Sample HRT GENPRO-I header

884A-19 GAMETAG 01JUN78 15/41/40                  FIRST TIME ON THIS FILE 15 41 40       THIS FILE I
S ALL OR PART OF TIME PERIOD 15 41 40 TO 18 34 29  DESCRIPTION OF RECORD -- 124 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  795 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
 THE  1 CYCLES OF 795 SAMP/CYC =  795 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 265 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     CORRECTED STATIC PRESSURE (MB)               PSXC1    MB     = (N/  500.0) -    0.0
  4)   1     AMBIENT TEMP (FUSELAGE ROSEMOUNT) (C)        ATF1     C      = (N/ 1000.0) -  100.0
  5)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
  6)   1     DEWPOINT TEMPERATURE (THERMOELEC) (C)      DPXC       C      = (N/ 1000.0) -  100.0
  7)   1     DEWPOINT TEMPERATURE (LYMAN-ALPHA) (C)    DPLAC1      C      = (N/ 1000.0) -  100.0
  8)   1     ABSOLUTE HUMIDITY (THERMOELEC) (G/M3)       RHOTD     G/M3   = (N/ 1000.0) -  100.0
  9)   1     ABSOLUTE HUMIDITY (LYMAN-ALPHA) (G/M3)    RHOLA1      G/M3   = (N/ 1000.0) -  100.0
 10)   1     HORIZONTAL WIND DIRECTION (DEG)             WDRCTN    DEG    = (N/ 1000.0) -    0.0
 11)   1     HORIZONTAL WIND SPEED (M/S)                  WSPD     M/S    = (N/ 1000.0) -    0.0
 12)   1     WIND VECTOR EAST COMPONENT (M/S)               UI1    M/S    = (N/ 1000.0) -  200.0
 13)   1     WIND VECTOR NORTH COMPONENT (M/S)              VI1    M/S    = (N/ 1000.0) -  200.0
 14)   1     WIND VECTOR VERT GUST COMPONENT (M/S)          WI1    M/S    = (N/ 1000.0) -  100.0
 15)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)            UX1    M/S    = (N/ 1000.0) -  200.0
 16)   1     WIND VECTOR LATERAL COMPONENT (M/S)            VY1    M/S    = (N/ 1000.0) -  200.0
 17)   1     RAW INS LATITUDE (DEG)                        ALAT    DEG    = (N/ 1000.0) -  200.0
 18)   1     RAW INS LONGITUDE (DEG)                      ALONG    DEG    = (N/ 1000.0) -  200.0
 19)   1     NACA PRESSURE ALTITUDE (M)                   HP       M      = (N/  100.0) -  100.0
 20)   1     PRESSURE DAMPED INERTIAL ALTITUDE (M)         HI31    M      = (N/  100.0) -  100.0
 21)   1     GEOMETRIC (RADIO) ALTITUDE (M)               HGM      M      = (N/ 1000.0) -  100.0
 22)   1     RAW AIRCRAFT (INS) GROUND SPEED (M/S)       GSF1      M/S    = (N/ 1000.0) -    0.0
 23)   1     AIRCRAFT GROUND SPD EAST COMP (M/S)        VEW1       M/S    = (N/ 1000.0) -  500.0
 24)   1     AIRCRAFT GROUND SPD NORTH COMP (M/S)      VNS1        M/S    = (N/ 1000.0) -  500.0
 25)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)          WP31     M/S    = (N/ 1000.0) -  100.0
 26)   1     AIRCRAFT C.G. VERT ACCELERATION (M/S2)     CGAC1      M/S2   = (N/ 1000.0) -  100.0
 27)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)            THF1     DEG    = (N/ 1000.0) -    0.0
 28)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)          ROLL1     DEG    = (N/ 1000.0) -  100.0
 29)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)      PITCH1       DEG    = (N/ 1000.0) -  100.0
 30)   1     AIRCRAFT TRUE AIRSPEED (M/S)                 TASX1    M/S    = (N/ 1000.0) -  100.0
 31)   1     CORCTD RADIOMTRC SURFACE TEMP (PRT-5)(C) PRT5C        C      = (N/ 1000.0) -  100.0
 32)   1     DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2)      UPYR1     W/M2   = (N/  500.0) -  100.0
 33)   1     DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2)      UPYR2     W/M2   = (N/  500.0) -  100.0
 34)   1     DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2)      UPYR3     W/M2   = (N/  500.0) -  100.0
 35)   1     UPWARD SW/WG-7 IRRADIANCE (WATTS/M2)        LPYR1     W/M2   = (N/  500.0) -  100.0
 36)   1     UPWARD SW/OG-1 IRRADIANCE (WATTS/M2)        LPYR2     W/M2   = (N/  500.0) -  100.0
 37)   1     UPWARD SW/RG-8 IRRADIANCE (WATTS/M2)        LPYR3     W/M2   = (N/  500.0) -  100.0
