DAF/CK em16_tgo_sc_smp_032_00_02_{start_date}_{finish_date}_f201802 P ., LTL-IEEE FTPSTR: : : : :::ENDFTP ExoMars2016 TGO CK file by ESA SPICE Service =========================================================================== This file contains quaternions and angular rates of the TGO spacecraft extracted from the corresponding predicted attitude data OASW file produced by the SOC on June 23, 2020. It has been created with the utility MEX2KER and ADCSng v1.4.1 by the ESA SPICE Service on June 23, 2020. Objects -------------------------------------------------------- This file contains orientation and angular velocity data for the ExoMars2016 TGO spacecraft frame, 'TGO_SPACECRAFT', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for TGO_SPACECRAFT is -143000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-SEP-05 13:03:10.000 End UTC: 2020-OCT-03 13:39:06.089 Status ------------------------------------------------------------------------ This kernelf c & is an operational product of the ExoMars2016 TGO Science Operations Team. It is intended to be used by ExoMars2016 TGO science operations engineers for science planning. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Auxiliary Data delivering. This file has been created using MEX2KER using as input the OASW file provided by the ExoMars2016 TGO Science Operations Team on June 23, 2020, and the configuration file appended at the end of this comments section. TGO source file name = SATP_DM_032_00_02_00000.EXM Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: em16_tgo_v19.tf a Frame Kernel file required to establish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used in conversions between ephemeris time and UTC (coordinated universal time). em16_tgo_fict_20180215.tsc a Spacecraft Clock Kernel file is used in conversions between the TGO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy -------------------------------------------------------- N/A References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MEX2KER User Guide [5] "EXOMARS Flight Dynamics Interface Control Document (ICD)'', EXM-GS-ICD-ESC-50001, issue 1.5, 2015-09-04 Contact Information ------------------------------------------------------------------------ If tp?^?Qr:?you have any questions regarding this file contact the ESA SPICE Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.int MEX2KER Setup Parameters -------------------------------------------------------- ******************************************************************************** MEX2KER RUN DATE/TIME: 2020-06-23T14:20:05 MEX2KER SETUP FILE: mex2ker_attitude_plan.setup MEX2KER INPUT FILE: SATP_DM_032_00_02_00000.EXM MEX2KER OUTPUT FILE: em16_tgo_sc_smp_032_00_02_{start_date}_{finish_date}_f20180215_v{version}.bc OUTPUT FILE STATUS: NEW FILE ******************************************************************************** The nominal SCLK rate shown below has units of seconds/tick. It is equivalent to 65536 ticks/second \begindata LEAPSECONDS_FILE = 'lsk/naif0012.tls' SCLK_KERNEL = 'sclk/em16_tgo_fict_20180215.tsc' KERNELS_TO_LOAD = ('fk/em16_tgGXZ/?z8-#?o_v19.tf') INTERPOLATION_METHOD = 'LAGRANGE' INTERPOLATION_DEGREE = 9 NOMINAL_SCLK_RATE = 1.52587890625e-05 APPEND_TO_OUTPUT = 'NO' STRING_MAPPING = ('EME2000','J2000', 'EXOMARS-ORBITER','TGO SPACECRAFT PLAN' ) NAIF_BODY_NAME = 'TGO SPACECRAFT PLAN' NAIF_BODY_CODE = -143002 ******************************************************************************** ******************************************************************************** MSOPCK SETUP FILE: msopck_plan.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/em16_tgo_step_20200411.tsc' FRAMES_FILE_NAME = 'fk/em16_tgo_v19.tf' INTERNAL_FILE_NAME = 'TGO_SPACECRAFT_PLAN CK; PLANNING ATTITUDE MAPPING' CK_TYPE = 3 CK_SEGMENT_ID = 'SPACECRAFT_PLAN TO SPACECRAFT MAPPING' INSTRUMENT_ID fk?O?׆0uz| = -143000 REFERENCE_FRAME_NAME = 'TGO_SPACECRAFT_PLAN' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' INPUT_TIME_TYPE = 'UTC' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-06-23T14:20:10 START_TIME = 2020-09-05T13:04:10.000 STOP_TIME = 2020-10-03T13:38:06.088 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -143000, COVERG: 2020-09-05T13:04:10.000 2020-10-03T13:38:06.088 ---------------------------------------------------------------------f ----------- 2020-09-05T13:04:10.000 2020-10-03T13:38:06.088 ******************************************************************************** j`>t?AD?m 5@ 9@ s_۠B_۠Bf _۠B a۠Bf / a۠B Sa۠Bf 0 D Sa۠BKc۠Bf E c Kc۠B1Ζc۠Bf d } 1Ζc۠Bz)c,v۠Bf ~ z)c,v۠BKv۠Bf Kv۠B"s~۠Bf "s~۠BQk۠Bf + Qk۠Bz]۠Bf , r z]۠B.sx۠Bf s .sx۠B6\c۠Bf 6\c۠BN`ܚ۠Bf N`ܚ۠Bs۠Bf 9 s۠B>\۠Bf : S >\۠B ۠Bf T r ۠B ׯ۠Bf s ׯ۠B ۠Bf ۠B ӳ۠Bf ӳ۠B 7۠Bf 7۠B۠Bf ۠BE۠Bf c E۠B۠Bf d } ۠B e۠Bf ~ e۠B%۠Bf SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM SATP_DM_032_00_02_00000.EXM GXZ/?z8-#?E?*W?H~ o8v?y?g0?h4|ț?_BxF?Wa;?&zIpP%Y|? s_۠B_۠B_۠B s_۠B > ? $@ ? @_BxF?Wa;?&zIpP%Y|?Z.??~Zܖ?u4}?V,Ī??y4?G?/?k?