PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2016-12-14, SONC, version 1.0" /* PVV version 3.13 */ /* Calibrated in Lander coordinates (Level 5) */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 10141 RECORD_BYTES = 119 FILE_NAME = "MAG_FSF_140417025012_00169.TAB" /* DATA OBJECT POINTERS */ ^ROMAP_MAG_CALSCF_TABLE = ("MAG_FSF_140417025012_00169.TAB",1 ) DATA_SET_ID = "RL-CAL-ROMAP-5-PHC-MAG-V1.0" DATA_SET_NAME = "ROSETTA-LANDER CAL ROMAP 5 PHC MAG V1.0" PRODUCT_ID = "MAG_FSF_140417025012_00169" PRODUCT_CREATION_TIME = 2016-12-14T16:04:48 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "POST HIBERNATION COMMISSIONING" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-LANDER" INSTRUMENT_HOST_ID = RL OBSERVATION_TYPE = "POST HIBERNATION COMMISSIONING" PRODUCT_TYPE = RDR START_TIME = 2014-04-17T02:50:12.000 STOP_TIME = 2014-04-17T05:39:40.000 SPACECRAFT_CLOCK_START_COUNT = "3/356323747.06" SPACECRAFT_CLOCK_STOP_COUNT = "3/356333915.05" PRODUCER_ID = "SONC" PRODUCER_FULL_NAME = "SCIENCE OPERATIONS AND NAVIGATION CENTER" PRODUCER_INSTITUTION_NAME = "CNES" INSTRUMENT_ID = ROMAP INSTRUMENT_NAME = "ROSETTA LANDER MAGNETOMETER AND PLASMA MONITOR" INSTRUMENT_TYPE = {"FLUXGATE MAGNETOMETER","ELECTROSTATIC ANALYZER", "FARADAY CUP"} DETECTOR_ID = MAG INSTRUMENT_MODE_ID = "N/A" INSTRUMENT_MODE_DESC = "N/A" TARGET_NAME = "CALIBRATION" TARGET_TYPE = "CALIBRATION" PROCESSING_LEVEL_ID = "5" DATA_QUALITY_ID = "1" DATA_QUALITY_DESC = "1 : ABSOLUTE ERROR LESS THAN 5 nT" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -107288571.0, 535679016.8, 296563029.9) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -1188110.8, -2935952.5, -749060.9) SC_TARGET_VELOCITY_VECTOR = ( 289.030,701.024,172.225) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 3254612.6 SUB_SPACECRAFT_LATITUDE = -14.30 SUB_SPACECRAFT_LONGITUDE = 17.54 NOTE = "The values of the keywords SC_SUN_POSITION_VECTOR, SC_TARGET_POSITION_VECTOR and SC_TARGET_VELOCITY_VECTOR are related to the equatorial J2000 inertial frame (EMEJ200). The values of SUB_SPACECRAFT_LATITUDE and SUB_SPACECRAFT_LONGITUDE are northern latitude and eastern longitude in the standard planetocentric IAU_ frame. All values are computed for the time = START_TIME. Distances are given in velocities in , angles in " /* DATA OBJECT DEFINITION */ OBJECT = ROMAP_MAG_CALSCF_TABLE NAME = "ROMAP_MAG_CALSCF" INTERCHANGE_FORMAT = ASCII ROWS = 10141 COLUMNS = 8 ROW_BYTES = 119 ^STRUCTURE = "ROMAP_MAG_CALSCF.FMT" END_OBJECT = ROMAP_MAG_CALSCF_TABLE END