PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = "2017-03-06, SONC, version 1.0" /* PVV version 3.13 */ /* Edited SC data from DIM Power Check Mode (SONC Level 2) */ RECORD_TYPE = FIXED_LENGTH FILE_RECORDS = 3 RECORD_BYTES = 64 FILE_NAME = "SES_FS2_DPC_1404152021.TAB" /* DATA OBJECT POINTERS */ ^PC_TABLE = ("SES_FS2_DPC_1404152021.TAB",1 ) DATA_SET_ID = "RL-CAL-SESAME-2-PHC-V1.0" DATA_SET_NAME = "ROSETTA-LANDER CAL SESAME 2 PHC V1.0" PRODUCT_ID = "SES_FS2_DPC_1404152021" PRODUCT_CREATION_TIME = 2017-03-06T15:48:50 MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "POST HIBERNATION COMMISSIONING" MISSION_ID = ROSETTA INSTRUMENT_HOST_NAME = "ROSETTA-LANDER" INSTRUMENT_HOST_ID = RL PRODUCT_TYPE = EDR START_TIME = 2014-04-15T20:21:33.459 STOP_TIME = 2014-04-15T20:25:13.209 SPACECRAFT_CLOCK_START_COUNT = "3/356214028.15" SPACECRAFT_CLOCK_STOP_COUNT = "3/356214248.07" PRODUCER_ID = "SONC" PRODUCER_FULL_NAME = "SCIENCE OPERATIONS AND NAVIGATION CENTER" PRODUCER_INSTITUTION_NAME = "CNES" INSTRUMENT_ID = SESAME INSTRUMENT_NAME = "SURFACE ELECTRIC SOUNDING AND ACOUSTIC MONITORING EXPERIMENT" INSTRUMENT_TYPE = {"ACOUSTIC SENSOR", "DUST IMPACT DETECTOR", "PERMITTIVITY PROBE"} TARGET_NAME = "CALIBRATION" TARGET_TYPE = "CALIBRATION" PROCESSING_LEVEL_ID = "2" DATA_QUALITY_ID = "-1" DATA_QUALITY_DESC = "-1 : NOT QUALIFIED" /* GEOMETRY PARAMETERS */ /* SPACECRAFT LOCATION: Position */ SC_SUN_POSITION_VECTOR = ( -106373245.3, 536581247.3, 296962608.3) /* TARGET PARAMETERS: Position , Velocity */ SC_TARGET_POSITION_VECTOR = ( -1219814.2, -3012881.2, -767967.4) SC_TARGET_VELOCITY_VECTOR = ( 288.864,701.239,172.404) /* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */ SPACECRAFT_ALTITUDE = 3339934.3 SUB_SPACECRAFT_LATITUDE = -16.90 SUB_SPACECRAFT_LONGITUDE = 219.25 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 = PC_TABLE NAME = "PC" INTERCHANGE_FORMAT = ASCII ROWS = 3 COLUMNS = 5 ROW_BYTES = 64 ^STRUCTURE = "DIM_PC.FMT" END_OBJECT = PC_TABLE END