DAF/CK < DAFCAT: CK CONCATENATION > 6 6 LTL-IEEE FTPSTR: : : : :::ENDFTP SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-27 08:55:28.884 End UTC: 2020-APR-27 15:34:14.549 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Scien ce Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_000__adcsng_temp.txt Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.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 ep hemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different inpu|OG>F>?>ǿt sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References erǿq?|ӿ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters ------------------------------------------------------------------------ ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' m,ӿL;$ҔɑWZ> INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:50 START_TIME = 2020-04-27T08:55:28.884 STOP_TIME = 2020-04-27T15:34:14.549 ******************************************************************************** INTERPOLATION INTERuQvq,>a?VALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-27T08:55:28.884 2020-04-27T15:34:14.549 -------------------------------------------------------------------------------- 2020-04-27T08:55:28.884 2020-04-27T15:34:14.549 ******************************************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth MeaJE? ǿcs%?n Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-27 15:34:14.549 End UTC: 2020-APR-27 15:38:26.550 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_001__adcsng_temp.txt Usage ------------------------------------------------------------------------ I&/? FӿhThis file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.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). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the numbe1 WY(@|ζ55>r of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTEB*P>P7?ݥǿRVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters --------------------------------------------------------------------t˥ǿez?z%8ӿ---- ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ****************************ӿ5u@ڀ~Շ**************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:50 START_TIME = 2020-04-27T15:34:14.549 STOP_TIME = 2020-04-27T15:38:26.550 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-27T15:34:14.549 2020-04-27T15:38:26.550 -------------------------------------------------------------------------------- 2020-04-27T15:34:14.549 2020-04-27T15:38:26.550 ******************************************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternSki*>UU?ions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-27 15:38:26.550 End UTC: 2020-APR-27 22:00:02.589 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------`?x?dNϥǿ(Re ?------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_002__adcsng_temp.txt Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.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). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used v?ϨCӿUE in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTRNY> q;wiz>ERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK YN{Ӑ>lKG_?7|ǿUser Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters ------------------------------------------------------------------------ ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSqjǿ?FӿTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:50 START_TIME = 2020-04-27T15:38:26.550 STOP_TIME = 2020-04-27T22:00:02.589 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-27T15:38:26.550 2020-04-27Kulӿ/z=V=WT22:00:02.589 -------------------------------------------------------------------------------- 2020-04-27T15:38:26.550 2020-04-27T22:00:02.589 ******************************************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ----------------------------------------------------------------x_4ֳ(P> E?-------- Begin UTC: 2020-APR-27 22:00:02.589 End UTC: 2020-APR-27 22:01:14.589 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_003__adcsng_temp.txt Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.tf a Frame Kernel file required to @N.??X!ǿyM? 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). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated qua硲詬?e2ӿzternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter ?3qL;>7 iSA>'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters ------------------------------------------------------------------------ ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ***************************************************i>F6%?y/Ċǿ***************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODU$ǿWq?JӿCT_CREATION_TIME = 2020-04-28T19:33:50 START_TIME = 2020-04-27T22:00:02.589 STOP_TIME = 2020-04-27T22:01:14.589 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-27T22:00:02.589 2020-04-27T22:01:14.589 -------------------------------------------------------------------------------- 2020-04-27T22:00:02.589 2020-04-27T22:01:14.589 ******************************************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service o!1ҫӿO?3؏>n April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-27 22:01:14.589 End UTC: 2020-APR-27 22:03:08.589 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the followi)d4/>OA>%E> ?ng processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_004__adcsng_temp.txt Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.