Sample LRT GENPRO-I header

    660-01 FUKUTA ONT 16JAN1982 09/37/00            FIRST TIME ON THIS FILE  9 37  2       THIS FILE I
  S ALL OR PART OF TIME PERIOD  9 37  0 TO 11 40 30  DESCRIPTION OF RECORD -- 106 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  106 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE 14 CYCLES OF 106 SAMP/CYC = 1484 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 495 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     PILOT MICROPHONE SWITCH (VDC)              XMIT      VDC     = (N/ 1000.0) -  100.0
    7)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
    8)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
    9)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
   10)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   11)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   12)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   13)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   14)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   15)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   16)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   17)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   18)   1     MAGNETIC RADIAL.DIST   RAD.NM              DMESLC   RAD.NM   = (N/ 1000.0) -  100.0
   19)   1     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
   20)   1     RAW DYNAMIC PRESSURE (BOOM)      (MB)      QCB       MB      = (N/ 1000.0) -  100.0
   21)   1     CORRECTED DYNAMIC PRESR (WING)  (MB)       QCWC      MB      = (N/ 1000.0) -  100.0
   22)   1     CORRECTED DYNAMIC PRESR (BOOM)      (MB)   QCBC      MB      = (N/ 1000.0) -  100.0
   23)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
   24)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
   25)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   26)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -    0.0
   27)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   28)   1     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   29)   1     TOTAL TEMPERATURE(REVERSE FLOW) (C)        TTRF      C       = (N/ 1000.0) -  100.0
   30)   1     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)     ATRF      C       = (N/ 1000.0) -  100.0
   31)   1     TOTAL TEMPERATURE(DEICED ROSE C)           TTBH      C       = (N/ 1000.0) -  100.0
   32)   1     AMBIENT TEMPERATURE(DEIC ROSE C)           ATBH      C       = (N/ 1000.0) -  100.0
   33)   1     DEW/FROST POINT TEMP ( E-G+G)(RT-BOT)(C)   DPRB      C       = (N/ 1000.0) -  100.0
   34)   1     DEW/FROST POINT TEMP(GN EAST)(RT-TOP)(C)   DPRT      C       = (N/ 1000.0) -  100.0
   35)   1     DEWPOINT TEMPERATURE ( E-G+G)(RT-BOT)(C)   DPRBC     C       = (N/ 1000.0) -  100.0
   36)   1     DEWPOINT TEMPERATURE(GN EAST)(RT-TOP)(C)   DPRTC     C       = (N/ 1000.0) -  100.0
   37)   1     ABSOLUTE HUMIDITY ( E-G+G)(RT-BOT)(G/M3)   RHOTDB    G/M3    = (N/ 1000.0) -  100.0
   38)   1     ABSOLUTE HUMIDITY(GN EAST)(RT-TOP)(G/M3)   RHOTDT    G/M3    = (N/ 1000.0) -  100.0
   39)   1     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
   40)   1     AIRCRAFT TRUE AIRSPEED (BOOM) (M/S)        TASB      M/S     = (N/ 1000.0) -  100.0
   41)   1     RAW J-W LIQUID WATER CONTENT (G/M3)        LWC       G/M3    = (N/ 1000.0) -  100.0
