Sample LRT GENPRO-I header

  ELECTRA 583 GAMETAG  23JULY76                     FIRST TIME ON THIS FILE 18 55 29       THIS FILE I
  S ALL OR PART OF TIME PERIOD 18 55 30 TO 21 27 52  DESCRIPTION OF RECORD --  82 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  221 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  6 CYCLES OF 221 SAMP/CYC = 1326 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 442 60 BIT PACKED WORDS          --METHOD OF SCALING--  A BIAS AD(I) WAS ADDED TO EACH SAMPLE
   OF EACH PARAMETER  TO ELIMINATE ANY NEGATIVE VALUES. THE BIASED SAMPLE WAS THEN MULTIPLIED BY P(I)
  TO INSURE THE PROPER NUMBER OF DECIMAL PLACES WERE SAVED.  THE PACKED RECORD MAY BE UNPACKED BY RIGH
  T JUSTIFYING 20 BITS AT A TIME AND REVERSING THE ABOVE SCALING PROCESS. AS EXAMPLE, S(I)=N/P(I)-AD(I
  ), WHERE N IS THE 20 BIT SCALED INTEGER, S(I) THE DESIRED UNSCALED PARAMETER, AD(I),P(I) THE CORRESP
  ONDING SCALE FACTORS  THE ORDER, RATE, PLOT TITLE, PRINT LAB, UNITS, AD AND P SCALE FACTORS OF EACH
  PARAMETER FOLLOW
    1)   1     TIME                                        TIME     SECONDS = (N/    1.0) -    0.0
    2)   1     UNALTERED TAPE TIME (SECONDS)               TPTIME  SECONDS  = (N/    1.0) -    0.0
    3)   1     CORRECTED STATIC PRESSURE (MB)             PSXC      (MB)    = (N/  500.0) -    0.0
    4)   1     AMBIENT TEMPERATURE FUSELAGE (DEG C)       ATX       (C)     = (N/ 1000.0) -  100.0
    5)   1     CORRECTED DEWPOINT TEMPERATURE (C)         DPXC      (C)     = (N/ 1000.0) -  100.0
    6)   1     ABSOLUTE HUMIDITY (THERMOELEC) (GM/M3)      RHOTD    (GM/M3) = (N/ 1000.0) -  100.0
    7)   1     HORIZONTAL WIND DIRECTION (DEG)           WDRCTN     DEGS    = (N/ 1000.0) -    0.0
    8)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      (M/S)   = (N/ 1000.0) -    0.0
    9)   1     WIND VECTOR EAST COMPONENT (M/S)           UI1       (M/S)   = (N/ 1000.0) -  200.0
   10)   1     WIND VECTOR NORTH COMPONENT (M/S)          VI1       (M/S)   = (N/ 1000.0) -  200.0
   11)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)        UX1       (M/S)   = (N/ 1000.0) -  200.0
   12)   1     WIND VECTOR LATERAL COMPONENT (M/S)        VY1       (M/S)   = (N/ 1000.0) -  200.0
   13)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   14)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   15)   1     NACA PRESSURE ALTITUDE (M)                   HP     (M)      = (N/  100.0) -  100.0
   16)   1     PRESSURE DAMPED INERTIAL ALTITUDE (M)       HI31     (M)     = (N/  100.0) -  100.0
   17)   1     GEOMETRIC (RADIO) ALTITUDE (M)               HGM     (M)     = (N/ 1000.0) -  100.0
   18)   1     AIRCRAFT GROUND SPEED (M/S)                GS        (M/S)   = (N/ 1000.0) -    0.0
   19)   1     AIRCRAFT GROUND SPD EAST COMP (M/S)        VEW       (M/S)   = (N/ 1000.0) -  500.0
   20)   1     AIRCRAFT GROUND SPD NORTH COMP (M/S)       VNS       (M/S)   = (N/ 1000.0) -  500.0
   21)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP31      (M/S)   = (N/ 1000.0) -  100.0
   22)   1     AIRCRAFT C.G. VERT ACCELERATION (M/S2)       CGAC1      M/S2 = (N/ 1000.0) -  100.0
   23)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)            THF        DEG  = (N/ 1000.0) -    0.0
   24)   1     ROLL    (DEG)                               ROLL        DEGS = (N/ 1000.0) -  100.0
   25)   1     PITCH   (DEG)                                PITCH      DEGS = (N/ 1000.0) -  100.0
   26)   1     TRUE AIR SPEED (M/SEC)                        TASX     M/SEC = (N/ 1000.0) -  100.0
   27)   1     CORCTD IR SURFACE TEMP (PRT-5) (C)         PRT5C     (C)     = (N/ 1000.0) -  100.0
   28)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   29)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   30)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   31)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   32)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   33)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   34)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   35)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   36)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   37)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   38)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   39)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   40)   1     NOSEBOOM TOTAL TEMP (ROSEMOUNT) (C)        TTB5       (C)    = (N/ 1000.0) -  100.0
