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Mission Operations Downlink Processing

An example of the first portion of the engineering information obtained for the project is illustrated by the Viking Lander 1, Sol 1,694 "MK4" output which lists data frames and Deep Space Network performance for the downlink. The standard "link" consists of 30 minutes of spacecraft commanding and low data rate communications between DSN and the lander at 8-1/3 bits/second followed by 30 minutes of engineering and science downlink at 1,000 bits/sec.

The downlinked Viking data are stored frame by frame and each frame is either an engineering or science frame for one of the instruments. A 31 bit pseudo-random synchronization word begins every data frame followed by the instrument's Format identifier, ID, which describes the structure and expected length of the frame. In the output below, the "ID" is followed by the type of frame. FMT4 and FMT5 contain engineering data, including our atmospheric pressure, while METE indicates a meteorology frame. Each meteorology frame nominally contains 16 sequential scans of wind and temperature sensor data, and room for a 17th; the 17th is used if the Guidance and Sequencing Computer is too busy to read out the VMIS memory after it sets its "data ready" flag bit. The total memory of VMIS is 5,120 bits. Note, each meteorology frame is surrounded by an engineering frame so we can obtain atmospheric pressure.

For more robust extraction under difficult conditions, i.e., low signal/noise, we search for a 15 bit subset of 31 bit synchronization word and, when found, then check the rest of the synch word and the instrument ID to see if it is a valid frame. "NO SYNCH" means that no synch word was found at the beginning of the frame, generally due to missing or corrupted data. These frames have a fair number of errors since the signal/noise ratio, S/N, expressed in decibels, is around 3.0 DB. 3.0 DB means that the signal is only twice as large as the system noise!

 *UW DECSET REV   8.01     11/12/87     14:13:01
 *
 *       INPUT DATA FILE: IDR>VL1.INPUT>E8197
 *   TAPE STRUCTURE FILE: DATA.V>DECSET>BYTE1.HIR
 *      DECOM/DECAL FILE: DATA.V>DECSET>DECAL.VL1.REV.8.00.870811
 *TIME UTILITY DATA BASE: DATA.V>TIMING>VL1.TABLE.REV.2
 *
 *     VIKING LANDER:     1
 *             EPOCH:    16
 *  EXTERNAL TAPE ID: E8197
 *DEEP SPACE STATION:    43	Canberra Australia, 64 meters diameter parabolic dish antenna
 *        SPACECRAFT:    26
 *       PASS NUMBER:  1697
 *       TAPE NUMBER:    01
 *         FILE TYPE:   TLM
 *         DATA TYPE:   TLM                                       INT BIT SYNCH.. ..SYMBOL SYNCH
 *   LINK START TIME: 81 119 00:35:00   RUN: 119  0:57:56.30      DEMODULATOR.. . . ..DDA
 *   LINK  STOP TIME: 81 119 02:00:00   RUN: 119  1: 1:27.90       RECEIVER.. . . . . ..BLOCK DECODER
 *-----------------------------------    . . . . . .
 *ID   TYPE    GCSC TIME  REC # SYNCH       ERT              LLT       BLCK . . . . . .  S/N  BITS * ERR
 *- ---- ------ --- --- -------- -------- -- - - - - - - --- -- - --
     NO SYNCH               270       119  0:57:55.40                   797 0 0 0 0 0 0   3.0   43
  24 BAD FID                270     1 119  0:57:55.45                   797 0 0 0 0 0 0   3.0    0
     NO SYNCH               270       119  0:57:55.45                   797 0 0 0 0 0 0   3.0  792
  25 FMT4          171008   270     2 119  0:57:56.24 1693 20:25: 5.89  797 0 0 0 0 0 0   3.0  792
  25 FMT4          540864   270     3 119  0:57:57.04 1693 21:26:44.40  798 0 0 0 0 0 0   3.0  792
  26 FMT5          540928   270     4 119  0:57:57.82 1693 21:26:45.04  799 0 0 0 0 0 0   3.0  768
  10 BAD FID                270     5 119  0:57:58.59                   800 0 0 0 0 0 0   3.0    0
     NO SYNCH               270       119  0:57:58.59                   800 0 0 0 0 0 0   3.0 1536
  26 FMT5          152704   271     6 119  0:58: 0.13 1693 20:22: 2.85  802 0 0 0 0 0 0   3.1  768
etc.
     NO SYNCH               279       119  0:58:41.86                   846 0 0 0 0 0 0   3.1   48    13
  25 FMT4         4239424   282    40 119  0:58:55.37 1694  7: 3:34.29  861 0 0 0 0 0 0   3.2  784
   7 METE         3742720   282    41 119  0:58:56.15 1694  5:40:47.31  861 0 0 0 0 0 0   3.2 5168
  25 FMT4         4609280   284    42 119  0:59: 1.32 1694  8: 5:12.81  867 0 0 0 0 0 0   3.7  792
  25 FMT4         4979136   284    43 119  0:59: 2.11 1694  9: 6:51.32  868 0 0 0 0 0 0   3.7  784
   7 METE         4388864   284    44 119  0:59: 2.89 1694  7:28:28.67  869 0 0 0 0 0 0   3.7 5168
  25 FMT4         5349056   285    45 119  0:59: 8.06 1694 10: 8:30.47  874 0 0 0 0 0 0   3.7  784
etc.
  25 FMT4        20883136   310    99 119  1: 1: 3.91 1696  3:58:18.84  998 0 0 0 0 0 0   3.9  784
   7 METE        18903040   310   100 119  1: 1: 4.69 1695 23: 7:53.38  999 0 0 0 0 0 0   3.9 5168
     NO SYNCH               310       119  1: 1: 4.69                   999 0 0 0 0 0 0   3.9   47    13
     NO SYNCH               311       119  1: 1: 9.90                  1004 0 0 0 0 0 0   4.0  737
      26           6             0            1
	
