From 62c7ca78e261b327492088208e9893c091c66f14 Mon Sep 17 00:00:00 2001
From: Jesse Mapel <jmapel@usgs.gov>
Date: Tue, 3 Sep 2019 09:54:56 -0700
Subject: [PATCH] Updated Kaguya test to use actual kernels (#254)
* Kaguya kernels
* Added Kaguya test
* Added debug
* Updated convert kernels to use regex
* Minor updates
* A comment
* Removed debug prints
* Updated to new parameterized fixture
* Updated with new loads logic
* Started porting test to using loads
* More test updates
* More tests
* Removed redundant tests
---
.gitignore | 3 +
ale/base/data_naif.py | 2 +-
ale/drivers/selene_drivers.py | 49 +-
tests/pytests/conftest.py | 37 +-
.../TC1S2B0_01_06691S820E0465/SEL_M_V01.TSC | 2151 ++++++++
.../TC1S2B0_01_06691S820E0465/SEL_TC_V01.TI | 906 ++++
.../TC1S2B0_01_06691S820E0465_pds3.lbl | 155 +
.../kaguyaTcAddendum006.ti | 58 +
.../TC1S2B0_01_06691S820E0465/naif0012.tls | 152 +
.../TC1S2B0_01_06691S820E0465/pck00009.tpc | 3639 ++++++++++++++
.../sel_TC1S2B0_01_06691S820E0465.xsp | 410 ++
.../sel_m_TC1S2B0_01_06691S820E0465.xc | 4322 +++++++++++++++++
tests/pytests/test_kaguya_drivers.py | 224 +-
tests/pytests/test_load.py | 21 +-
tests/pytests/test_mdis_drivers.py | 6 +-
15 files changed, 11982 insertions(+), 153 deletions(-)
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_M_V01.TSC
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_TC_V01.TI
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/TC1S2B0_01_06691S820E0465_pds3.lbl
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/kaguyaTcAddendum006.ti
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/naif0012.tls
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/pck00009.tpc
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_TC1S2B0_01_06691S820E0465.xsp
create mode 100644 tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_m_TC1S2B0_01_06691S820E0465.xc
diff --git a/.gitignore b/.gitignore
index 36e641b..56596c2 100644
--- a/.gitignore
+++ b/.gitignore
@@ -212,3 +212,6 @@ dmypy.json
# Binary Kernels
*.bsp
*.bc
+
+# Binary Images
+*.cub
diff --git a/ale/base/data_naif.py b/ale/base/data_naif.py
index ecb7a12..f2a9377 100644
--- a/ale/base/data_naif.py
+++ b/ale/base/data_naif.py
@@ -289,7 +289,7 @@ class NaifSpice():
sun_state, _ = spice.spkezr("SUN",
self.center_ephemeris_time,
self.reference_frame,
- self.light_time_correction,
+ 'NONE',
self.target_name)
positions = 1000 * np.asarray([sun_state[:3]])
velocities = 1000 * np.asarray([sun_state[3:6]])
diff --git a/ale/drivers/selene_drivers.py b/ale/drivers/selene_drivers.py
index 3fdbd74..aa5f699 100644
--- a/ale/drivers/selene_drivers.py
+++ b/ale/drivers/selene_drivers.py
@@ -91,7 +91,7 @@ class KaguyaTcPds3NaifSpiceDriver(LineScanner, Pds3Label, NaifSpice, Driver):
: int
Sensor frame id
"""
- return spice.bods2c("LISM_{}_HEAD".format(super().instrument_id))
+ return spice.namfrm("LISM_{}_HEAD".format(super().instrument_id))
@property
@@ -158,19 +158,6 @@ class KaguyaTcPds3NaifSpiceDriver(LineScanner, Pds3Label, NaifSpice, Driver):
"""
return self.label.get('CORRECTED_SC_CLOCK_STOP_COUNT').value
- @property
- def ephemeris_stop_time(self):
- """
- Returns the ephemeris stop time of the image. Expects spacecraft_id to
- be defined. This should be the integer naif ID code of the spacecraft.
-
- Returns
- -------
- : float
- ephemeris stop time of the image
- """
- return spice.sct2e(self.spacecraft_id, self.spacecraft_clock_stop_count)
-
@property
def spacecraft_clock_start_count(self):
"""
@@ -211,7 +198,7 @@ class KaguyaTcPds3NaifSpiceDriver(LineScanner, Pds3Label, NaifSpice, Driver):
: int
The detector line of the principle point
"""
- return spice.gdpool('INS{}_CENTER'.format(self.ikid), 0, 2)[0] - 0.5
+ return spice.gdpool('INS{}_CENTER'.format(self.ikid), 0, 2)[1] - 0.5
@property
def detector_center_sample(self):
@@ -229,38 +216,6 @@ class KaguyaTcPds3NaifSpiceDriver(LineScanner, Pds3Label, NaifSpice, Driver):
"""
return spice.gdpool('INS{}_CENTER'.format(self.ikid), 0, 2)[0] - 0.5
- @property
- def _sensor_orientation(self):
- """
- Returns quaternions describing the orientation of the sensor.
- Expects ephemeris_time to be defined. This should be a list containing
- ephemeris times during which the image was taken.
- Expects instrument_id to be defined in the Pds3Label mixin. This should be
- a string of the form TC1 or TC2self.
- Expects reference_frame to be defined. This should be a string containing
- the name of the reference_frame.
-
- Returns
- -------
- : list
- Quaternions describing the orentiation of the sensor
- """
- if not hasattr(self, '_orientation'):
- ephem = self.ephemeris_time
-
- qua = np.empty((len(ephem), 4))
- for i, time in enumerate(ephem):
- instrument = super().instrument_id
- # Find the rotation matrix
- camera2bodyfixed = spice.pxform("LISM_{}_HEAD".format(instrument),
- self.reference_frame,
- time)
- q = spice.m2q(camera2bodyfixed)
- qua[i,:3] = q[1:]
- qua[i,3] = q[0]
- self._orientation = qua
- return self._orientation.tolist()
-
@property
def reference_frame(self):
diff --git a/tests/pytests/conftest.py b/tests/pytests/conftest.py
index 85185ef..120469a 100644
--- a/tests/pytests/conftest.py
+++ b/tests/pytests/conftest.py
@@ -1,5 +1,7 @@
import subprocess
import os
+import re
+import warnings
import numpy as np
import ale
@@ -40,6 +42,24 @@ class SimpleSpice():
def get_mockkernels(self, *args):
return "some_metakernel"
+def compare_dicts(ldict, rdict):
+ differences = []
+ for key in rdict:
+ if key not in ldict:
+ differences.append(f'Key {key} is present in the right dict, but not the left dict.')
+ for key, item in ldict.items():
+ if key not in rdict:
+ differences.append(f'Key {key} is present in the left dict, but not the right dict.')
+ elif isinstance(item, dict):
+ differences.extend(compare_dicts(item, rdict[key]))
+ elif isinstance(item, np.ndarray):
+ if not np.allclose(item, rdict[key]):
+ differences.append(f'Array values of key {key} are not almost equal {item} : {rdict[key]}.')
+ else:
+ if item != rdict[key]:
+ differences.append(f'Values of key {key} are not equal {item} : {rdict[key]}.')
+ return differences
+
ale_root = os.path.split(ale.__file__)[0]
data_root = os.path.join(ale_root, '../tests/pytests/data')
dirs = next(os.walk(data_root, topdown=True))[1]
@@ -109,17 +129,18 @@ def convert_kernels(kernels):
binary_kernels : list
The list of binary kernels created.
"""
- ext_map = {
- '.xc' : '.bc',
- '.xsp' : '.bsp'
- }
binary_kernels = []
updated_kernels = []
for kernel in kernels:
split_kernel = os.path.splitext(kernel)
- if split_kernel[1] in ext_map:
- subprocess.call(['tobin', os.path.join(data_root, kernel)])
- kernel = split_kernel[0] + ext_map[split_kernel[1]]
- binary_kernels.append(kernel)
+ if 'x' in split_kernel[1].lower():
+ bin_output = subprocess.run(['tobin', os.path.join(data_root, kernel)],
+ capture_output=True, check=True)
+ matches = re.search(r'To: (.*\.b\w*)', str(bin_output.stdout))
+ if not matches:
+ warnings.warn('Failed to convert transfer kernel, ' + kernel + ', skipping...')
+ else:
+ kernel = matches.group(1)
+ binary_kernels.append(kernel)
updated_kernels.append(kernel)
return updated_kernels, binary_kernels
diff --git a/tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_M_V01.TSC b/tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_M_V01.TSC
new file mode 100644
index 0000000..f1f3fe8
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_M_V01.TSC
@@ -0,0 +1,2151 @@
+SELENE SCLK FILE
+------------------------------------------------------------
+# Correction Method Version 002. 2008/2/15 LISM team.
+# (1) Light time correction of SELENE - Ground Station
+# distance was applied.
+# (2) Offset correction of Ground Station was applied.
+# (3) Thinning out (nominal: 6 hours) was applied.
+#
+\begindata
+SCLK_KERNEL_ID = ( @2009-06-10T12:57:27.4670 )
+SCLK_DATA_TYPE_131 = ( 1 )
+SCLK01_N_FIELDS_131 = ( 1 )
+SCLK01_MODULI_131 = ( 4294967296 )
+SCLK01_OFFSETS_131 = ( 0 0 )
+SCLK01_OUTPUT_DELIM_131 = ( 2 )
+SCLK_PARTITION_START_131 = ( 0.0000000000000E+00 )
+SCLK_PARTITION_END_131 = ( 1.2614400000000E+09 )
+SCLK01_COEFFICIENTS_131 = (
+ 0.0000000000000E+00 -6.3076313228103E+08 9.9999999881993E-01
+ 8.7653781200000E+08 2.4577467868459E+08 1.0000003366190E+00
+ 8.7655718100000E+08 2.4579404769111E+08 1.0000002993192E+00
+ 8.7663442300000E+08 2.4587128971423E+08 1.0000002870738E+00
+ 8.7665375600000E+08 2.4589062271978E+08 1.0000002934423E+00
+ 8.7672170800000E+08 2.4595857473972E+08 1.0000002915723E+00
+ 8.7674331500000E+08 2.4598018174602E+08 1.0000002879502E+00
+ 8.7676491600000E+08 2.4600178275224E+08 1.0000002907410E+00
+ 8.7678651600000E+08 2.4602338275852E+08 1.0000002879488E+00
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+ 8.7682973000000E+08 2.4606659677092E+08 1.0000002648143E+00
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+ )
diff --git a/tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_TC_V01.TI b/tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_TC_V01.TI
new file mode 100644
index 0000000..5bf4267
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_TC_V01.TI
@@ -0,0 +1,906 @@
+KPL/IK
+
+TC/LISM/SELENE Instrument Kernel
+===========================================================================
+
+ This Terrein Camera (TC) instrument kernel (I-kernel) contains
+ the instrument mounting offset, fields-of-view specifications, and optics
+ and detector parameters. Details of TC instrument are described in
+ Haruyama et al., 2007.
