Sample HRT GENPRO-I header
437-01 DESTRUCTION 02JUN80 FIRST TIME ON THIS FILE 10 15 0 THIS FILE I
S ALL OR PART OF TIME PERIOD 10 15 0 TO 14 27 36 DESCRIPTION OF RECORD -- 79 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 1314 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 1 CYCLES OF1314 SAMP/CYC = 1314 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 438 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 PILOT MICROPHONE SWITCH (XMIT) (VDC) XMIT VDC = (N/ 1000.0) - 100.0
6) 1 POSITIVE REFERENCE (+10.0 VDC) SIXP VDC = (N/ 1000.0) - 100.0
7) 1 NEGATIVE REFERENCE (-10.0 VDC) SIXN VDC = (N/ 1000.0) - 100.0
8) 1 RX CHAMBER PRESSURE (1HZ) (VDC) O3RXP VDC = (N/ 1000.0) - 100.0
9) 1 RX CHAMBER TEMPERATURE (1HZ) (VDC) O3RXT VDC = (N/ 1000.0) - 100.0
10) 1 RX CHAMBER TEMPERATURE (1HZ) (C) O3RXTC C = (N/ 1000.0) - 100.0
11) 1 O3 PMT TEMPERATURE (VDC) O3PMT VDC = (N/ 1000.0) - 100.0
12) 1 MEAN OZONE (VDC) MO3 VDC = (N/ 1000.0) - 100.0
13) 1 MEAN OZONE (PPBV) MO3C PPBV = (N/ 1000.0) - 100.0
14) 1 COOLER TEMPERATURE (HS1) (VDC) CHS1 VDC = (N/ 1000.0) - 100.0
15) 20 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 100.0
16) 20 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
17) 20 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
18) 20 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
19) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
20) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
21) 20 RAW INS GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0
22) 20 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
23) 20 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0
24) 20 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
25) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 1000.0) - 500.0
26) 20 RAW DYNAMIC PRESSURE (WING) (MB) QCW MB = (N/ 1000.0) - 100.0
27) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
28) 20 CORRECTED DYNAMIC PRESR (WING) (MB) QCWC MB = (N/ 1000.0) - 100.0
29) 20 CORRECTED DYNAMIC PRESR (GUST PROBE)(MB) QCGC MB = (N/ 1000.0) - 100.0
30) 20 RAW STATIC PRESSURE (FUSELAGE) (MB) PSF MB = (N/ 1000.0) - 0.0
31) 20 RAW STATIC PRESSURE (BOOM) (MB) PSB MB = (N/ 1000.0) - 0.0
32) 20 CORRECTED STATIC PRESR (FUSELAGE) (MB) PSFC MB = (N/ 1000.0) - 0.0
33) 20 CORRECTED STATIC PRESSURE (BOOM) (MB) PSBC MB = (N/ 1000.0) - 0.0
34) 20 NACA PRESSURE ALTITUDE (M) HP M = (N/ 10.0) - 500.0
35) 20 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
36) 20 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB C = (N/ 1000.0) - 100.0
37) 20 TOTAL TEMPERATURE (REVERSE FLOW) (C) TTRF C = (N/ 1000.0) - 100.0
38) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0
39) 20 TOTAL TEMPERATURE (FAST RESPONSE 2) (C) TTKP2 C = (N/ 1000.0) - 100.0
40) 20 AMBIENT TEMPERATURE (BOOM) (C) ATB C = (N/ 1000.0) - 100.0
41) 20 AMBIENT TEMPERATURE (REVERSE-FLOW) (C) ATRF C = (N/ 1000.0) - 100.0
42) 20 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
43) 20 AMBIENT TEMPERATURE (FAST RESPONSE 2)(C) ATKP2 C = (N/ 1000.0) - 100.0
44) 20 RADIOMETRIC SURFACE TEMP (PRT-5) (C) PRT5 C = (N/ 1000.0) - 100.0
45) 20 DEW/FROSTPOINT TEMP (THERMOELEC) (C) DP C = (N/ 1000.0) - 100.0
46) 20 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPC C = (N/ 1000.0) - 100.0
47) 20 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
48) 20 REFRACTIVE INDEX (N-UNITS) RFI N = (N/ 1000.0) - 100.0
49) 20 ABSOLUTE HUMIDITY (REFRACT) (G/M3) RHORF G/M3 = (N/ 1000.0) - 100.0
50) 20 AIRCRAFT TRUE AIRSPEED (WING) (M/S) TASW M/S = (N/ 1000.0) - 100.0
51) 20 AIRCRAFT TRUE AIRSPEED (GUST) (M/S) TASG M/S = (N/ 1000.0) - 100.0
52) 20 ATTACK ANGLE (FIXED VANE) (DEG) AFIX DEG = (N/ 1000.0) - 100.0
53) 20 ATTACK ANGLE (FIXED VANE 2) (DEG) AFIX2 DEG = (N/ 1000.0) - 100.0
54) 20 SIDESLIP ANGLE (FIXED VANE) (DEG) BFIX DEG = (N/ 1000.0) - 100.0
55) 20 SIDESLIP ANGLE (FIXED VANE 2) (DEG) BFIX2 DEG = (N/ 1000.0) - 100.0
56) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
57) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
58) 20 WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI M/S = (N/ 1000.0) - 100.0
59) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
60) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
61) 20 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 100.0
62) 20 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 100.0
63) 20 RAW INS GROUND SPD EAST COMP (M/S) VEW M/S = (N/ 1000.0) - 500.0
64) 20 RAW INS GROUND SPD NORTH COMP (M/S) VNS M/S = (N/ 1000.0) - 500.0
65) 20 DISTANCE EAST OF START (KM) DEI KM = (N/ 100.0) - 1000.0
66) 20 DISTANCE NORTH OF START (KM) DNI KM = (N/ 100.0) - 1000.0
67) 20 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
68) 20 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0
69) 20 PRESSURE-DAMPED INERTIAL ALTITUDE (M) HI3 M = (N/ 10.0) - 500.0
70) 20 RAW LYMAN ALPHA HYGROMETER OUTPUT (VDC) VLA VDC = (N/ 1000.0) - 100.0
71) 20 ABSOLUTE HUMIDITY (LYMANALPHA) (G/M3) RHOLA G/M3 = (N/ 1000.0) - 100.0
72) 20 FIXED ZERO VOLTAGE (VDC) FZV VDC = (N/ 1000.0) - 100.0
73) 20 FAST OZONE (25HZ) (VDC) O3F25 VDC = (N/ 1000.0) - 100.0
74) 20 FAST OZONE (25HZ) (PPBV) O3F25C PPBV = (N/ 1000.0) - 100.0
75) 20 JNO2 RADIOMETER (5HZ) (VDC) JNO2 VDC = (N/ 1000.0) - 100.0
76) 20 JNO2 RADIOMETER (5HZ) (S**-1) JNO2C S**-1 = (N/ 1000.0) - 100.0
77) 20 POTENTIAL TEMPERATURE (K) THETA K = (N/ 1000.0) - 100.0
78) 20 VIRTUAL POTENTIAL TEMPERATURE (K) VTHETA K = (N/ 1000.0) - 100.0
79) 20 PITCH MINUS ATTACK PHMATK DEG = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
437-01 DESTRUCTION 02JUN80
THIS FILE IS ALL OR PART OF THE TIME PERIOD 10 15 0 TO 14 27 36
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
1325 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
****** BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 26280 BITS PER LOGICAL DATA RECORD
1 LOGICAL DATA RECORDS PER PHYSICAL RECORD
26280 BITS PER PHYSICAL DATA RECORD
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