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Commit a1748cf2 authored by paarongiroux's avatar paarongiroux Committed by Jesse Mapel
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Updated Dawn Test (#265)

* updated dawn test

* used new kernel slice to reduce size of kernels

* re-sliced kernels to get load test passing

* added sliced kernels

* added more sliced kerenels

* resliced kernels
parent 23a0c847
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KPL/SCLK
DAWN SCLK File
===========================================================================
This file is a SPICE spacecraft clock (SCLK) kernel containing
information required for DAWN spacecraft on-board clock to UTC
conversion.
Production/History of this SCLK file
--------------------------------------------------------
This file was generated by the NAIF utility program MAKCLK, version
3.5.2, from the most recent DAWN spacecraft SCLKvSCET file (see
corresponding sections of these comments for a copy of the source
SCLKvSCET file and MAKCLK setup file).
Usage
--------------------------------------------------------
This file must be loaded into the user's program by a call to the
FURNSH subroutine
CALL FURNSH( 'this_file_name' )
in order to use the SPICELIB SCLK family of subroutines to convert
DAWN spacecraft on-board clock to ET and vice versa.
SCLK Format
--------------------------------------------------------
The on-board clock, the conversion for which is provided by this SCLK
file, consists of two fields:
SSSSSSSSSS:FFF
where:
SSSSSSSSSS -- count of on-board seconds
FFF -- count of fractions of a second with one fraction
being 1/256 of a second; normally this field value
is within 0..255 range.
References
--------------------------------------------------------
1. SCLK Required Reading Document
2. MAKCLK User's Guide Document
3. SFOC SCLKvSCET SIS Document
Inquiries
--------------------------------------------------------
If you have any questions regarding this file contact NAIF at JPL
Charles H. Acton, Jr
(818) 354-3869
Chuck.Acton@jpl.nasa.gov
Boris V. Semenov
(818) 354-8136
Boris.Semenov@jpl.nasa.gov
Source SCLKvSCET File
--------------------------------------------------------
CCSD3ZS00001$$sclk$$NJPL3KS0L015$$scet$$
MISSION_NAME=DAWN;
SPACECRAFT_NAME=DAWN;
DATA_SET_ID=SCLK_SCET;
FILE_NAME=DAWN_203_SCLKSCET.00091;
PRODUCT_CREATION_TIME=2018-270T19:25:38.266;
PRODUCT_VERSION_ID=00091;
PRODUCER_ID=DSMS_TIME_SERVICES;
APPLICABLE_START_TIME=2000-001T11:58:55.816;
APPLICABLE_STOP_TIME=2019-038T23:42:07.704;
MISSION_ENVIRONMENT=ops;
MISSION_ID=30;
SPACECRAFT_ID=203;
CCSD3RE00000$$scet$$NJPL3IS00613$$data$$
*____SCLK0_____ ________SCET0________ _DUT__ __SCLKRATE__
0.000 2000-001T11:58:55.816 64.184 1.000000000
189345665.000 2006-001T00:00:00.816 64.184 0.000010000
189345666.000 2006-001T00:00:00.817 65.184 1.000000000
244538000.000 2007-274T19:12:14.817 65.184 1.006101025
244539000.000 2007-274T19:29:00.918 65.184 1.000007143
244710000.000 2007-276T18:59:02.139 65.184 1.000010166
244711000.000 2007-276T19:15:42.150 65.184 1.000007152
245501801.000 2007-285T22:55:48.806 65.184 1.000033235
245502801.000 2007-285T23:12:28.839 65.184 0.998999041
245513651.000 2007-286T02:13:07.979 65.184 0.999015999
245514651.000 2007-286T02:29:46.995 65.184 1.000000001
249480000.000 2007-331T23:58:55.999 65.184 0.999158298
249481000.000 2007-332T00:15:35.157 65.184 1.000000089
251201000.000 2007-351T22:02:15.310 65.184 0.999909591
251202000.000 2007-351T22:18:55.220 65.184 1.000000046
253726000.000 2008-016T03:25:35.336 65.184 1.000108749
253727000.000 2008-016T03:42:15.445 65.184 1.000000089
256097000.000 2008-043T14:02:15.656 65.184 1.000049672
256098000.000 2008-043T14:18:55.706 65.184 1.000000113
256990800.000 2008-053T22:18:55.807 65.184 0.999863733
256991800.000 2008-053T22:35:35.671 65.184 0.999045412
256992650.000 2008-053T22:49:44.860 65.184 0.998760856
256992750.000 2008-053T22:51:24.736 65.184 1.000000009
283350000.000 2008-359T00:18:54.973 65.184 1.000103304
283351000.000 2008-359T00:35:35.077 65.184 1.000000017
284040065.000 2009-001T00:00:00.088 65.184 0.000010000
284040066.000 2009-001T00:00:00.089 66.184 1.000000017
284117000.000 2009-001T21:22:14.090 66.184 0.999868379
284118000.000 2009-001T21:38:53.959 66.184 0.999999981
298300000.000 2009-166T01:05:33.690 66.184 1.000061283
298301000.000 2009-166T01:22:13.751 66.184 1.000000048
305000000.000 2009-243T14:12:14.073 66.184 0.999996197
305001000.000 2009-243T14:28:54.069 66.184 1.000000058
312850000.000 2009-334T10:45:34.524 66.184 1.000002922
312851000.000 2009-334T11:02:14.527 66.184 1.000000003
313250000.000 2009-339T01:52:14.528 66.184 0.999996604
313251000.000 2009-339T02:08:54.525 66.184 1.000000068
316200000.000 2010-008T05:18:54.726 66.184 1.000007841
316201000.000 2010-008T05:35:34.733 66.184 1.000000110
320100000.000 2010-053T08:38:55.162 66.184 1.000001320
320101000.000 2010-053T08:55:35.163 66.184 1.000000120
322563668.000 2010-081T21:00:03.459 66.184 0.998988697
322564668.000 2010-081T21:16:42.447 66.184 0.998995216
322565041.000 2010-081T21:22:55.072 66.184 1.000005173
322566041.000 2010-081T21:39:35.077 66.184 1.000000475
322600000.000 2010-082T07:05:34.093 66.184 0.999987228
322601000.000 2010-082T07:22:14.080 66.184 1.000000040
330000000.000 2010-167T22:38:54.376 66.184 1.000004084
330001000.000 2010-167T22:55:34.380 66.184 0.999999933
330700000.000 2010-176T01:05:34.333 66.184 1.000001626
330701000.000 2010-176T01:22:14.335 66.184 1.000000020
345200000.000 2010-343T20:52:14.625 66.184 1.000013470
345201000.000 2010-343T21:08:54.638 66.184 0.999999936
351000000.000 2011-045T23:58:54.267 66.184 0.999984584
351001000.000 2011-046T00:15:34.251 66.184 0.999999939
354510000.000 2011-086T14:58:54.037 66.184 1.000016119
354511000.000 2011-086T15:15:34.053 66.184 0.999999950
363003503.000 2011-184T22:17:16.628 66.184 1.000034882
363004503.000 2011-184T22:33:56.663 66.184 1.000000019
364302689.000 2011-199T23:10:22.688 66.184 1.000027169
364303689.000 2011-199T23:27:02.715 66.184 0.999999951
365098745.000 2011-209T04:17:58.676 66.184 0.999999455
365099745.000 2011-209T04:34:38.675 66.184 1.000000025
365597963.000 2011-214T22:58:16.688 66.184 0.999996218
365598963.000 2011-214T23:14:56.684 66.184 0.999999955
