Sample HRT GENPRO-I header

  638-1 O3-F&B 15 JUN 82                            FIRST TIME ON THIS FILE  8  9  4       THIS FILE I
  S ALL OR PART OF TIME PERIOD  8  8 54 TO 10 32 20  DESCRIPTION OF RECORD --  85 PARAMETERS WERE SAVE
  D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  750 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
   THE  2 CYCLES OF 750 SAMP/CYC = 1500 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
  D INTO 500 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     PILOT MICROPHONE SWITCH (XMIT) (VDC)       XMIT      VDC     = (N/ 1000.0) -  100.0
    5)   1     FIXED ZERO VOLTAGE  (VDC)                  FZV               = (N/ 1000.0) -  100.0
    6)   1     RADIOMET.SURF.TEMP(PRT-5)(9.5-11.5)(C)     PRT5      C       = (N/ 1000.0) -  100.0
    7)   1     TOP PYRGEOMETER DOME TEMP (C)              TPGDT      C      = (N/ 1000.0) -  100.0
    8)   1     BOTTOM PYRGEOMETER DOME TEMP (C)           BPGDT      C      = (N/ 1000.0) -  100.0
    9)   1     TOP PYRGEOMETER SINK TEMP (C)              TPGST      C      = (N/ 1000.0) -  100.0
   10)   1     BOTTOM PYRGEOMETER SINK TEMP (C)           BPGST      C      = (N/ 1000.0) -  100.0
   11)   1     RAW DWNWARD IR IRRADIANCE (WATTS/M2)        TPYRG  WATTS/M2  = (N/  100.0) - 1000.0
   12)   1     RAW UPWARD IR IRRADIANCE (WATTS /M2)        BPYRG  WATTS/M2  = (N/  100.0) - 1000.0
   13)   1     TOP PYRANOMETER IRRADIANCE                  TPYR1  WATTS/M2  = (N/  500.0) -  100.0
   14)   1     BOTTOM PYRANOMETER IRRADIANCE               BPYR1  WATTS/M2  = (N/  500.0) -  100.0
   15)   1     TOP PYRGEOMETER CORRECTED (WAT  TS/M2)     TPYRGC   WATTS/M2 = (N/ 1000.0) -  100.0
   16)   1     BOTTOM PYRGEOMETER CORRECTED (WATTS/M2)    BPYRGC   WATTS/M2 = (N/ 1000.0) -  100.0
   17)   1     RX CHAMBER PRESSURE  (VDC) (CH.32)         O3RXP    VDC      = (N/ 1000.0) -  100.0
   18)   1     RX CHAMBER TEMPERATURE (VDC) (CH.33)       O3RXT    VDC      = (N/ 1000.0) -  100.0
   19)   1     O3 PMT TEMPERATURE   (VDC) (CH.34)         O3PMT    VDC      = (N/ 1000.0) -  100.0
   20)   1     COOLER TEMPERATURE  (VDC) (CH.35)          CHS1    VDC       = (N/ 1000.0) -  100.0
   21)   1     DASIBI-OZONE  (PPBV) (CH.28)               DO3     PPBV      = (N/ 1000.0) -  100.0
   22)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
   23)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
   24)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
   25)   1     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
   26)   1     CORRECTED DYNAMIC PRESR (WING)  (MB)       QCWC      MB      = (N/ 1000.0) -  100.0
   27)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
   28)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
   29)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB1      MB      = (N/ 1000.0) -    0.0
   30)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC1     MB      = (N/ 1000.0) -    0.0
   31)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
   32)   1     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
   33)   1     TOTAL TEMPERATURE (REVERSE FLOW) (C)       TTRF      C       = (N/ 1000.0) -  100.0
   34)   1     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)     ATRF      C       = (N/ 1000.0) -  100.0
   35)   1     DEW/FROST POINT TEMP ( E-G+G)(RT-BOT)(C)   DPRB      C       = (N/ 1000.0) -  100.0
   36)   1     DEW/FROST POINT TEMP( E- G+G)(RT-TOP)(C)   DPRT      C       = (N/ 1000.0) -  100.0
   37)   1     DEWPOINT TEMPERATURE ( E-G+G)(RT-BOT)(C)   DPRBC     C       = (N/ 1000.0) -  100.0
   38)   1     DEWPOINT TEMPERATURE(E- G+G )(RT-TOP)(C)   DPRTC     C       = (N/ 1000.0) -  100.0
   39)   1     ABSOLUTE HUMIDITY ( E-G+G)(RT-BOT)(G/M3)   RHOTDB    G/M3    = (N/ 1000.0) -  100.0
   40)   1     ABSOLUTE HUMIDITY( E- G+G)(RT-TOP)(G/M3)   RHOTDT    G/M3    = (N/ 1000.0) -  100.0
   41)   1     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
   42)  20     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
   43)  20     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
   44)  20     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
   45)  20     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
   46)  20     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
