Sample LRT GENPRO-I header

  488A-1 MTN-INDUCED CNVCTN 22MAY78 10/35/          FIRST TIME ON THIS FILE 10 35  9       THIS FILE I
  S ALL OR PART OF TIME PERIOD 10 35  0 TO 12 10 50  DESCRIPTION OF RECORD --  63 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  585 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  2 CYCLES OF 585 SAMP/CYC = 1170 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 390 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)  10     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
    4)  10     CORRECTED STATIC PRESSURE (BOOM) (MB)    PSBC      MB        = (N/ 1000.0) -    0.0
    5)  10     AMBIENT TEMPERATURE (ROSEMOUNT) (C)      ATW       C         = (N/ 1000.0) -  100.0
    6)  10     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)   ATRF      C         = (N/ 1000.0) -  100.0
    7)  10     AMBIENT TEMPERATURE (FAST RESPONSE) (C)  ATKP      C         = (N/ 1000.0) -  100.0
    8)  10     DEWPOINT TEMPERATURE (THERMOELEC) (C)    DPC       C         = (N/ 1000.0) -  100.0
    9)  10     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)    RHOTD      G/M3     = (N/ 1000.0) -  100.0
   10)  10     HORIZONTAL WIND DIRECTION (DEG)             WDRCTN    DEG    = (N/ 1000.0) -  100.0
   11)  10     HORIZONTAL WIND SPEED (M/S)                 WSPD      M/S    = (N/ 1000.0) -  100.0
   12)  10     WIND VECTOR EAST GUST COMPONENT (M/S)    UI        M/S       = (N/ 1000.0) -  200.0
   13)  10     WIND VECTOR NORTH GUST COMPONENT (M/S)   VI        M/S       = (N/ 1000.0) -  200.0
   14)  10     WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI        M/S       = (N/ 1000.0) -  100.0
   15)  10     WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX        M/S       = (N/ 1000.0) -  200.0
   16)  10     WIND VECTOR LATERAL GUST COMPONENT (M/S) VY        M/S       = (N/ 1000.0) -  200.0
   17)  10     RAW INS LATITUDE (DEG)                   ALAT      DEG       = (N/ 1000.0) -  100.0
   18)  10     RAW INS LONGITUDE (DEG)                  ALONG     DEG       = (N/ 1000.0) -  200.0
   19)  10     NACA PRESSURE ALTITUDE (M)               HP        M         = (N/   10.0) -  500.0
   20)  10     PRESSURE-DAMPED INERTIAL ALTITUDE (M)       HI3        M     = (N/   10.0) -  500.0
   21)  10     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   22)  10     RAW INS GROUND SPEED (M/S)                  GSF       M/S    = (N/ 1000.0) -  100.0
   23)  10     RAW INS GROUND SPD EAST COMP (M/S)        VEW      M/S       = (N/ 1000.0) -  500.0
   24)  10     RAW INS GROUND SPD NORTH COMP (M/S)      VNS       M/S       = (N/ 1000.0) -  500.0
   25)  10     DAMPED AIRCRAFT VERT VELOCITY (M/S)         WP3       M/S    = (N/ 1000.0) -  100.0
   26)  10     AIRCRAFT C.G. ACCELERATION (M/S2)        CGAC      M/S2      = (N/ 1000.0) -  100.0
   27)  10     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF     DEG       = (N/ 1000.0) -  100.0
   28)  10     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)       ROLL      DEG       = (N/ 1000.0) -  100.0
   29)  10     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)      PITCH     DEG       = (N/ 1000.0) -  100.0
   30)  10     AIRCRAFT TRUE AIRSPEED (WING) (M/S)         TASW      M/S    = (N/ 1000.0) -  100.0
   31)  10     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)         TASG      M/S    = (N/ 1000.0) -  100.0
   32)  10     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 5000.0