+
+Version and Date
+---------------------------------------------------------------------------
+ Version 3.01 -- July 14, 2009 -- S. Hara (CCS)
+
+ - Angles of LISM_LRU_TC_MI, LISM_TC1_HEAD and LISM_TC2_HEAD were updated.
+ - Comment of distortion equation is corrected.
+
+ Version 3.00 -- July 8, 2009 -- S. Hara (CCS)
+
+ - Distortion coefficients of the LISM_TC2 (-131371) were corrected.
+ - Y-AXIS angles of the LISM_TC1_HEAD and LISM_TC2_HEAD were updated
+ to correct DTM vertical offset.
+
+ Version 2.00 -- July 7, 2008 -- S. Hara (CCS)
+
+ - X-AXIS angle of the LISM_LRU_TC_MI (-131320) was corrected.
+ - Distortion coefficients of the LISM_TC2 (-131371) were corrected.
+
+ Version 1.03-- December 7, 2007 -- J. Haruyama, M. Ohtake, Y.Yokota (JAXA)
+
+ - ANGLES of the Frames (from -131310 to -131370) were updated
+ by using the laboratory measurement values.
+ - Pixel coordinates of Along-track center are corrected.
+ - Comments were updated.
+
+ Version 1.02 -- October 10, 2007 -- Y.Yokota (JAXA)
+
+ FOV_BOUNDARY_CORNERS data for Level 2A software were corrected.
+
+ Version 1.0 -- October 2, 2007 -- Naru Hirata (Univ. of Aizu.),
+ Jun'ichi Haruyama (JAXA), Makiko Ohtake (JAXA),
+ Tsuneo Matsunaga (NIES), Y.Yokota (JAXA)
+
+ Initial version after launch.
+ Preliminary versions have been developed since March 12, 2005.
+
+References
+---------------------------------------------------------------------------
+Haruyama, J. et al., " Global lunar-surface mapping experiment using the
+Lunar Imager/Spectrometer on SELENE", Earth Planets Space, vol.59, 1-13,
+2007.
+
+
+Implementation Notes
+---------------------------------------------------------------------------
+
+
+TC NAIF IDs
+---------------------------------------------------------------------------
+
+ The following NAIF IDs are assigned to individual TC sensors:
+
+ End
+ Start Pixel
+ Sensor Pixel (+dummy) NAIF ID
+ -----------------------------------------------------------------
+ LISM_TC1 1 4096 -131351
+ LISM_TC2 1 4096 -131371
+
+ LISM_TC1_WDF (Double DCT Full) 1 4096 -131352
+ LISM_TC1_WTF (Double Through Full) 1 1600 -131353
+ LISM_TC1_SDF (Single DCT Full) 1 4096 -131354
+ LISM_TC1_STF (Single Through Full) 1 3208 -131355
+ LISM_TC1_WDN (Double DCT Nominal) 297 3796(+4) -131356
+ LISM_TC1_WTN (Double Through Nominal) 297 1896 -131357
+ LISM_TC1_SDN (Single DCT Nominal) 297 3796(+4) -131358
+ LISM_TC1_STN (Single Through Nominal) 297 3504 -131359
+ LISM_TC1_WDH (Double DCT Half) 1172 2921(+2) -131360
+ LISM_TC1_WTH (Double Through Half) 1172 2771 -131361
+ LISM_TC1_SDH (Single DCT Half) 1172 2921(+2) -131362
+ LISM_TC1_STH (Single Through Half) 1172 2923 -131363
+ LISM_TC1_SSH (Single SP_support Half) 1172 2921 -131364
+
+ LISM_TC2_WDF (Double DCT Full) 1 4096 -131372
+ LISM_TC2_WTF (Double Through Full) 1 1600 -131373
+ LISM_TC2_SDF (Single DCT Full) 1 4096 -131374
+ LISM_TC2_STF (Single Through Full) 1 3208 -131375
+ LISM_TC2_WDN (Double DCT Nominal) 297 3796(+4) -131376
+ LISM_TC2_WTN (Double Through Nominal) 297 1896 -131377
+ LISM_TC2_SDN (Single DCT Nominal) 297 3796(+4) -131378
+ LISM_TC2_STN (Single Through Nominal) 297 3504 -131379
+ LISM_TC2_WDH (Double DCT Half) 1172 2921(+2) -131380
+ LISM_TC2_WTH (Double Through Half) 1172 2771 -131381
+ LISM_TC2_SDH (Single DCT Half) 1172 2921(+2) -131382
+ LISM_TC2_STH (Single Through Half) 1172 2923 -131383
+ LISM_TC2_SSH (Single SP_support Half) 1172 2921 -131384
+ -----------------------------------------------------------------
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'LISM_TC1' )
+ NAIF_BODY_CODE += ( -131351 )
+ NAIF_BODY_NAME += ( 'LISM_TC2' )
+ NAIF_BODY_CODE += ( -131371 )
+
+ NAIF_BODY_NAME += ( 'LISM_TC1_WDF' )
+ NAIF_BODY_CODE += ( -131352 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_WTF' )
+ NAIF_BODY_CODE += ( -131353 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_SDF' )
+ NAIF_BODY_CODE += ( -131354 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_STF' )
+ NAIF_BODY_CODE += ( -131355 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_WDN' )
+ NAIF_BODY_CODE += ( -131356 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_WTN' )
+ NAIF_BODY_CODE += ( -131357 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_SDN' )
+ NAIF_BODY_CODE += ( -131358 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_STN' )
+ NAIF_BODY_CODE += ( -131359 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_WDH' )
+ NAIF_BODY_CODE += ( -131360 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_WTH' )
+ NAIF_BODY_CODE += ( -131361 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_SDH' )
+ NAIF_BODY_CODE += ( -131362 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_STH' )
+ NAIF_BODY_CODE += ( -131363 )
+ NAIF_BODY_NAME += ( 'LISM_TC1_SSH' )
+ NAIF_BODY_CODE += ( -131364 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_WDF' )
+ NAIF_BODY_CODE += ( -131372 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_WTF' )
+ NAIF_BODY_CODE += ( -131373 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_SDF' )
+ NAIF_BODY_CODE += ( -131374 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_STF' )
+ NAIF_BODY_CODE += ( -131375 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_WDN' )
+ NAIF_BODY_CODE += ( -131376 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_WTN' )
+ NAIF_BODY_CODE += ( -131377 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_SDN' )
+ NAIF_BODY_CODE += ( -131378 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_STN' )
+ NAIF_BODY_CODE += ( -131379 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_WDH' )
+ NAIF_BODY_CODE += ( -131380 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_WTH' )
+ NAIF_BODY_CODE += ( -131381 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_SDH' )
+ NAIF_BODY_CODE += ( -131382 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_STH' )
+ NAIF_BODY_CODE += ( -131383 )
+ NAIF_BODY_NAME += ( 'LISM_TC2_SSH' )
+ NAIF_BODY_CODE += ( -131384 )
+
+ \begintext
+
+
+
+Optical Parameters
+---------------------------------------------------------------------------
+
+ The following table summarizes TC individual camera optics
+ parameters:
+
+ -----------------------------------------------------------------
+ parameter TC1 TC2
+ -----------------------------------------------------------------
+ Focal Length, mm 72.45 72.63
+ f/ratio f/4.0 f/4.0
+ IFOV, rad/pixel 0.0000966 0.0000966
+ Field of view (rad)
+ Cross-track (full swath) 0.3909538 0.3909538
+ Cross-track (nominal swath) 0.3368485 0.3368485
+ Cross-track (full swath) 0.1684243 0.1684243
+ Along-track 0.0000966 0.0000966
+ -----------------------------------------------------------------
+
+ These values are incorporated in the keywords below; pixel sizes
+ are converted to MILLIMETERS.
+ ^^^^^^^^^^^
+
+ \begindata
+
+ INS-131351_FOCAL_LENGTH = ( 72.45 )
+ INS-131351_F_NUMBER = ( 4.0 )
+
+ INS-131371_FOCAL_LENGTH = ( 72.63 )
+ INS-131371_F_NUMBER = ( 4.0 )
+
+
+ \begintext
+
+Mounting Alignment
+---------------------------------------------------------------------------
+
+Detector CCD Parameters
+---------------------------------------------------------------------------
+
+ The following table summarizes TC individual camera detector
+ parameters. As these data show the detectors are all line arrays.
+
+
+ -----------------------------------------------------------------
+ parameter TC1 TC2
+ -----------------------------------------------------------------
+ Pixel Size, microns
+ Cross-track 7.0 7.0
+ Along-track 7.0 7.0
+ Detector Array Size
+ Cross-track 4096 4096
+ Along-track 1 1
+ Detector Array Center (*1)
+ Cross-track 2048.5 2048.5
+ Along-track 1.0 1.0
+ -----------------------------------------------------------------
+
+ (*1) Center of the first pixel is defined as "1.0".
+
+
+ These values are incorporated in the keywords below; pixel sizes
+ are converted to MILLIMETERS.
