Sample LRT GENPRO-I header

  NCAR ELECTRA GRAVE-1  FEB 01,1976                 FIRST TIME ON THIS FILE 20 40 58       THIS FILE I
  S ALL OR PART OF TIME PERIOD 20 40 58 TO 27 18 49  DESCRIPTION OF RECORD --  83 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  203 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  7 CYCLES OF 203 SAMP/CYC = 1421 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 474 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)                    TIME     SECONDS = (N/      1) -    0.0
    2)   1     UNALTERED TAPE TIME (SECONDS)               TPTIME SECONDS   = (N/      1) -    0.0
    3)   1     CORRECTED STATIC PRESSURE (MB)               PSWC    (MB)    = (N/    500) -    0.0
    4)   1     AMBIENT TEMPERATURE (ROSEMOUNT) (C)          ATF     (C)     = (N/   1000) -  100.0
    5)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)       DPXC       DEG C = (N/   1000) -  100.0
    6)   1     ABSOLUTE HUMIDITY (THERMOELEC) (GM/M3)      RHOTD    (GM/M3) = (N/   1000) -  100.0
    7)   1     HORIZONTAL WIND DIRECTION (DEG)             WDRCTN   (DEG)   = (N/   1000) -    0.0
    8)   1     HORIZONTAL WIND SPEED (M/S)                  WSPD    (M/S)   = (N/   1000) -    0.0
    9)   1     WIND VECTOR EAST COMPONENT (M/S)               UI1   (M/S)   = (N/   1000) -  200.0
   10)   1     WIND VECTOR NORTH COMPONENT (M/S)              VI1   (M/S)   = (N/   1000) -  200.0
   11)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)            UX1   (M/S)   = (N/   1000) -  200.0
   12)   1     WIND VECTOR LATERAL COMPONENT (M/S)            VY1   (M/S)   = (N/   1000) -  200.0
   13)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   14)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   15)   1     NACA PRESSURE ALTITUDE (M)                   HP      (M)     = (N/    100) -  100.0
   16)   1     PRESSURE DAMPED INERTIAL ALTITUDE (M)       HI31     (M)     = (N/    100) -  100.0
   17)   1     GEOMETRIC (RADIO) ALTITUDE (M)               HGM     (M)     = (N/   1000) -  100.0
   18)   1     AIRCRAFT GROUND SPEED (M/S)                 GS       (M/S)   = (N/   1000) -    0.0
   19)   1     AIRCRAFT GROUND SPD EAST COMP (M/S)            VEW   (M/S)   = (N/   1000) -  500.0
   20)   1     AIRCRAFT GROUND SPD NORTH COMP (M/S)           VNS   (M/S)   = (N/   1000) -  500.0
   21)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)          WP31    (M/S)   = (N/   1000) -  100.0
   22)   1     AIRCRAFT C.G. VERT ACCELERATION (M/S2)      CGAC1    (M/S2)  = (N/   1000) -  100.0
   23)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)             THF    (DEG)   = (N/   1000) -    0.0
   24)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)            ROLL   (DEG)   = (N/   1000) -  100.0
   25)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)          PITCH   (DEG)   = (N/   1000) -  100.0
   26)   1     AIRCRAFT TRUE AIRSPEED (M/S)                 TASW    (M/S)   = (N/   1000) -  100.0
   27)   1     CORCTD IR SURFACE TEMP (PRT-5) (C)          PRT5C     (C)    = (N/   1000) -  100.0
   28)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   29)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   30)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   31)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   32)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   33)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   34)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   35)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   36)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   37)   1     PRT-6 FILTER POSITION                       P6FP             = (N/      1) -    0.0
   38)   1     PRT-6 MIRROR POSITION (DEG)                 P6MP      (DEG)  = (N/   1000) -  100.0
   39)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   40)   1     NOSEBOOM TOTAL TEMP (ROSEMOUNT) (C)           TTB5     DEG C = (N/   1000) -  100.0
   41)   1     FUSELAGE TOTAL TEMP (ROSEMOUNT) (C)           TTF    (C)     = (N/   1000) -  100.0
   42)   1     LHS DEW/FROSTPOINT TEMP (C)                   DPLH   (C)     = (N/   1000) -  100.0
   43)   1     RHS DEW/FROSTPOINT TEMP (C)                   DPRH   (C)     = (N/   1000) -  100.0
