+
+
+ The second equatorial radius for Larissa is not given in the 2000
+ report. The available values are:
+
+ BODY807_RADII = ( 104 --- 89 )
+
+ For use within the SPICE system, we use only the mean radius.
+ \begindata
+
+ BODY807_RADII = ( 96 96 96 )
+ BODY808_RADII = ( 218 208 201 )
+
+ \begintext
+
+
+
+
+Satellites of Pluto
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ Current values:
+
+
+ The value in the data assignment below is the
+ "effective radius."
+
+ The first principal axis length is
+
+ 3.5 km
+
+ The lengths of the other semi-axes are not provided
+ by [1].
+
+ \begindata
+
+ BODY1000005_RADII = ( 4.22 4.22 4.22 )
+
+ \begintext
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ Current values:
+
+
+ The value in the data assignment below is the
+ "effective radius."
+
+ According to [1]:
+
+ The maximum and minimum radii are not properly
+ the values of the principal semi-axes, they
+ are half the maximum and minimum values of the
+ diameter. Due to the large deviations from a
+ simple ellipsoid, they may not correspond with
+ measurements along the principal axes, or be
+ orthogonal to each other.
+
+ \begindata
+
+ BODY1000093_RADII = ( 3.0 3.0 3.0 )
+
+ \begintext
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \begintext
+
+
+Kleopatra
+
+
+ Old values:
+
+ Values are from the 2003 report.
+
+
+ body2000216_radii = ( 108.5 47 40.5 )
+
+
+ Current values:
+
+
+ No values are provided in the 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/LUA3107H.161/uvvisAddendum004.ti b/tests/pytests/data/LUA3107H.161/uvvisAddendum004.ti
new file mode 100644
index 0000000000000000000000000000000000000000..8c74fa87c94e5d71ae3c3c468986d24271a75479
--- /dev/null
+++ b/tests/pytests/data/LUA3107H.161/uvvisAddendum004.ti
@@ -0,0 +1,91 @@
+\begintext
+history ????-??-?? - v01 - Original version
+history ????-??-?? - v02 - Removed camera orientation information (added to fk)
+history ????-??-?? - v03 - Added reference frame information for producing CKs in ISIS
+history 2018—09-14 - v04 - Emerson Speyerer - Added filter dependent frames; transferred camera model information out of the IAK and created an traditional IK for the UVVIS camera
+
+
+\begindata
+INS-40021_PLATFORM_ID = -40000
+INS-40022_PLATFORM_ID = -40000
+INS-40023_PLATFORM_ID = -40000
+INS-40024_PLATFORM_ID = -40000
+INS-40025_PLATFORM_ID = -40000
+INS-40026_PLATFORM_ID = -40000
+
+INS-40021_SPK_TIME_BIAS = 0.0
+INS-40021_CK_TIME_BIAS = 0.0
+INS-40021_CK_TIME_TOLERANCE = 1
+
+INS-40022_SPK_TIME_BIAS = 0.0
+INS-40022_CK_TIME_BIAS = 0.0
+INS-40022_CK_TIME_TOLERANCE = 1
+
+INS-40023_SPK_TIME_BIAS = 0.0
+INS-40023_CK_TIME_BIAS = 0.0
+INS-40023_CK_TIME_TOLERANCE = 1
+
+INS-40024_SPK_TIME_BIAS = 0.0
+INS-40024_CK_TIME_BIAS = 0.0
+INS-40024_CK_TIME_TOLERANCE = 1
+
+INS-40025_SPK_TIME_BIAS = 0.0
+INS-40025_CK_TIME_BIAS = 0.0
+INS-40025_CK_TIME_TOLERANCE = 1
+
+INS-40026_SPK_TIME_BIAS = 0.0
+INS-40026_CK_TIME_BIAS = 0.0
+INS-40026_CK_TIME_TOLERANCE = 1
+
+\begintext
+These are the parameters required for writing c-kernels. Isis will
+create ck with the same frame endpoints as the mission ck. For
+the Clementine spacecraft the ck frame is CLEM_SC_BUS (-40000), and the
+ck reference frame is J2000 (1).