366103895.000 2011-220T19:30:28.661 66.184 1.000399965
366104895.000 2011-220T19:47:09.061 66.184 0.999999957
368192017.000 2011-244T23:32:30.971 66.184 1.000001152
368193017.000 2011-244T23:49:10.972 66.184 0.999999965
370469447.000 2011-271T08:09:40.892 66.184 1.000000367
370470447.000 2011-271T08:26:20.893 66.184 0.999999974
372177293.000 2011-291T02:33:46.849 66.184 1.000000430
372178293.000 2011-291T02:50:26.849 66.184 0.999999970
373710776.000 2011-308T20:31:49.803 66.184 0.999995066
373711776.000 2011-308T20:48:29.798 66.184 0.999999962
375566583.000 2011-330T08:01:56.728 66.184 1.000001256
375567583.000 2011-330T08:18:36.729 66.184 0.999999964
380261967.000 2012-019T16:18:20.560 66.184 1.000007313
380262967.000 2012-019T16:35:00.567 66.184 0.999999975
382547079.000 2012-046T03:03:32.510 66.184 1.000004978
382548079.000 2012-046T03:20:12.515 66.184 0.999999970
382831366.000 2012-049T10:01:39.507 66.184 0.999999884
382832366.000 2012-049T10:18:19.506 66.184 0.999999970
386733873.000 2012-094T14:03:26.390 66.184 1.000001124
386734873.000 2012-094T14:20:06.391 66.184 0.999999965
388743414.000 2012-117T20:15:47.321 66.184 1.000001119
388744414.000 2012-117T20:32:27.322 66.184 0.999999963
393247117.000 2012-169T23:17:30.155 66.184 1.000000821
393248117.000 2012-169T23:34:10.156 66.184 0.999999971
394372867.000 2012-183T00:00:00.123 66.184 0.001000000
394372868.000 2012-183T00:00:00.124 67.184 0.999999971
395935394.000 2012-201T02:02:06.079 67.184 0.999997719
395936394.000 2012-201T02:18:46.076 67.184 0.999999877
396458801.000 2012-207T03:25:33.012 67.184 1.000004553
396459801.000 2012-207T03:42:13.016 67.184 0.999999947
396458802.000 2012-207T03:25:34.016 67.184 0.999997868
396459802.000 2012-207T03:42:14.014 67.184 0.999999958
399831062.000 2012-246T04:09:53.872 67.184 1.000002964
399832062.000 2012-246T04:26:33.875 67.184 0.999999955
403589662.000 2012-289T16:13:13.706 67.184 0.999987958
403590662.000 2012-289T16:29:53.694 67.184 1.001005661
403590670.000 2012-289T16:30:01.702 67.184 1.001027377
403591670.000 2012-289T16:46:42.730 67.184 0.999999952
404793615.000 2012-303T14:39:07.672 67.184 1.000035139
404794615.000 2012-303T14:55:47.707 67.184 0.999999985
407168114.000 2012-331T02:14:06.673 67.184 1.000004694
407169114.000 2012-331T02:30:46.677 67.184 0.999999926
410795207.000 2013-007T01:45:39.408 67.184 1.000003090
410796207.000 2013-007T02:02:19.411 67.184 0.999999873
413148390.000 2013-034T07:25:22.112 67.184 0.999999480
413149390.000 2013-034T07:42:02.112 67.184 0.999999880
417789946.000 2013-088T00:44:37.555 67.184 1.000014166
417790946.000 2013-088T01:01:17.569 67.184 1.000999128
417791014.000 2013-088T01:02:25.637 67.184 1.000993452
417792014.000 2013-088T01:19:06.630 67.184 0.999999880
417792050.000 2013-088T01:19:42.630 67.184 0.999999514
417793050.000 2013-088T01:36:22.630 67.184 1.000000050
420450171.000 2013-118T19:41:43.763 67.184 0.999996596
420451171.000 2013-118T19:58:23.759 67.184 1.000000055
425387236.000 2013-175T23:06:09.030 67.184 0.999999476
425388236.000 2013-175T23:22:49.030 67.184 1.000000175
427825000.000 2013-204T04:15:33.456 67.184 1.000000911
427826000.000 2013-204T04:32:13.457 67.184 1.000000179
432650675.000 2013-260T00:43:29.321 67.184 0.999984498
432651675.000 2013-260T01:00:09.305 67.184 0.999002693
432653540.000 2013-260T01:31:12.445 67.184 0.999004269
432654540.000 2013-260T01:47:51.449 67.184 1.000000179
437467056.000 2013-315T18:36:28.310 67.184 0.999997839
437468056.000 2013-315T18:53:08.308 67.184 1.000000043
437636875.000 2013-317T17:46:47.315 67.184 0.999998904
437637875.000 2013-317T18:03:27.314 67.184 1.000000057
439397277.000 2013-338T02:46:49.414 67.184 0.999999870
439398277.000 2013-338T03:03:29.414 67.184 1.000000044
439942407.000 2013-344T10:12:19.438 67.184 1.000003201
439943407.000 2013-344T10:28:59.441 67.184 1.000000179
447144330.000 2014-062T18:44:23.730 67.184 1.000004998
447145330.000 2014-062T19:01:03.735 67.184 0.998999316
447146200.000 2014-062T19:15:32.864 67.184 0.998954949
447147200.000 2014-062T19:32:11.819 67.184 1.000000012
447150674.000 2014-062T20:30:05.819 67.184 0.999994818
447151674.000 2014-062T20:46:45.814 67.184 1.000000007
449540958.000 2014-090T12:28:09.831 67.184 0.999998809
449541958.000 2014-090T12:44:49.830 67.184 1.000000046
454418290.000 2014-146T23:17:02.054 67.184 1.000001622
454419290.000 2014-146T23:33:42.056 67.184 0.999999943
456785475.000 2014-174T08:50:06.921 67.184 0.999997231
456786475.000 2014-174T09:06:46.918 67.184 1.000000035
459299072.000 2014-203T11:03:24.006 67.184 0.999997491
459300072.000 2014-203T11:20:04.003 67.184 0.999999942
461579147.000 2014-229T20:24:38.871 67.184 0.999999225
461580147.000 2014-229T20:41:18.870 67.184 0.999999950
464042321.000 2014-258T08:37:32.747 67.184 0.999982002
464043321.000 2014-258T08:54:12.729 67.184 0.998999156
464043323.000 2014-258T08:54:14.727 67.184 0.999016267
464044323.000 2014-258T09:10:53.743 67.184 1.000000035
464074136.000 2014-258T17:27:46.744 67.184 1.000000001
464075136.000 2014-258T17:44:26.744 67.184 1.000000119
466486049.000 2014-286T15:26:20.031 67.184 0.999998207
466487049.000 2014-286T15:43:00.029 67.184 1.000998881
466488040.000 2014-286T15:59:32.019 67.184 1.001004303
466489040.000 2014-286T16:16:13.023 67.184 1.000000119
470734841.000 2014-335T19:39:34.528 67.184 0.999991158
470735841.000 2014-335T19:56:14.519 67.184 1.000000113
472894550.000 2014-360T19:34:43.763 67.184 1.000001546
472895550.000 2014-360T19:51:23.765 67.184 1.000000040
475520629.000 2015-026T05:02:42.870 67.184 0.999994304
475521629.000 2015-026T05:19:22.864 67.184 0.999014960
475521641.000 2015-026T05:19:34.852 67.184 0.999004631
475522641.000 2015-026T05:36:13.857 67.184 1.000000040
478542692.000 2015-061T04:30:24.978 67.184 0.999999679
478543692.000 2015-061T04:47:04.977 67.184 0.999999976
478586024.000 2015-061T16:32:36.976 67.184 1.000007092
478587024.000 2015-061T16:49:16.983 67.184 1.000000042
481375766.000 2015-093T23:28:19.100 67.184 1.000000166
481376766.000 2015-093T23:44:59.100 67.184 1.000000038
483046971.000 2015-113T07:41:44.163 67.184 1.000003860
483047971.000 2015-113T07:58:24.167 67.184 1.000000043
486616634.000 2015-154T15:16:07.320 67.184 0.999995347
486617634.000 2015-154T15:32:47.316 67.184 1.000000049