   41)   1     FUSELAGE TOTAL TEMP (ROSEMOUNT) (C)        TTF        (C)    = (N/ 1000.0) -  100.0
   42)   1     LHS DEW/FROSTPOINT TEMP (C)                DPLH       (C)    = (N/ 1000.0) -  100.0
   43)   1     RHS DEW/FROSTPOINT TEMP (C)                DPRH       (C)    = (N/ 1000.0) -  100.0
   44)   1     RAW WINGTIP STATIC PRESSURE (MB)           PSW       (MB)    = (N/  500.0) -    0.0
   45)   1     RAW WINGTIP DYNAMIC PRESSURE (MB)          QCW       (MB)    = (N/ 1000.0) -  100.0
   46)   1     RAW NOSEBOOM STATIC PRESSURE (MB)          PSB       (MB)    = (N/  500.0) -    0.0
   47)   1     RAW NOSEBOOM DYNAMIC PRESSURE (MB)         QCB       (MB)    = (N/ 1000.0) -  100.0
   48)   1     RAW INS LATITUDE  (DEG)                     ALAT        DEGS = (N/ 1000.0) -  200.0
   49)   1     RAW INS LONGITUDE  (DEG)                   ALONG        DEGS = (N/ 1000.0) -  200.0
   50)   1     RAW VLF LATITUDE  (DEG)                       VLAT      DEGS = (N/ 1000.0) -  200.0
   51)   1     RAW VLF LONGITUDE  (DEG)                     VLONG      DEGS = (N/ 1000.0) -  200.0
   52)   1      INS VERTICAL VELOCITY (M/S)                 VZI     (M/S)   = (N/  100.0) - 5000.0
   53)   1     INS WANDER ANGLE (DEG)                       ALPHA      DEGS = (N/ 1000.0) -  100.0
   54)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)            THF        DEG  = (N/ 1000.0) -  100.0
   55)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   56)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   57)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   58)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   59)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   60)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   61)   1     PRT-5 IRTRAN WINDOW TEMP (C)              PRTWT      (C)     = (N/ 1000.0) -  100.0
   62)   1     RAW IR SURFACE TEMP(PRT-5) (C)             PRT5      (C)     = (N/ 1000.0) -  100.0
   63)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   64)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   65)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   66)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   67)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   68)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   69)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   70)   1     16MM CAMERA FRAME COUNT                    CAMFC             = (N/    1.0) -    0.0
   71)   1     EVENT MARKERS                             EVENT      MARKS   = (N/    1.0) -    0.0
   72)   1     INS/KNLBRG UPDATE FLAGS                     UPDATE           = (N/    1.0) -    0.0
   73)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       (M/S)   = (N/ 1000.0) -  100.0
   74)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       (M/S)   = (N/ 1000.0) -  100.0
   75)   1      UNUSED                                   UNUSED             = (N/    1.0) -    0.0
   76)  20            ACCELERATION AT C.G.  M/S2          CGAC      (M/S2)  = (N/ 1000.0) -  100.0
   77)  20            LEFT WING STRAIN GAGE M-IN/IN       STRLW   UIN/IN    = (N/  500.0) - 1000.0
   78)  20           RIGHT WING STRAIN GAGE M-IN/IN       STRRW   UIN/IN    = (N/  500.0) - 1000.0
   79)  64     KNOLLENBERG 64 WORDS                      KNLBG       COUNTS = (N/    1.0) -    0.0
   80)   1     CCN OUTPUT CHANNEL 55 (VDC) (DRI)         CCN(55)    VDC     = (N/ 1000.0) -  100.0
   81)   1     CCN OUTPUT CHANNEL 56 (VDC) (DRI)         CCN(56)    VDC     = (N/ 1000.0) -  100.0
   82)  20     NEPHELOMETER BACKSCATTER(VDC) (NCAR)      NEPHSK     VDC     = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  ELECTRA 583 GAMETAG  23JULY76
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 18        55        30         TO   21        27        52
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          232 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       193024 BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  4420 BITS PER LOGICAL DATA RECORD
                            6 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        26520 BITS PER PHYSICAL DATA RECORD