+
+\begindata
+
+INS-40021_CK_FRAME_ID=-40002
+INS-40021_CK_REFERENCE_ID=-40000
+
+INS-40022_CK_FRAME_ID=-40002
+INS-40022_CK_REFERENCE_ID=-40000
+
+INS-40023_CK_FRAME_ID=-40002
+INS-40023_CK_REFERENCE_ID=-40000
+
+INS-40024_CK_FRAME_ID=-40002
+INS-40024_CK_REFERENCE_ID=-40000
+
+INS-40025_CK_FRAME_ID=-40002
+INS-40025_CK_REFERENCE_ID=-40000
+
+INS-40026_CK_FRAME_ID=-40002
+INS-40026_CK_REFERENCE_ID=-40000
+
+INS-40021_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-40021_LIGHTTIME_CORRECTION = 'NONE'
+INS-40021_LT_SURFACE_CORRECT = 'TRUE'
+
+INS-40022_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-40022_LIGHTTIME_CORRECTION = 'NONE'
+INS-40022_LT_SURFACE_CORRECT = 'TRUE'
+
+INS-40023_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-40023_LIGHTTIME_CORRECTION = 'NONE'
+INS-40023_LT_SURFACE_CORRECT = 'TRUE'
+
+INS-40024_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-40024_LIGHTTIME_CORRECTION = 'NONE'
+INS-40024_LT_SURFACE_CORRECT = 'TRUE'
+
+INS-40025_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-40025_LIGHTTIME_CORRECTION = 'NONE'
+INS-40025_LT_SURFACE_CORRECT = 'TRUE'
+
+INS-40026_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-40026_LIGHTTIME_CORRECTION = 'NONE'
+INS-40026_LT_SURFACE_CORRECT = 'TRUE'
+
+
+
diff --git a/tests/pytests/data/isds/clem_uvvis_isd.json b/tests/pytests/data/isds/clem_uvvis_isd.json
new file mode 100644
index 0000000000000000000000000000000000000000..68666f5c0820e91e5926ad3c0dfd937ca7588167
--- /dev/null
+++ b/tests/pytests/data/isds/clem_uvvis_isd.json
@@ -0,0 +1,340 @@
+{
+ "isis_camera_version": 1,
+ "image_lines": 288,
+ "image_samples": 384,
+ "name_platform": "CLEMENTINE 1",
+ "name_sensor": "CLEM_UVVIS_A",
+ "reference_height": {
+ "maxheight": 1000,
+ "minheight": -1000,
+ "unit": "m"
+ },
+ "name_model": "USGS_ASTRO_FRAME_SENSOR_MODEL",
+ "center_ephemeris_time": -182119484.4628324,
+ "radii": {
+ "semimajor": 1737.4,
+ "semiminor": 1737.4,
+ "unit": "km"
+ },
+ "body_rotation": {
+ "time_dependent_frames": [
+ 310002,
+ 1
+ ],
+ "ck_table_start_time": -182119484.4628324,
+ "ck_table_end_time": -182119484.4628324,
+ "ck_table_original_size": 1,
+ "ephemeris_times": [
+ -182119484.4628324
+ ],
+ "quaternions": [
+ [
+ -0.96885432787622,
+ 0.20669697894775604,
+ 0.03957524503488252,
+ -0.13050459850065885
+ ]
+ ],
+ "angular_velocities": [
+ [
+ 5.995309552408776e-08,
+ -1.0943667483827817e-06,
+ 2.425386964592493e-06
+ ]
+ ],
+ "constant_frames": [
+ 310001,
+ 310003,
+ 310000,
+ 310002
+ ],
+ "constant_rotation": [
+ 0.9999998785270937,
+ -0.00030978912711655305,
+ 0.00038337513559243597,
+ 0.00030978942161770135,
+ 0.9999999520150048,
+ -7.087975496937869e-07,
+ -0.0003833748976184077,
+ 8.275630251118771e-07,
+ 0.9999999265114988
+ ],
+ "reference_frame": 1
+ },
+ "instrument_pointing": {
+ "time_dependent_frames": [
+ -40000,
+ 1
+ ],
+ "ck_table_start_time": -182119484.4628324,
+ "ck_table_end_time": -182119484.4628324,
+ "ck_table_original_size": 1,
+ "ephemeris_times": [
+ -182119484.4628324
+ ],
+ "quaternions": [
+ [
+ -0.7558493895743924,
+ 0.1793162979127797,
+ -0.6195142642465334,
+ -0.1128691365163656
+ ]
+ ],
+ "angular_velocities": [
+ [
+ 0.00018037439261772692,