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). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these?;ǿ6m? files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in betwee${?YtӿOS)w>n quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA S)m>Yaa3_hB>PICE Service (ESS) at ESAC: Marc Costa Sitja (+34) 91-8131-457 esa_spice@sciops.esa.int, marc.costa@esa.int MSOPCK Setup Parameters ------------------------------------------------------------------------ ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_T2cL>ɴz?x~ǿIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:51 START_TIME = 2020-04-27T22:01:14.589 STOP_TIME = 2020-04-27T22:03:08.589 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-27T22:01:14.589 2020-04-27T22:03:08.589 -------------------------------------------------------------------------------- 2020-04-27T22:01:14.589 2020-04-27T22:03:08.589 **********************cǿe)݁ ? hӿ********************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-27 22:03:08.589 End UTC: 2020-APR-28 07:02:08.644 Status ------------------------------------------------------------------------ This ke)SEӿ&%o>3c^>rnel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_005__adcsng_temp.txt Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.tf a Frame Kernel file required to establish relationships between frames used in geometry computations. naif0012.tls a Leapseconds Kernel file is used bpou>RB?in conversions between ephemeris time and UTC (coordinated universal time). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile?@?1Sǿͷxհ? resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors 0O尩?ʭӿi> (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters ------------------------------------------------------------------------ ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' ~2g~EP12N>FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:51 START_TIME = 2020-04-27T22:03:08.589 STOP_TIME = 2020-04-28T07:02:08.644 ****************************************/:b>L ?~Gd;ǿ**************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-27T22:03:08.589 2020-04-28T07:02:08.644 -------------------------------------------------------------------------------- 2020-04-27T22:03:08.589 2020-04-28T07:02:08.644 ******************************************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service =========================================================================== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOL8W.ǿ[wֱ?VmӿO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-28 07:02:08.644 End UTC: 2020-APR-28 07:06:20.645 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis. Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_006__adcsng_temp.txt Usage -----------------ӿ"A >EjnS>------------------------------------------------------- This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.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). solo_ANC_soc-sclk_20200416_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quatereLÜ>#/ǩ>{?nions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation intervals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provixI?[}1ǿIc"N?de information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Required Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters --------j?oz?ӿź ---------------------------------------------------------------- ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 CK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID ȀZKFA>G?բ> = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:51 START_TIME = 2020-04-28T07:02:08.644 STOP_TIME = 2020-04-28T07:06:20.645 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUMMARY: ID -144000, COVERG: 2020-04-28T07:02:08.644 2020-04-28T07:06:20.645 -------------------------------------------------------------------------------- 2020-04-28T07:02:08.644 2020-04-28T07:06:20.645 ******************************************************************************** SOLAR-ORBITER Measured CK file by ESA SPICE Service ================================================================7 {>Fu?U%ǿ=========== This file contains SOLO S/C attitude quaternions extracted from the corresponding telemetry housekeeping quaternions data. It has been created with the utility MSOPCK and ADCSng v1.0.9 by the ESA SPICE Service on April 28, 2020. Objects ------------------------------------------------------------------------ This file contains orientation and angular velocity data for the SOLO spacecraft frame, 'SOLO_SRF', relative to the Earth Mean Equator and Equinox of J2000, J2000. The NAIF ID code for SOLO_SRF is -144000. Approximate Time Coverage ------------------------------------------------------------------------ Begin UTC: 2020-APR-28 07:06:20.645 End UTC: 2020-APR-28 18:26:08.714 Status ------------------------------------------------------------------------ This kernel is an operational product of the SOLAR-ORBITER Science Operations Team. It is intended to be used by SOLAR-ORBITER Instrument Teams and scientists for data analysis.B#ǿ)ީW?wʯӿ Pedigree ------------------------------------------------------------------------ ESOC/FD is responsible for Housekeeping data delivering. This file has been created using MSOPCK using as input quaternions from the following processed telemetry file by the SOLAR-ORBITER Science Ground Segment: solo_ANC_soc-quaternions_0641292917-0641413557_007__adcsng_temp.txt Usage ------------------------------------------------------------------------ This file should be used together with the kernel set described below: solo_ANC_soc-sc-fk_V06.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). solo_ANC_soc-sclk_202004RFlbӿ`φ>|e显16_V01.tsca Spacecraft Clock Kernel file is used in conversions between the SOLO Clock time and ephemeris time. The usage of this CK with other versions of these files shall be analysed and handled with care. Accuracy ------------------------------------------------------------------------ In some occasions the measured quaternions may be of reduced quality. For example if the number of stars tracked by the star tracker is not sufficient and the attitude is controlled only based on gyro-information for a period of time, the on-board estimated quaternions can drift. Another reason can be noise in the used telemetry. In such cases the available information would have to be analysed specifically. An attitude profile resulting from such an analysis (based on different input sources) is called "reconstructed" in the current terminology. The CK file is divided in interpolation inte-tw(ʊ> 6]?rvals. The intervals are defined by the MAXIMUM_VALID_INTERVAL of the configuration file (available below). The time set by that parameter determines the maximum time allowed in between two quaternions; if the time in between quaternions exceeds that value a new interpolation interval is defined and no interpolation is performed in between those intervals and therefore this CK does not provide information for that period. If the MAXIMUM_VALID_INTERVAL is not set interpolation is performed for the whole CK coverage. Please note that the current CK incorporate Angular Rates made-up by MSOPCK using the parameter 'MAKE_UP/NO AVERAGING' in the configuration. If this parameter was not present the CK would not be usable by any high level SPICE interfaces that compute state vectors (6x1) or state transformation matrices (6x6). References ------------------------------------------------------------------------ [1] CK Required Reading [2] SCLK Re`&:S?z d ǿ_?quired Reading [3] TIME Required Reading [4] MSOPCK User Guide Contact Information ------------------------------------------------------------------------ If 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 MSOPCK Setup Parameters ------------------------------------------------------------------------ ******************************************************************************** MSOPCK SETUP FILE: msopck_quat.setup ******************************************************************************** \begindata LSK_FILE_NAME = 'lsk/naif0012.tls' SCLK_FILE_NAME = 'sclk/solo_ANC_soc-sclk_20200416_V01.tsc' FRAMES_FILE_NAME = 'fk/solo_ANC_soc-sc-fk_V06.tf' INTERNAL_FILE_NAME = 'SOLO CK; MEASURED; OBTAINED FROM TELEMETRY' CK_TYPE = 3 1T?L;.ӿ-OluCK_SEGMENT_ID = 'SOLO MEASURED ATTITUDE' INSTRUMENT_ID = -144000 REFERENCE_FRAME_NAME = 'J2000' ANGULAR_RATE_PRESENT = 'MAKE UP/NO AVERAGING' MAXIMUM_VALID_INTERVAL = 60 INPUT_TIME_TYPE = 'SCLK' INPUT_DATA_TYPE = 'MSOP QUATERNIONS' INCLUDE_INTERVAL_TABLE = 'YES' CHECK_TIME_ORDER = 'NO' PRODUCER_ID = 'ESA SPICE Service' ******************************************************************************** RUN-TIME OBTAINED META INFORMATION: ******************************************************************************** PRODUCT_CREATION_TIME = 2020-04-28T19:33:52 START_TIME = 2020-04-28T07:06:20.645 STOP_TIME = 2020-04-28T18:26:08.714 ******************************************************************************** INTERPOLATION INTERVALS IN THE FILE SEGMENTS: ******************************************************************************** SEG.SUM=$>MРju>ш>MARY: ID -144000, COVERG: 2020-04-28T07:06:20.645 2020-04-28T18:26:08.714 -------------------------------------------------------------------------------- 2020-04-28T07:06:20.645 2020-04-28T18:26:08.714 ******************************************************************************** m6>.;?qǿ @ :B B J BsB K sB+ B MB + BO B NB B O B B B C BHB C HB 0IB 0IB ژB SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE SOLO MEASURED ATTITUDE p'LhdӿEEp=>q;d?G0?}ǿBYإ?0%ӿY9V:>N>S?M ǿ>?<>ӿ?~>it呰S>*e?.Lǿklb?cӿA>1%.GhM=;>{?2tFǿ? 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