Sample HRT GENPRO-I header

  583A-03 ELECTRA GAMETAG 09AUG 19/52/25            FIRST TIME ON THIS FILE 19 52 26       THIS FILE I
  S ALL OR PART OF TIME PERIOD 19 52 25 TO 26  0 13  DESCRIPTION OF RECORD -- 116 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  749 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  2 CYCLES OF 749 SAMP/CYC = 1498 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 500 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     PROCESSOR TIME (SECONDS) AFTER MIDNIGHT    TIME       SEC    = (N/    1.0) -    0.0
    2)   1     UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT    TPTIME    SEC    = (N/    1.0) -    0.0
    3)   1     CORRECTED STATIC PRESSURE (MB)               PSXC1    MB     = (N/  500.0) -    0.0
    4)   1     AMBIENT TEMP (FUSELAGE ROSEMOUNT) (C)        ATF1     C      = (N/ 1000.0) -  100.0
    5)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
    6)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPXC       C      = (N/ 1000.0) -  100.0
    7)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
    8)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)       RHOTD     G/M3   = (N/ 1000.0) -  100.0
    9)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   10)   1     HORIZONTAL WIND DIRECTION (DEG)             WDRCTN    DEG    = (N/ 1000.0) -    0.0
   11)   1     HORIZONTAL WIND SPEED (M/S)                  WSPD     M/S    = (N/ 1000.0) -    0.0
   12)   1     WIND VECTOR EAST COMPONENT (M/S)               UI1    M/S    = (N/ 1000.0) -  200.0
   13)   1       T                         (M/S)              VI1    M/S    = (N/ 1000.0) -  200.0
   14)   1     WIND VECTOR VERT GUST COMPONENT (M/S)          WI1    M/S    = (N/ 1000.0) -  100.0
   15)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)            UX1    M/S    = (N/ 1000.0) -  200.0
   16)   1     WIND VECTOR LATERAL COMPONENT (M/S)            VY1    M/S    = (N/ 1000.0) -  200.0
   17)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   18)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   19)   1     NACA PRESSURE ALTITUDE (M)                   HP       M      = (N/  100.0) -  100.0
   20)   1     PRESSURE DAMPED INERTIAL ALTITUDE (M)         HI31    M      = (N/  100.0) -  100.0
   21)   1     GEOMETRIC (RADIO) ALTITUDE (M)               HGM      M      = (N/ 1000.0) -  100.0
   22)   1     RAW AIRCRAFT (INS) GROUND SPEED (M/S)       GSF1      M/S    = (N/ 1000.0) -    0.0
   23)   1     AIRCRAFT GROUND SPD EAST COMP (M/S)        VEW1       M/S    = (N/ 1000.0) -  500.0
   24)   1     AIRCRAFT GROUND SPD NORTH COMP (M/S)      VNS1        M/S    = (N/ 1000.0) -  500.0
   25)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)          WP31     M/S    = (N/ 1000.0) -  100.0
   26)   1     AIRCRAFT C.G. VERT ACCELERATION (M/S2)     CGAC1      M/S2   = (N/ 1000.0) -  100.0
   27)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)            THF1     DEG    = (N/ 1000.0) -    0.0
   28)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)          ROLL1     DEG    = (N/ 1000.0) -  100.0
   29)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)      PITCH1       DEG    = (N/ 1000.0) -  100.0
   30)   1     AIRCRAFT TRUE AIRSPEED (M/S)                 TASX1    M/S    = (N/ 1000.0) -  100.0
   31)   1     CORCTD RADIOMTRC SURFACE TEMP (PRT-5)(C)    PRT5C     C      = (N/ 1000.0) -  100.0
   32)   1     DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2)      UPYR1     W/M2   = (N/  500.0) -  100.0
   33)   1     DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2)      UPYR2     W/M2   = (N/  500.0) -  100.0