+ -0.0007110656713082156,
+ -0.00018642325246887433
+ ]
+ ],
+ "reference_frame": 1,
+ "constant_frames": [
+ -40021,
+ -40002,
+ -40000
+ ],
+ "constant_rotation": [
+ -0.006108611041259038,
+ -0.9999660726077593,
+ -0.005526165448164337,
+ 0.9999807939399818,
+ -0.00610272721183136,
+ -0.0010809587141711275,
+ 0.0010471973598032407,
+ -0.005532662468635599,
+ 0.9999841463861805
+ ]
+ },
+ "naif_keywords": {
+ "BODY301_RADII": [
+ 1737.4,
+ 1737.4,
+ 1737.4
+ ],
+ "BODY_FRAME_CODE": 310001,
+ "BODY_CODE": 301,
+ "INS-40021_FOV_CROSS_ANGLE": 2.1085,
+ "INS-40021_ITRANSL": [
+ 0.0,
+ 0.0,
+ 43.47826087
+ ],
+ "INS-40021_ITRANSS": [
+ 0.0,
+ 43.47826087,
+ 0.0
+ ],
+ "INS-40021_PP": [
+ 0.0,
+ 0.0
+ ],
+ "INS-40021_FOV_REF_ANGLE": 2.8115,
+ "INS-40021_CK_FRAME_ID": -40002.0,
+ "TKFRAME_-40021_RELATIVE": "CLEM_UVVIS",
+ "INS-40021_FOCAL_LENGTH": 89.874444,
+ "INS-40021_OD_K": [
+ 0.0,
+ -2.422842e-05,
+ 0.0
+ ],
+ "TKFRAME_-40021_ANGLES": [
+ -0.00553269372882,
+ -0.0010471975512,
+ 1.5769049791768799
+ ],
+ "INS-40021_FILTER_NAME": "A",
+ "INS-40021_FOV_CLASS_SPEC": "ANGLES",
+ "FRAME_-40021_CENTER": -40.0,
+ "INS-40021_BORESIGHT_SAMPLE": 192.5,
+ "INS-40021_BORESIGHT": [
+ 0.0,
+ 0.0,
+ 1.0
+ ],
+ "INS-40021_FOV_REF_VECTOR": [
+ 1.0,
+ 0.0,
+ 0.0
+ ],
+ "INS-40021_DECENTER": [
+ 2.255006e-05,
+ 2.1089410000000002e-05
+ ],
+ "INS-40021_FILTER_BANDCENTER": 415.0,
+ "INS-40021_SWAP_OBSERVER_TARGET": "TRUE",
+ "INS-40021_F/RATIO": -999.9999,
+ "INS-40021_BORESIGHT_LINE": 144.5,
+ "INS-40021_FOV_SHAPE": "RECTANGLE",
+ "INS-40021_FILTER_BANDWIDTH": 40.0,
+ "INS-40021_LIGHTTIME_CORRECTION": "NONE",
+ "INS-40021_PIXEL_LINES": 288.0,
+ "INS-40021_IFOV": -999.999,
+ "INS-40021_CK_TIME_TOLERANCE": 1.0,
+ "INS-40021_TRANSX": [
+ 0.0,
+ 0.023,
+ 0.0
+ ],
+ "INS-40021_TRANSY": [
+ 0.0,
+ 0.0,
+ 0.023
+ ],
+ "FRAME_-40021_CLASS": 4.0,
+ "INS-40021_PIXEL_SIZE": [
+ 0.023,
+ 0.023
+ ],
+ "INS-40021_PLATFORM_ID": -40000.0,
+ "INS-40021_PIXEL_SAMPLES": 384.0,
+ "INS-40021_CK_REFERENCE_ID": -40000.0,
+ "INS-40021_FOV_FRAME": "CLEM_UVVIS_A",
+ "INS-40021_FOV_ANGLE_UNITS": "DEGREES",
+ "INS-40021_LT_SURFACE_CORRECT": "TRUE",
+ "INS-40021_SPK_TIME_BIAS": 0.0,
+ "INS-40021_CCD_CENTER": [
+ 512.5,
+ 512.5
+ ],
+ "FRAME_-40021_NAME": "CLEM_UVVIS_A",
+ "TKFRAME_-40021_UNITS": "RADIANS",
+ "TKFRAME_-40021_AXES": [
+ 1.0,
+ 2.0,
+ 3.0
+ ],
+ "INS-40021_CK_TIME_BIAS": 0.0,
+ "TKFRAME_-40021_SPEC": "ANGLES",
+ "INS-40021_PIXEL_PITCH": 0.023,
+ "FRAME_-40021_CLASS_ID": -40021.0,
+ "BODY301_POLE_RA": [
+ 269.9949,
+ 0.0031,
+ 0.0
+ ],
+ "BODY301_NUT_PREC_PM": [
+ 3.561,
+ 0.1208,
+ -0.0642,
+ 0.0158,
+ 0.0252,
+ -0.0066,
+ -0.0047,
+ -0.0046,
+ 0.0028,
+ 0.0052
+ ],
+ "BODY301_NUT_PREC_RA": [
+ -3.8787000000000003,
+ -0.1204,
+ 0.07,
+ -0.0172,
+ 0.0,
+ 0.0072,
+ 0.0,
+ 0.0,
+ 0.0,
+ -0.0052
+ ],
+ "BODY301_LONG_AXIS": 0.0,
+ "BODY301_NUT_PREC_DEC": [
+ 1.5419,
+ 0.0239,
+ -0.0278,
+ 0.0068,
+ 0.0,
+ -0.0029,
+ 0.0009,
+ 0.0,
+ 0.0,
+ 0.0008
+ ],
+ "BODY301_POLE_DEC": [
+ 66.5392,
+ 0.013,
+ 0.0
+ ],
+ "BODY301_PM": [
+ 38.3213,
+ 13.17635815,
+ -1.3999999999999999e-12
+ ],
+ "OBJECT_301_FRAME": "LUNAR_MEAN_EARTH"
+ },
+ "detector_sample_summing": 1,
+ "detector_line_summing": 1,
