PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2007-07-16, SONC, version 1.0"
/* PVV version 3.8 */

/* Raw data for both housekeeping and science */

/* IDENTIFICATION & DESCRIPTIVE DATA ELEMENTS */

/* FILE CHARACTERISTIC DATA ELEMENTS */

RECORD_TYPE           = UNDEFINED
^FILE="PTO_FRB1_141006184903_0036.DAT" 

/* IDENTIFICATION AND DESCRIPTIVE DATA ELEMENTS */

DATA_SET_ID           = "RL-CAL-PTOLEMY-1-PDCS-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER CAL PTOLEMY 1 PDCS V1.0"
PRODUCT_ID            = "PTO_FRB1_141006184903_0036"
PRODUCT_CREATION_TIME = 2015-06-26T08:10:21
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "PRE DELIVERY CALIB SCIENCE"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL
OBSERVATION_TYPE    = "PRE DELIVERY CALIB SCIENCE"

PRODUCT_TYPE           = UDR
START_TIME            = 2014-10-06T18:49:03.172
STOP_TIME             = 2014-10-06T19:25:03.172
SPACECRAFT_CLOCK_START_COUNT = "3/371242073.40960"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/371244232.61440"

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

INSTRUMENT_ID          = PTOLEMY
INSTRUMENT_NAME        = "PTOLEMY - GAS CHROMATOGRAPH ISOTOPE RATIO
                          MASS SPECTROMETER"
INSTRUMENT_TYPE        = "GAS ISOTOPE RATIO ANALYSER"
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 PTOLEMY TM packets is described in the file
               RO-LPT-RAL-TN-3403.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 = ( -223095807.8, 368243222.0, 219379557.2)
/* 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 EMEJ2000 reference frame.
       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 <km/s>, Angles in <deg>"

END