N307D Sample LRT GENPRO-I header

   791-01 CCOPE 18MAY1981 16/31/00                  FIRST TIME ON THIS FILE 16 31  4       THIS FILE I
  S ALL OR PART OF TIME PERIOD 16 31  0 TO 17 50 15  DESCRIPTION OF RECORD --  74 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS   98 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE 15 CYCLES OF  98 SAMP/CYC = 1470 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 490 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     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
    6)   1     POSITIVE REFERENCE (+10.0 VDC)             SIXP      VDC     = (N/ 1000.0) -  100.0
    7)   1     NEGATIVE REFERENCE (-10.0 VDC)             SIXN      VDC     = (N/ 1000.0) -  100.0
    8)   1     PILOT MICROPHONE SWITCH (1) (VDC)          XMIT1     VDC     = (N/ 1000.0) -  100.0
    9)   1     PILOT MICROPHONE SWITCH (2) (VDC)          XMIT2     VDC     = (N/ 1000.0) -  100.0
   10)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
   11)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
   12)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
   13)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   14)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   15)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   16)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   17)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   18)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   19)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   20)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   21)   1     RAW DYNAMIC PRESSURE (FUSELAGE)(MB)        QCF       MB      = (N/ 1000.0) -  100.0
   22)   1     RAW DYNAMIC PRESSURE (BOOM)(MB)            QCB       MB      = (N/ 1000.0) -  100.0
   23)   1     CORRECTED DYNAMIC PRESR (FUSELAGE)(MB)     QCFC      MB      = (N/ 1000.0) -  100.0
   24)   1     CORRECTED DYNAMIC PRESR (BOOM)(MB)         QCBC      MB      = (N/ 1000.0) -  100.0
   25)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
   26)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   27)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   28)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -    0.0
   29)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   30)   1     TOTAL TEMPERATURE (REVERSE FLOW) (C)       TTRF      C       = (N/ 1000.0) -  100.0
   31)   1     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)     ATRF      C       = (N/ 1000.0) -  100.0
   32)   1     AMBIENT TEMPERATURE2(REVERSE-FLOW) (C)     ATRF2     C       = (N/ 1000.0) -  100.0
   33)   1     TOTAL TEMPERATURE (FUSELAGE ROSEMOUNT) (   TTF       C       = (N/ 1000.0) -  100.0
   34)   1     TOTAL TEMPERATURE (DEICED ROSEMOUNT) (C)   TTFH      C       = (N/ 1000.0) -  100.0
   35)   1     AMBIENT TEMPERATURE (FUSELAGE ROSEMOUNT)   ATF       C       = (N/ 1000.0) -  100.0
   36)   1     AMBIENT TEMP (DEICED ROSEMOUNT) (C)        ATFH      C       = (N/ 1000.0) -  100.0
   37)   1     DEW/FROST POINT TEMP (GE )(C)              DPGE      C       = (N/ 1000.0) -  100.0
   38)   1     DEW/FROST POINT TEMP ( E-G+G) (C)          DPEGG     C       = (N/ 1000.0) -  100.0
   39)   1     DEWPOINT TEMPERATURE (GE)   (C)            DPGEC     C       = (N/ 1000.0) -  100.0
   40)   1     DEWPOINT TEMPERATURE (E-G+G ) (C)          DPEGGC    C       = (N/ 1000.0) -  100.0
   41)   1     ABSOLUTE HUMIDITY     (G/M3)               RHOTDT    G/M3    = (N/ 1000.0) -  100.0
   42)   1     AIRCRAFT TRUE AIRSPEED (FUSELAGE) (M/S)    TASF      M/S     = (N/ 1000.0) -  100.0
   43)   1     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)        TASG      M/S     = (N/ 1000.0) -  100.0
   44)   1     RAW J-W LIQUID WATER CONTENT (G/M3)        LWC       G/M3    = (N/ 1000.0) -  100.0
   45)   1     CORRCTD J-W LIQUID WATER CONTENT (G/M3)    LWCC      G/M3    = (N/ 1000.0) -  100.0
   46)   1     VERTICAL DIFF PRESSURE(GUST PRO.)(MB)      ADIF     MB       = (N/ 1000.0) -  100.0
   47)   1     ATTACK ANGLE (ROSEMOUNT) (DEG)            ATTACK    DEG      = (N/ 1000.0) -  100.0
   48)   1     HORIZONTAL DIFF PRESSURE(GUST PRO.)(MB)    BDIF     MB       = (N/ 1000.0) -  100.0
   49)   1     SIDESLIP ANGLE (ROSEMOUNT) (DEG)          SSLIP      DEG     = (N/ 1000.0) -  100.0
   50)   1     HORIZONTAL WIND DIRECTION        (DEG)     WDRCTN    DEG     = (N/ 1000.0) -  100.0
   51)   1     HORIZONTAL WIND SPEED        (M/S)         WSPD      M/S     = (N/ 1000.0) -  100.0
   52)   1     WIND VECTOR EAST GUST COMPONENT (M/S)      UI1       M/S     = (N/ 1000.0) -  200.0
   53)   1     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI1       M/S     = (N/ 1000.0) -  200.0
   54)   1     WIND VECTOR VERTICAL GUST COMP (H) (M/S)   WI1       M/S     = (N/ 1000.0) -  100.0
   55)   1     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX1       M/S     = (N/ 1000.0) -  200.0
   56)   1     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY1       M/S     = (N/ 1000.0) -  200.0
   57)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   58)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   59)   1     DISTANCE EAST OF SUNDAY CREEK (KM)         DEI       KM      = (N/  100.0) - 1000.0
   60)   1     DISTANCE NORTH OF SUNDAY CREEK (KM)        DNI       KM      = (N/  100.0) - 1000.0
   61)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   62)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   63)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   64)   1     WATER VAPOR MIXING RATIO  (G/KG)           MIXR      G/KG    = (N/ 1000.0) -  100.0
   65)   1     EQUIVALENT POTENTIAL TEMPERATURE (K)       ETHETA    K       = (N/ 1000.0) -  100.0
   66)   1     POTENTIAL TEMPERATURE (K)                  THETA     K       = (N/ 1000.0) -  100.0
   67)   1     SPECIFIC HUMIDITY (G/KG)                   SPHUM    G/KG     = (N/ 1000.0) -  100.0
   68)   1     VIRTUAL POTENTIAL TEMPERATURE (K)          VTHETA    K       = (N/ 1000.0) -  100.0
   69)   1     MEAN OZONE MIXING RATIO   (PPBV)           MO3       PPBV    = (N/ 1000.0) -  100.0
   70)   1     RX CHAMBER PRESSURE (O3RXP)     (VDC)      O3RXP     TORR    = (N/ 1000.0) -  100.0
   71)   1     RX CHAMBER TEMPERATURE (O3RXT)(DEG C)      O3RXT    DEG C    = (N/ 1000.0) -  100.0
   72)   1     O3 PMT TEMPERATURE (O3PMT) (DEG C)         O3PMT    DEG C    = (N/ 1000.0) -  100.0
   73)   1     COOLER TEMPERATURE (CHS1) (DEG C)          CHS1     DEG C    = (N/ 1000.0) -  100.0
   74)  25     FAST OZONE MIXING RATIO (25HZ)(PPBV)       O3F25     PPBV    = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
   791-01 CCOPE 18MAY1981 16/31/00
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 16        31         0         TO   17        50        15
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          109 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                        90688 BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  1960 BITS PER LOGICAL DATA RECORD
                           15 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        29400 BITS PER PHYSICAL DATA RECORD