   34)   1     DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2)      UPYR3     W/M2   = (N/  500.0) -  100.0
   35)   1     UPWARD SW/WG-7 IRRADIANCE (WATTS/M2)        LPYR1     W/M2   = (N/  500.0) -  100.0
   36)   1     UPWARD SW/OG-1 IRRADIANCE (WATTS/M2)        LPYR2     W/M2   = (N/  500.0) -  100.0
   37)   1     UPWARD SW/RG-8 IRRADIANCE (WATTS/M2)        LPYR3     W/M2   = (N/  500.0) -  100.0
   38)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   39)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   40)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   41)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   42)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   43)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   44)   1     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)        TTB1     DEG   = (N/ 1000.0) -  100.0
   45)   1     TOTAL TEMP (FUSELAGE ROSEMOUNT) (C)           TTF1    C      = (N/ 1000.0) -  100.0
   46)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   47)   1     DEW/FROST POINT TEMP (L THERMOELEC) (C)       DPL     C      = (N/ 1000.0) -  100.0
   48)   1     DEW/FROST POINT TEMP (R THERMOELEC) (C)       DPR     C      = (N/ 1000.0) -  100.0
   49)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   50)   1     RAW STATIC PRESSURE (WINGTIP) (MB)            PSW1    MB     = (N/  500.0) -    0.0
   51)   1     RAW DYNAMIC PRESSURE (WINGTIP) (MB)           QCW1    MB     = (N/ 1000.0) -  100.0
   52)   1     RAW STATIC PRESSURE (BOOM) (MB)               PSB1    MB     = (N/  500.0) -    0.0
   53)   1     RAW DYNAMIC PRESSURE (BOOM) (MB)              QCB1    MB     = (N/ 1000.0) -  100.0
   54)   1     RAW INS LATITUDE (DEG)                        ALAT    DEG    = (N/ 1000.0) -  200.0
   55)   1     RAW INS LONGITUDE (DEG)                      ALONG    DEG    = (N/ 1000.0) -  200.0
   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     INS WANDER ANGLE (DEG)                       ALPHA    DEG    = (N/ 1000.0) -  100.0
   60)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)           THI     DEG    = (N/ 1000.0) -  100.0
   61)   1     SULFUR DIOXIDE (DREXEL)(GAIN=1) (VDC)       DRSO2      VDC   = (N/ 1000.0) -  100.0
   62)   1     SULFUR DIOXIDE (DREXEL)(GAIN=10) (VDC)      DRSO2      VDC   = (N/ 1000.0) -  100.0
   63)   1     PRESSURE,BANDY (DREXEL)  (VDC)              DRPRB      VDC   = (N/ 1000.0) -  100.0
   64)   1     NITROGEN OXIDES (YORK)  (VDC)               NOX        VDC   = (N/ 1000.0) -  100.0
   65)   1     NITROGEN OXIDES HOUSEKEEPING (YORK)(VCD)    NOXHK      VDC   = (N/ 1000.0) -  100.0
   66)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   67)   1     PRT-5 IRTRAN WINDOW TEMPERATURE (C)        PRT5WT     C      = (N/ 1000.0) -  100.0
   68)   1     RAW RADIOMETRIC SURFACE TEMP (PRT-5) (C)   PRT5       C      = (N/ 1000.0) -  100.0
   69)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   70)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   71)   1     U-V SPECTROMETER OUTPUT  (VDC)              UVSPO      VDC   = (N/ 1000.0) -  100.0
   72)   1     U-V SPECTROMETER HOUSEKEEPING (VDC)         UVSPH      VDC   = (N/ 1000.0) -  100.0
   73)   1     OZONE,DASIBI (GA.TECH) (VDC)                GTDO3      VDC   = (N/ 1000.0) -  100.0
   74)   1     OZONE,DASIBI (NCAR) (VDC)                    NDO3      VDC   = (N/ 1000.0) -  100.0
   75)   1     OZONE,ETHYLENE (NCAR) (VDC)                  NEO3      VDC   = (N/ 1000.0) -  100.0
   76)   1     16MM CAMERA FRAME COUNT                    CAMFC             = (N/    1.0) -    0.0
   77)   1     EVENT MARKER WORD (16 BITS)               EVMRKS             = (N/    1.0) -    0.0
