PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2016-12-05, SONC, version 1.0"
/* PVV version 3.13 */

/*  Draft Calibrated in ECLIP J2000 coordinates (Level 3)      */

/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE          = FIXED_LENGTH
FILE_RECORDS         = 7140
RECORD_BYTES         = 119
FILE_NAME            = "MAG_FSD_141113063107_00119.TAB"


/* DATA OBJECT POINTERS  */

^ROMAP_MAG_CALSCD_TABLE     = ("MAG_FSD_141113063107_00119.TAB",1 <BYTES>)



DATA_SET_ID         = "RL-C-ROMAP-3-FSS-MAG-V1.0"
DATA_SET_NAME       = "ROSETTA-LANDER 67P ROMAP 3 FSS MAG V1.0"
PRODUCT_ID          = "MAG_FSD_141113063107_00119"
PRODUCT_CREATION_TIME = 2016-12-05T16:36:46
MISSION_NAME         = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME  = "FIRST SCIENCE SEQUENCE"
MISSION_ID           = ROSETTA
INSTRUMENT_HOST_NAME = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID   = RL
OBSERVATION_TYPE    = "FIRST SCIENCE SEQUENCE"

PRODUCT_TYPE         = RDR
START_TIME           = 2014-11-13T06:31:07.239
STOP_TIME            = 2014-11-13T08:30:35.398
SPACECRAFT_CLOCK_START_COUNT = "3/374480996.02"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374488164.07"

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         = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)"
TARGET_TYPE         = "COMET"

PROCESSING_LEVEL_ID = "3"
DATA_QUALITY_ID      = "2"
DATA_QUALITY_DESC    =  "2: absolute error less than 10 nT"


/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -242829654.1, 319760816.1, 195750863.8)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (         14.7,        -0.0,       -11.5)
SC_TARGET_VELOCITY_VECTOR = (  0.092, 0.421,-0.254)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          16.7 <km>
SUB_SPACECRAFT_LATITUDE =   -12.38 <deg>
SUB_SPACECRAFT_LONGITUDE =   219.57 <deg>
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_<TARGET_NAME> frame.
       All values are computed for the time = START_TIME.
       Distances are given in <km> velocities in <m/s>, angles in <deg>"

/* DATA OBJECT DEFINITION  */


OBJECT               = ROMAP_MAG_CALSCD_TABLE
  NAME               = "ROMAP_MAG_CALSCD"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 7140
  COLUMNS            = 8
  ROW_BYTES          = 119
  ^STRUCTURE         = "ROMAP_MAG_CALSCD.FMT"
END_OBJECT           = ROMAP_MAG_CALSCD_TABLE



END