+ ^^^^^^^^^^^
+
+ \begindata
+
+ INS-131351_PIXEL_SAMPLES = ( 4096 )
+ INS-131351_PIXEL_LINES = ( 1 )
+ INS-131351_CENTER = ( 2048.5, 1.0 )
+ INS-131351_PIXEL_SIZE = ( 0.007 )
+
+ INS-131371_PIXEL_SAMPLES = ( 4096 )
+ INS-131371_PIXEL_LINES = ( 1 )
+ INS-131371_CENTER = ( 2048.5, 1.0 )
+ INS-131371_PIXEL_SIZE = ( 0.007 )
+
+ \begintext
+
+
+FOV Definitions
+---------------------------------------------------------------------------
+
+ In this section, definitions for FOVs of TC1 and TC2 are described in
+ a format consistent required by the SPICE (CSPICE) function GETFOV
+ (getfov_c).
+
+ On each focal plane of TC1 and TC2, a one-dimensional CCD is located.
+ The direction along the row of pixels of each CCD is defined to be Y axis.
+ The +Y is the direction toward the radiator side from the CCDs.
+ Z axis is defined to be "ideal" boresight.
+
+
+ Corner pixel
+ view direction
+ ^
+ Boresight \ +X
+ vector <. \ ^ Focal plane
+ direction `-. \ |
+ `-. \ | .^ -Y
+ `-. \ | .'
+ `-.\ F | .'
+ <-----------`o.-----o'
+ +Z Focal \`-. | . 1-line CCD
+ point \ `-*'
+ \ .'| Detector center
+ * |
+ Corner
+ pixel
+
+
+ The "actual" boresight vector (INS<INSTID>_BORESIGHT) is along the
+ view direction of the middle point of pixels of no. 2048 and no. 2049.
+
+ Corner vectors (FOV_BOUNDARY_CORNERS) are defined as line-of-sight
+ vectors from the middle points of the upper and lower edges of corner
+ pixels. We note that these points are A and B, but not C and D in the
+ below diagram. These corner vectors are only used in LISM Level 2A:
+
+
+ C A A' C'
+ / / \ \
+ o------o-------o------o-------o----- ---o------o-------o
+ | | | | |
+ | Pixel no.1 | Pixel no.2 | .... | Last Pixel |
+ | | | | |
+ | | | | |
+ o------o-------o------o-------o----- ---o------o-------o
+ \ \ / /
+ D B B' D'
+
+
+ When the coordinates of the first and last pixel of each CCD are
+ (Xf,Yf) and (Xl,Yl) and those of the two middle pixels of the first
+ and last pixels are (Xm1,Ym1) and (Xm2,Ym2), the FOV definition can
+ be expressed as:
+
+ INS<INSTID>_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS<INSTID>_FOV_SHAPE = 'RECTANGLE'
+ INS<INSTID>_BORESIGHT = (
+ -Xm, -(Ym1+Ym2)/2, FL
+ )
+ INS<INSTID>_FOV_BOUNDARY_CORNERS = (
+ -(Xf-HP), -Yf, FL
+ -(Xf+HP), -Yf, FL
+ -(Xl+HP), -Yl, FL
+ -(Xl-HP), -Yl, FL
+ )
+
+ where HP is 1/2 of the pixel size [mm], and FL is the focal length.
+
+
+ \begindata
+
+ INS-131351_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131351_FOV_SHAPE = 'RECTANGLE'
+ INS-131351_BORESIGHT = (
+ -0.0725 0.0214 72.4500
+ )
+ INS-131351_FOV_BOUNDARY_CORNERS = (
+ -0.0690 14.3574 72.4500
+ -0.0760 14.3574 72.4500
+ -0.0760 -14.3146 72.4500
+ -0.0690 -14.3146 72.4500
+ )
+
+ INS-131371_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131371_FOV_SHAPE = 'RECTANGLE'
+ INS-131371_BORESIGHT = (
+ -0.0474 0.0126 72.6300
+ )
+ INS-131371_FOV_BOUNDARY_CORNERS = (
+ -0.0439 14.3486 72.6300
+ -0.0509 14.3486 72.6300
+ -0.0509 -14.3234 72.6300
+ -0.0439 -14.3234 72.6300
+ )
+
+ INS-131352_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131352_FOV_SHAPE = 'RECTANGLE'
+ INS-131352_BORESIGHT = (
+ -0.0725 0.0214 72.4500
+ )
+ INS-131352_FOV_BOUNDARY_CORNERS = (
+ -0.0690 14.3574 72.4500
+ -0.0760 14.3574 72.4500
+ -0.0760 -14.3146 72.4500
+ -0.0690 -14.3146 72.4500
+ )
+
+ INS-131353_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131353_FOV_SHAPE = 'RECTANGLE'
+ INS-131353_BORESIGHT = (
+ -0.0725 8.7574 72.4500
+ )
+ INS-131353_FOV_BOUNDARY_CORNERS = (
+ -0.0690 14.3574 72.4500
+ -0.0760 14.3574 72.4500
+ -0.0760 3.1574 72.4500
+ -0.0690 3.1574 72.4500
+ )
+
+ INS-131354_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131354_FOV_SHAPE = 'RECTANGLE'
+ INS-131354_BORESIGHT = (
+ -0.0725 0.0214 72.4500
+ )
+ INS-131354_FOV_BOUNDARY_CORNERS = (
+ -0.0690 14.3574 72.4500
+ -0.0760 14.3574 72.4500
+ -0.0760 -14.3146 72.4500
+ -0.0690 -14.3146 72.4500
+ )
+
+ INS-131355_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131355_FOV_SHAPE = 'RECTANGLE'
+ INS-131355_BORESIGHT = (
+ -0.0725 3.1294 72.4500
+ )
+ INS-131355_FOV_BOUNDARY_CORNERS = (
+ -0.0690 14.3574 72.4500
+ -0.0760 14.3574 72.4500
+ -0.0760 -8.0986 72.4500
+ -0.0690 -8.0986 72.4500
+ )
+
+ INS-131356_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131356_FOV_SHAPE = 'RECTANGLE'
+ INS-131356_BORESIGHT = (
+ -0.0725 0.0354 72.4500
+ )
+ INS-131356_FOV_BOUNDARY_CORNERS = (
+ -0.0690 12.2854 72.4500
+ -0.0760 12.2854 72.4500
+ -0.0760 -12.2146 72.4500
+ -0.0690 -12.2146 72.4500
+ )
+
+ INS-131357_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131357_FOV_SHAPE = 'RECTANGLE'
+ INS-131357_BORESIGHT = (
+ -0.0725 6.6854 72.4500
+ )
+ INS-131357_FOV_BOUNDARY_CORNERS = (
+ -0.0690 12.2854 72.4500
+ -0.0760 12.2854 72.4500
+ -0.0760 1.0854 72.4500
+ -0.0690 1.0854 72.4500
+ )
+
+ INS-131358_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131358_FOV_SHAPE = 'RECTANGLE'
+ INS-131358_BORESIGHT = (
+ -0.0725 0.0354 72.4500
+ )
+ INS-131358_FOV_BOUNDARY_CORNERS = (
+ -0.0690 12.2854 72.4500
+ -0.0760 12.2854 72.4500
+ -0.0760 -12.2146 72.4500
+ -0.0690 -12.2146 72.4500
+ )
+
+ INS-131359_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131359_FOV_SHAPE = 'RECTANGLE'
+ INS-131359_BORESIGHT = (
+ -0.0725 1.0574 72.4500
+ )
+ INS-131359_FOV_BOUNDARY_CORNERS = (
+ -0.0690 12.2854 72.4500
+ -0.0760 12.2854 72.4500
+ -0.0760 -10.1706 72.4500
+ -0.0690 -10.1706 72.4500
+ )
+
+ INS-131360_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131360_FOV_SHAPE = 'RECTANGLE'
+ INS-131360_BORESIGHT = (
+ -0.0725 0.0354 72.4500
+ )
+ INS-131360_FOV_BOUNDARY_CORNERS = (
+ -0.0690 6.1604 72.4500
+ -0.0760 6.1604 72.4500
+ -0.0760 -6.0896 72.4500
+ -0.0690 -6.0896 72.4500
+ )
+
+ INS-131361_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131361_FOV_SHAPE = 'RECTANGLE'
+ INS-131361_BORESIGHT = (
+ -0.0725 0.5604 72.4500
+ )
+ INS-131361_FOV_BOUNDARY_CORNERS = (
+ -0.0690 6.1604 72.4500
+ -0.0760 6.1604 72.4500
+ -0.0760 -5.0396 72.4500
+ -0.0690 -5.0396 72.4500
+ )
+
+ INS-131362_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131362_FOV_SHAPE = 'RECTANGLE'
+ INS-131362_BORESIGHT = (
+ -0.0725 0.0354 72.4500
+ )
+
+ INS-131362_FOV_BOUNDARY_CORNERS = (
+ -0.0690 6.1604 72.4500
+ -0.0760 6.1604 72.4500
+ -0.0760 -6.0896 72.4500
+ -0.0690 -6.0896 72.4500
+ )
+
+ INS-131363_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131363_FOV_SHAPE = 'RECTANGLE'
+ INS-131363_BORESIGHT = (
+ -0.0725 0.0284 72.4500
+ )
+ INS-131363_FOV_BOUNDARY_CORNERS = (
+ -0.0690 6.1604 72.4500
+ -0.0760 6.1604 72.4500
+ -0.0760 -6.1036 72.4500
+ -0.0690 -6.1036 72.4500
+ )
+
+ INS-131364_FOV_FRAME = 'LISM_TC1_HEAD'
+ INS-131364_FOV_SHAPE = 'RECTANGLE'
+ INS-131364_BORESIGHT = (
+ -0.0725 0.0354 72.4500
+
+ )
+ INS-131364_FOV_BOUNDARY_CORNERS = (
+ -0.0690 6.1604 72.4500
+ -0.0760 6.1604 72.4500
+ -0.0760 -6.0896 72.4500
+ -0.0690 -6.0896 72.4500
