PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2009-10-06, SONC, version 1.0"
/* PVV version 3.13 */

/* Raw data for both housekeeping and science */

/* IDENTIFICATION & DESCRIPTIVE DATA ELEMENTS */

/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE           = UNDEFINED
^FILE=("COS_FXXB1_140409083025_1027.DAT",1<BYTES>)

/* IDENTIFICATION AND DESCRIPTIVE DATA ELEMENTS */

DATA_SET_ID           = "RL-CAL-COSAC-1-PHC-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER CAL COSAC 1 PHC V1.0"
PRODUCT_ID            = "COS_FXXB1_140409083025_1027"
PRODUCT_CREATION_TIME = 2016-12-12T14:06:37
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           = UDR
START_TIME            = 2014-04-09T08:30:25.552
STOP_TIME             = 2014-04-10T01:38:02.552
SPACECRAFT_CLOCK_START_COUNT = "N/A"
SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"

PRODUCER_ID            = "SONC"
PRODUCER_FULL_NAME     = "SCIENCE OPERATIONS AND NAVIGATION CENTER"
PRODUCER_INSTITUTION_NAME = "CNES"

INSTRUMENT_ID          = COSAC
INSTRUMENT_NAME        = "COMETARY SAMPLING AND COMPOSITION EXPERIMENT"
INSTRUMENT_TYPE        = {"GAS CHROMATOGRAPH","MASS SPECTROMETER"}
INSTRUMENT_MODE_ID     = "N/A"
INSTRUMENT_MODE_DESC   = "N/A"
TARGET_NAME           = "CALIBRATION"
TARGET_TYPE           = "CALIBRATION"

PROCESSING_LEVEL_ID    = "1"
DESCRIPTION = "This is a rolbin file, containing raw telemetry packets. 
               The format of COSAC TM packets is described in the file
               RO-LCO-IF-340001.PDF located in the DOCUMENT directory"

DATA_QUALITY_ID   = "-1"
DATA_QUALITY_DESC = "-1 : NOT QUALIFIED"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -101681723.0, 541139602.9, 298975293.2)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (   -1381658.1,  -3406706.3,   -864985.7)
SC_TARGET_VELOCITY_VECTOR = ( 288.031,702.600,173.441)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =     3776614.1 <km>
SUB_SPACECRAFT_LATITUDE =   -20.54 <deg>
SUB_SPACECRAFT_LONGITUDE =    77.23 <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>"

END