Decoding engineering data from this downlink from a few of the above frames produces the below results. These values come from the above MK4 frames with the corresponding "SYNCH" numbers. For example at Lander Local time "1693 20:25: 5.89" below, frame "2", had a digital value of "123" "DN" for AMBPRESS, which converts to atmospheric pressure of "8.2610" millibars at the surface of Mars. "CAMBT" is the temperature in degrees Kelvin, K of the footpad temperature sensor. ( 0° K = Absolute zero, 273° K = 0° Celsius, 373° K = 100° C )
 *----------------------------------------
 *PG 1   LLT      SYNCH      AMBPRESS           CAMBT              CAMBPOST           EP & ID  
 *                         DN     EU          DN     EU          DN     EU          DN     EU  
 *-------- --- --- ------ --- ------ --- ------ --- ----
  1693 20:25: 5.89     2   123   8.2610             229.00             227.06        16 E8197
  1693 21:26:44.40     3   124   8.3480             216.67             215.13        16 E8197
  1693 21:26:45.04     4     1  0.00000                                              16 E8197  
  1693 20:22: 2.85     6   129   8.7830                                              16 E8197  
etc.
  1694  7: 3:34.29    40   127   8.6090             198.28             346.72        16 E8197
  1694  8: 5:12.81    42   170   12.370             197.26             197.74        16 E8197
  1694  9: 6:51.32    43   129   8.7830             196.11             197.74        16 E8197
  1694 10: 8:30.47    45   128   8.6960             268.62             197.12        16 E8197
etc.
  1696  3:58:18.84    99   125   8.4350             204.02             275.15        16 E8197
  1696  6: 1:35.87   102   125   8.4350             200.07             200.58        16 E8197
  1696  7: 3:14.38   103   126   8.5220             199.17             200.82        16 E8197

	

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Next: Real time from Mars Up: UW Viking Computer Facility: Previous: Enabling Mission Continuation for
Jim Tillman
2004-08-05