Sample HRT GENPRO-I header

  601-2  M.E.T.  08AUG78          06/14/05          FIRST TIME ON THIS FILE  6 14  7       THIS FILE I
  S ALL OR PART OF TIME PERIOD  6 14  5 TO  9 40  0  DESCRIPTION OF RECORD --  68 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS 1208 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  1 CYCLES OF1208 SAMP/CYC = 1208 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 403 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 16 BIT WORD               EVMRKS    COUNTS    = (N/    1.0) -    0.0
    5)   1     MAIN CONSOLE SPECIAL EVENTS              EVMAIN    COUNTS    = (N/ 1000.0) -  100.0
    6)   1     EVENT MARKS REMOTE (COUNTS)              EVRMT     COUNTS    = (N/ 1000.0) -  100.0
    7)   1     PILOT MICROPHONE SWITCH (XMIT) (VDC)          XMIT  VDC      = (N/ 1000.0) -  100.0
    8)   1     FIXED ZERO VOLTAGE (VDC)                   FZV     V         = (N/ 1000.0) -  100.0
    9)  20     RAW INS LATITUDE (DEG)                   ALAT      DEG       = (N/ 1000.0) -  100.0
   10)  20     RAW INS LONGITUDE (DEG)                  ALONG     DEG       = (N/ 1000.0) -  200.0
   11)  20     AIRCRAFT TRUE HEADING (ARINC) (DEG)      THI       DEG       = (N/ 1000.0) -  100.0
   12)  20     INS WANDER ANGLE (DEG)                   ALPHA     DEG       = (N/ 1000.0) -  100.0
   13)  20     RAW INS GROUND SPD X COMPONENT (M/S)     XVI       M/S       = (N/ 1000.0) -  500.0
   14)  20     RAW INS GROUND SPD Y COMPONENT (M/S)     YVI       M/S       = (N/ 1000.0) -  500.0
   15)  20     RAW INS GROUND SPEED (M/S)                  GSF       M/S    = (N/ 1000.0) -  100.0
   16)  20     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)      PITCH     DEG       = (N/ 1000.0) -  100.0
   17)  20     AIRCRAFT COARSE ROLL ANGLE (DEG)         CROLL     DEG       = (N/ 1000.0) -  100.0
   18)  20     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)       ROLL      DEG       = (N/ 1000.0) -  100.0
   19)  20     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF     DEG       = (N/ 1000.0) -  100.0
   20)  20     RAW INS VERTICAL VELOCITY (M/S)          VZI       M/S       = (N/ 1000.0) -  500.0
   21)  20     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
   22)  20     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)     QCG       MB      = (N/ 1000.0) -  100.0
   23)  20     CORRECTED DYNAMIC PRESR (WING) (MB)        QCWC      MB      = (N/ 1000.0) -  100.0
   24)  20     CORRCTD DYNAMIC PRESR (GUST PROBE) (MB)    QCGC      MB      = (N/ 1000.0) -  100.0
   25)  20     RAW STATIC PRESSURE (FUSELAGE) (MB)           PSF    MB      = (N/ 1000.0) -    0.0
   26)  20     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   27)  20     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   28)  20     CORRECTED STATIC PRESSURE (BOOM) (MB)    PSBC      MB        = (N/ 1000.0) -    0.0
   29)  20     NACA PRESSURE ALTITUDE (M)               HP        M         = (N/   10.0) -  500.0
   30)  20     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   31)  20     TOTAL TEMPERATURE (WING ROSEMOUNT) (C)        TTW     C      = (N/ 1000.0) -  100.0
   32)  20     TOTAL TEMPERATURE (REVERSE FLOW) (C)       TTRF        C     = (N/ 1000.0) -  100.0
   33)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)    TTKP        C       = (N/ 1000.0) -  100.0
   34)  20     AMBIENT TEMPERATURE (ROSEMOUNT) (C)      ATW       C         = (N/ 1000.0) -  100.0