+ )
+
+ INS-131372_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131372_FOV_SHAPE = 'RECTANGLE'
+ INS-131372_BORESIGHT = (
+ -0.0474 0.0126 72.6300
+ )
+ INS-131372_FOV_BOUNDARY_CORNERS = (
+ -0.0439 14.3486 72.6300
+ -0.0509 14.3486 72.6300
+ -0.0509 -14.3234 72.6300
+ -0.0439 -14.3234 72.6300
+ )
+
+ INS-131373_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131373_FOV_SHAPE = 'RECTANGLE'
+ INS-131373_BORESIGHT = (
+ -0.0474 8.7486 72.6300
+ )
+ INS-131373_FOV_BOUNDARY_CORNERS = (
+ -0.0439 14.3486 72.6300
+ -0.0509 14.3486 72.6300
+ -0.0509 3.1486 72.6300
+ -0.0439 3.1486 72.6300
+ )
+
+ INS-131374_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131374_FOV_SHAPE = 'RECTANGLE'
+ INS-131374_BORESIGHT = (
+ -0.0474 0.0126 72.6300
+ )
+ INS-131374_FOV_BOUNDARY_CORNERS = (
+ -0.0439 14.3486 72.6300
+ -0.0509 14.3486 72.6300
+ -0.0509 -14.3234 72.6300
+ -0.0439 -14.3234 72.6300
+ )
+
+ INS-131375_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131375_FOV_SHAPE = 'RECTANGLE'
+ INS-131375_BORESIGHT = (
+ -0.0474 3.1206 72.6300
+ )
+ INS-131375_FOV_BOUNDARY_CORNERS = (
+ -0.0439 14.3486 72.6300
+ -0.0509 14.3486 72.6300
+ -0.0509 -8.1074 72.6300
+ -0.0439 -8.1074 72.6300
+ )
+
+ INS-131376_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131376_FOV_SHAPE = 'RECTANGLE'
+ INS-131376_BORESIGHT = (
+ -0.0474 0.0266 72.6300
+ )
+ INS-131376_FOV_BOUNDARY_CORNERS = (
+ -0.0439 12.2766 72.6300
+ -0.0509 12.2766 72.6300
+ -0.0509 -12.2234 72.6300
+ -0.0439 -12.2234 72.6300
+ )
+
+ INS-131377_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131377_FOV_SHAPE = 'RECTANGLE'
+ INS-131377_BORESIGHT = (
+ -0.0474 6.6766 72.6300
+ )
+ INS-131377_FOV_BOUNDARY_CORNERS = (
+ -0.0439 12.2766 72.6300
+ -0.0509 12.2766 72.6300
+ -0.0509 1.0766 72.6300
+ -0.0439 1.0766 72.6300
+ )
+
+ INS-131378_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131378_FOV_SHAPE = 'RECTANGLE'
+ INS-131378_BORESIGHT = (
+ -0.0474 0.0266 72.6300
+ )
+ INS-131378_FOV_BOUNDARY_CORNERS = (
+ -0.0439 12.2766 72.6300
+ -0.0509 12.2766 72.6300
+ -0.0509 -12.2234 72.6300
+ -0.0439 -12.2234 72.6300
+ )
+
+ INS-131379_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131379_FOV_SHAPE = 'RECTANGLE'
+ INS-131379_BORESIGHT = (
+ -0.0474 1.0486 72.6300
+ )
+ INS-131379_FOV_BOUNDARY_CORNERS = (
+ -0.0439 12.2766 72.6300
+ -0.0509 12.2766 72.6300
+ -0.0509 -10.1794 72.6300
+ -0.0439 -10.1794 72.6300
+ )
+
+ INS-131380_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131380_FOV_SHAPE = 'RECTANGLE'
+ INS-131380_BORESIGHT = (
+ -0.0474 0.0266 72.6300
+ )
+ INS-131380_FOV_BOUNDARY_CORNERS = (
+ -0.0439 6.1516 72.6300
+ -0.0509 6.1516 72.6300
+ -0.0509 -6.0984 72.6300
+ -0.0439 -6.0984 72.6300
+ )
+
+ INS-131381_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131381_FOV_SHAPE = 'RECTANGLE'
+ INS-131381_BORESIGHT = (
+ -0.0474 0.5516 72.6300
+ )
+ INS-131381_FOV_BOUNDARY_CORNERS = (
+ -0.0439 6.1516 72.6300
+ -0.0509 6.1516 72.6300
+ -0.0509 -5.0484 72.6300
+ -0.0439 -5.0484 72.6300
+ )
+
+ INS-131382_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131382_FOV_SHAPE = 'RECTANGLE'
+ INS-131382_BORESIGHT = (
+ -0.0474 0.0266 72.6300
+ )
+ INS-131382_FOV_BOUNDARY_CORNERS = (
+ -0.0439 6.1516 72.6300
+ -0.0509 6.1516 72.6300
+ -0.0509 -6.0984 72.6300
+ -0.0439 -6.0984 72.6300
+
+ )
+
+ INS-131383_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131383_FOV_SHAPE = 'RECTANGLE'
+ INS-131383_BORESIGHT = (
+ -0.0474 0.0196 72.6300
+ )
+ INS-131383_FOV_BOUNDARY_CORNERS = (
+ -0.0439 6.1516 72.6300
+ -0.0509 6.1516 72.6300
+ -0.0509 -6.1124 72.6300
+ -0.0439 -6.1124 72.6300
+ )
+
+ INS-131384_FOV_FRAME = 'LISM_TC2_HEAD'
+ INS-131384_FOV_SHAPE = 'RECTANGLE'
+ INS-131384_BORESIGHT = (
+ -0.0474 0.0266 72.6300
+ )
+ INS-131384_FOV_BOUNDARY_CORNERS = (
+ -0.0439 6.1516 72.6300
+ -0.0509 6.1516 72.6300
+ -0.0509 -6.0984 72.6300
+ -0.0439 -6.0984 72.6300
+ )
+
+ \begintext
+
+SELENE/LISM NAIF frame IDs
+---------------------------------------------------------------------------
+
+ The following NAIF IDs are assigned to individual LISM frames and sensors:
+
+ Definition of the keywords used in these assignment are attached
+ at bottom of the table.
+
+ NAIF ID
+ ------------------------------------------------
+ SELENE_M -131
+ SELENE_M_SPACECRAFT -131000
+
+ LISM_LRU_SP -131310
+ LISM_SP -131311
+ LISM_SP_HIGH -131312
+
+ LISM_LRU_TC_MI -131320
+
+ LISM_MI_V_HEAD -131330
+ LISM_MI_N_HEAD -131340
+
+ LISM_MI-VIS1 -131331
+ LISM_MI-VIS2 -131332
+ LISM_MI-VIS3 -131333
+ LISM_MI-VIS4 -131334
+ LISM_MI-VIS5 -131335
+ LISM_MI-NIR1 -131341
+ LISM_MI-NIR2 -131342
+ LISM_MI-NIR3 -131343
+ LISM_MI-NIR4 -131344
+
+ LISM_TC1_HEAD -131350
+ LISM_TC2_HEAD -131370
+
+ LISM_TC1 -131351
+ LISM_TC2 -131371
+
+ LISM_TC1_WDF (Double DCT Full) -131352
+ LISM_TC1_WTF (Double Through Full) -131353
+ LISM_TC1_SDF (Single DCT Full) -131354
+ LISM_TC1_STF (Single Through Full) -131355
+ LISM_TC1_WDN (Double DCT Nominal) -131356
+ LISM_TC1_WTN (Double Through Nominal) -131357
+ LISM_TC1_SDN (Single DCT Nominal) -131358
+ LISM_TC1_STN (Single Through Nominal) -131359
+ LISM_TC1_WDH (Double DCT Half) -131360
+ LISM_TC1_WTH (Double Through Half) -131361
+ LISM_TC1_SDH (Single DCT Half) -131362
+ LISM_TC1_STH (Single Through Half) -131363
+ LISM_TC1_SSH (Single SP_support Half) -131364
+
+ LISM_TC2_WDF (Double DCT Full) -131372
+ LISM_TC2_WTF (Double Through Full) -131373
+ LISM_TC2_SDF (Single DCT Full) -131374
+ LISM_TC2_STF (Single Through Full) -131375
+ LISM_TC2_WDN (Double DCT Nominal) -131376
+ LISM_TC2_WTN (Double Through Nominal) -131377
+ LISM_TC2_SDN (Single DCT Nominal) -131378
+ LISM_TC2_STN (Single Through Nominal) -131379
+ LISM_TC2_WDH (Double DCT Half) -131380
+ LISM_TC2_WTH (Double Through Half) -131381
+ LISM_TC2_SDH (Single DCT Half) -131382
+ LISM_TC2_STH (Single Through Half) -131383
+ LISM_TC2_SSH (Single SP_support Half) -131384
+
+ Definition of the keywords
+ SELENE_M: SELENE mission
+ SELENE_M_SPACECRAFT: SELENE main satellite
+ LISM_LRU_SP: LISM Radiometer SP Unit
+ LISM_SP: SP nominal resolution
+ LISM_SP_HIGH: SP high resolution
+ LISM_LRU_TC_MI: LISM Radiometer TC/MI Unit
+ LISM_MI_V_HEAD: MI-VIS optics
+ LISM_MI_N_HEAD: MI-NIR optics
+ LISM_TC1_HEAD: TC1 optics
+ LISM_TC2_HEAD: TC2 optics
+
+SELENE/LISM Frames
+---------------------------------------------------------------------------
+
+ The following SELENE/LISM frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ SELENE_M_SPACECRAFT J2000 CK -131000
+ LISM_LRU_SP SELENE_M FIXED -131310
+ LISM_LRU_TC_MI SELENE_M FIXED -131320
+ LISM_MI_V_HEAD LISM_LRU_TC_MI FIXED -131330
+ LISM_MI_N_HEAD LISM_LRU_TC_MI FIXED -131340
+ LISM_TC1_HEAD LISM_LRU_TC_MI FIXED -131350
+ LISM_TC2_HEAD LISM_LRU_TC_MI FIXED -131370
+
+
+SELENE/LISM Frame Tree
+--------------------------------------
+
+ The diagram below shows the SELENE/LISM frame hierarchy.