 38)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 39)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 40)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 41)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 42)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 43)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 44)   1     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)        TTB1     (C)   = (N/ 1000.0) -  100.0
 45)   1     TOTAL TEMP (FUSELAGE ROSEMOUNT) (C)           TTF1    C      = (N/ 1000.0) -  100.0
 46)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 47)   1     DEW/FROST POINT TEMP (L THERMOELEC) (C)       DPL     C      = (N/ 1000.0) -  100.0
 48)   1     DEW/FROST POINT TEMP (R THERMOELEC) (C)       DPR     C      = (N/ 1000.0) -  100.0
 49)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 50)   1     RAW STATIC PRESSURE (WINGTIP) (MB)            PSW1    MB     = (N/  500.0) -    0.0
 51)   1     RAW DYNAMIC PRESSURE (WINGTIP) (MB)           QCW1    MB     = (N/ 1000.0) -  100.0
 52)   1     RAW STATIC PRESSURE (BOOM) (MB)               PSB1    MB     = (N/  500.0) -    0.0
 53)   1     RAW DYNAMIC PRESSURE (BOOM) (MB)              QCB1    MB     = (N/ 1000.0) -  100.0
 54)   1     DISTANCE EAST OF START (KM)                    DEI    KM     = (N/   50.0) -10000.0
 55)   1     DISTANCE NORTH OF START (KM)                   DNI    KM     = (N/   50.0) -10000.0
 56)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 57)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 58)   1     CABIN PRESSURE (MB)                        PCAB        MB    = (N/  500.0) -    0.0
 59)   1     INS WANDER ANGLE (DEG)                       ALPHA    DEG    = (N/ 1000.0) -  100.0
 60)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)           THI     DEG    = (N/ 1000.0) -  100.0
 61)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 62)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 63)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 64)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 65)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 66)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 67)   1     PRT-5 IRTRAN WINDOW TEMPERATURE (C)        PRT5WT     C      = (N/ 1000.0) -  100.0
 68)   1     RAW IR SURFACE TEMP(RANGE)                 PRT5R     RANGE   = (N/ 1000.0) -  100.0
 69)   1     RAW RADIOMETRIC SURFACE TEMP (PRT-5) (C)   PRT5              = (N/ 1000.0) -  100.0
 70)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 71)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 72)   1     16MM CAMERA FRAME COUNT                    CAMFC             = (N/    1.0) -    0.0
 73)   1     EVENT MARKER WORD (16 BITS)               EVMRKS             = (N/    1.0) -    0.0
 74)   1     INS/KNOLLENBERG UPDATE FLAGS                UPDATE           = (N/    1.0) -    0.0
 75)   1               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 76)  20     AMBIENT TEMPERATURE (FAST RESPONSE) (C)     ATKP      C      = (N/ 1000.0) -  100.0
 77)  20     AMBIENT TEMP (COMPNSTD BOOM ROSMNT) (C)     ATBC      C      = (N/ 1000.0) -  100.0
 78)  20     TOTAL TEMP (COMPENSATED BOOM ROSMNT) (C)   TTBC       C      = (N/ 1000.0) -  100.0
 79)  20     WIND VECTOR EAST GUST COMPONENT (M/S)           UI    M/S    = (N/ 1000.0) -  200.0
 80)  20     WIND VECTOR NORTH GUST COMPONENT (M/S)          VI    M/S    = (N/ 1000.0) -  200.0
 81)  20     WIND VECTOR VERT GUST COMPONENT(HR)(M/S)        WI    M/S    = (N/ 1000.0) -  100.0
 82)  20     WIND VECTOR LNGTDNL GUST COMPONENT (M/S)        UX    M/S    = (N/ 1000.0) -  200.0
 83)  20     WIND VECTOR LATERAL GUST COMPONENT (M/S)        VY    M/S    = (N/ 1000.0) -  200.0
 84)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 85)  20     ABSOLUTE HUMIDITY (LYMN-ALPHA HR) (G/M3)  RHOLA       G/M3   = (N/ 1000.0) -  100.0
 86)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
 87)  20     RAW LYMAN-ALPHA HYGROMETER OUTPUT (VDC)      LAV      VDC    = (N/ 1000.0) -  100.0
 88)  20     TOTAL TEMPERATURE (FAST RESPONSE) (C)        TTKP     C      = (N/ 1000.0) -  100.0
 89)  20     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)        TTB     C      = (N/ 1000.0) -  100.0
