PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-02-28, SONC, version 1.0"
/* PVV version 3.13 */

/* Edited SC data from DIM Burst Continuous Test Mode (SONC Level 2) */

DATA_SET_ID           = "RL-C-SESAME-2-SDL-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER 67P SESAME 2 SDL V1.0"
PRODUCT_ID            = "SES_FS2_DBT_1411121440"
PRODUCT_CREATION_TIME = 2017-02-28T17:39:12
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "SEPARATION DESCENT LANDING"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = EDR
START_TIME            = 2014-11-12T14:40:04.002
STOP_TIME             = 2014-11-12T14:44:23.595
SPACECRAFT_CLOCK_START_COUNT = "3/374423932.25"
SPACECRAFT_CLOCK_STOP_COUNT  = "3/374424192.12"

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

INSTRUMENT_ID          = SESAME
INSTRUMENT_NAME        = "SURFACE ELECTRIC SOUNDING AND
                       ACOUSTIC MONITORING EXPERIMENT"
INSTRUMENT_TYPE        = {"ACOUSTIC SENSOR", "DUST IMPACT DETECTOR",
                       "PERMITTIVITY PROBE"}
TARGET_NAME           = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)"
TARGET_TYPE           = "COMET"

PROCESSING_LEVEL_ID   = "2"
DATA_QUALITY_ID        = "-1"
DATA_QUALITY_DESC      = "-1 : NOT QUALIFIED"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -242511485.0, 320656823.2, 196192545.8)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (          0.7,       -17.5,        -0.7)
SC_TARGET_VELOCITY_VECTOR = (  0.514, 0.064, 0.005)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =          15.5 <km>
SUB_SPACECRAFT_LATITUDE =    -7.82 <deg>
SUB_SPACECRAFT_LONGITUDE =   217.18 <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                        = FILE
   RECORD_TYPE                   = FIXED_LENGTH
   RECORD_BYTES                  = 76
   FILE_RECORDS                  = 3
   ^BCT_PAR_TABLE                  = "SES_FS2_DBT_1411121440_PAR.TAB"
   OBJECT               = BCT_PAR_TABLE
      NAME               = "BCT_PAR"
      INTERCHANGE_FORMAT = ASCII
      ROWS               = 3
      COLUMNS            = 12
      ROW_BYTES          = 76
      ^STRUCTURE         = "DIM_BCTEST2_PAR_FM3.FMT"
   END_OBJECT           = BCT_PAR_TABLE
END_OBJECT                  = FILE

OBJECT                        = FILE
   RECORD_TYPE                   = FIXED_LENGTH
   RECORD_BYTES                  = 42
   FILE_RECORDS                  = 483
   ^BCT_SIG_TABLE                  = "SES_FS2_DBT_1411121440_SIG.TAB"
   OBJECT               = BCT_SIG_TABLE
      NAME               = "BCT_SIG"
      INTERCHANGE_FORMAT = ASCII
      ROWS               = 483
      COLUMNS            = 6
      ROW_BYTES          = 42
      ^STRUCTURE         = "DIM_BCTEST2_SIG_FM3.FMT"
   END_OBJECT           = BCT_SIG_TABLE
END_OBJECT                  = FILE



END