+
+
+ "J2000" INERTIAL
+ +-----------------------------------------------------+
+ | | |
+ |<-pck | |<-pck
+ | | |
+ V | V
+ "MOON_ME" | "IAU_EARTH"
+ MOON BODY-FIXED |<-ck EARTH BODY-FIXED
+ --------------- | ----------------
+ V
+ "SELENE_M_SPACECRAFT"
+ +-----------------------------------------------------+
+ | |
+ |<-fixed |<-fixed
+ | |
+ V V
+ "LISM_LRU_TC_MI" "LISM_LRU_SP"
+ -----------------------------------------------+ -------------
+ | | | |
+ |<-fixed | |<-fixed |
+ | | | |
+ V | V |
+ "LISM_TC1_HEAD" | "LISM_MI_V_HEAD" |
+ --------------- | -------------- |
+ | |
+ |<-fixed |<-fixed
+ | |
+ V V
+ "LISM_TC2_HEAD" "LISM_MI_N_HEAD"
+ --------------- ----------------
+
+ \begindata
+
+ FRAME_SELENE_M_SPACECRAFT = -131000
+ FRAME_-131000_NAME = 'SELENE_M_SPACECRAFT'
+ FRAME_-131000_CLASS = 3
+ FRAME_-131000_CLASS_ID = -131000
+ FRAME_-131000_CENTER = -131
+ CK_-131000_SCLK = -131
+ CK_-131000_SPK = -131
+
+ FRAME_LISM_LRU_SP = -131310
+ FRAME_-131310_NAME = 'LISM_LRU_SP'
+ FRAME_-131310_CLASS = 4
+ FRAME_-131310_CLASS_ID = -131310
+ FRAME_-131310_CENTER = -131
+ TKFRAME_-131310_RELATIVE = 'SELENE_M_SPACECRAFT'
+ TKFRAME_-131310_SPEC = 'ANGLES'
+ TKFRAME_-131310_UNITS = 'DEGREES'
+ TKFRAME_-131310_AXES = ( 3, 2, 1 )
+ TKFRAME_-131310_ANGLES = ( 0.1429, -0.0202, 0.0689 )
+
+
+ FRAME_LISM_LRU_TC_MI = -131320
+ FRAME_-131320_NAME = 'LISM_LRU_TC_MI'
+ FRAME_-131320_CLASS = 4
+ FRAME_-131320_CLASS_ID = -131320
+ FRAME_-131320_CENTER = -131
+ TKFRAME_-131320_RELATIVE = 'SELENE_M_SPACECRAFT'
+ TKFRAME_-131320_SPEC = 'ANGLES'
+ TKFRAME_-131320_UNITS = 'DEGREES'
+ TKFRAME_-131320_AXES = ( 3, 2, 1 )
+ TKFRAME_-131320_ANGLES = ( 0.0099, 0.0396, -0.0179 )
+
+ FRAME_LISM_MI_V_HEAD = -131330
+ FRAME_-131330_NAME = 'LISM_MI_V_HEAD'
+ FRAME_-131330_CLASS = 4
+ FRAME_-131330_CLASS_ID = -131330
+ FRAME_-131330_CENTER = -131
+ TKFRAME_-131330_RELATIVE = 'LISM_LRU_TC_MI'
+ TKFRAME_-131330_SPEC = 'ANGLES'
+ TKFRAME_-131330_UNITS = 'DEGREES'
+ TKFRAME_-131330_AXES = ( 3, 2, 1 )
+ TKFRAME_-131330_ANGLES = ( 0.0138, -0.0899, -0.0536 )
+
+ FRAME_LISM_MI_N_HEAD = -131340
+ FRAME_-131340_NAME = 'LISM_MI_N_HEAD'
+ FRAME_-131340_CLASS = 4
+ FRAME_-131340_CLASS_ID = -131340
+ FRAME_-131340_CENTER = -131
+ TKFRAME_-131340_RELATIVE = 'LISM_LRU_TC_MI'
+ TKFRAME_-131340_SPEC = 'ANGLES'
+ TKFRAME_-131340_UNITS = 'DEGREES'
+ TKFRAME_-131340_AXES = ( 3, 2, 1 )
+ TKFRAME_-131340_ANGLES = ( 0.0232, -0.0068, -0.0332 )
+
+ FRAME_LISM_TC1_HEAD = -131350
+ FRAME_-131350_NAME = 'LISM_TC1_HEAD'
+ FRAME_-131350_CLASS = 4
+ FRAME_-131350_CLASS_ID = -131350
+ FRAME_-131350_CENTER = -131
+ TKFRAME_-131350_RELATIVE = 'LISM_LRU_TC_MI'
+ TKFRAME_-131350_SPEC = 'ANGLES'
+ TKFRAME_-131350_UNITS = 'DEGREES'
+ TKFRAME_-131350_AXES = ( 3, 2, 1 )
+ TKFRAME_-131350_ANGLES = ( 0.04903647, -14.97465222, 0.05110624 )
+
+ FRAME_LISM_TC2_HEAD = -131370
+ FRAME_-131370_NAME = 'LISM_TC2_HEAD'
+ FRAME_-131370_CLASS = 4
+ FRAME_-131370_CLASS_ID = -131370
+ FRAME_-131370_CENTER = -131
+ TKFRAME_-131370_RELATIVE = 'LISM_LRU_TC_MI'
+ TKFRAME_-131370_SPEC = 'ANGLES'
+ TKFRAME_-131370_UNITS = 'DEGREES'
+ TKFRAME_-131370_AXES = ( 3, 2, 1 )
+ TKFRAME_-131370_ANGLES = ( -0.04379912, 15.01058661, 0.09222246 )
+
+ \begintext
+
+Distortion information
+---------------------------------------------------------------------------
+ Line-of-sight vector of pixel no. n can be expressed as below.
+
+ Distortion coefficients information:
+ INS<INSTID>_DISTORTION_COEF_X = ( a0, a1, a2, a3)
+ INS<INSTID>_DISTORTION_COEF_Y = ( b0, b1, b2, b3),
+
+ Distance r from the center:
+ r = - (n - INS<INSTID>_CENTER) * INS<INSTID>_PIXEL_SIZE.
+
+ Line-of-sight vector v is calculated as
+ v[X] = INS<INSTID>BORESIGHT[X]
+ +a0 +a1*r +a2*r^2 +a3*r^3 ,
+ v[Y] = INS<INSTID>BORESIGHT[Y]
+ +r +a0 +a1*r +a2*r^2 +a3*r^3 ,
+ v[Z] = INS<INSTID>BORESIGHT[Z] .
+
+
+ \begindata
+
+ INS-131351_DISTORTION_COEF_X = (
+ -9.6499e-4, 9.8441e-4,
+ 8.5773e-6, -3.7438e-6
+ )
+ INS-131351_DISTORTION_COEF_Y = (
+ -1.3796e-3, 1.3502e-5,
+ 2.7251e-6, -6.1938e-6
+ )
+ INS-131371_DISTORTION_COEF_X = (
+ 2.9786e-3, 7.7836e-5,
+ 3.9265e-6, -4.4088e-6
+ )
+ INS-131371_DISTORTION_COEF_Y = (
+ 9.2410e-4, -1.1994e-4,
+ 2.9281e-5, -3.7239e-7
+ )
+ \begintext
diff --git a/tests/pytests/data/TC1S2B0_01_06691S820E0465/TC1S2B0_01_06691S820E0465_pds3.lbl b/tests/pytests/data/TC1S2B0_01_06691S820E0465/TC1S2B0_01_06691S820E0465_pds3.lbl
new file mode 100644
index 0000000..db40dc7
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/TC1S2B0_01_06691S820E0465_pds3.lbl
@@ -0,0 +1,155 @@
+PDS_VERSION_ID = PDS3
+
+/* ** FILE FORMAT ** */
+RECORD_TYPE = UNDEFINED
+FILE_NAME = TC1S2B0_01_06691S820E0465.img
+PRODUCT_ID = TC1S2B0_01_06691S820E0465
+DATA_FORMAT = PDS
+
+/* ** POINTERS TO START BYTE OFFSET OF OBJECTS IN FILE ** */
+^IMAGE = 7599 <BYTES>
+
+/* ** GENERAL DATA DESCRIPTION PARAMETERS ** */
+SOFTWARE_NAME = "RGC_TC_s_Level2B0 (based on RGC_TC_MI
+ version 2.10.1)"
+SOFTWARE_VERSION = 1.0.0
+PROCESS_VERSION_ID = L2B
+PRODUCT_CREATION_TIME = 2013-06-10T09:23:07Z
+PROGRAM_START_TIME = 2013-06-10T09:23:01Z
+PRODUCER_ID = LISM
+PRODUCT_SET_ID = TC_s_Level2B0
+PRODUCT_VERSION_ID = 01
+REGISTERED_PRODUCT = Y
+ILLUMINATION_CONDITION = MORNING
+LEVEL2A_FILE_NAME = TC1S2A0_02TLF06691_001_0001.img
+SPICE_METAKERNEL_FILE_NAME = RGC_INF_TCv401IK_MIv200IK_SPv105IK_RISE100h-
+ _02_LongCK_D_V02_de421_110706.mk
+
+/* ** SCENE RELATED PARAMETERS ** */
+MISSION_NAME = SELENE
+SPACECRAFT_NAME = SELENE-M
+DATA_SET_ID = TC1_Level2B
+INSTRUMENT_NAME = "Terrain Camera 1"
+INSTRUMENT_ID = TC1
+MISSION_PHASE_NAME = Extended
+REVOLUTION_NUMBER = 6691
+STRIP_SEQUENCE_NUMBER = 1
+SCENE_SEQUENCE_NUMBER = 1
+UPPER_LEFT_DAYTIME_FLAG = Day
+UPPER_RIGHT_DAYTIME_FLAG = Day
+LOWER_LEFT_DAYTIME_FLAG = Day
+LOWER_RIGHT_DAYTIME_FLAG = Day
+TARGET_NAME = MOON
+OBSERVATION_MODE_ID = NORMAL
+SENSOR_DESCRIPTION = "Imagery type:Pushbroom.
+ ImageryMode:Mono,Stereo.
+ ExposureTimeMode:Long,Middle,Short.
+ CompressionMode:NonComp,DCT. Q-table:32
+ patterns. H-table:4 patterns.