   78)   1     INS/KNOLLENBERG UPDATE FLAGS                UPDATE           = (N/    1.0) -    0.0
   79)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   80)  20     AMBIENT TEMPERATURE (FAST RESPONSE) (C)     ATKP      C      = (N/ 1000.0) -  100.0
   81)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   82)  20               *** SPARE***                     SPARE             = (N/ 1000.0) -  100.0
   83)  20     WIND VECTOR EAST GUST COMPONENT (M/S)           UI    M/S    = (N/ 1000.0) -  200.0
   84)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)          VI    M/S    = (N/ 1000.0) -  200.0
   85)  20     WIND VECTOR VERT GUST COMPONENT(HR)(M/S)        WI    M/S    = (N/ 1000.0) -  100.0
   86)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)        UX    M/S    = (N/ 1000.0) -  200.0
   87)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)        VY    M/S    = (N/ 1000.0) -  200.0
   88)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   89)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   90)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   91)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
   92)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)        TTKP     C      = (N/ 1000.0) -  100.0
   93)  20     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)        TTB     C      = (N/ 1000.0) -  100.0
   94)  20     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)        QCG     MB     = (N/ 1000.0) -  100.0
   95)  20     ATTACK ANGLE (ROTATING VANE) (DEG)         AROT       DEG    = (N/ 1000.0) -  100.0
   96)  20     ATTACK ANGLE (FIXED VANE) (DEG)               AFIX    DEG    = (N/ 1000.0) -  100.0
   97)  20     SIDESLIP ANGLE (ROTATING VANE) (DEG)       BROT       DEG    = (N/ 1000.0) -  100.0
   98)  20     SIDESLIP ANGLE (FIXED VANE) (DEG)             BFIX    DEG    = (N/ 1000.0) -  100.0
   99)  20     GUST PROBE TIP VERT ACCELERATION (M/S2)        VAC    M/S2   = (N/ 1000.0) -  100.0
  100)  20     GUST PROBE TIP LATERAL ACCEL. (M/S2)           LAC    M/S2   = (N/ 1000.0) -  100.0
  101)  20     AIRCRAFT C.G. VERT ACCEL. (HR) (M/S2)        CGAC     M/S2   = (N/ 1000.0) -  100.0
  102)  20     RAW INS VERTICAL VELOCITY (M/S)              VZI      M/S    = (N/  100.0) - 5000.0
  103)  20     AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG)       ROLL    DEG    = (N/ 1000.0) -  100.0
  104)  20     AIRCRAFT PITCH ATTITUDE ANGLE (HR) (DEG)     PITCH    DEG    = (N/ 1000.0) -  100.0
  105)  20     AIRCRAFT TRUE HEADING (YAW) (HR) (DEG)        THF     DEG    = (N/ 1000.0) -  100.0
  106)  20     RAW INS GROUND SPD X COMPONENT (M/S)         XVI      M/S    = (N/ 1000.0) -  500.0
  107)  20     RAW INS GROUND SPD Y COMPONENT (M/S)         YVI      M/S    = (N/ 1000.0) -  500.0
  108)  20     LEFT WING STRAIN (HR) (MICRO-IN/IN)          STRLW  UIN/IN   = (N/  500.0) - 1000.0
  109)  20     RIGHT WING STRAIN (HR) (MICRO-IN/IN)         STRRW  UIN/IN   = (N/  500.0) - 1000.0
  110)  64     KNOLLENBERG 64 WORDS                       KNLBG     COUNTS  = (N/    1.0) -    0.0
  111)   1     ENVIRONMENT 1 CN OUTPUT  (VDC)              ENV1O      VDC   = (N/ 1000.0) -  100.0
  112)   1     ENVIORNMENT 1 CN RANGE  (VDC)               ENV1R      VDC   = (N/ 1000.0) -  100.0
  113)   1     GAS CHROMATOGRAPH (FLUOROCARBONS) (VDC)     GCFLU      VDC   = (N/ 1000.0) -  100.0
  114)   1     GAS CHROMATOGRAPH (NITROUS OXIDE)  (VDC)    GCN2O      VDC   = (N/ 1000.0) -  100.0
  115)   1     GAS CHROMATOGRAPH SAMPLE PRESR  (VDC)       GCSPR      VDC   = (N/ 1000.0) -  100.0
  116)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0