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

/*  Edited Science data   */

/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE          = FIXED_LENGTH
FILE_RECORDS         = 36900
RECORD_BYTES         = 65
FILE_NAME            = "MAG_FS2_141112174718_00618.TAB"


/* DATA OBJECT POINTERS  */

^ROMAP_MAG_RAWSC_TABLE     = ("MAG_FS2_141112174718_00618.TAB",1 <BYTES>)



DATA_SET_ID         = "RL-C-ROMAP-2-FSS-MAG-V1.0"
DATA_SET_NAME       = "ROSETTA-LANDER 67P ROMAP 2 FSS MAG V1.0"
PRODUCT_ID          = "MAG_FS2_141112174718_00618"
PRODUCT_CREATION_TIME = 2016-12-05T16:26:49
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         = EDR
START_TIME           = 2014-11-12T17:47:18.287
STOP_TIME            = 2014-11-13T04:05:34.268
SPACECRAFT_CLOCK_START_COUNT = "3/374435167.04"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374472263.03"

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 = "2"
DATA_QUALITY_ID      = "4"
DATA_QUALITY_DESC    =  "4: absolute error exceed 100 nT"


/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -242574214.1, 320480542.3, 196105666.9)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (          6.4,       -16.6,        -0.7)
SC_TARGET_VELOCITY_VECTOR = (  0.509, 0.088, 0.006)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          15.9 <km>
SUB_SPACECRAFT_LATITUDE =    -4.89 <deg>
SUB_SPACECRAFT_LONGITUDE =   311.16 <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_RAWSC_TABLE
  NAME               = "ROMAP_MAG EDITED SCIENCE DATA"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 36900
  COLUMNS            = 5
  ROW_BYTES          = 65
  ^STRUCTURE         = "ROMAP_MAG_RAWSC.FMT"
END_OBJECT           = ROMAP_MAG_RAWSC_TABLE



END