Sample LRT GENPRO-I header

  735-01 L.A.S.    29 JAN 1981 18/30/15             FIRST TIME ON THIS FILE 18 30 15       THIS FILE I
  S ALL OR PART OF TIME PERIOD 18 30 15 TO 19 37  0  DESCRIPTION OF RECORD --  63 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS   63 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE 23 CYCLES OF  63 SAMP/CYC = 1449 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 483 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 SWITCH1                   TRMT1     VDC     = (N/ 1000.0) -  100.0
    6)   1     PILOT MICROPHONE SWITCH2                   TRMT2     VDC     = (N/ 1000.0) -  100.0
    7)   1     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
    8)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
    9)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
   10)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
   11)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   12)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   13)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   14)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   15)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   16)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   17)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   18)   1     RAW DYNAMIC PRESSURE (FUSELAGE) (MB)       QCF       MB      = (N/ 1000.0) -  100.0
   19)   1     RAW DYNAMIC PRESSURE (BOOM) (MB)           QCB       MB      = (N/ 1000.0) -  100.0
   20)   1     CORRECTED DYNAMIC PRESR (FUSELAGE) (MB)    QCFC      MB      = (N/ 1000.0) -  100.0
   21)   1     CORRECTED DYNAMIC PRESSURE (BOOM) (MB)     QCBC      MB      = (N/ 1000.0) -  100.0
   22)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
   23)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   24)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   25)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -    0.0
   26)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   27)   1     TOTAL TEMPERATURE (FUS. ROSEMOUNT) (C)     TTF       C       = (N/ 1000.0) -  100.0
   28)   1     TOTAL TEMPERATURE (DEICED ROSEMNT) (C)     TTFH      C       = (N/ 1000.0) -  100.0
   29)   1     AMBIENT TEMPERATURE (ROSEMOUNT) (C)        ATF       C       = (N/ 1000.0) -  100.0
   30)   1     AMBIENT TEMP (DEICED ROSEMOUNT) (C)        ATFH      C       = (N/ 1000.0) -  100.0
   31)   1     DEW/FROSTPOINT TEMP (THERMOELEC) (C)       DP        C       = (N/ 1000.0) -  100.0
   32)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPC       C       = (N/ 1000.0) -  100.0
   33)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)      RHOTD     G/M3    = (N/ 1000.0) -  100.0
   34)   1     AIRCRAFT TRUE AIRSPEED (FUSELAGE) (M/S)    TASF      M/S     = (N/ 1000.0) -  100.0
   35)   1     AIRCRAFT TRUE AIRSPEED (BOOM) (M/S)        TASB      M/S     = (N/ 1000.0) -  100.0
   36)   1     VERTICAL DIFF. PRESR (GUST PROBE) (MB)     ADIF      MB      = (N/ 1000.0) -  100.0
   37)   1     ATTACK ANGLE (ROSEMOUNT) (DEG)             ATTACK    DEG     = (N/ 1000.0) -  100.0
   38)   1     HORIZONTAL DIFF. PRESR (GUST PROBE) (MB)   BDIF      MB      = (N/ 1000.0) -  100.0
   39)   1     SIDESLIP ANGLE (ROSEMOUNT) (DEG)           SSLIP     DEG     = (N/ 1000.0) -  100.0
   40)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   41)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   42)   1     WIND VECTOR EAST COMPONENT (M/S)           UI1       M/S     = (N/ 1000.0) -  200.0
   43)   1     WIND VECTOR NORTH COMPONENT (M/S)          VI1       M/S     = (N/ 1000.0) -  200.0
   44)   1     WIND VECTOR VERTICAL GUST COMP (L) (M/S)   WI1       M/S     = (N/ 1000.0) -  100.0
   45)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)        UX1       M/S     = (N/ 1000.0) -  200.0
   46)   1     WIND VECTOR LATERAL COMPONENT (M/S)        VY1       M/S     = (N/ 1000.0) -  200.0
   47)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   48)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   49)   1     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 1000.0
   50)   1     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 1000.0
   51)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   52)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   53)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   54)   1     AMPLITUDE (D1) (VDC)                       AMPL1     VDC     = (N/ 1000.0) -  100.0
   55)   1     AMPLITUDE (D2) (VDC)                       AMPL2     VDC     = (N/ 1000.0) -  100.0
   56)   1     FM FUNDAMENTAL (D1) (VDC)                  FUND-1    VDC     = (N/ 1000.0) -  100.0
   57)   1     FM HARMONIC (D1) (VDC)                     HARM-1    VDC     = (N/ 1000.0) -  100.0
   58)   1     FM HARMONIC (D2) (VDC)                     HARM-2    VDC     = (N/ 1000.0) -  100.0
   59)   1     DETECTOR RATIO (VDC)                       RATIO     VDC     = (N/ 1000.0) -  100.0
   60)   1     DIODE TEMPERATURE (VDC)                    DIO-T     VDC     = (N/ 1000.0) -  100.0
   61)   1     DIODE CURRENT (VDC)                        DIO-I     VDC     = (N/ 1000.0) -  100.0
   62)   1     CELL PRESSURE (VDC)                        C-PRESS   VDC     = (N/ 1000.0) -  100.0
   63)   1     DEWAR  PRESSURE (VDC)                      D-PRESS   VDC     = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  735-01 L.A.S.    29 JAN 1981 18/30/15
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 18        30        15         TO   19        37         0
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                           74 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                        61568 BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  1260 BITS PER LOGICAL DATA RECORD
                           23 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        28980 BITS PER PHYSICAL DATA RECORD