488980867.000 2015-182T00:00:00.432 67.184 0.001000000
488980868.000 2015-182T00:00:00.433 68.184 1.000000049
490149181.000 2015-195T12:31:53.490 68.184 0.999993443
490150181.000 2015-195T12:48:33.484 68.184 1.000000091
490359500.000 2015-197T22:57:12.503 68.184 1.000000067
490360500.000 2015-197T23:13:52.503 68.184 1.000000100
492729000.000 2015-225T09:08:52.740 68.184 0.999998821
492730000.000 2015-225T09:25:32.739 68.184 1.000000038
493006500.000 2015-228T14:13:52.750 68.184 1.000031572
493007500.000 2015-228T14:30:32.781 68.184 0.999000031
493007520.000 2015-228T14:30:52.761 68.184 0.999005712
493008520.000 2015-228T14:47:31.767 68.184 0.999999955
493521208.000 2015-234T13:12:19.744 68.184 0.999998904
493522208.000 2015-234T13:28:59.743 68.184 0.999999951
498923349.000 2015-297T01:48:00.478 68.184 1.000006901
498924349.000 2015-297T02:04:40.485 68.184 1.000000007
502827339.000 2015-342T06:14:30.512 68.184 0.999989274
502828339.000 2015-342T06:31:10.502 68.184 0.999999982
503095945.000 2015-345T08:51:16.497 68.184 0.999998308
503096945.000 2015-345T09:07:56.495 68.184 0.999999958
504002507.000 2015-355T20:40:38.457 68.184 0.999999595
504003507.000 2015-355T20:57:18.457 68.184 0.999999954
505174338.000 2016-004T10:11:09.403 68.184 1.000001430
505175338.000 2016-004T10:27:49.405 68.184 0.999999950
521621125.000 2016-194T18:44:15.583 68.184 1.000009038
521622125.000 2016-194T19:00:55.592 68.184 1.000993976
521622382.000 2016-194T19:05:12.847 68.184 1.000975686
521623382.000 2016-194T19:21:53.823 68.184 0.999999950
521624383.000 2016-194T19:38:34.823 68.184 1.000004113
521625383.000 2016-194T19:55:14.827 68.184 1.000000035
526120965.000 2016-246T20:41:36.984 68.184 1.000002711
526121965.000 2016-246T20:58:16.987 68.184 1.000000099
526120966.000 2016-246T20:41:37.987 68.184 0.999997995
526121966.000 2016-246T20:58:17.985 68.184 1.000000103
528975910.000 2016-279T21:44:02.279 68.184 1.000002764
528976910.000 2016-279T22:00:42.282 68.184 1.000000034
531574692.000 2016-309T23:37:04.370 68.184 1.000005309
531575692.000 2016-309T23:53:44.376 68.184 1.000000111
534276216.000 2016-341T06:02:28.676 68.184 0.999999100
534277216.000 2016-341T06:19:08.675 68.184 1.000000037
534579150.000 2016-344T18:11:22.686 68.184 0.999998770
534580150.000 2016-344T18:28:02.685 68.184 1.000000032
536500868.000 2017-001T00:00:00.745 68.184 0.001000000
536500869.000 2017-001T00:00:00.746 69.184 1.000000032
537636435.000 2017-014T03:26:06.782 69.184 1.000002303
537637435.000 2017-014T03:42:46.785 69.184 1.000000036
538758841.000 2017-027T03:12:52.825 69.184 0.999999511
538759841.000 2017-027T03:29:32.825 69.184 1.000000030
539867709.000 2017-039T23:14:00.858 69.184 1.000028416
539868709.000 2017-039T23:30:40.887 69.184 0.998991865
539868780.000 2017-039T23:31:51.815 69.184 0.998983481
539869780.000 2017-039T23:48:30.799 69.184 1.000000027
541081505.000 2017-054T00:23:55.832 69.184 1.000002171
541082505.000 2017-054T00:40:35.834 69.184 1.000000078
541480395.000 2017-058T15:12:05.865 69.184 1.000006843
541481395.000 2017-058T15:28:45.872 69.184 1.000000040
542690315.000 2017-072T15:17:25.920 69.184 1.000022148
542691315.000 2017-072T15:34:05.943 69.184 1.000000031
544533731.000 2017-093T23:21:02.000 69.184 1.000065076
544534731.000 2017-093T23:37:42.065 69.184 1.000000028
550547497.000 2017-163T13:50:28.233 69.184 1.000028872
550548497.000 2017-163T14:07:08.262 69.184 1.000000099
551288740.000 2017-172T03:44:31.335 69.184 1.000003471
551289740.000 2017-172T04:01:11.339 69.184 1.000000049
551297264.000 2017-172T06:06:35.339 69.184 1.000011735
551298264.000 2017-172T06:23:15.351 69.184 1.000000029
556800005.000 2017-235T22:38:56.511 69.184 1.000001888
556801005.000 2017-235T22:55:36.512 69.184 1.000000026
559406112.000 2017-266T02:34:03.580 69.184 0.999996210
559407112.000 2017-266T02:50:43.576 69.184 1.000000028
562818799.000 2017-305T14:32:10.672 69.184 1.000001292
562819799.000 2017-305T14:48:50.673 69.184 1.000000031
565955293.000 2017-341T21:47:04.770 69.184 0.999999939
565956293.000 2017-341T22:03:44.770 69.184 1.000000027
567592189.000 2017-360T20:28:40.814 69.184 1.000002032
567593189.000 2017-360T20:45:20.816 69.184 1.000000031
570466832.000 2018-029T02:59:23.905 69.184 0.999998690
570467832.000 2018-029T03:16:03.904 69.184 0.998998875
570467916.000 2018-029T03:17:27.820 69.184 0.998998261
570468916.000 2018-029T03:34:06.818 69.184 1.000000031
571815371.000 2018-044T17:35:01.860 69.184 0.999998116
571816371.000 2018-044T17:51:41.858 69.184 1.000000035
577218094.000 2018-107T06:20:25.047 69.184 1.000000875
577219094.000 2018-107T06:37:05.048 69.184 1.000000136
579212589.000 2018-130T08:22:00.319 69.184 0.999999670
579213589.000 2018-130T08:38:40.319 69.184 1.000000107
579582887.000 2018-134T15:13:38.359 69.184 1.000007697
579583887.000 2018-134T15:30:18.366 69.184 1.000000037
581075680.000 2018-151T21:53:31.421 69.184 1.000016584
581076680.000 2018-151T22:10:11.438 69.184 1.000000069
581548472.000 2018-157T09:13:23.471 69.184 1.000013882
581549472.000 2018-157T09:30:03.484 69.184 1.000000039
587129196.000 2018-221T23:25:27.702 69.184 1.000002286
587130196.000 2018-221T23:42:07.704 69.184 1.000000037
CCSD3RE00000$$data$$CCSD3RE00000$$sclk$$
MAKCLK Setup file
--------------------------------------------------------
SCLKSCET_FILE = DAWN_203_SCLKSCET.00091.clean
OLD_SCLK_KERNEL = /sdma/naif/ops/projects/DAWN/scet/bin/dawn_template.tsc
FILE_NAME = DAWN_203_SCLKSCET.00091.tsc
NAIF_SPACECRAFT_ID = -203
LEAPSECONDS_FILE = /sdma/naif/ops/projects/DAWN/lsk/dawn.tls
PARTITION_TOLERANCE = 10
LOG_FILE = DAWN_203_SCLKSCET.00091.log
Kernel DATA
--------------------------------------------------------
\begindata
SCLK_KERNEL_ID = ( @2018-09-28/01:15:03.00 )
SCLK_DATA_TYPE_203 = ( 1 )
SCLK01_TIME_SYSTEM_203 = ( 2 )
SCLK01_N_FIELDS_203 = ( 2 )
SCLK01_MODULI_203 = ( 4294967296 256 )
SCLK01_OFFSETS_203 = ( 0 0 )
SCLK01_OUTPUT_DELIM_203 = ( 1 )
SCLK_PARTITION_START_203 = ( 0.0000000000000E+00 )
SCLK_PARTITION_END_203 = ( 1.0995116277750E+12 )
SCLK01_COEFFICIENTS_203 = (
0.0000000000000E+00 -3.5763036976277E-10 1.0000000000053E+00
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~NAIF/SPC BEGIN COMMENTS~
; /home/pgiroux/Desktop/FC21A0038582_15170161546F6F/FC21A0038582_15170161546F6F_0.bsp LOG FILE