 90)  20     RAW DYNAMIC PRESSURE (GUST PROBE) (MB)        QCG     MB     = (N/ 1000.0) -  100.0
 91)  20     ATTACK ANGLE (ROTATING VANE) (DEG)         AROT       DEG    = (N/ 1000.0) -  100.0
 92)  20     ATTACK ANGLE (FIXED VANE) (DEG)               AFIX    DEG    = (N/ 1000.0) -  100.0
 93)  20     SIDESLIP ANGLE (ROTATING VANE) (DEG)       BROT       DEG    = (N/ 1000.0) -  100.0
 94)  20     SIDESLIP ANGLE (FIXED VANE) (DEG)             BFIX    DEG    = (N/ 1000.0) -  100.0
 95)  20     GUST PROBE TIP VERT ACCELERATION (M/S2)        VAC    M/S2   = (N/ 1000.0) -  100.0
 96)  20     GUST PROBE TIP LATERAL ACCEL. (M/S2)           LAC    M/S2   = (N/ 1000.0) -  100.0
 97)  20     AIRCRAFT C.G. VERT ACCEL. (HR) (M/S2)        CGAC     M/S2   = (N/ 1000.0) -  100.0
 98)  20     RAW INS VERTICAL VELOCITY (M/S)              VZI      M/S    = (N/  100.0) - 5000.0
 99)  20     AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG)       ROLL    DEG    = (N/ 1000.0) -  100.0
100)  20     AIRCRAFT PITCH ATTITUDE ANGLE (HR) (DEG)     PITCH    DEG    = (N/ 1000.0) -  100.0
101)  20     AIRCRAFT TRUE HEADING (YAW) (HR) (DEG)        THF     DEG    = (N/ 1000.0) -  100.0
102)  20     RAW INS GROUND SPD X COMPONENT (M/S)         XVI      M/S    = (N/ 1000.0) -  500.0
103)  20     RAW INS GROUND SPD Y COMPONENT (M/S)         YVI      M/S    = (N/ 1000.0) -  500.0
104)  20     LEFT WING STRAIN (HR) (MICRO-IN/IN)          STRLW  UIN/IN   = (N/  500.0) - 1000.0
105)  20               *** UNUSED ***                   UNUSED            = (N/    1.0) -    0.0
106)  64     KNOLLENBERG 64 WORDS                       KNLBG     COUNTS  = (N/    1.0) -    0.0
107)   1     U-V SPECTROMETER OUTPUT  (VDC)   (3)       UVSPO       VDC   = (N/10000.0) -   10.0
108)   1     U-V SPECTROMETER HOUSEKEEPING(VDC) (4)     UVSPH       VDC   = (N/10000.0) -   10.0
109)   1     P. I. G. PRESSURE (MB)      (5)            PIGPR       MB    = (N/  500.0) -    0.0
110)   1     GEORGIA TECH. DASIBI OZONE (PPB) (6)       GTDO3       PPB   = (N/ 1000.0) -  100.0
111)   1     NCAR DASIBI OZONE (PPB)    (7)             NDO3        PPB   = (N/ 1000.0) -  100.0
112)   1     EYTHLENE (CSI) OZONE  (PPB)   (8)          NEO3        PPB   = (N/ 1000.0) -  100.0
113)   1     DREXEL OUTPUT X1 (VDC)    (9)              DRSO2       VDC   = (N/10000.0) -   10.0
114)   1     DREXEL OUTPUT X10 (VDC)    (10)            DRSO2       VDC   = (N/10000.0) -   10.0
115)   1     DREXEL PRESSURE X2 (VDC)   (11)            DRPRB       VDC   = (N/10000.0) -   10.0
116)   1     C.N. COUNTER RANGE (VDC)   (19)            ENV1R       VDC   = (N/10000.0) -   10.0
117)   1     C. N. COUNTER OUTPUT (VDC)    (12)         ENV1O       VDC   = (N/10000.0) -   10.0
118)   1     NCAR G.C. ECD OUTPUT (VDC)   (14)          GCECD       VDC   = (N/10000.0) -   10.0
119)   1     NCAR GC FID OUTPUT (VDC)   (15)            GCFID       VDC   = (N/10000.0) -   10.0
120)   1     NCAR G.C. SAMPLE PRESSURE (VDC) (16)       GCSPR       VDC   = (N/10000.0) -   10.0
121)   1     YORK UNIV. OUTPUT (VDC)    (17)            NOX         VDC   = (N/10000.0) -   10.0
122)   1     YORK UNIV. HOUSEKEEPING (VDC)  (18)        NOXHK       VDC   = (N/ 1000.0) -  100.0
123)  20     SAMOVAR PRESSURE (MB) (2)                 SAMPR        MB    = (N/ 1000.0) -  300.0
124)  20        USER ONE                             USER 1               = (N/ 1000.0) -  100.0

HERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
 884A-19 GAMETAG 01JUN78 15/41/40
THIS FILE IS ALL OR PART OF THE TIME PERIOD 15        41        40         TO   18        34        29
DESCRIPTION OF TAPE:
        HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
                         806 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
                      670592 BITS PER PHYSICAL HEADER RECORD
          DATA FILE -- 15900 BITS PER LOGICAL DATA RECORD
                           1 LOGICAL DATA RECORDS PER PHYSICAL RECORD
                       15900 BITS PER PHYSICAL DATA RECORD