PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2016-12-14, SONC, version 1.0"
/* PVV version 3.13 */

/*  Edited Science data   */

/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE          = FIXED_LENGTH
FILE_RECORDS         = 6870
RECORD_BYTES         = 65
FILE_NAME            = "MAG_FS2_141112153406_00116.TAB"


/* DATA OBJECT POINTERS  */

^ROMAP_MAG_RAWSC_TABLE     = ("MAG_FS2_141112153406_00116.TAB",1 <BYTES>)



DATA_SET_ID         = "RL-C-ROMAP-2-RBD-MAG-V1.0"
DATA_SET_NAME       = "ROSETTA-LANDER 67P ROMAP 2 RBD MAG V1.0"
PRODUCT_ID          = "MAG_FS2_141112153406_00116"
PRODUCT_CREATION_TIME = 2016-12-14T17:09:38
MISSION_NAME         = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME  = "REBOUNDS"
MISSION_ID           = ROSETTA
INSTRUMENT_HOST_NAME = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID   = RL
OBSERVATION_TYPE    = "REBOUNDS"

PRODUCT_TYPE         = EDR
START_TIME           = 2014-11-12T15:34:06.690
STOP_TIME            = 2014-11-12T17:30:47.755
SPACECRAFT_CLOCK_START_COUNT = "3/374427175.17"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374434176.19"

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    =  "Absolute error exceed 100 nT"


/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -242529595.9, 320605947.2, 196167472.6)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (          2.4,       -17.2,        -0.7)
SC_TARGET_VELOCITY_VECTOR = (  0.513, 0.071, 0.005)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          15.5 <km>
SUB_SPACECRAFT_LATITUDE =    -8.01 <deg>
SUB_SPACECRAFT_LONGITUDE =   240.37 <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               = 6870
  COLUMNS            = 5
  ROW_BYTES          = 65
  ^STRUCTURE         = "ROMAP_MAG_RAWSC.FMT"
END_OBJECT           = ROMAP_MAG_RAWSC_TABLE



END