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;
; BEGIN SPKMERGE COMMANDS
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'6^1'
'5^1'
'5^1'
'5^1'
'1D1656029A5E35^8'
'1^1'
'1^1'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-29DA975A2EA9DC^3'
'4BE50E65D885C^-1'
'7BBDDE600E6A3C^3'
'-19D19A848FCBFD^0'
'-112E3363B29FF5^4'
'-C5611959AA754^-1'
'6172D3529FEC0C^-5'
'-B07A2785D^-9'
'-B07A2785D^-9'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-1201375B008B99^-4'
'3C0BD8EBEB^-8'
'3C0BD8EBEB^-8'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'27FFC9CE5403BC^-4'
'1CBD8BE016^-8'
'1CBD8BE016^-8'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'3^1'
'2^1'
'2^1'
'2^1'
'1D165605A15A75^8'
'206FC4^1'
'306FC4^1'
'406FC4^1'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-29D9B1971E298C^3'
'4BE63563E02784^-1'
'7BB8FBC8471EE4^3'
'-19D1D104E7B571^0'
'-112E58BB5C4F8^4'
'-C55987E510764^-1'
'6170BD0E0F4868^-5'
'-165C9889089872^-8'
'-2B0FF2A0ACB568^-C'
'F9^-10'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-12008193066502^-4'
'79BBF79ED5FCDC^-8'
'7FAAA732EE9E38^-C'
'-373^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'280020CD877FAE^-4'
'3A4203FF226C16^-8'
'-11B81752FDE6C8^-B'
'-16E^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'4^1'
'3^1'
'3^1'
'3^1'
'1D1656491D602C^8'
'223E493BB3BA^2'
'379F0909928C^2'
'437C05B7597^2'
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'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
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'-29C5AC2FC419E4^3'
'4BFFDEF79C8868^-1'
'7B4C0B0AA64B38^3'
'-19D68DC9375022^0'
'-113197B81F1B38^4'
'-C4B0C157621378^-1'
'61422EFA2657B8^-5'
'-17A17AA6B8D932^-7'
'-3427CDF8EF7FDE^-A'
'2CB643D1D81D3^-D'
'-7352BC^-D'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-11F0ABC9E9BCAC^-4'
'8095A58E2B16F8^-7'
'9A77744219EB68^-A'
'-24036AB9712FBC^-C'
'E007B^-D'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'2807B0C9A3D26^-4'
'3D5907ECE83F9A^-7'
'-157DBD8F8F1408^-9'
'-16D6D1A98E2216^-C'
'2C53C^-D'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'5^1'
'4^1'
'4^1'
'4^1'
'1D1657009A5E35^8'
'28C6B23024^2'
'80A318DA7249^2'
'B77CFE08A3DC^2'
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'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-298F1A3B626B58^3'
'4C4567515C27B8^-1'
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'-19E35A24664062^0'
'-113A5D1445C1AF^4'
'-C2E53B500C05A^-1'
'60C34BAB0F255C^-5'
'-1C3C9765710592^-7'
'-8F32EF45C8C998^-A'
'-142257A6A274EE^-B'
'-2FA03578^-B'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-11C58F28E08F74^-4'
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'1648B96645C788^-B'
'5833F9F^-B'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'281C2025CC1608^-4'
'486707C48BB1F^-7'
'-3B4E650053C10A^-9'
'CF97CC631C37^-C'
'33F056C^-B'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
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'4^1'
'4^1'
'4^1'
'1D1657019A5E35^8'
'1^1'
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'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-298ECDF5AE6978^3'
'4C45E4634B5EAC^-1'
'7A21D385CA18B^3'
'-19E36875C5B7C8^0'
'-113A694269A31A^4'
'-C2E0FD3520184^-1'
'60C29A53A2FAA4^-5'
'-B1577F6EFC^-9'
'-B1577F6EFC^-9'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-11C552F434E866^-4'
'3C34ADE273^-8'
'3C34ADE273^-8'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'281C3C87770C7^-4'
'1C61AC4196^-8'
'1C61AC4196^-8'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'3^1'
'2^1'
'2^1'
'2^1'
'1D165704A15A75^8'
'206FC4^1'
'306FC4^1'
'406FC4^1'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-298DE70D7AA988^3'
'4C47094BD5131C^-1'
'7A1CED8FB0CD0C^3'
'-19E39E40CD538B^0'
'-113A8E20F61328^4'
'-C2D9665EB22C78^-1'
'60C08171045AEC^-5'
'-1678A3F48515E3^-8'
'-2AF09830DF2C74^-C'
'B48^-10'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-11C49CB0A1519A^-4'
'7A0EBC8904B31C^-8'
'7E523CB5C69BA8^-C'
'-2A^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'281C927088722A^-4'
'3987C1C4CEB86E^-8'
'-11C3D85201D1B3^-B'
'-11C^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'4^1'
'3^1'
'3^1'
'3^1'
'1D1657879A5E35^8'
'323CBB0554^2'
'5D938FB4E379^2'
'75A0677C7E26^2'
'82F903BFFDE7^2'
'84FFFFFFFDE7^2'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-2966D422F78764^3'
'4C7871EF3D5B28^-1'
'7948DC1E54D3B^3'
'-19ECAD7EC3D61E^0'
'-1140C3DF569D83^4'
'-C190D2A8708768^-1'
'6065A7B0BFB3CC^-5'
'-22DFE2578EC3DA^-7'
'-7FF5AC33858368^-A'
'3D34E890826DDA^-C'
'-109ECA1EB301A4^-D'
'-BE84^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-11A5C9B67322FF^-4'
'BD40313F56B5D^-7'
'178113318B7122^-9'
'-DFBD259F73A3C^-C'
'2CEF2EAB8CDCE8^-D'
'-607^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'282B0ADD44AC62^-4'
'58A09C9BA9E588^-7'
'-3534D42738D668^-9'
'-5F882A07A1A818^-C'
'F554548E84028^-E'
'24^-F'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'6^1'
'5^1'
'5^1'
'5^1'
'1D16557A9A5E35^8'
'1D16557B9A5E35^8'
'1D16557EA15A75^8'
'1D1655BE1A5E35^8'
'1D1655BF1A5E35^8'
'1D1655C2215A75^8'
'1D1656019A5E35^8'
'1D1656029A5E35^8'
'1D165605A15A75^8'
'1D1656491D602D^8'
'1D1657009A5E35^8'
'1D1657019A5E35^8'
'1D165704A15A75^8'
'1D1657879A5E35^8'
'E^1'
END_ARRAY 2 1009
BEGIN_ARRAY 3 39
'DE-0421LE-0421 '
'1D16543087CADE^8'
'1D16570A87CADA^8'
'A'
'0'
'1'
'2'
39
'1D156F4^8'
'A8C^5'
'7C2C876241EB2^5'
'BB81A3E3633198^3'
'-167B5991B48B4B^2'
'2BBB17392AA0A6^0'
'ECDBD5495F487^-2'
'-41CF36D0163C1C^-3'
'-1087525F8A6B6C^-3'
'-25FEF23CCB262E^-4'
'-3F8B7F47ECB90E^-5'
'-A8F01712362A98^-7'
'-12DBCD2E2A6261^-7'
'65E8829E2904DC^4'
'1AD4088EA673DE^4'
'50191FFD11DD14^1'
'-16EF8BCBC2F82C^0'
'17806F93E79E88^-1'
'1221E53E94C4EA^-2'
'1208A7B0D30B67^-3'
'A95BE445AE5F8^-5'
'-FA29A8B3502C4^-6'
'-662D66E5EF1A14^-6'
'-96CCCF8BD7CD78^-7'
'-345FA725507372^4'
'B4B26DF63A189^3'
'2AF41D0555FD5E^1'
'-C857185A3DE73^-1'
'A3BF138A19D33^-2'
'9AE2E5F88E427^-3'
'B6DD1F9A250CE^-4'
'99B835D61D526^-5'
'-1C4C043B38C76D^-6'
'-2E07B8AEB2CB4^-6'
'-4F728EDD2B1074^-7'
'1D0AE34^8'
'1518^6'
'23^2'
'1^1'
END_ARRAY 3 39
TOTAL_ARRAYS 3
~NAIF/SPC BEGIN COMMENTS~
; /home/pgiroux/Desktop/FC21A0038582_15170161546F6F/FC21A0038582_15170161546F6F_1.bsp LOG FILE
; Created 2019-09-06/10:01:26.00.
;
; BEGIN SPKMERGE COMMANDS
LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
SPK_KERNEL = /home/pgiroux/Desktop/FC21A0038582_15170161546F6F/FC21A0038582_15170161546F6F_1.bsp
SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/dawn/kernels/tspk/sb_ceres_140724.bsp
INCLUDE_COMMENTS = NO
BODIES = 2000001
BEGIN_TIME = 2015 JUN 19 16:15:41.346
END_TIME = 2015 JUN 19 16:27:51.346
SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/dawn/kernels/spk/dawn_rec_150509-150630_150730_v1.bsp
INCLUDE_COMMENTS = NO
BODIES = -203
BEGIN_TIME = 2015 JUN 19 16:15:41.346
END_TIME = 2015 JUN 19 16:27:51.346
SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/dawn/kernels/tspk/de421.bsp
INCLUDE_COMMENTS = NO
BODIES = 10
BEGIN_TIME = 2015 JUN 19 16:15:41.346
END_TIME = 2015 JUN 19 16:27:51.346
; END SPKMERGE COMMANDS
~NAIF/SPC END COMMENTS~
PDS_VERSION_ID = PDS3
LABEL_REVISION_NOTE = "20080201, PGM, DAWN FC V1.5"
/* FILE CHARACTERISTICS */
RECORD_TYPE = FIXED_LENGTH
RECORD_BYTES = 512
FILE_RECORDS = 4301
LABEL_RECORDS = 24
FILE_NAME = "FC21A0038582_15170161546F6F.IMG"
/* POINTERS TO DATA OBJECTS */
^IMAGE = 26
^FRAME_2_IMAGE = 4122
^FRAME_3_IMAGE = 4205
^FRAME_4_IMAGE = 4238
^FRAME_5_IMAGE = 4270
^HISTORY = 25
/* SOFTWARE */
SOFTWARE_DESC = "TRAP.EXE"
SOFTWARE_LICENSE_TYPE = "COMMERCIAL"
SOFTWARE_ID = "TRAP"
SOFTWARE_NAME = "TRAP"
SOFTWARE_VERSION_ID = "Trap v4.10"
SOFTWARE_RELEASE_DATE = 2016-03-17
/* TELEMETRY IDENTIFICATION */
TELEMETRY_FORMAT_ID = "309"
/* PRODUCT IDENTIFICATION */
DATA_SET_NAME = "DAWN FC2 RAW (EDR) CERES IMAGES V1.0"
DATA_SET_ID = "DAWN-A-FC2-2-EDR-CERES-IMAGES-V1.0"
PRODUCT_ID = "0038582"
PRODUCT_TYPE = "DATA"
STANDARD_DATA_PRODUCT_ID = "FC_IMAGE"
PRODUCER_FULL_NAME = "PABLO GUTIERREZ-MARQUES"
PRODUCER_INSTITUTION_NAME =
"MAX PLANCK INSTITUT FUER SONNENSYSTEMFORSCHUNG"
PRODUCT_CREATION_TIME = 2016-04-06T15:24:21.000
PRODUCT_VERSION_ID = "F"
RELEASE_ID = "N/A"
/* MISSION IDENTIFICATION */
INSTRUMENT_HOST_ID = "DAWN"
INSTRUMENT_HOST_NAME = "DAWN"
MISSION_ID = "DAWN"
MISSION_NAME = "DAWN MISSION TO VESTA AND CERES"
MISSION_PHASE_NAME = "CERES SCIENCE SURVEY (CSS)"
/* INSTRUMENT DESCRIPTION */
INSTRUMENT_ID = "FC2"
INSTRUMENT_NAME = "FRAMING CAMERA 2"
OBSERVATION_ID = "FC2_CSS_C5NadirSouthColor_001"
OBSERVATION_TYPE = "N/A"
INSTRUMENT_TYPE = "FRAME CCD REFRACTING TELESCOPE"
DETECTOR_DESC = "1092x1056 PIXELS FRONTLIT FRAMETRANSFER CCD"
DETECTOR_TYPE = "SI CCD"
DETECTOR_TEMPERATURE = 217.927 <kelvin>
/* TIME IDENTIFICATION */
SPACECRAFT_CLOCK_START_COUNT = "488002612:246"
SPACECRAFT_CLOCK_STOP_COUNT = "488002614:244"
START_TIME = 2015-170T16:15:46.345
DAWN:ALT_START_TIME = 2015-06-19T16:15:46.345
STOP_TIME = 2015-170T16:15:48.337
DAWN:ALT_STOP_TIME = 2015-06-19T16:15:48.337
/* SYSTEM HARDWARE AND SOFTWARE CONFIGURATION */
DAWN:DPU_HARDWARE_ID = "1.04"
DAWN:DPU_SOFTWARE_VERSION = "3.09"
DAWN:UDPLIB_SOFTWARE_VERSION = "3.09.03"
DAWN:PCU_HARDWARE_ID = 2.04
DAWN:FEE_HARDWARE_ID = "017.09.09"
DAWN:MCU_HARDWARE_ID = "12"
/* MECHANISM STATUS */
DAWN:FILTER_ENCODER = 23
FILTER_NUMBER = "6"
DAWN:FRONT_DOOR_ENCODER = 53
DAWN:FRONT_DOOR_STATUS_ID = OPEN
/* IMAGE ACQUISITION OPTIONS */
DAWN:DATA_ROUTING_ID = "SCIENCE 2"
EXPOSURE_DURATION = 1800.000 <millisecond>
DAWN:USE_PRE_CLEAR = ON
DAWN:IMAGE_ACQUIRE_MODE = NORMAL
DAWN:CALLAMP_STROBE_TIME = "N/A"
DAWN:CALLAMP_DELAY_TIME = "N/A"
DAWN:CALLAMP_FREQUENCY = "N/A"
DAWN:CALLAMP_DUTY = "N/A"
/* POWER CONVERTER SWITCH STATUS */
DAWN:FEE_FLAG = ON
DAWN:HEATER0_FLAG = OFF
DAWN:HEATER1_FLAG = OFF
DAWN:CALLAMP_ENABLE_FLAG = OFF
DAWN:MCU_MOTOR_POWER_FLAG = ON
DAWN:MCU_FLAG = ON
DAWN:FSA_SHOOT_FLAG = OFF
DAWN:FSA_SHOOT_ENABLE_FLAG = OFF
/* POWER SYSTEM STATUS */
DAWN:V_28 = 30.080 <volt>
DAWN:V_16 = 16.120 <volt>
DAWN:V_12 = 12.079 <volt>
DAWN:V_5 = 5.181 <volt>
DAWN:V_M5 = -5.045 <volt>
DAWN:V_5_ANALOG = 5.292 <volt>
DAWN:V_M5_ANALOG = -5.161 <volt>
DAWN:V_3_3 = 3.335 <volt>
DAWN:V_2_5 = 2.506 <volt>
DAWN:I_28 = 563.200 <milliampere>
DAWN:I_16 = 58.545 <milliampere>
DAWN:I_12 = 82.380 <milliampere>
DAWN:I_5 = 301.300 <milliampere>
DAWN:I_M5 = -88.905 <milliampere>
DAWN:I_5_ANALOG = 249.200 <milliampere>
DAWN:I_M5_ANALOG = -27.150 <milliampere>
DAWN:I_3_3 = 240.300 <milliampere>
DAWN:I_2_5 = 665.550 <milliampere>
/* CALIBRATED TEMPERATURES */
DAWN:T_CCD = 217.927 <kelvin>
DAWN:T_DPU = 292.427 <kelvin>
DAWN:T_DCDC = 284.224 <kelvin>
DAWN:T_F12 = 289.181 <kelvin>
DAWN:T_CSC = 289.223 <kelvin>
DAWN:T_COVER_MOTOR = 244.295 <kelvin>
DAWN:T_LENS_BARREL = 248.285 <kelvin>
DAWN:T_BAFFLE = 243.295 <kelvin>
DAWN:T_FILTER_MOTOR = 255.267 <kelvin>
DAWN:T_STRUCTURE = 255.267 <kelvin>
DAWN:T_RAD_MOTOR = 201.400 <kelvin>
/* TEST SETUP CONFIGURATION */
DAWN:PURPOSE = "N/A"
DAWN:OPERATOR = "N/A"
DAWN:SUBJECT = "N/A"
DAWN:TEST_LAMP = "N/A"
DAWN:TARGET = "N/A"
DAWN:CHAMBER = "N/A"
/* POINTING */
RIGHT_ASCENSION = 289.753 <degree>
DECLINATION = 64.400 <degree>
TWIST_ANGLE = 95.606 <degree>
CELESTIAL_NORTH_CLOCK_ANGLE = 275.606 <degree>
QUATERNION = (
0.5213655224
, -0.1747575947
, 0.1361764644
, -0.8240714445
)
/* SPICE KERNELS */
SPICE_FILE_NAME = (
"sclk\DAWN_203_SCLKSCET.00065.tsc"
, "lsk\naif0011.tls"
, "spk\dawn_rec_150509-150630_150730_v1.bsp"
, "ck\dawn_sc_150615_150621.bc"
, "ik\dawn_fc_v10.mk"
, "fk\dawn_v13.tf"
, "fk\dawn_ceres_v00.tf"
, "pck\pck00010.tpc"
, "spk\de421.bsp"
, "pck\dawn_ceres_v05.tpc"
, "spk\sb_ceres_140724.bsp"
, "fk\dawn_ceres_v00.tf"
)
/* COORDINATE SYSTEM */
COORDINATE_SYSTEM_NAME = "CERES_FIXED"
COORDINATE_SYSTEM_CENTER_NAME = "CERES"
DESCRIPTION = ""
/* ORBIT GEOMETRY */
SUB_SPACECRAFT_LATITUDE = "N/A"
SUB_SPACECRAFT_LONGITUDE = "N/A"
SUB_SPACECRAFT_AZIMUTH = "N/A"
SPACECRAFT_ALTITUDE = "N/A"
TARGET_CENTER_DISTANCE = "N/A"
ORBIT_NUMBER = "N/A"
SC_TARGET_POSITION_VECTOR = (
"N/A"
, "N/A"
, "N/A"
)
SC_TARGET_VELOCITY_VECTOR = (
"N/A"
, "N/A"
, "N/A"
)
LOCAL_HOUR_ANGLE = "N/A"
SUB_SOLAR_LATITUDE = "N/A"
SUB_SOLAR_LONGITUDE = "N/A"
SUB_SOLAR_AZIMUTH = "N/A"
SOLAR_LONGITUDE = "N/A"
SOLAR_ELONGATION = "N/A"
TARGET_NAME = "1 CERES"
TARGET_TYPE = "ASTEROID"
/* SOLAR GEOMETRY */
SPACECRAFT_SOLAR_DISTANCE = "N/A"
SC_SUN_POSITION_VECTOR = (
"N/A"
, "N/A"
, "N/A"
)
SC_SUN_VELOCITY_VECTOR = (
"N/A"
, "N/A"
, "N/A"
)
/* ILLUMINATION */
INCIDENCE_ANGLE = "N/A"
EMISSION_ANGLE = "N/A"
PHASE_ANGLE = "N/A"
/* IMAGE PARAMETERS */