+ SwathMode:F(Full),N(Nominal),H(Half). First
+ pixel number:1(F),297(N),1172(H)."
+SENSOR_DESCRIPTION2 = "Pixel size:7x7[micron^2](TC1/TC2).
+ Wavelength range:430-850[nm](TC1/TC2). A/D
+ rate:10[bit](TC1/TC2). Slant
+ angle:+/-15[degree] (from nadir to +x of
+ S/C)(TC1/TC2). Focal
+ length:72.45/72.63[mm](TC1/TC2). F
+ number:3.97/3.98(TC1/TC2)."
+DETECTOR_STATUS = (TC1:ON, TC2:OFF, MV:OFF, MN:OFF, SP:ON)
+EXPOSURE_MODE_ID = LONG
+LINE_EXPOSURE_DURATION = 6.500000 <msec>
+SPACECRAFT_CLOCK_START_COUNT = 922997380.1775 <sec>
+SPACECRAFT_CLOCK_STOP_COUNT = 922997410.4350 <sec>
+CORRECTED_SC_CLOCK_START_COUNT = 922997380.174174 <sec>
+CORRECTED_SC_CLOCK_STOP_COUNT = 922997410.431674 <sec>
+START_TIME = 2009-04-05T20:09:53.610804Z
+STOP_TIME = 2009-04-05T20:10:23.868304Z
+CORRECTED_START_TIME = 2009-04-05T20:09:53.607478Z
+CORRECTED_STOP_TIME = 2009-04-05T20:10:23.864978Z
+LINE_SAMPLING_INTERVAL = 6.500000 <msec>
+CORRECTED_SAMPLING_INTERVAL = 6.500000 <msec>
+UPPER_LEFT_LATITUDE = -81.172073 <deg>
+UPPER_LEFT_LONGITUDE = 44.883039 <deg>
+UPPER_RIGHT_LATITUDE = -81.200350 <deg>
+UPPER_RIGHT_LONGITUDE = 48.534829 <deg>
+LOWER_LEFT_LATITUDE = -82.764677 <deg>
+LOWER_LEFT_LONGITUDE = 43.996992 <deg>
+LOWER_RIGHT_LATITUDE = -82.797271 <deg>
+LOWER_RIGHT_LONGITUDE = 48.427901 <deg>
+LOCATION_FLAG = D
+ROLL_CANT = NO
+SCENE_CENTER_LATITUDE = -81.988555 <deg>
+SCENE_CENTER_LONGITUDE = 46.482457 <deg>
+INCIDENCE_ANGLE = 83.460 <deg>
+EMISSION_ANGLE = 15.557 <deg>
+PHASE_ANGLE = 68.069 <deg>
+SOLAR_AZIMUTH_ANGLE = 4.187 <deg>
+FOCAL_PLANE_TEMPERATURE = 19.73 <degC>
+TELESCOPE_TEMPERATURE = 19.91 <degC>
+SATELLITE_MOVING_DIRECTION = +1
+FIRST_SAMPLED_LINE_POSITION = UPPERMOST
+FIRST_DETECTOR_ELEMENT_POSITION = LEFT
+A_AXIS_RADIUS = 1737.400 <km>
+B_AXIS_RADIUS = 1737.400 <km>
+C_AXIS_RADIUS = 1737.400 <km>
+DEFECT_PIXEL_POSITION = N/A
+
+/* ** CAMERA RELATED PARAMETERS ** */
+SWATH_MODE_ID = FULL
+FIRST_PIXEL_NUMBER = 1
+LAST_PIXEL_NUMBER = 3208
+SPACECRAFT_ALTITUDE = 52.939 <km>
+SPACECRAFT_GROUND_SPEED = 1.603 <km/sec>
+TC1_TELESCOPE_TEMPERATURE = 20.06 <degC>
+TC2_TELESCOPE_TEMPERATURE = 19.72 <degC>
+DPU_TEMPERATURE = 14.60 <degC>
+TM_TEMPERATURE = 19.72 <degC>
+TM_RADIATOR_TEMPERATURE = 18.01 <degC>
+Q_TABLE_ID = N/A
+HUFFMAN_TABLE_ID = N/A
+DATA_COMPRESSION_PERCENT_MEAN = 100.0
+DATA_COMPRESSION_PERCENT_MAX = 100.0
+DATA_COMPRESSION_PERCENT_MIN = 100.0
+
+/* ** DESCRIPTION OF OBJECTS CONTAINED IN THE FILE ** */
+Object = IMAGE
+ ENCODING_TYPE = N/A
+ ENCODING_COMPRESSION_PERCENT = 100.0
+ NOMINAL_LINE_NUMBER = 4088
+ NOMINAL_OVERLAP_LINE_NUMBER = 568
+ OVERLAP_LINE_NUMBER = 568
+ LINES = 400
+ LINE_SAMPLES = 3208
+ SAMPLE_TYPE = MSB_INTEGER
+ SAMPLE_BITS = 16
+ IMAGE_VALUE_TYPE = RADIANCE
+ UNIT = W/m**2/micron/sr
+ SCALING_FACTOR = 1.30000e-02
+ OFFSET = 0.00000e+00
+ MIN_FOR_STATISTICAL_EVALUATION = 0
+ MAX_FOR_STATISTICAL_EVALUATION = 32767
+ SCENE_MAXIMUM_DN = 3612
+ SCENE_MINIMUM_DN = 0
+ SCENE_AVERAGE_DN = 401.1
+ SCENE_STDEV_DN = 420.5
+ SCENE_MODE_DN = 0
+ SHADOWED_AREA_MINIMUM = 0
+ SHADOWED_AREA_MAXIMUM = 0
+ SHADOWED_AREA_PERCENTAGE = 12
+ INVALID_TYPE = (SATURATION, MINUS, DUMMY_DEFECT, OTHER)
+ INVALID_VALUE = (-20000, -21000, -22000, -23000)
+ INVALID_PIXELS = (3314, 0, 0, 0)
+End_Object
+
+Object = PROCESSING_PARAMETERS
+ DARK_FILE_NAME = TC1_DRK_04740_07536_L_N_b05.csv
+ FLAT_FILE_NAME = TC1_FLT_04740_07536_N_N_b05.csv
+ EFFIC_FILE_NAME = TC1_EFF_PRFLT_N_N_v01.csv
+ NONLIN_FILE_NAME = TC1_NLT_PRFLT_N_N_v01.csv
+ RAD_CNV_COEF = 3.790009 <W/m**2/micron/sr>
+ L2A_DEAD_PIXEL_THRESHOLD = 30
+ L2A_SATURATION_THRESHOLD = 1023
+ DARK_VALID_MINIMUM = -5
+ RADIANCE_SATURATION_THRESHOLD = 425.971000 <W/m**2/micron/sr>
+End_Object
+End
diff --git a/tests/pytests/data/TC1S2B0_01_06691S820E0465/kaguyaTcAddendum006.ti b/tests/pytests/data/TC1S2B0_01_06691S820E0465/kaguyaTcAddendum006.ti
new file mode 100644
index 0000000..3e457a4
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/kaguyaTcAddendum006.ti
@@ -0,0 +1,58 @@
+\begintext
+The instrument addendum kernel for Kaguya TC camera.
+See 02_Haruyama.etal_EPS08_SeleneLISM_60040243.pdf
+
+history 2018-10-06 Jeannie Backer - Original version.
+history 2019-04-04 Stuart Sides - Changed to only use 131351 and 131371
+history 2019-04-05 Stuart Sides - Changed TRANS X/Y S/L to reflect +-X
+history 2019-04-11 Stuart Sides - Changed the sign on the Y coefficients
+ to negative to reflect that +Y is
+history 2019-04-12 Stuart Sides - Changed the sign on the X coefficients
+ to negative to match the MI coordinate
+ system
+history 2019-04-16 Stuart Sides - Changed to boresight values to be zero
+ based insted on one, and added the line
+ boresight
+
+\begintext
+
+
+\begindata
+ INS-131351_PIXEL_PITCH = 0.007
+ INS-131351_BORESIGHT_SAMPLE = 2047.5
+ INS-131351_BORESIGHT_LINE = 0.0
+ INS-131351_FOCAL_LENGTH = 72.45
+
+ INS-131371_PIXEL_PITCH = 0.007
+ INS-131371_BORESIGHT_SAMPLE = 2047.5
+ INS-131371_BORESIGHT_LINE = 0.0
+ INS-131371_FOCAL_LENGTH = 72.63
+
+\begintext
+Calculated using pixel pitch and 1/pixel pitch
+
+\begindata
+ INS-131351_TRANSX = ( 0.0, 0.0, -0.007 )
+ INS-131351_TRANSY = ( 0.0, -0.007, 0.0 )
+ INS-131351_ITRANSS = ( 0.0, 0.0, -142.857142857 )
+ INS-131351_ITRANSL = ( 0.0, -142.857142857, 0.0 )
+
+ INS-131371_TRANSX = ( 0.0, 0.0, -0.007 )
+ INS-131371_TRANSY = ( 0.0, -0.007, 0.0 )
+ INS-131371_ITRANSS = ( 0.0, 0.0, -142.857142857 )
+ INS-131371_ITRANSL = ( 0.0, -142.857142857, 0.0 )
+
+\begintext
+
+ OBSERVER/TARGET SWAPPING, STELLAR ABERRATION & LIGHT TIME CORRECTION:
+------------------------------------------------------------------------------
+
+\begindata
+ INS-131351_SWAP_OBSERVER_TARGET = 'TRUE'
+ INS-131351_LIGHTTIME_CORRECTION = 'LT+S'
+ INS-131351_LT_SURFACE_CORRECT = 'TRUE'
+
+ INS-131371_SWAP_OBSERVER_TARGET = 'TRUE'
+ INS-131371_LIGHTTIME_CORRECTION = 'LT+S'
+ INS-131371_LT_SURFACE_CORRECT = 'TRUE'
+
diff --git a/tests/pytests/data/TC1S2B0_01_06691S820E0465/naif0012.tls b/tests/pytests/data/TC1S2B0_01_06691S820E0465/naif0012.tls
new file mode 100644
index 0000000..e1afdee
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/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/TC1S2B0_01_06691S820E0465/pck00009.tpc b/tests/pytests/data/TC1S2B0_01_06691S820E0465/pck00009.tpc
new file mode 100644
index 0000000..bfadaab
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/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/TC1S2B0_01_06691S820E0465/sel_TC1S2B0_01_06691S820E0465.xsp b/tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_TC1S2B0_01_06691S820E0465.xsp
new file mode 100644
index 0000000..d3aafcb
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_TC1S2B0_01_06691S820E0465.xsp
@@ -0,0 +1,410 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
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+END_ARRAY 4 45
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; sel_TC1S2B0_01_06691S820E0465.bsp LOG FILE
+
+; Created 2019-08-27/16:00:51.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = tests/pytests/data/TC1S2B0_01_06691S820E0465/naif0012.tls
+
+SPK_KERNEL = sel_TC1S2B0_01_06691S820E0465.bsp
+ SOURCE_SPK_KERNEL = SEL_M_071020_090610_SGMH_02.BSP
+ INCLUDE_COMMENTS = NO
+ BODIES = -131
+ BEGIN_TIME = 2009 APR 05 20:02:23.989
+ END_TIME = 2009 APR 05 20:20:05.919
+ SOURCE_SPK_KERNEL = de421.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 301, 3, 10
+ BEGIN_TIME = 2009 APR 05 20:02:23.989
+ END_TIME = 2009 APR 05 20:20:05.919
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_m_TC1S2B0_01_06691S820E0465.xc b/tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_m_TC1S2B0_01_06691S820E0465.xc
new file mode 100644
index 0000000..d3c6987
--- /dev/null
+++ b/tests/pytests/data/TC1S2B0_01_06691S820E0465/sel_m_TC1S2B0_01_06691S820E0465.xc
@@ -0,0 +1,4322 @@
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+'3703D2920CCCCC^8'
+'3703D35A0CCCCC^8'
+'3703D4220CCCCC^8'
+'3703D4EA0CCCCC^8'
+'3703D105^8'
+'1^1'
+'215^3'
+END_ARRAY 1 4272
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+
+********************************************************************************
+
+ This CK file was created using CKSLICER Utility Ver. 1.3.0, October 28, 2011
+ linked against SPICE Toolkit Ver. N0066.