   42)   1     CORRCTD J-W LIQUID WATER CONTENT (G/M3)    LWCC      G/M3    = (N/ 1000.0) -  100.0
   43)   1     VERT DIFF PRESSURE GUST       (MB)         ADIF      MB      = (N/ 1000.0) -  100.0
   44)   1     ATTACK ANGLE ROSEMOUNT          (DEG)      ATTACK    DEG     = (N/ 1000.0) -  100.0
   45)   1     HORZ DIFF PRESSURE GUST          (MB)      BDIF      MB      = (N/ 1000.0) -  100.0
   46)   1     SIDESLIP ANGLE (ROSEMOUNT)         (DEG)   SSLIP     DEG     = (N/ 1000.0) -  100.0
   47)   1     WIND VECTOR EAST GUST COMPONENT (M/S)      UI        M/S     = (N/ 1000.0) -  200.0
   48)   1     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI        M/S     = (N/ 1000.0) -  200.0
   49)   1     WIND VECTOR VERTICAL GUST COMP (M/S)       WI        M/S     = (N/ 1000.0) -  100.0
   50)   1     WIND VECTOR LNGTDNL GUST COMP. (M/S)       UX        M/S     = (N/ 1000.0) -  200.0
   51)   1     WIND VECTOR LATERAL GUST COMP. (M/S)       VY        M/S     = (N/ 1000.0) -  200.0
   52)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
   53)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
   54)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  200.0
   55)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  200.0
   56)   1     DIST EAST OF SALT LAKE AIRPORT (KM)        DEI       KM      = (N/  100.0) - 1000.0
   57)   1     DIST NORTH OF SALT LAKE AIRPORT (KM)       DNI       KM      = (N/  100.0) - 1000.0
   58)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   59)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   60)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   61)   1     RELATIVE HUMIDITY (PER CENT)               RHUM     PER CENT = (N/ 1000.0) -  100.0
   62)   1     MIXING RATIO      (G/KG)                   RM     G/KG       = (N/ 1000.0) -  100.0
   63)   1     EQUIVALENT POTENTIAL TEMPERATURE (K)       ETHETA    K       = (N/ 1000.0) -  100.0
   64)   1     POTENTIAL TEMPERATURE (K)                  THETA     K       = (N/ 1000.0) -  100.0
   65)   1     SPECIFIC HUMIDITY (G/KG)                   SPHUM    G/KG     = (N/ 1000.0) -  100.0
   66)   1     VIRTUAL POTENTIAL TEMPERATURE (K)          VTHETA    K       = (N/ 1000.0) -  100.0
   67)   1     FSSP RANGE           (RANGE)               IRNG     RANGE    = (N/    1.0) -    0.0
   68)   1     FSSP FAST RESET      (RESET)              IRESET    RESET    = (N/    1.0) -    0.0
   69)   1     FSSP TOTAL STROBES   (STROBE)             ISTROB    STROBE   = (N/    1.0) -    0.0
   70)   1     PROBE 1/CELL 1 ACCMULATION(COUNTS)         SUM1/ 1   COUNTS  = (N/ 1000.0) -  100.0
   71)   1     PROBE 1/CELL 2 ACCMULATION(COUNTS)         SUM1/ 2   COUNTS  = (N/ 1000.0) -  100.0
   72)   1     PROBE 1/CELL 3 ACCMULATION(COUNTS)         SUM1/ 3   COUNTS  = (N/ 1000.0) -  100.0
   73)   1     PROBE 1/CELL 4 ACCMULATION(COUNTS)         SUM1/ 4   COUNTS  = (N/ 1000.0) -  100.0
   74)   1     PROBE 1/CELL 5 ACCMULATION(COUNTS)         SUM1/ 5   COUNTS  = (N/ 1000.0) -  100.0
   75)   1     PROBE 1/CELL 6 ACCMULATION(COUNTS)         SUM1/ 6   COUNTS  = (N/ 1000.0) -  100.0
   76)   1     PROBE 1/CELL 7 ACCMULATION(COUNTS)         SUM1/ 7   COUNTS  = (N/ 1000.0) -  100.0
   77)   1     PROBE 1/CELL 8 ACCMULATION(COUNTS)         SUM1/ 8   COUNTS  = (N/ 1000.0) -  100.0
   78)   1     PROBE 1/CELL 9 ACCMULATION(COUNTS)         SUM1/ 9   COUNTS  = (N/ 1000.0) -  100.0
