PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2016-12-14, SONC, version 1.0" /* PVV version 3.13 */ /* Calibrated HK data (Level 5) */ /* FILE CHARACTERISTIC DATA ELEMENTS */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 33 RECORD_BYTES = 168 FILE_NAME = "RHK_FH3_140410121541_00017.TAB" /* DATA OBJECT POINTERS */ ^ROMAP_CALHK_TABLE = ("RHK_FH3_140410121541_00017.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 = "RHK_FH3_140410121541_00017" PRODUCT_CREATION_TIME = 2016-12-14T16:05:11 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 = 2014-04-10T12:15:41.041 STOP_TIME = 2014-04-10T12:33:02.823 SPACECRAFT_CLOCK_START_COUNT = "3/355752876.09" SPACECRAFT_CLOCK_STOP_COUNT = "3/355753918.02" 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 = "N/A" DATA_QUALITY_DESC = "N/A : NOT APPLICABLE" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -102518489.3, 540334601.0, 298620607.1) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -1352871.7, -3336518.2, -847665.9) SC_TARGET_VELOCITY_VECTOR = ( 288.185,702.351,173.249) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 3698802.1 SUB_SPACECRAFT_LATITUDE = -13.98 SUB_SPACECRAFT_LONGITUDE = 165.85 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_CALHK_TABLE NAME = "ROMAP_CALIBRATED_HK" INTERCHANGE_FORMAT = ASCII ROWS = 33 COLUMNS = 18 ROW_BYTES = 168 ^STRUCTURE = "ROMAP_CALHK.FMT" END_OBJECT = ROMAP_CALHK_TABLE END