+
+ This file contains a subset of the pointing data between:
+ UTC 2009 APR 05 20:03:30.174
+ and
+ UTC 2009 APR 05 20:21:12.104
+ for all applicable segments from the source CK file:
+ SEL_M_ALL_D_V02.BC
+
+ LSK file:
+ tests/pytests/data/TC1S2B0_01_06691S820E0465/naif0012.tls
+ and SCLK file(s):
+ tests/pytests/data/TC1S2B0_01_06691S820E0465/SEL_M_V01.TSC
+ were used by CKSLICER to support required time conversions.
+
+ This file was created on 2019-08-27 16:22:07.
+
+ Text below is the contents of the comment area of the source CK file.
+
+********************************************************************************
+
+
+
+********************************************************************************
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/test_kaguya_drivers.py b/tests/pytests/test_kaguya_drivers.py
index 9465ab3..2f51af3 100644
--- a/tests/pytests/test_kaguya_drivers.py
+++ b/tests/pytests/test_kaguya_drivers.py
@@ -1,119 +1,169 @@
import pytest
+import os
import numpy as np
-import pvl
-
-import ale
-from ale.drivers import selene_drivers
+import datetime
+import spiceypy as spice
+from importlib import reload
+import json
from unittest.mock import PropertyMock, patch
-# 'Mock' the spice module where it is imported
-from conftest import SimpleSpice, get_mockkernels
+from conftest import get_image_label, get_image_kernels, convert_kernels, compare_dicts
-simplespice = SimpleSpice()
-selene_drivers.spice = simplespice
+import ale
from ale.drivers.selene_drivers import KaguyaTcPds3NaifSpiceDriver
-KaguyaTcPds3NaifSpiceDriver.metakernel = get_mockkernels
+@pytest.fixture()
+def test_kernels():
+ kernels = get_image_kernels('TC1S2B0_01_06691S820E0465')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
-@pytest.fixture
-def driver():
- return KaguyaTcPds3NaifSpiceDriver("")
+@pytest.fixture(params=["Pds3NaifDriver"])
+def driver(request):
+ if request.param == "Pds3NaifDriver":
+ label = get_image_label("TC1S2B0_01_06691S820E0465", "pds3")
+ return KaguyaTcPds3NaifSpiceDriver(label)
def test_short_mission_name(driver):
- assert driver.short_mission_name=='selene'
+ assert driver.short_mission_name == 'selene'
+
+def test_utc_start_time(driver):
+ assert driver.utc_start_time == datetime.datetime(2009, 4, 5, 20, 9, 53, 607478, tzinfo=datetime.timezone.utc)
+
+def test_utc_stop_time(driver):
+ assert driver.utc_stop_time == datetime.datetime(2009, 4, 5, 20, 10, 23, 864978, tzinfo=datetime.timezone.utc)
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
def test_instrument_id(driver):
- with patch.dict(driver.label, {'SWATH_MODE_ID':'NOMINAL', 'PRODUCT_SET_ID':'TC_w_Level2B0' }) as f:
- assert driver.instrument_id == 'LISM_123_WTN'
+ assert driver.instrument_id == 'LISM_TC1_STF'
+
+def test_sensor_frame_id(driver):
+ with patch('ale.drivers.selene_drivers.spice.namfrm', return_value=12345) as namfrm:
+ assert driver.sensor_frame_id == 12345
+ namfrm.assert_called_with('LISM_TC1_HEAD')
+
+def test_instrument_host_name(driver):
+ assert driver.instrument_host_name == 'SELENE-M'
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
def test_ikid(driver):
- assert driver.ikid == -12345
+ with patch('ale.drivers.selene_drivers.spice.bods2c', return_value=12345) as bods2c:
+ assert driver.ikid == 12345
+ bods2c.assert_called_with('LISM_TC1')
-def test_spacecraft_clock_stop_count(driver):
- with patch.dict(driver.label, {'CORRECTED_SC_CLOCK_STOP_COUNT':
- pvl._collections.Units(value=105, units='<sec>')}) as f:
- assert driver.spacecraft_clock_stop_count == 105
+def test_spacecraft_name(driver):
+ assert driver.spacecraft_name == 'SELENE'
def test_spacecraft_clock_start_count(driver):
- with patch.dict(driver.label, {'CORRECTED_SC_CLOCK_START_COUNT':
- pvl._collections.Units(value=501, units='<sec>')}) as f:
- assert driver.spacecraft_clock_start_count == 501
+ assert driver.spacecraft_clock_start_count == 922997380.174174
-@patch('ale.base.data_naif.NaifSpice.spacecraft_id', -131)
-def test_ephemeris_stop_time(driver):
- with patch.dict(driver.label, {'CORRECTED_SC_CLOCK_STOP_COUNT':
- pvl._collections.Units(value=501, units='<sec>')}) as f:
- assert driver.ephemeris_stop_time == 0.1
+def test_spacecraft_clock_stop_count(driver):
+ assert driver.spacecraft_clock_stop_count == 922997410.431674
-@patch('ale.base.data_naif.NaifSpice.spacecraft_id', -131)
def test_ephemeris_start_time(driver):
- with patch.dict(driver.label, {'CORRECTED_SC_CLOCK_START_COUNT':
- pvl._collections.Units(value=501, units='<sec>')}) as f:
- assert driver.ephemeris_start_time == 0.1
+ with patch('ale.drivers.selene_drivers.spice.sct2e', return_value=12345) as sct2e, \
+ patch('ale.drivers.selene_drivers.spice.bods2c', return_value=-12345) as bods2c:
+ assert driver.ephemeris_start_time == 12345
+ sct2e.assert_called_with(-12345, 922997380.174174)
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
def test_detector_center_line(driver):
- assert driver.detector_center_line == 0.5
+ with patch('ale.drivers.selene_drivers.spice.gdpool', return_value=[54321, 12345]) as gdpool, \
+ patch('ale.drivers.selene_drivers.spice.bods2c', return_value=-12345) as bods2c:
+ assert driver.detector_center_line == 12344.5
+ gdpool.assert_called_with('INS-12345_CENTER', 0, 2)
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
def test_detector_center_sample(driver):
- assert driver.detector_center_sample == 0.5
-
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
-@patch('ale.base.label_pds3.Pds3Label.target_name', 'MOON')
-def test_sensor_orientation(driver):
- with patch('ale.base.type_sensor.LineScanner.ephemeris_time', new_callable=PropertyMock) as mock_time:
- mock_time.return_value = np.linspace(100,200,2)
- assert driver._sensor_orientation == [[2,3,4,1], [2,3,4,1]]
+ with patch('ale.drivers.selene_drivers.spice.gdpool', return_value=[54321, 12345]) as gdpool, \
+ patch('ale.drivers.selene_drivers.spice.bods2c', return_value=-12345) as bods2c:
+ assert driver.detector_center_sample == 54320.5
+ gdpool.assert_called_with('INS-12345_CENTER', 0, 2)
def test_reference_frame(driver):
- with patch('ale.base.label_pds3.Pds3Label.target_name', new_callable=PropertyMock) as mock_target_name:
- mock_target_name.return_value = 'MOOn'
- assert driver.reference_frame == 'MOON_ME'
- mock_target_name.return_value = 'sun'
- assert driver.reference_frame == 'NO TARGET'
+ assert driver.reference_frame == 'MOON_ME'
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
def test_focal2pixel_samples(driver):
- assert driver.focal2pixel_samples == [0, 0, -1]
+ with patch('ale.drivers.selene_drivers.spice.gdpool', return_value=[2]) as gdpool, \
+ patch('ale.drivers.selene_drivers.spice.bods2c', return_value=-12345) as bods2c:
+ assert driver.focal2pixel_samples == [0, 0, -1/2]
+ gdpool.assert_called_with('INS-12345_PIXEL_SIZE', 0, 1)
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
def test_focal2pixel_lines(driver):
- assert driver.focal2pixel_lines == [0, -1, 0]
-
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
-def test_odkx(driver):
- assert driver._odkx == [1, 1, 1, 1]
-
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
-def test_odky(driver):
- assert driver._odky == [1, 1, 1, 1]
-
-def test_line_exposure_duration(driver):
- with patch.dict(driver.label, {'CORRECTED_SAMPLING_INTERVAL':
- pvl._collections.Units(value=1000, units='<msec>')}) as f:
- assert driver.line_exposure_duration == 1
- with patch.dict(driver.label, {'CORRECTED_SAMPLING_INTERVAL':
- [pvl._collections.Units(value=10000, units='<msec>'), 1]}) as f:
