Sample HRT GENPRO-I header

  410-01 NOCT BNDY LAYER  1MAY79  16/56/50          FIRST TIME ON THIS FILE 16 56 59       THIS FILE I
  S ALL OR PART OF TIME PERIOD 16 56 50 TO 18 24 27  DESCRIPTION OF RECORD --  66 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS 1446 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  1 CYCLES OF1446 SAMP/CYC = 1446 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 482 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     LTN-51 ARINC TIME LAG (SEC)                TMLAG     SEC     = (N/ 1000.0) -  100.0
    4)   1     EVENT MARKER WORD                          EVMRKS            = (N/    1.0) -    0.0
    5)   1     PILOT MICROPHONE SWITCH (XMIT) (VDC)       XMIT      VDC     = (N/ 1000.0) -  100.0
    6)   1     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
    7)  20     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
    8)  20     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
    9)  20     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
   10)  20     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   11)  20     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   12)  20     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   13)  20     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   14)  20     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   15)  20     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   16)  20     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   17)  20     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   18)  20     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
   19)  20     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)     QCG       MB      = (N/ 1000.0) -  100.0
   20)  20     CORRECTED DYNAMIC PRESR (WING)  (MB)       QCWC      MB      = (N/ 1000.0) -  100.0
   21)  20     CORRECTED DYNAMIC PRESR (GUST PROBE)(MB)   QCGC      MB      = (N/ 1000.0) -  100.0
   22)  20     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
   23)  20     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   24)  20     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   25)  20     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -    0.0
   26)  20     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   27)  20     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   28)  20     TOTAL TEMPERATURE (WING ROSEMOUNT) (C)     TTW       C       = (N/ 1000.0) -  100.0
   29)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)      TTKP      C       = (N/ 1000.0) -  100.0
   30)  20     AMBIENT TEMP (WING ROSEMOUNT) (C)          ATW       C       = (N/ 1000.0) -  100.0
   31)  20     AMBIENT TEMPERATURE (FAST RESPONSE) (C)    ATKP      C       = (N/ 1000.0) -  100.0
   32)  20     RADIOMETRIC SURFACE TEMP (PRT-5) (C)       PRT5      C       = (N/ 1000.0) -  100.0
   33)  20     DEW/FROSTPOINT TEMP (THERMOELEC) (C)       DP        C       = (N/ 1000.0) -  100.0
   34)  20     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPC       C       = (N/ 1000.0) -  100.0
   35)  20     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
   36)  20     REFRACTIVE INDEX (N-UNITS)                 RFI       N       = (N/ 1000.0) -  100.0
   37)  20     ABSOLUTE HUMIDITY (REFRACT) (G/M3)         RHORF     G/M3    = (N/ 1000.0) -  100.0
   38)  20     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
   39)  20     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)        TASG      M/S     = (N/ 1000.0) -  100.0
   40)  20     ATTACK ANGLE (FIXED VANE) (DEG)            AFIX      DEG     = (N/ 1000.0) -  100.0
   41)  20     ATTACK ANGLE (FIXED VANE 2) (DEG)          AFIX2     DEG     = (N/ 1000.0) -  100.0
   42)  20     SIDESLIP ANGLE (FIXED VANE) (DEG)          BFIX      DEG     = (N/ 1000.0) -  100.0
   43)  20     SIDESLIP ANGLE (FIXED VANE 2) (DEG)        BFIX2     DEG     = (N/ 1000.0) -  100.0
   44)  20     WIND VECTOR EAST GUST COMPONENT (M/S)      UI        M/S     = (N/ 1000.0) -  200.0
   45)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI        M/S     = (N/ 1000.0) -  200.0
   46)  20     WIND VECTOR VERTICAL GUST COMP (H) (M/S)   WI        M/S     = (N/ 1000.0) -  100.0
   47)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX        M/S     = (N/ 1000.0) -  200.0
   48)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY        M/S     = (N/ 1000.0) -  200.0
   49)  20     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   50)  20     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   51)  20     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   52)  20     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   53)  20     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 1000.0
   54)  20     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 1000.0
   55)  20     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   56)  20     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   57)  20     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   58)  20     POTENTIAL TEMPERATURE (K)                  THETA     K       = (N/ 1000.0) -  100.0
   59)  20     VIRTUAL POTENTIAL TEMPERATURE (K)          VTHETA    K       = (N/ 1000.0) -  100.0
   60)  20     PITCH MINUS ATTACK                         PHMATK    DEG     = (N/ 1000.0) -  100.0
   61)  20     RMS1 (CENTER FREQUENCY 25HZ) (VDC)         RMS1      VDC     = (N/ 1000.0) -  100.0
   62)  20     RMS2 (CENTER FREQUENCY 100HZ) (VDC)        RMS2      VDC     = (N/ 1000.0) -  100.0
   63)  20     RMS3 (CENTER FREQUENCY 200HZ) (VDC)        RMS3      VDC     = (N/ 1000.0) -  100.0
   64) 100     HOT WIRE VOLTAGE    (VDC)                  HWV       VDC     = (N/ 1000.0) -  100.0
   65) 100     HOT WIRE VOLTAGE DERIVATIVE  (VDC)         HWDIF     VDC     = (N/ 1000.0) -  100.0
   66) 100     HOT WIRE DERIVATIVE FILTERED FC=57HZ       HWDIFF    VDC     = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  410-01 NOCT BNDY LAYER  1MAY79  16/56/50
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 16        56        50         TO   18        24        27
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                         1457 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       ****** BITS PER PHYSICAL HEADER RECORD
           DATA FILE -- 28920 BITS PER LOGICAL DATA RECORD
                            1 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        28920 BITS PER PHYSICAL DATA RECORD