SAMPLE_DISPLAY_DIRECTION = "RIGHT"
LINE_DISPLAY_DIRECTION = "UP"
SLANT_DISTANCE = "N/A"
MINIMUM_LATITUDE = "N/A"
CENTER_LATITUDE = "N/A"
MAXIMUM_LATITUDE = "N/A"
WESTERNMOST_LONGITUDE = "N/A"
CENTER_LONGITUDE = "N/A"
EASTERNMOST_LONGITUDE = "N/A"
HORIZONTAL_PIXEL_SCALE = "N/A"
VERTICAL_PIXEL_SCALE = "N/A"
RETICLE_POINT_RA = (
)
RETICLE_POINT_DECLINATION = (
)
RETICLE_POINT_LONGITUDE = (
)
RETICLE_POINT_LATITUDE = (
)
NORTH_AZIMUTH = "N/A"
/* IMAGE OBJECT */
OBJECT = IMAGE
INTERCHANGE_FORMAT = BINARY
LINE_SAMPLES = 1024
LINES = 1024
BANDS = 1
SAMPLE_BITS = 16
SAMPLE_TYPE = "LSB_UNSIGNED_INTEGER"
FIRST_LINE = 17
FIRST_LINE_SAMPLE = 35
UNIT = "DU"
INST_CMPRS_NAME =
"SET PARTITIONING IN HIERARCHICAL TREES (SPIHT TAP)"
INST_CMPRS_RATIO = 2.52
INST_CMPRS_TYPE = "LOSSLESS"
PIXEL_AVERAGING_WIDTH = 1
PIXEL_AVERAGING_HEIGHT = 1
END_OBJECT = IMAGE
/* FRAME_2_IMAGE OBJECT */
OBJECT = FRAME_2_IMAGE
INTERCHANGE_FORMAT = BINARY
LINE_SAMPLES = 10
LINES = 1054
BANDS = 1
SAMPLE_BITS = 32
SAMPLE_TYPE = "PC_REAL"
FIRST_LINE = 2
FIRST_LINE_SAMPLE = 2
UNIT = "DU"
INST_CMPRS_NAME = "N/A"
INST_CMPRS_RATIO = 0.00
INST_CMPRS_TYPE = "LOSSLESS"
PIXEL_AVERAGING_WIDTH = 1
PIXEL_AVERAGING_HEIGHT = 1
END_OBJECT = FRAME_2_IMAGE
/* FRAME_3_IMAGE OBJECT */
OBJECT = FRAME_3_IMAGE
INTERCHANGE_FORMAT = BINARY
LINE_SAMPLES = 8
LINES = 1054
BANDS = 1
SAMPLE_BITS = 16
SAMPLE_TYPE = "LSB_UNSIGNED_INTEGER"
FIRST_LINE = 2
FIRST_LINE_SAMPLE = 16
UNIT = "DU"
INST_CMPRS_NAME = "N/A"
INST_CMPRS_RATIO = 0.00
INST_CMPRS_TYPE = "LOSSLESS"
PIXEL_AVERAGING_WIDTH = 1
PIXEL_AVERAGING_HEIGHT = 1
END_OBJECT = FRAME_3_IMAGE
/* FRAME_4_IMAGE OBJECT */
OBJECT = FRAME_4_IMAGE
INTERCHANGE_FORMAT = BINARY
LINE_SAMPLES = 1024
LINES = 8
BANDS = 1
SAMPLE_BITS = 16
SAMPLE_TYPE = "LSB_UNSIGNED_INTEGER"
FIRST_LINE = 3
FIRST_LINE_SAMPLE = 35
UNIT = "DU"
INST_CMPRS_NAME = "N/A"
INST_CMPRS_RATIO = 0.00
INST_CMPRS_TYPE = "LOSSLESS"
PIXEL_AVERAGING_WIDTH = 1
PIXEL_AVERAGING_HEIGHT = 1
END_OBJECT = FRAME_4_IMAGE
/* FRAME_5_IMAGE OBJECT */
OBJECT = FRAME_5_IMAGE
INTERCHANGE_FORMAT = BINARY
LINE_SAMPLES = 1024
LINES = 8
BANDS = 1
SAMPLE_BITS = 16
SAMPLE_TYPE = "LSB_UNSIGNED_INTEGER"
FIRST_LINE = 1047
FIRST_LINE_SAMPLE = 35
UNIT = "DU"
INST_CMPRS_NAME = "N/A"
INST_CMPRS_RATIO = 0.00
INST_CMPRS_TYPE = "LOSSLESS"
PIXEL_AVERAGING_WIDTH = 1
PIXEL_AVERAGING_HEIGHT = 1
END_OBJECT = FRAME_5_IMAGE
END
OBJECT = HISTORY
GROUP = LEVEL_1A_GENERATION
VERSION_DATE = 2016-03-17
DATE_TIME = 2016-04-06T15:24:21.000Z
SOFTWARE_DESC = "TRAP.EXE"
GROUP = PARAMETERS
FILENAME = "FC21A0038582_15170161546F6F.IMG"
END_GROUP = PARAMETERS
END_GROUP = LEVEL_1A_GENERATION
END_OBJECT = HISTORY
END
KPL/PCK
\beginlabel
PDS_VERSION_ID = PDS3
RECORD_TYPE = STREAM
RECORD_BYTES = "N/A"
^SPICE_KERNEL = "dawn_ceres_v05.tpc"
MISSION_NAME = "DAWN MISSION TO VESTA AND CERES"
SPACECRAFT_NAME = DAWN
DATA_SET_ID = "DAWN-M/A-SPICE-6-V1.0"
KERNEL_TYPE_ID = PCK
PRODUCT_ID = "dawn_ceres_v05.tpc"
PRODUCT_CREATION_TIME = 2015-10-19T11:30:28
PRODUCER_ID = "NAIF/JPL"
MISSION_PHASE_NAME = {
"INITIAL CHECKOUT (ICO)",
"EARTH-MARS CRUISE (EMC)",
"MARS GRAVITY ASSIST (MGA)",
"MARS-VESTA CRUISE (MVC)",
"VESTA ENCOUNTER",
"VESTA-CERES CRUISE (VCC)",
"CERES ENCOUNTER",
"END OF MISSION"
}
PRODUCT_VERSION_TYPE = ACTUAL
PLATFORM_OR_MOUNTING_NAME = "N/A"
START_TIME = "N/A"
STOP_TIME = "N/A"
SPACECRAFT_CLOCK_START_COUNT = "N/A"
SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
TARGET_NAME = "1 CERES"
INSTRUMENT_NAME = "N/A"
NAIF_INSTRUMENT_ID = "N/A"
SOURCE_PRODUCT_ID = "N/A"
NOTE = "See comments in the file for details"
OBJECT = SPICE_KERNEL
INTERCHANGE_FORMAT = ASCII
KERNEL_TYPE = TARGET_CONSTANTS
DESCRIPTION = "SPICE PCK file containing constants for
Ceres, created by NAIF, JPL. This PCK incorporates shape and rotation
constants from the ``Ceres Coordinate System Description'' document dated
14-Oct-2015. "
END_OBJECT = SPICE_KERNEL
\endlabel
Asteroid Ceres P_constants (PcK) SPICE kernel file
===========================================================================
Organization
--------------------------------------------------------
The sections of this file are as follows.
Introductory Information:
-- Version description
-- Disclaimer
-- Sources
Pck Data:
-- Orientation constants for asteroid Ceres
-- Radii for asteroid Ceres
-- GM for asteroid Ceres
Version Description
--------------------------------------------------------
Version 0.5 -- October 16, 2015 -- Carol Raymond, DAWN; Boris Semenov,
NAIF
Ceres rotation constants and radii were updated based on [6];
Ceres GM was updated based on [7]. A typo in the shape section
comments for versions 0.3 and 0.4 was fixed ("as a sphere with a
radius of 480 km" -> "as a sphere with a radius of 470 km")
Version 0.4 -- July 15, 2015 -- Don Han, DAWN NAV; Boris Semenov,
NAIF
Fixed typo in Ceres rotation rate in BODY2000001_PM: 951.1532 ->
952.1532.
Version 0.3 -- June 11, 2015 -- Don Han, DAWN NAV; Boris Semenov,
NAIF
Ceres rotation constants and radii were updated based on [5].
Version 0.2 -- March 2, 2015 -- Don Han, DAWN NAV; Boris Semenov,
NAIF
Ceres rotation constants were updated based on [4]; Keyword for
Ceres GM was added to the file and set to the value from [4].
Version 0.1 -- February 25, 2011 -- Boris Semenov, NAIF
Ceres pole orientation constants and radii were set to the
values from [3].
Version 0.0 -- October 12, 2004 -- Boris Semenov, NAIF
Initial PCK containing draft values for the pole direction,
rotation period and shape (from [1] and [2]) and placeholder
value for prime meridian.
Disclaimer
--------------------------------------------------------
This constants file may not contain the parameter values that you
prefer. Note that this file may be readily modified by you or
anyone else. NAIF suggests that you inspect this file visually
before proceeding with any critical or extended data processing.
NAIF requests that you update the ``Version Description'' section
if you modify the file.
Sources
--------------------------------------------------------
The sources for the constants listed in this and the earlier
versions of this file are:
1) Saint-Pe, O., M. Combes, F. Rigaut (1993). Ceres surface
properties by high-resolution imaging from Earth. Icarus 105,
271-281.
2) JPL Solar System Dynamic Group Horizon's System.