- assert driver.line_exposure_duration == 10
-
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
-def test_focal_length(driver):
- assert driver.focal_length == 1
-
-@patch('ale.base.label_pds3.Pds3Label.instrument_id', 123)
-def test_usgscsm_distortion_model(driver):
- distortion_model = driver.usgscsm_distortion_model
- assert distortion_model['kaguyatc']['x'] == [1, 1, 1, 1]
- assert distortion_model['kaguyatc']['y'] == [1, 1, 1, 1]
-
-def test_detector_start_sample(driver):
- with patch.dict(driver.label, {'FIRST_PIXEL_NUMBER': 123}) as f:
- assert driver.detector_start_sample == 123
-
-def test_sensor_model_version(driver):
- assert driver.sensor_model_version == 1
+ with patch('ale.drivers.selene_drivers.spice.gdpool', return_value=[2]) as gdpool, \
+ patch('ale.drivers.selene_drivers.spice.bods2c', return_value=-12345) as bods2c:
+ assert driver.focal2pixel_lines == [0, -1/2, 0]
+ gdpool.assert_called_with('INS-12345_PIXEL_SIZE', 0, 1)
+
+def test_load(test_kernels):
+ isd = {
+ 'radii': {
+ 'semimajor': 1737.4,
+ 'semiminor': 1737.4,
+ 'unit': 'km'},
+ 'sensor_position': {
+ 'positions': np.array([[ 195493.28614388, 211984.05137213, -1766966.32185819],
+ [ 194937.01104181, 211343.39987087, -1767100.47633473],
+ [ 194380.68920347, 210702.70097122, -1767234.22276254],
+ [ 193824.32093681, 210061.95495794, -1767367.56104995],
+ [ 193267.90484827, 209421.16305764, -1767500.49120063],
+ [ 192711.44397634, 208780.32318594, -1767633.01318365]]),
+ 'velocities': np.array([[-1069.71225785, -1231.97438089, -258.37880523],
+ [-1069.80205939, -1232.06556741, -257.5939851 ],
+ [-1069.89161639, -1232.15647191, -256.80910187],
+ [-1069.98092881, -1232.24709434, -256.02415587],
+ [-1070.06999666, -1232.33743471, -255.2391471 ],
+ [-1070.15881991, -1232.42749298, -254.4540759 ]]),
+ 'unit': 'm'},
+ 'sun_position': {
+ 'positions': np.array([[9.50347435e+10, 1.15913462e+11, 3.78747288e+09]]),
+ 'velocities': np.array([[ 285730.03370329, -232701.52529823, 592.79276721]]),
+ 'unit': 'm'},
+ 'sensor_orientation': {
+ 'quaternions': np.array([[-0.19095485, -0.08452708, 0.88748467, -0.41080698],
+ [-0.19073945, -0.08442789, 0.88753312, -0.41082276],
+ [-0.19052404, -0.08432871, 0.88758153, -0.41083852],
+ [-0.19030862, -0.08422952, 0.88762988, -0.41085426],
+ [-0.19009352, -0.08412972, 0.88767854, -0.41086914],
+ [-0.18987892, -0.08402899, 0.88772773, -0.41088271]])},
+ 'detector_sample_summing': 1,
+ 'detector_line_summing': 1,
+ 'focal_length_model': {
+ 'focal_length': 72.45},
+ 'detector_center': {
+ 'line': 0.5,
+ 'sample': 2048.0},
+ 'starting_detector_line': 0,
+ 'starting_detector_sample': 1,
+ 'focal2pixel_lines': [0, -142.85714285714286, 0],
+ 'focal2pixel_samples': [0, 0, -142.85714285714286],
+ 'optical_distortion': {
+ 'kaguyatc': {
+ 'x': [-0.0009649900000000001, 0.00098441, 8.5773e-06, -3.7438e-06],
+ 'y': [-0.0013796, 1.3502e-05, 2.7251e-06, -6.193800000000001e-06]}},
+ 'image_lines': 400,
+ 'image_samples': 3208,
+ 'name_platform': 'SELENE-M',
+ 'name_sensor': 'Terrain Camera 1',
+ 'reference_height': {
+ 'maxheight': 1000,
+ 'minheight': -1000,
+ 'unit': 'm'},
+ 'name_model': 'USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL',
+ 'interpolation_method': 'lagrange',
+ 'line_scan_rate': [[0.5, -1.300000011920929, 0.006500000000000001]],
+ 'starting_ephemeris_time': 292234259.82293594,
+ 'center_ephemeris_time': 292234261.12293595,
+ 't0_ephemeris': -1.300000011920929,
+ 'dt_ephemeris': 0.5200000047683716,
+ 't0_quaternion': -1.300000011920929,
+ 'dt_quaternion': 0.5200000047683716}
+
+ label_file = get_image_label('TC1S2B0_01_06691S820E0465')
+
+ with patch('ale.drivers.selene_drivers.KaguyaTcPds3NaifSpiceDriver.reference_frame', \
+ new_callable=PropertyMock) as mock_reference_frame:
+ mock_reference_frame.return_value = 'IAU_MOON'
+ usgscsm_isd = ale.load(label_file, props={'kernels': test_kernels}, formatter='usgscsm')
+
+ assert compare_dicts(usgscsm_isd, isd) == []
diff --git a/tests/pytests/test_load.py b/tests/pytests/test_load.py
index 57f3aca..e054753 100644
--- a/tests/pytests/test_load.py
+++ b/tests/pytests/test_load.py
@@ -1,6 +1,7 @@
import pytest
from importlib import reload
import json
+import os
import ale
from ale import util
@@ -10,13 +11,21 @@ from ale.base.data_isis import IsisSpice
from conftest import get_image_label, get_image_kernels, convert_kernels
+@pytest.fixture()
+def mess_kernels():
+ kernels = get_image_kernels('EN1072174528M')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
def test_priority(tmpdir, monkeypatch):
drivers = [type('FooNaifSpice', (NaifSpice,), {}), type('BarIsisSpice', (IsisSpice,), {}), type('BazNaifSpice', (NaifSpice,), {}), type('FubarIsisSpice', (IsisSpice,), {})]
sorted_drivers = sort_drivers(drivers)
assert all([IsisSpice in klass.__bases__ for klass in sorted_drivers[:2]])
-def test_mess_load():
- updated_kernels, _ = convert_kernels(get_image_kernels('EN1072174528M'))
+def test_mess_load(mess_kernels):
+ updated_kernels = mess_kernels
label_file = get_image_label('EN1072174528M')
usgscsm_isd_str = ale.loads(label_file, props={'kernels': updated_kernels}, formatter='usgscsm')
@@ -43,13 +52,13 @@ def test_load_invalid_spice_root(monkeypatch):
ale.load(label_file)
-def test_load_mes_from_metakernels(tmpdir, monkeypatch):
+def test_load_mes_from_metakernels(tmpdir, monkeypatch, mess_kernels):
monkeypatch.setenv('ALESPICEROOT', str(tmpdir))
# reload module to repopulate ale.spice_root
reload(ale)
- updated_kernels, _ = convert_kernels(get_image_kernels('EN1072174528M'))
+ updated_kernels = mess_kernels
label_file = get_image_label('EN1072174528M')
tmpdir.mkdir('mes')
with open(tmpdir.join('mes', 'mes_2015_v1.tm'), 'w+') as mk_file:
@@ -64,13 +73,13 @@ def test_load_mes_from_metakernels(tmpdir, monkeypatch):
assert usgscsm_isd_obj['name_model'] == 'USGS_ASTRO_FRAME_SENSOR_MODEL'
-def test_load_mes_with_no_metakernels(tmpdir, monkeypatch):
+def test_load_mes_with_no_metakernels(tmpdir, monkeypatch, mess_kernels):
monkeypatch.setenv('ALESPICEROOT', str(tmpdir))
# reload module to repopulate ale.spice_root
reload(ale)
- updated_kernels, _ = convert_kernels(get_image_kernels('EN1072174528M'))
+ updated_kernels = mess_kernels
label_file = get_image_label('EN1072174528M')
tmpdir.mkdir('mes')
diff --git a/tests/pytests/test_mdis_drivers.py b/tests/pytests/test_mdis_drivers.py
index 9a88eab..7e74df4 100644
--- a/tests/pytests/test_mdis_drivers.py
+++ b/tests/pytests/test_mdis_drivers.py
@@ -1,7 +1,5 @@
import pytest
-import pvl
import os
-import subprocess
import numpy as np
import spiceypy as spice
from importlib import reload
@@ -23,7 +21,7 @@ def test_kernels():
for kern in binary_kernels:
os.remove(kern)
-@pytest.fixture(scope="module", params=["Pds3NaifDriver", "IsisNaifDriver"])
+@pytest.fixture(params=["Pds3NaifDriver", "IsisNaifDriver"])
def driver(request):
if request.param == "IsisNaifDriver":
label = get_image_label("EN1072174528M", "isis3")
@@ -166,7 +164,7 @@ def test_frame_chain(driver):
def test_sun_position(driver):
position, velocity, time = driver.sun_position
image_et = spice.scs2e(-236, '2/0072174528:989000') + 0.0005
- expected_state, _ = spice.spkez(10, image_et, 'IAU_MERCURY', 'LT+S', 199)
+ expected_state, _ = spice.spkez(10, image_et, 'IAU_MERCURY', 'NONE', 199)
expected_position = 1000 * np.asarray(expected_state[:3])
expected_velocity = 1000 * np.asarray(expected_state[3:])
np.testing.assert_allclose(position,
--
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