   47)  20     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
   48)  20     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
   49)  20     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
   50)  20     RAW DYNAMIC PRESSURE (GUST PROBE)(MB)      QCG       MB      = (N/ 1000.0) -  100.0
   51)  20     CORRECTED DYNAMIC PRESR (GUST PROBE)(MB)   QCGC      MB      = (N/ 1000.0) -  100.0
   52)  20     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)     TTB       C       = (N/ 1000.0) -  100.0
   53)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)      TTKP      C       = (N/ 1000.0) -  100.0
   54)  20     AMBIENT TEMPERATURE (BOOM ROSEMOUNT)(C)    ATB       C       = (N/ 1000.0) -  100.0
   55)  20     AMBIENT TEMP (FAST RESPONSE)  (C)          ATKP      C       = (N/ 1000.0) -  100.0
   56)  20     RAW LYMAN ALPHA HYGROMETER OUTPUT (VDC)    VLA       VDC     = (N/ 1000.0) -  100.0
   57)  20     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)        TASG      M/S     = (N/ 1000.0) -  100.0
   58)  20     ATTACK ANGLE ( LEFT FIXED VANE) (DEG)      AFIXL     DEG     = (N/ 1000.0) -  100.0
   59)  20     ATTACK ANGLE (RIGHT FIXED VANE) (DEG)      AFIXR     DEG     = (N/ 1000.0) -  100.0
   60)  20     SIDESLIP ANGLE (TOP FIXED VANE)  (DEG)     BFIXT     DEG     = (N/ 1000.0) -  100.0
   61)  20     SIDESLIP ANGLE (BOTTOM FIXED VANE) (DEG)   BFIXB     DEG     = (N/ 1000.0) -  100.0
   62)  20     WIND VECTOR EAST GUST COMPONENT (M/S)      UI        M/S     = (N/ 1000.0) -  200.0
   63)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI        M/S     = (N/ 1000.0) -  200.0
   64)  20     WIND VECTOR VERTICAL GUST COMP     (M/S)   WI        M/S     = (N/ 1000.0) -  100.0
   65)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)   UX        M/S     = (N/ 1000.0) -  200.0
   66)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)   VY        M/S     = (N/ 1000.0) -  200.0
   67)  20     HORIZONTAL WIND DIRECTION (BOOM) (DEG)     WDRCTN    DEG     = (N/ 1000.0) -  100.0
   68)  20     HORIZONTAL WIND SPEED (BOOM) (M/S)         WSPD      M/S     = (N/ 1000.0) -  100.0
   69)  20     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
   70)  20     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
   71)  20     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
   72)  20     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
   73)  20     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
   74)  20     POTENTIAL TEMPERATURE (K)                  THETA     K       = (N/ 1000.0) -  100.0
   75)  20     VIRTUAL POTENTIAL TEMPERATURE  (K)         VTHETA    K       = (N/ 1000.0) -  100.0
   76)  20     FAST OZONE MIXING RATIO  (VDC) (CH.30)     O3F25  VDC        = (N/ 1000.0) -  100.0
   77)   1     DISTANCE EAST OF START  (KM)               DEI       KM      = (N/  100.0) - 1000.0
   78)   1     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 1000.0
   79)   1     RELATIVE HUMIDITY (PER CENT)               RHUM     PER CENT = (N/ 1000.0) -  100.0
   80)   1     TEMP. AT LF. COND. LEVEL  (C)              TLCL       (C)    = (N/ 1000.0) -  100.0
   81)   1     PRESS. AT LF. COND. LEVEL (MB)             PLCL      MB      = (N/ 1000.0) -  100.0
   82)   1     WATER VAPOR MIXING RATIO  (G/KG)           RM        G/KG    = (N/ 1000.0) -  100.0
   83)   1     SPECIFIC HUMIDITY     (G/KG)               SPHUM     G/KG    = (N/ 1000.0) -  100.0
   84)   1     SURFACE PRESSURE          (MB)             SURFP     MB      = (N/ 1000.0) -    0.0
   85)   1     MEAN OZONE MIXING RATIO  (PPBV) (CH.31)    OMO3   PPBV       = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
  638-1 O3-F&B 15 JUN 82
 THIS FILE IS ALL OR PART OF THE TIME PERIOD  8         8        54         TO   10        32        20
 DESCRIPTION OF TAPE:
         HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                          761 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                       633152 BITS PER PHYSICAL HEADER RECORD
           DATA FILE -- 15000 BITS PER LOGICAL DATA RECORD
                            2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                        30000 BITS PER PHYSICAL DATA RECORD