   33)  10     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 5000.0
   34)  10     TOTAL TEMPERATURE (WING ROSEMOUNT) (C)        TTW     C      = (N/ 1000.0) -  100.0
   35)  10     TOTAL TEMPERATURE (REVERSE FLOW) (C)         TTRF       C    = (N/ 1000.0) -  100.0
   36)  10     TOTAL TEMPERATURE (FAST RESPONSE) (C)    TTKP        C       = (N/ 1000.0) -  100.0
   37)  10     DEW/FROSTPOINT TEMP (THERMOELEC) (C)          DP        C    = (N/ 1000.0) -  100.0
   38)  10     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)     QCG       MB      = (N/ 1000.0) -  100.0
   39)  10     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
   40)  10     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   41)  10     RAW STATIC PRESSURE (FUSELAGE) (MB)           PSF    MB      = (N/ 1000.0) -    0.0
   42)  10     REFRACTIVE INDEX (N-UNITS)                 RFI       N       = (N/ 1000.0) -  100.0
   43)  10     INS WANDER ANGLE (DEG)                   ALPHA     DEG       = (N/ 1000.0) -  100.0
   44)  10     AIRCRAFT TRUE HEADING (ARINC) (DEG)      THI       DEG       = (N/ 1000.0) -  100.0
   45)  10     RAW INS GROUND SPD X COMPONENT (M/S)     XVI       M/S       = (N/ 1000.0) -  500.0
   46)  10     RAW INS GROUND SPD Y COMPONENT (M/S)     YVI       M/S       = (N/ 1000.0) -  500.0
   47)  10     RAW INS VERTICAL VELOCITY (M/S)          VZI       M/S       = (N/ 1000.0) -  500.0
   48)   1     LTN-51 ARINC TIME LAG (SEC)               TMLAG    SEC       = (N/ 1000.0) -  100.0
   49)  10     ATTACK ANGLE (ROTATING VANE) (DEG)          AROT      DEG    = (N/ 1000.0) -  100.0
   50)  10     ATTACK ANGLE (FIXED VANE) (DEG)          AFIX      DEG       = (N/ 1000.0) -  100.0
   51)  10     SIDESLIP ANGLE (ROTATING VANE) (DEG)       BROT       DEG    = (N/ 1000.0) -  100.0
   52)  10     SIDESLIP ANGLE (FIXED VANE) (DEG)        BFIX      DEG       = (N/ 1000.0) -  100.0
   53)  10     GUST PROBE TIP VERT ACCEL (M/S2)         VAC       M/S2      = (N/ 1000.0) -  100.0
   54)  10     GUST PROBE TIP LATERAL ACCEL (M/S2)      LAC       M/S2      = (N/ 1000.0) -  100.0
   55)   1     EVENT MARKER WORD                        EVMRKS              = (N/    1.0) -    0.0
   56)   1     FIXED ZERO VOLTAGE (VDC)                   FZV     VDC       = (N/ 1000.0) -  100.0
   57)  10     ABSOLUTE HUMIDITY (REFRACT) (G/M3)       RHORFW     G/M3     = (N/ 1000.0) -  100.0
   58)  10     VAPOR PRESSURE (THERMOELEC) (MB)          EDPC       MB      = (N/ 1000.0) -  100.0
   59)  10     VAPOR PRESSURE  (REFRACTOMETER) (MB)       ERW       MB      = (N/ 1000.0) -  100.0
   60)  10     VIRTUAL POTENTIAL TEMP (THERMOELEC) (K)   VTHETA     K       = (N/ 1000.0) -  100.0
   61)  10     VIRTUAL POTENTIAL TEMP (REFRACT)(K)       VTHETAW    K       = (N/ 1000.0) -  100.0
   62)  10       MIXING RATIO (THERMOELEC) (G/KG)         RM        G/KG    = (N/ 1000.0) -  100.0
   63)  10       MIXING RATIO (REFRACTOMETER) (G/KG)      RMW       G/KG    = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  488A-1 MTN-INDUCED CNVCTN 22MAY78 10/35/
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 10        35         0         TO   12        10        50
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          596 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       495872 BITS PER PHYSICAL HEADER RECORD
           DATA FILE -- 11700 BITS PER LOGICAL DATA RECORD
                            2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        23400 BITS PER PHYSICAL DATA RECORD