Sample LRT GENPRO-I header

  789-09 CB-FLOW 19AUG1982 13/35/40                 FIRST TIME ON THIS FILE 13 35 40       THIS FILE I
  S ALL OR PART OF TIME PERIOD 13 35 40 TO 15 33  0  DESCRIPTION OF RECORD --  62 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS   62 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE 24 CYCLES OF  62 SAMP/CYC = 1488 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 496 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     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
    5)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
    6)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
    7)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
    8)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
    9)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   10)   1     AIRCRAFT GROUND SPEED   (M/S)               GSF       M/S    = (N/ 1000.0) -  100.0
   11)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   12)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   13)   1     AIRCRAFT TRUE HEADING ANGLE (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   14)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   15)   1     RAW DYNAMIC PRESSURE (BOOM)      (MB)      QCB       MB      = (N/ 1000.0) -  100.0
   16)   1     CORRECTED DYNAMIC PRESR (BOOM)      (MB)   QCBC      MB      = (N/ 1000.0) -  100.0
   17)   1     RAW DYNAMIC PRESSURE (FUSL) (MB)           QCF       MB      = (N/ 1000.0) -  100.0
   18)   1     CORRECTED DYNAMIC PRESR (FUSL)  (MB)       QCFC      MB      = (N/ 1000.0) -  100.0
   19)   1     RAW STATIC PRESSURE (FUSL) (MB)            PSF       MB      = (N/ 1000.0) -    0.0
   20)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -  100.0
   21)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   22)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -  100.0
   23)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   24)   1     TOTAL TEMPERATURE (FUSL) (C)                TTF        C     = (N/ 1000.0) -  100.0
   25)   1     AMBIENT TEMPERATURE (FUSL) (C)             ATF       C       = (N/ 1000.0) -  100.0
   26)   1     DEW/FROST POINT TEMPERATURE  (C)            DP         C     = (N/ 1000.0) -  100.0
   27)   1     DEW POINT TEMPERATURE(C)                   DPC       C       = (N/ 1000.0) -  100.0
   28)   1     DEW/FROST POINT TEMP. GE (C)               DPGE        C     = (N/ 1000.0) -  100.0
   29)   1     DEWPOINT TEMPERATURE(GE)(C)                DPGEC     C       = (N/ 1000.0) -  100.0
   30)   1     DEW PT GE. CONTROL VOLTAGE (C)             DPGEV       C     = (N/ 1000.0) -  100.0
   31)   1     ABSOLUTE HUMIDITY   (G/M3)                 RHOTD     G/M3    = (N/ 1000.0) -  100.0
   32)   1     LYMAN ALPHA         (VDC)                  VLA       VDC     = (N/ 1000.0) -  100.0
   33)   1     AIRCRAFT TRUE AIRSPEED (FUSL) (M/S)        TASF      M/S     = (N/ 1000.0) -  100.0
   34)   1     AIRCRAFT TRUE AIRSPEED (BOOM) (M/S)        TASB      M/S     = (N/ 1000.0) -  100.0
   35)   1     TOTAL TEMP.  (DEICED ROSE) (C)              TTFH       C     = (N/ 1000.0) -  100.0
   36)   1     AMBIENT TEMPERATURE(DEIC ROSE)(C)          ATFH      C       = (N/ 1000.0) -  100.0
   37)   1     VERTICAL DIFFERENTIAL PRESSURE (MB)        ADIF      MB      = (N/ 1000.0) -  100.0
   38)   1     ATTACK ANGLE ROSEMOUNT   (DEG)             ATTACK    DEG     = (N/ 1000.0) -  100.0
   39)   1     HORIZONTAL DIFF PRESSURE (MB)              BDIF      MB      = (N/ 1000.0) -  100.0
   40)   1     SIDESLIP ANGLE (ROSEMOUNT)  (DEG)          SSLIP     DEG     = (N/ 1000.0) -  100.0
   41)   1     WIND VECTOR EAST GUST COMPONENT (M/S)      UI        M/S     = (N/ 1000.0) -  200.0
   42)   1     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI        M/S     = (N/ 1000.0) -  200.0
   43)   1     WIND VECTOR VERTICAL GUST COMP (M/S)       WI        M/S     = (N/ 1000.0) -  100.0
   44)   1     WIND VECTOR LNGTDNL GUST COMP. (M/S)       UX        M/S     = (N/ 1000.0) -  200.0
   45)   1     WIND VECTOR LATERAL GUST COMP. (M/S)       VY        M/S     = (N/ 1000.0) -  200.0
   46)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   47)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   48)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   49)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   50)   1     DIST EAST OF START (KM)                    DEI       KM      = (N/  100.0) - 1000.0
   51)   1     DIST NORTH OF START (KM)                   DNI       KM      = (N/  100.0) - 1000.0
   52)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   53)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   54)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   55)   1     FIXED ZERO VOLTAGE    (VDC)                FZV       VDC     = (N/ 1000.0) -  100.0
   56)   1     EVENT MARKER (VDC)                         EVMK      VDC     = (N/ 1000.0) -  100.0
   57)   1     RELATIVE HUMIDITY (PER CENT)               RHUM    PER CENT  = (N/ 1000.0) -  100.0
   58)   1     MIXING RATIO      (G/KG)                   RM        G/KG    = (N/ 1000.0) -  100.0
   59)   1     EQUIVALENT POTENTIAL TEMP (K)              ETHETA    K       = (N/ 1000.0) -  100.0
   60)   1     POTENTIAL TEMPERATURE   (K)                THETA     K       = (N/ 1000.0) -  100.0
   61)   1     SPECIFIC HUMIDITY (G/KG)                   SPHUM     G/KG    = (N/ 1000.0) -  100.0
   62)   1     VIRTUAL POTENTIAL TEMP (K)                 VTHETA    K       = (N/ 1000.0) -  100.0

 THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
   789-09 CB-FLOW 19AUG1982 13/35/40
  THIS FILE IS ALL OR PART OF THE TIME PERIOD 13        35        40         TO   15        33         0
  DESCRIPTION OF TAPE:
          HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                            73 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                         60736 BITS PER PHYSICAL HEADER RECORD
            DATA FILE --  1240 BITS PER LOGICAL DATA RECORD
                            24 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                         29760 BITS PER PHYSICAL DATA RECORD