N306D Sample HRT GENPRO-I header

  692-01   PHOENIX - 78   01SEP78 08/25/30          FIRST TIME ON THIS FILE  8 25 34       THIS FILE I
  S ALL OR PART OF TIME PERIOD  8 25 30 TO 11 47 30  DESCRIPTION OF RECORD --  67 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS 1226 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  1 CYCLES OF1226 SAMP/CYC = 1226 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 409 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                  *** UNUSED ***                UNUSED            = (N/    1.0) -    0.0
   30)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)      TTKP      C       = (N/ 1000.0) -  100.0
   31)  20     AMBIENT TEMPERATURE (ROSEMOUNT) (C)        ATW       C       = (N/ 1000.0) -  100.0
   32)  20                  *** UNUSED ***                UNUSED            = (N/    1.0) -    0.0
   33)  20     AMBIENT TEMPERATURE (FAST RESPONSE) (C)    ATKP      C       = (N/ 1000.0) -  100.0
   34)  20     RADIOMETRIC SURFACE TEMP (PRT-5) (C)       PRT5      C       = (N/ 1000.0) -  100.0
   35)  20     DEW/FROSTPOINT TEMP (THERMOELEC) (C)       DP        C       = (N/ 1000.0) -  100.0
   36)  20     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPC       C       = (N/ 1000.0) -  100.0
   37)  20     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
   38)  20     REFRACTIVE INDEX (N-UNITS)                 RFI       N       = (N/ 1000.0) -  100.0
   39)  20     ABSOLUTE HUMIDITY (REFRACT) (G/M3)         RHORF     G/M3    = (N/ 1000.0) -  100.0
   40)  20     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
   41)  20     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)        TASG      M/S     = (N/ 1000.0) -  100.0
   42)  20     ATTACK ANGLE (FIXED VANE) (DEG)            AFIX      DEG     = (N/ 1000.0) -  100.0
   43)  20     ATTACK ANGLE (ROTATING VANE) (DEG)         AROT      DEG     = (N/ 1000.0) -  100.0
   44)  20     SIDESLIP ANGLE (FIXED VANE) (DEG)          BFIX      DEG     = (N/ 1000.0) -  100.0
   45)  20     SIDESLIP ANGLE (ROTATING VANE) (DEG)       BROT      DEG     = (N/ 1000.0) -  100.0
   46)  20     GUST PROBE TIP VERT ACCEL (M/S2)           VAC       M/S2    = (N/ 1000.0) -  100.0
   47)  20     GUST PROBE TIP LATERAL ACCEL (M/S2)        LAC       M/S2    = (N/ 1000.0) -  100.0
   48)  20     WIND VECTOR EAST GUST COMPONENT (M/S)      UI        M/S     = (N/ 1000.0) -  200.0
   49)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI        M/S     = (N/ 1000.0) -  200.0
   50)  20     WIND VECTOR VERTICAL GUST COMP (H) (M/S)   WI        M/S     = (N/ 1000.0) -  100.0
   51)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX        M/S     = (N/ 1000.0) -  200.0
   52)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY        M/S     = (N/ 1000.0) -  200.0
   53)  20     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   54)  20     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   55)  20     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   56)  20     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   57)  20     DISTANCE EAST OF BAO TOWER (KM)            DEIBAO    KM      = (N/  100.0) - 1000.0
   58)  20     DISTANCE NORTH OF BAO TOWER (KM)           DNIBAO    KM      = (N/  100.0) - 1000.0
   59)  20     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   60)  20     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   61)  20     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   62)  20     AIRCRAFT INDICATED AIRSPEED (GUST) (M/S)   IASG      M/S     = (N/ 1000.0) -  100.0
   63)  20       MIXING RATIO (G/KG)                      RM        G/KG    = (N/ 1000.0) -  100.0
   64)  20     SPECIFIC HUMIDITY (G/KG)                   SPHUM     G/KG    = (N/ 1000.0) -  100.0
   65)  20      POTENTIAL TEMPERATURE (K)                 THETA     K       = (N/ 1000.0) -  100.0
   66)  20     VIRTUAL POTENTIAL TEMPERATURE (K)          VTHETA    K       = (N/ 1000.0) -  100.0
   67)  20     DEWPOINT TEMPERATURE (REFRACT) (C)         DPCRF     C       = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  692-01   PHOENIX - 78   01SEP78 08/25/30
 THIS FILE IS ALL OR PART OF THE TIME PERIOD  8        25        30         TO   11        47        30
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                         1237 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       ****** BITS PER PHYSICAL HEADER RECORD
           DATA FILE -- 24520 BITS PER LOGICAL DATA RECORD
                            1 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        24520 BITS PER PHYSICAL DATA RECORD