PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2010-12-09, 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=("MUP_XXXB1_141112153423.DAT",1<BYTES>)

/* IDENTIFICATION AND DESCRIPTIVE DATA ELEMENTS */

DATA_SET_ID           = "RL-C-MUPUS-1-RBD-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER 67P MUPUS 1 RBD V1.0"
PRODUCT_ID            = "MUP_XXXB1_141112153423"
PRODUCT_CREATION_TIME = 2017-02-14T16:33:41
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           = UDR
START_TIME            = 2014-11-12T15:34:23.552
STOP_TIME             = 2014-11-12T17:30:16.552
SPACECRAFT_CLOCK_START_COUNT = "3/374427192.25"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374434145.25"

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

INSTRUMENT_ID          = MUPUS
INSTRUMENT_NAME        = "MULTI PURPOSE SUITE FOR SURFACE AND
                         SUBSURFACE SCIENCE"
INSTRUMENT_TYPE        = {"PENETROMETER THERMAL PROBE","INFRARED 
                          RADIOMETER","ACCELEROMETER"}
TARGET_NAME           = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)"
TARGET_TYPE           = "COMET"

PROCESSING_LEVEL_ID    = "1"
DESCRIPTION = "This is a rolbin file, containing raw telemetry packets. 
               The format of MUPUS 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 = ( -242529690.1, 320605682.6, 196167342.3)
/* 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 =   240.51 <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