+ "focal_length_model": {
+ "focal_length": 89.874444
+ },
+ "detector_center": {
+ "line": 144.5,
+ "sample": 192.5
+ },
+ "focal2pixel_lines": [
+ 0.0,
+ 0.0,
+ 43.47826087
+ ],
+ "focal2pixel_samples": [
+ 0.0,
+ 43.47826087,
+ 0.0
+ ],
+ "optical_distortion": {
+ "radial": {
+ "coefficients": [
+ 0.0,
+ 0.0,
+ 0.0
+ ]
+ }
+ },
+ "starting_detector_line": 0,
+ "starting_detector_sample": 0,
+ "instrument_position": {
+ "spk_table_start_time": -182119484.4628324,
+ "spk_table_end_time": -182119484.4628324,
+ "spk_table_original_size": 1,
+ "ephemeris_times": [
+ -182119484.4628324
+ ],
+ "positions": [
+ [
+ 2161.526643750674,
+ 288.7562569425208,
+ -368.62333558477275
+ ]
+ ],
+ "velocities": [
+ [
+ 0.49612747663310774,
+ -0.6539736578870095,
+ 1.52452216984493
+ ]
+ ],
+ "reference_frame": 1
+ },
+ "sun_position": {
+ "spk_table_start_time": -182119484.4628324,
+ "spk_table_end_time": -182119484.4628324,
+ "spk_table_original_size": 1,
+ "ephemeris_times": [
+ -182119484.4628324
+ ],
+ "positions": [
+ [
+ 149015833.32233897,
+ 11369707.322623711,
+ 4963566.246318031
+ ]
+ ],
+ "velocities": [
+ [
+ -1.6858633435768788,
+ 28.27644180767442,
+ 12.229762748807639
+ ]
+ ],
+ "reference_frame": 1
+ }
+}
\ No newline at end of file
diff --git a/tests/pytests/test_clementine_drivers.py b/tests/pytests/test_clementine_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..70f408dc79f3ed50fcbe160dcfd616cba7f26e15
--- /dev/null
+++ b/tests/pytests/test_clementine_drivers.py
@@ -0,0 +1,52 @@
+import os
+import json
+import unittest
+from unittest.mock import PropertyMock, patch
+
+import pytest
+
+import ale
+from ale.drivers.clementine_drivers import ClementineUvvisIsisLabelNaifSpiceDriver
+
+from conftest import get_image, get_image_kernels, get_isd, convert_kernels, get_image_label, compare_dicts
+
+@pytest.fixture(scope='module')
+def test_uvvis_kernels():
+ kernels = get_image_kernels('LUA3107H.161')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+def test_uvvis_load(test_uvvis_kernels):
+ label_file = get_image_label('LUA3107H.161', 'isis3')
+ isd_str = ale.loads(label_file, props={'kernels': test_uvvis_kernels, 'exact_ck_times': False})
+ isd_obj = json.loads(isd_str)
+ compare_isd = get_isd('clem_uvvis')
+ assert compare_dicts(isd_obj, compare_isd) == []
+
+# ========= Test uvvis isislabel and naifspice driver =========
+class test_uvvis_isis_naif(unittest.TestCase):
+
+ def setUp(self):
+ label = get_image_label("LUA3107H.161", "isis3")
+ self.driver = ClementineUvvisIsisLabelNaifSpiceDriver(label)
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "ULTRAVIOLET/VISIBLE CAMERA"
+
+ def test_ephemeris_start_time(self):
+ with patch('ale.drivers.clementine_drivers.spice.utc2et', return_value=12345) as scs2e:
+ assert self.driver.ephemeris_start_time == 12345
+
+ def test_ephemeris_stop_time(self):
+ with patch('ale.drivers.clementine_drivers.spice.utc2et', return_value=12345) as scs2e:
+ assert self.driver.ephemeris_stop_time >= 12345
+
+ def test_spacecraft_name(self):
+ assert self.driver.sensor_name == "CLEM_UVVIS_A" # this is probly not correct
+
+ def test_sensor_model_version(self):
+ assert self.driver.sensor_model_version == 1
+
+