3) "Dawn Planetary Constants and Models Document", Revision 2.0,
Feb 16, 2011
4) "DAWN Planetary Constants and Models Document", Revision 4.0,
Mar 2, 2015
5) "DAWN Planetary Constants and Models Document", Revision 5.0,
Jun 10, 2015
6) "Ceres Coordinate System Description", C. Raymond, JPL and
T. Roatsch, DLR, 14-OCT-2015, in PDS peer-review, to be
archived.
7) "Physical Properties of Ceres from the Dawn Mission", R. Park,
et al., Geophys. Res. Let., to be submitted, Oct. 2015
Orientation constants for asteroid Ceres
--------------------------------------------------------
The inertial reference frame for Ceres constants is J2000; this is
the default reference frame for PCK orientation data.
The epoch of the constants is J2000; this is Julian ephemeris date
(JED) 2451545.0.
The NAIF integer code for Ceres is 2000001. See the NAIF_IDs
required reading for further information on NAIF integer codes.
Values in the Version 0.0
The PCK version 0.0 provided the pole direction RA = 300.4 deg and
DEC = 53.1 deg (derived from the ecliptic equinox B1950.0 latitude
= 70 deg and longitude = 332 deg values given in [1]), the W1 term
= 952.06611570 deg/day (derived from the rotation period of 9.075
hours provided in [2]), and the W0 term arbitrarily set to 0.
The corresponding keywords were set as follows:
body2000001_pole_ra = ( 300.4 0.0 0.0 )
body2000001_pole_dec = ( 53.1 0.0 0.0 )
body2000001_pm = ( 0.0 952.0661157 0.0 )
Values in the Version 0.1
In the PCK version 0.1 the pole direction, prime meridian
location, and rotation period were set to the following values
from [3]:
6.3 Ceres Pole and Prime Meridian
The Ceres pole and prime meridian values are shown below.
RA Ceres 291 deg Right Ascension in EME2000 [17]
DEC Ceres 59 deg Declination in EME2000
W Ceres 0 + w * D deg Prime Meridian
w Ceres 951.5418502 deg/day Rotation rate
...
9 References
...
17. "Ceres: High-resolution imaging with HGA and the determination
of physical properties," J. W. Parker et al., Advances in
Space Research 38 (2006) 2039-2042.
18. "Differentiation of the asteroid Ceres as revealed by its
shape", P. C. Thomas, et al, Nature, 437, 224, 2005.
..."
The corresponding keywords were set as follows:
body2000001_pole_ra = ( 291.0 0.0 0.0 )
body2000001_pole_dec = ( 59.0 0.0 0.0 )
body2000001_pm = ( 0.0 951.5418502 0.0 )
Values in the Version 0.2
In the PCK version 0.2 the pole direction, prime meridian
location, and rotation period were set to the following values from
[4]:
6.3 Ceres Pole and Prime Meridian
The Ceres pole and prime meridian values are shown below.
RA Ceres 291.82 deg Right Ascension in EME2000 [29]
DEC Ceres 66.88 deg Declination in EME2000 [29]
W Ceres 353.7987 + w * D deg Prime Meridian [*]
w Ceres 952.055 deg/day Rotation rate [29]
[*] This document overlooked the Ceres prime meridian and
rotation rate recommended by Archinal et. al. [28] in IAU
working group report and listed the prime meridian with zero
offset until revision 4 date. While updating the prime meridian
definition, Dawn project decided to update other physical
parameters of Ceres by navigation team~s latest estimation
result. The rotation rate is from navigation team report [29]
and the prime meridian offset was calculated to match the value
from IAU recommendation [28] at the time of RC2 (2015/02/20
12:00:00 UTC).
...
9 References
29. "Ceres Parameters from OD", Brian Kennedy, JPL internal
E-mail, Feb. 26, 2015
The corresponding keywords were set as follows:
body2000001_pole_ra = ( 291.82 0.0 0.0 )
body2000001_pole_dec = ( 66.88 0.0 0.0 )
body2000001_pm = ( 353.7987 952.055 0.0 )
Values in the Versions 0.3 and 0.4
In the PCK versions 0.3 and 0.4 the pole direction, prime meridian
location, and rotation period were set to the following values from
[5]:
6.3 Ceres Pole and Prime Meridian
The Ceres pole and prime meridian values are shown below.
RA Ceres 291.41 deg Right Ascension in EME2000 [31]
DEC Ceres 66.79 deg Declination in EME2000 [31]
W Ceres 170.9 + w * D deg Prime Meridian [30]
w Ceres 952.1532 deg/day Rotation rate [30]
...
9 References
30. "Ceres lightcurve analysis ~ Period determination",
M. A. Chamberlain, et al., Icarus 188, 2007
31. "Shape model and rotational state of dwarf planet Ceres
from Dawn-FC RC3 stereo images", Frank Preusker, Dawn
internal presentation, May 26, 2015
The corresponding keywords were set as follows:
body2000001_pole_ra = ( 291.41 0.0 0.0 )
body2000001_pole_dec = ( 66.79 0.0 0.0 )
body2000001_pm = ( 170.9 952.1532 0.0 )
Values in the Current Version 0.5
In the current PCK version 0.5 the pole direction, prime meridian
location, and rotation period are set to the values obtained from
the Dawn Approach, RC3 and Survey mission phases, as summarized in
[6]:
...
Table 1: Comparison of pre-Dawn and post-Survey Dawn coordinate
systems; row 2 -- "Dawn Update":
RA Ceres 291.418 deg Right Ascension in EME2000
DEC Ceres 66.764 deg Declination in EME2000
W Ceres 170.650 + w * D deg Prime Meridian
w Ceres 952.1532 deg/day Rotation rate
...
References:
"Shape model and rotational state of dwarf planet Ceres from
Dawn FC stereo images", Frank Preusker, et al., Euro. Plan.
Sci. Congress, Oct. 2015
..."
\begindata
BODY2000001_POLE_RA = ( 291.418 0.0 0.0 )
BODY2000001_POLE_DEC = ( 66.764 0.0 0.0 )
BODY2000001_PM = ( 170.65 952.1532 0.0 )
\begintext
Radii for asteroid Ceres
--------------------------------------------------------
Values in the Version 0.0
In the PCK version 0.0 the radii were set to the following values
from [2]:
body2000001_radii = ( 475.0 475.0 475.0 )
Values in the Versions 0.1 and 0.2
In the versions 0.1 and 0.2 the radii were set to the following
values from [3]/[4]:
6.4 Ceres Shape Parameters
The Ceres shape is described by an oblate spheroid with values
487.3 km and 454.7 km [18] or as a sphere with a radius of 480
km. ...
9 References
...
18. "Differentiation of the asteroid Ceres as revealed by its
shape", P. C. Thomas, et al, Nature, 437, 224, 2005.
..."
The corresponding keyword was set as follows:
body2000001_radii = ( 487.3 487.3 454.7 )
Values in the Versions 0.3 and 0.4
In the PCK versions 0.3 and 0.4 the radii were set to the following
values from [5]:
6.4 Ceres Shape Parameters
The Ceres shape is described by triaxial ellipsoid with values
482.64 km, 480.60 km, 445.57 km [31] or as a sphere with a
radius of 470 km. ...
9 References
...
31. "Shape model and rotational state of dwarf planet Ceres
from Dawn-FC RC3 stereo images", Frank Preusker, Dawn
internal presentation, May 26, 2015
..."
The corresponding keyword was set as follows:
body2000001_radii = ( 482.64 480.60 445.57 )
Values in the Current Version 0.5
In the current PCK version 0.5 the radii are set to the spheroid
values from [6]:
Table 1: Comparison of pre-Dawn and post-Survey Dawn coordinate
systems; row 2 -- "Dawn Update":
Sphere:
Rsp = 470 km Equivalent spherical body radius
Spheroid:
Re = 482 km Average equatorial radius of the oblate spheroid
Rp = 446 km Polar radius
References:
"Shape model and rotational state of dwarf planet Ceres from
Dawn FC stereo images", Frank Preusker, et al., Euro. Plan.
Sci. Congress, Oct. 2015
..."
\begindata
BODY2000001_RADII = ( 482 482 446 )
\begintext
GM for asteroid Ceres
--------------------------------------------------------
Value in the Versions 0.0 and 0.1
No Ceres GM was provided in the PCK version 0.0 and 0.1.
Value in the Versions 0.2, 0.3, and 0.4
In the PCK versions 0.2, 0.3, and 0.4 the Ceres GM was set to the
following value from [4]:
6.2 Ceres Gravity Model
GM Ceres = 62.68 km3/s2 Gravitational Parameter [29]
...
9 References
29. "Ceres Parameters from OD", Brian Kennedy, JPL internal
E-mail, Feb. 26, 2015
The corresponding keyword was set as follows:
body2000001_gm = ( 62.68 )
Value in the Current Version 0.5
In the PCK version 0.5 the Ceres GM is set to the following value
from [7]:
GM Ceres = 62.6325 km3/s2
\begindata
BODY2000001_GM = ( 62.6325 )
\begintext
End of PCK file.
