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
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