   79)   1     PROBE 1/CELL10 ACCMULATION(COUNTS)         SUM1/10   COUNTS  = (N/ 1000.0) -  100.0
   80)   1     PROBE 1/CELL11 ACCMULATION(COUNTS)         SUM1/11   COUNTS  = (N/ 1000.0) -  100.0
   81)   1     PROBE 1/CELL12 ACCMULATION(COUNTS)         SUM1/12   COUNTS  = (N/ 1000.0) -  100.0
   82)   1     PROBE 1/CELL13 ACCMULATION(COUNTS)         SUM1/13   COUNTS  = (N/ 1000.0) -  100.0
   83)   1     PROBE 1/CELL14 ACCMULATION(COUNTS)         SUM1/14   COUNTS  = (N/ 1000.0) -  100.0
   84)   1     PROBE 1/CELL15 ACCMULATION(COUNTS)         SUM1/15   COUNTS  = (N/ 1000.0) -  100.0
   85)   1     SUM OF 15 CELLS                            SUM15     SUM     = (N/  500.0) -    0.0
   86)   1     FSSP BEAM FRACTION                         BMFRAC            = (N/ 1000.0) -    0.0
   87)   1     FSSP ACTIVITY                              FACTIV            = (N/ 1000.0) -    0.0
   88)   1     PROBE 1/CELL 1 CONCENTRATION (CTS/CC)      FCN/01    N/CC    = (N/  500.0) -    0.0
   89)   1     PROBE 1/CELL 2 CONCENTRATION (CTS/CC)      FCN/02    N/CC    = (N/  500.0) -    0.0
   90)   1     PROBE 1/CELL 3 CONCENTRATION (CTS/CC)      FCN/03    N/CC    = (N/  500.0) -    0.0
   91)   1     PROBE 1/CELL 4 CONCENTRATION (CTS/CC)      FCN/04    N/CC    = (N/  500.0) -    0.0
   92)   1     PROBE 1/CELL 5 CONCENTRATION (CTS/CC)      FCN/05    N/CC    = (N/  500.0) -    0.0
   93)   1     PROBE 1/CELL 6 CONCENTRATION (CTS/CC)      FCN/06    N/CC    = (N/  500.0) -    0.0
   94)   1     PROBE 1/CELL 7 CONCENTRATION (CTS/CC)      FCN/07    N/CC    = (N/  500.0) -    0.0
   95)   1     PROBE 1/CELL 8 CONCENTRATION (CTS/CC)      FCN/08    N/CC    = (N/  500.0) -    0.0
   96)   1     PROBE 1/CELL 9 CONCENTRATION (CTS/CC)      FCN/09    N/CC    = (N/  500.0) -    0.0
   97)   1     PROBE 1/CELL10 CONCENTRATION (CTS/CC)      FCN/10    N/CC    = (N/  500.0) -    0.0
   98)   1     PROBE 1/CELL11 CONCENTRATION (CTS/CC)      FCN/11    N/CC    = (N/  500.0) -    0.0
   99)   1     PROBE 1/CELL12 CONCENTRATION (CTS/CC)      FCN/12    N/CC    = (N/  500.0) -    0.0
  100)   1     PROBE 1/CELL13 CONCENTRATION (CTS/CC)      FCN/13    N/CC    = (N/  500.0) -    0.0
  101)   1     PROBE 1/CELL14 CONCENTRATION (CTS/CC)      FCN/14    N/CC    = (N/  500.0) -    0.0
  102)   1     PROBE 1/CELL15 CONCENTRATION (CTS/CC)      FCN/15    N/CC    = (N/  500.0) -    0.0
  103)   1     WATER CONTENT  (FSSP PROBE) (G/M3)         FLWC      G/M3    = (N/10000.0) -    0.0
  104)   1     CONCENTRATION (FSSP PROBE)  (N/CC)         FCONC     N/CC    = (N/  500.0) -    0.0
  105)   1     MEAN DIAMETER (FSSP PROBE)  (MICRONS)      FDBAR     MICRONS = (N/10000.0) -    0.0
  106)   1     DISPERSION (FSSP PROBE)                    FDISP             = (N/10000.0) -    0.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
    660-01 FUKUTA ONT 16JAN1982 09/37/00
 THIS FILE IS ALL OR PART OF THE TIME PERIOD  9        37         0         TO   11        40        30
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          117 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                        97344 BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  2120 BITS PER LOGICAL DATA RECORD
                           14 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        29680 BITS PER PHYSICAL DATA RECORD