   44)   1     RAW WINGTIP STATIC PRESSURE (MB)              PSW    (MB)    = (N/    500) -    0.0
   45)   1     RAW WINGTIP DYNAMIC PRESSURE (MB)             QCW       MB   = (N/   1000) -  100.0
   46)   1     RAW NOSEBOOM STATIC PRESSURE (MB)             PSB    (MB)    = (N/    500) -    0.0
   47)   1     RAW NOSEBOOM DYNAMIC PRESSURE (MB)            QCB       MB   = (N/   1000) -  100.0
   48)   1     RAW INS LATITUDE (DEG)                        ALAT   (DEG)   = (N/   1000) -  200.0
   49)   1     RAW INS LONGITUDE (DEG)                      ALONG   (DEG)   = (N/   1000) -  200.0
   50)   1     RAW VLF LATITUDE (DEG)                        VLAT    (DEG)  = (N/   1000) -  200.0
   51)   1     RAW VLF LONGITUDE (DEG)                      VLONG   (DEG)   = (N/   1000) -  200.0
   52)   1     RAW INS VERTICAL VELOCITY (M/S)              VZI     (M/S)   = (N/    100) - 5000.0
   53)   1     INS WANDER ANGLE (DEG)                       ALPHA   (DEG)   = (N/   1000) -  100.0
   54)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)           THI    (DEG)   = (N/   1000) -  100.0
   55)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   56)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   57)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   58)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   59)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   60)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   61)   1     PRT-5 IRTRAN WINDOW TEMP (C)                PRT5WT    (C)    = (N/   1000) -  100.0
   62)   1     RAW IR SURFACE TEMP(PRT-5) (C)                PRT5    (C)    = (N/   1000) -  100.0
   63)   1     PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC)       P6RADV    (C)    = (N/   1000) -  100.0
   64)   1     PRT-6 OVEN TEMP DEVIATION (C)               P6OVNT  (C)      = (N/   1000) -  100.0
   65)   1     PRT-6 ROTATING MIRROR TEMP (DEG)            P6RMT     (C)    = (N/   1000) -  100.0
   66)   1     PRT-6 FIXED MIRROR TEMP (C)                 P6FMT     (C)    = (N/   1000) -  100.0
   67)   1     PRT-6 CALIBRATION PLATE TEMP (C)            P6CPT     (C)    = (N/   1000) -  100.0
   68)   1     PRT-6 MODE INDICATOR                        P6MV     (VDC)   = (N/      1) -    0.0
   69)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   70)   1     16MM CAMERA FRAME COUNT                    CAMFC             = (N/      1) -    0.0
   71)   1     EVENT MARKERS                              EVMKS    VDC      = (N/      1) -    0.0
   72)   1     INS/KNLBRG UPDATE FLAGS                     UPDATE           = (N/      1) -    0.0
   73)   1     ZERO INPUT(A/D CHECK)                    A/D CHK    (VDC)    = (N/   1000) -  100.0
   74)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   75)   1     UNUSED                                      UNUSED           = (N/      1) -    0.0
   76)  20     AIRCRAFT C.G. VERT ACCELERATION (M/S2)       CGAC    (M/S2)  = (N/   1000) -  100.0
   77)  20            LEFT WING STRAIN (MICRO-IN/IN)        STRLW (UIN/IN)  = (N/    500) - 1000.0
   78)  20            RIGHT WING STRAIN (MICRO-IN/IN)       STRRW (UIN/IN)  = (N/    500) - 1000.0
   79)  64     KNOLLENBERG 64 WORDS                      KNLBG       COUNTS = (N/      1) -    0.0
   80)   1     OZONE (WASH. ST. UNIV.) (VDC)            O3(W ST)   (VDC)    = (N/   1000) -  100.0
   81)   1     SO2 U. OF ARIZONA                             SO2      VDC   = (N/   1000) -  100.0
   82)   1     FIXED NEPHELOMETER CHANNEL 56             FIXNEP56   (VDC)   = (N/   1000) -  100.0
   83)   1     FIXED NEPHELOMETER CHANNEL 57             FIXNEP57   (VDC)   = (N/   1000) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  NCAR ELECTRA GRAVE-1  FEB 01,1976
 THIS FILE IS ALL OR PART OF THE TIME PERIOD 20        40        58         TO   27        18        49
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          214 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       178048 BITS PER PHYSICAL HEADER RECORD
           DATA FILE --  4060 BITS PER LOGICAL DATA RECORD
                            7 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        28420 BITS PER PHYSICAL DATA RECORD