PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2018-02-20, SONC, version 1.0"
/* PVV version 3.13 */

/*  Calibrated HK data (Level 3) */

/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE          = FIXED_LENGTH
FILE_RECORDS         = 19
RECORD_BYTES         = 168
FILE_NAME            = "RHK_FH3_140410125040_00009.TAB"


/* DATA OBJECT POINTERS  */

^ROMAP_CALHK_TABLE     = ("RHK_FH3_140410125040_00009.TAB",1 <BYTES>)



DATA_SET_ID         = "RL-CAL-ROMAP-3-PHC-MAG-V1.0"
DATA_SET_NAME       = "ROSETTA-LANDER CAL ROMAP 3 PHC MAG V1.0"
PRODUCT_ID          = "RHK_FH3_140410125040_00009"
PRODUCT_CREATION_TIME = 2018-02-20T09:30:44
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           = 2014-04-10T12:50:40.698
STOP_TIME            = 2014-04-10T13:00:02.448
SPACECRAFT_CLOCK_START_COUNT = "3/355754975.30"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/355755537.22"

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 = "3"
DATA_QUALITY_ID      = "N/A"
DATA_QUALITY_DESC    = "N/A : NOT APPLICABLE"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -102536067.5, 540317653.1, 298613136.3)
/* TARGET PARAMETERS: Position <km>, Velocity <km/s> */
SC_TARGET_POSITION_VECTOR = ("N/A", "N/A", "N/A")
SC_TARGET_VELOCITY_VECTOR = ("N/A", "N/A", "N/A")
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =  "N/A"
SUB_SPACECRAFT_LATITUDE =  "N/A"
SUB_SPACECRAFT_LONGITUDE =  "N/A"
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_CALHK_TABLE
  NAME               = "ROMAP_CALIBRATED_HK"
  INTERCHANGE_FORMAT = ASCII
  ROWS               = 19
  COLUMNS            = 18
  ROW_BYTES          = 168
  ^STRUCTURE         = "ROMAP_CALHK.FMT"
END_OBJECT           = ROMAP_CALHK_TABLE



END