   35)  20     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)   ATRF      C         = (N/ 1000.0) -  100.0
   36)  20     AMBIENT TEMPERATURE (FAST RESPONSE) (C)  ATKP      C         = (N/ 1000.0) -  100.0
   37)  20     DEW/FROSTPOINT TEMP (THERMOELEC) (C)          DP      DEG C  = (N/ 1000.0) -  100.0
   38)  20     DEWPOINT TEMPERATURE (THERMOELEC) (C)    DPC       C         = (N/ 1000.0) -  100.0
   39)  20     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)    RHOTD      G/M3     = (N/ 1000.0) -  100.0
   40)  20     REFRACTIVE INDEX (N-UNITS)                 RFI      VOLTS    = (N/ 1000.0) -  100.0
   41)  20     ABSOLUTE HUMIDITY (REFRACT) (G/M3)       RHORF      G/M3     = (N/ 1000.0) -  100.0
   42)  20     AIRCRAFT TRUE AIRSPEED (WING) (M/S)         TASW      M/S    = (N/ 1000.0) -  100.0
   43)  20     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)         TASG      M/S    = (N/ 1000.0) -  100.0
   44)  20     RAW J-W LIQUID WATER CONTENT (G/M3)        LWC       G/M3    = (N/ 1000.0) -  100.0
   45)  20     CORRCTD J-W LIQUID WATER CONTENT (G/M3)   LWCC       G/M3    = (N/ 1000.0) -  100.0
   46)  20     ATTACK ANGLE (FIXED VANE) (DEG)          AFIX      DEG       = (N/ 1000.0) -  100.0
   47)  20     ATTACK ANGLE (ROTATING VANE) (DEG)          AROT      DEG    = (N/ 1000.0) -  100.0
   48)  20     SIDESLIP ANGLE (FIXED VANE) (DEG)        BFIX      DEG       = (N/ 1000.0) -  100.0
   49)  20     SIDESLIP ANGLE (ROTATING VANE) (DEG)       BROT       DEG    = (N/ 1000.0) -  100.0
   50)  20     GUST PROBE TIP VERT ACCEL (M/S2)         VAC       M/S2      = (N/ 1000.0) -  100.0
   51)  20     GUST PROBE TIP LATERAL ACCEL (M/S2)      LAC       M/S2      = (N/ 1000.0) -  100.0
   52)  20     WIND VECTOR EAST GUST COMPONENT (M/S)    UI        M/S       = (N/ 1000.0) -  200.0
   53)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)   VI        M/S       = (N/ 1000.0) -  200.0
   54)  20     WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI        M/S       = (N/ 1000.0) -  100.0
   55)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX        M/S       = (N/ 1000.0) -  200.0
   56)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S) VY        M/S       = (N/ 1000.0) -  200.0
   57)  20     HORIZONTAL WIND DIRECTION (DEG)             WDRCTN    DEG    = (N/ 1000.0) -  100.0
   58)  20     HORIZONTAL WIND SPEED (M/S)                 WSPD      M/S    = (N/ 1000.0) -  200.0
   59)  20     RAW INS GROUND SPD EAST COMP (M/S)        VEW      M/S       = (N/ 1000.0) -  500.0
   60)  20     RAW INS GROUND SPD NORTH COMP (M/S)      VNS       M/S       = (N/ 1000.0) -  500.0
   61)  20     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 1000.0
   62)  20     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/ 1000.0) -  100.0
   63)  20     AIRCRAFT C.G. ACCELERATION (M/S2)        CGAC      M/S2      = (N/ 1000.0) -  100.0
   64)  20     DAMPED AIRCRAFT VERT VELOCITY (M/S)         WP3       M/S    = (N/ 1000.0) -  100.0
   65)  20     PRESSURE-DAMPED INERTIAL ALTITUDE (M)       HI3        M     = (N/   10.0) -  500.0
   66)  20     SECONDARY BOOM PITOT PRESSURE (MB)         QCB       MB      = (N/ 1000.0) -  100.0
   67)  20     DASIBI OZONE (VDC)                        DASIBI     VDC     = (N/ 1000.0) -  100.0
   68)  20     CCN (MEE) (VDC)                            CCN       VDC     = (N/ 1000.0) -  100.0