This diff is collapsed.
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INS-203126_TRANSY=(0.0,0.0,0.014)
INS-203126_ITRANSS=(0.0,71.383701673233967,0.0)
INS-203126_ITRANSL=(0.0,0.0,71.428571428571429)
INS-203127_TRANSX=(0.0,0.0140088,0.0)
INS-203127_TRANSY=(0.0,0.0,0.014)
INS-203127_ITRANSS=(0.0,71.383701673233967,0.0)
INS-203127_ITRANSL=(0.0,0.0,71.428571428571429)
INS-203128_TRANSX=(0.0,0.0140088,0.0)
INS-203128_TRANSY=(0.0,0.0,0.014)
INS-203128_ITRANSS=(0.0,71.383701673233967,0.0)
INS-203128_ITRANSL=(0.0,0.0,71.428571428571429)
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
import pytest import pytest
import os
import numpy as np
import spiceypy as spice
from importlib import reload
import json
import ale import unittest
from ale.drivers import dawn_drivers from unittest.mock import patch
from conftest import get_image_label, get_image_kernels, convert_kernels, compare_dicts
from unittest.mock import PropertyMock, patch
# 'Mock' the spice module where it is imported
from conftest import SimpleSpice, get_mockkernels
simplespice = SimpleSpice()
dawn_drivers.spice = simplespice
import ale
from ale.drivers.dawn_drivers import DawnFcPds3NaifSpiceDriver from ale.drivers.dawn_drivers import DawnFcPds3NaifSpiceDriver
DawnFcPds3NaifSpiceDriver.metakernel = get_mockkernels @pytest.fixture()
def usgscsm_compare_dict():
@pytest.fixture return {
def driver(): 'radii': {
return DawnFcPds3NaifSpiceDriver("") 'semimajor': 482.0,
'semiminor': 446.0,
def test_short_mission_name(driver): 'unit': 'km'},
assert driver.short_mission_name=='dawn' 'sensor_position': {
'positions': [[ 257925.27016132, 15117.796357 , -4862708.42068566]],
@patch('ale.base.label_pds3.Pds3Label.instrument_id', 1) 'velocities': [[-104.55545524, -85.0501252 , -5.78752004]],
@patch('ale.base.label_pds3.Pds3Label.filter_number', 2) 'unit': 'm'},
def test_instrument_id(driver): 'sun_position': {
assert driver.instrument_id == 'DAWN_1_FILTER_2' 'positions': [[3.60779830e+11, 2.46614935e+11, 3.05966427e+10]],
'velocities': [[ 4.74251599e+07, -6.93781387e+07, 1.94478534e+02]],
@patch('ale.base.label_pds3.Pds3Label.instrument_host_id', 'DAWN') 'unit': 'm'},
def test_spacecraft_name(driver): 'sensor_orientation': {
assert driver.spacecraft_name == 'DAWN' 'quaternions': [[ 0.00184844, 0.02139268, -0.27802966, -0.96033246]]},
'detector_sample_summing': 1,
def test_target_name(driver): 'detector_line_summing': 1,
with patch('ale.base.label_pds3.Pds3Label.target_name', new_callable=PropertyMock) as mock_target_name: 'focal_length_model': {
mock_target_name.return_value = '4 VESTA' 'focal_length': 150.08},
assert driver.target_name == 'VESTA' 'detector_center': {
mock_target_name.return_value = 'VESTA' 'line': 512.0,
assert driver.target_name == 'VESTA' 'sample': 512.0},
'starting_detector_line': 0,
@patch('ale.base.label_pds3.Pds3Label.spacecraft_clock_start_count', 123) 'starting_detector_sample': 0,
@patch('ale.base.label_pds3.Pds3Label.instrument_host_id', 'DAWN') 'focal2pixel_lines': [0.0, 0.0, 71.40816909454442],
def test_ephemeris_start_time(driver): 'focal2pixel_samples': [0.0, 71.40816909454442, 0.0],
assert driver.ephemeris_start_time == .1 + 193.0 / 1000.0 'optical_distortion': {
'dawnfc': {
@patch('ale.base.data_naif.NaifSpice.ikid', 123) 'coefficients': [9.2e-06]}},
def test_odtk(driver): 'image_lines': 1024,
assert driver.odtk == [1] 'image_samples': 1024,
'name_platform': 'DAWN',
@patch('ale.base.data_naif.NaifSpice.ikid', 123) 'name_sensor': 'FRAMING CAMERA 2',
def test_usgscsm_distortion_model(driver): 'reference_height': {
distortion_model = driver.usgscsm_distortion_model 'maxheight': 1000,
assert distortion_model['dawnfc']['coefficients'] == [1] 'minheight': -1000,
'unit': 'm'},
@patch('ale.base.data_naif.NaifSpice.ikid', 123) 'name_model': 'USGS_ASTRO_FRAME_SENSOR_MODEL',
def test_focal2pixel_samples(driver): 'center_ephemeris_time': 488002614.62294483}
assert driver.focal2pixel_samples == [0, 1000, 0]
@pytest.fixture(scope="module", autouse=True)
@patch('ale.base.data_naif.NaifSpice.ikid', 123) def test_kernels():
def test_focal2pixel_lines(driver): kernels = get_image_kernels('FC21A0038582_15170161546F6F')
assert driver.focal2pixel_lines == [0, 0, 1000] updated_kernels, binary_kernels = convert_kernels(kernels)
yield updated_kernels
def test_sensor_model_version(driver): for kern in binary_kernels:
assert driver.sensor_model_version == 2 os.remove(kern)
def test_dawn_load(test_kernels, usgscsm_compare_dict):
label_file = get_image_label('FC21A0038582_15170161546F6F')
usgscsm_isd = ale.load(label_file, props={'kernels': test_kernels}, formatter='usgscsm')
print(usgscsm_isd)
assert compare_dicts(usgscsm_isd, usgscsm_compare_dict) == []
# ========= Test pds3label and naifspice driver =========
class test_pds3_naif(unittest.TestCase):
def setUp(self):
label = get_image_label("FC21A0038582_15170161546F6F", "pds3")
self.driver = DawnFcPds3NaifSpiceDriver(label)
def test_short_mission_name(self):
assert self.driver.short_mission_name == 'dawn'
def test_instrument_id(self):
assert self.driver.instrument_id == 'DAWN_FC2_FILTER_6'
def test_spacecraft_name(self):
assert self.driver.spacecraft_name == 'DAWN'
def test_target_name(self):
assert self.driver.target_name == 'CERES'
def test_ephemeris_start_time(self):
with patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=12345) as scs2e:
assert self.driver.ephemeris_start_time == 12345.193
scs2e.assert_called_with(-203, '488002612:246')
def test_usgscsm_distortion_model(self):
with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=np.array([12345])) as gdpool, \
patch('ale.drivers.dawn_drivers.spice.bods2c', return_value=54321) as bods2c:
dist = self.driver.usgscsm_distortion_model
assert dist['dawnfc']['coefficients'] == [12345]
bods2c.assert_called_with('DAWN_FC2_FILTER_6')
gdpool.assert_called_with('INS54321_RAD_DIST_COEFF', 0, 1)
def test_focal2pixel_samples(self):
with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=np.array([1000])) as gdpool, \
patch('ale.drivers.dawn_drivers.spice.bods2c', return_value=54321) as bods2c:
assert self.driver.focal2pixel_samples == [0, 1, 0]
bods2c.assert_called_with('DAWN_FC2_FILTER_6')
gdpool.assert_called_with('INS54321_PIXEL_SIZE', 0, 1)
def test_focal2pixel_lines(self):
with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=np.array([1000])) as gdpool, \
patch('ale.drivers.dawn_drivers.spice.bods2c', return_value=54321) as bods2c:
assert self.driver.focal2pixel_lines == [0, 0, 1]
bods2c.assert_called_with('DAWN_FC2_FILTER_6')
gdpool.assert_called_with('INS54321_PIXEL_SIZE', 0, 1)
def sensor_model_version(self):
assert self.driver.sensor_model_version == 2
def test_detector_center_sample(self):
with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=np.array([12345, 100])) as gdpool, \
patch('ale.drivers.dawn_drivers.spice.bods2c', return_value=54321) as bods2c:
assert self.driver.detector_center_sample == 12345.5
bods2c.assert_called_with('DAWN_FC2_FILTER_6')
gdpool.assert_called_with('INS54321_CCD_CENTER', 0, 2)
def test_detector_center_line(self):
with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=np.array([12345, 100])) as gdpool, \
patch('ale.drivers.dawn_drivers.spice.bods2c', return_value=54321) as bods2c:
assert self.driver.detector_center_line == 100.5
bods2c.assert_called_with('DAWN_FC2_FILTER_6')
gdpool.assert_called_with('INS54321_CCD_CENTER', 0, 2)
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