Sample HRT GENPRO-I header
572-02 ELECTRA MONEX-77 11JUN77 03/28/50 FIRST TIME ON THIS FILE 8 29 36 THIS FILE I
S ALL OR PART OF TIME PERIOD 3 28 50 TO 10 40 0 DESCRIPTION OF RECORD -- 110 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 743 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 2 CYCLES OF 743 SAMP/CYC = 1486 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 496 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) PSWC1 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 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
8) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
9) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
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 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
18) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
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 CORCTD DOWNWARD IR IRRADIANCE (WATTS/M2) UPYRGC W/M2 = (N/ 1000.0) - 100.0
39) 1 CORCTD UPWARD IR IRRADIANCE (WATTS/M2) LPYRGC W/M2 = (N/ 1000.0) - 100.0
40) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
41) 1 PRT-6 FILTER POSITION P6FP = (N/ 1.0) - 0.0
42) 1 PRT-6 MIRROR POSITION P6MP = (N/ 1000.0) - 100.0
43) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
44) 1 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB1 DEG = (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 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
55) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
56) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
57) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
58) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 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 RAW DOWNWARD IR IRRADIANCE (WATTS/M2) UPYRG W/M2 = (N/ 100.0) - 1000.0
62) 1 RAW UPWARD IR IRRADIANCE (WATTS/M2) LPYRG W/M2 = (N/ 100.0) - 1000.0
63) 1 UPPER PYRGEOMETER DOME TEMPERATURE (C) UPYRWT C = (N/ 1000.0) - 100.0
64) 1 UPPER PYRGEOMETER SINK TEMPERATURE (C) UPYRST C = (N/ 1000.0) - 100.0
65) 1 LOWER PYRGEOMETER DOME TEMPERATURE (C) LPYRWT C = (N/ 1000.0) - 100.0
66) 1 LOWER PYRGEOMETER SINK TEMPERATURE (C) LPYRST C = (N/ 1000.0) - 100.0
67) 1 PRT-5 IRTRAN WINDOW TEMPERATURE (C) PRT5WT C = (N/ 1000.0) - 100.0
68) 1 RAW RADIOMETRIC SURFACE TEMP (PRT-5) (C) PRT5 C = (N/ 1000.0) - 100.0
69) 1 PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC) P6RADV VDC = (N/ 1000.0) - 100.0
70) 1 PRT-6 OVEN TEMP DEVIATION (C) P6OVNT C = (N/ 1000.0) - 100.0
71) 1 PRT-6 ROTATING MIRROR TEMP (C) P6RMT C = (N/ 1000.0) - 100.0
72) 1 PRT-6 FIXED MIRROR TEMP (C) P6FMT C = (N/ 1000.0) - 100.0
73) 1 PRT-6 CALIBRATION PLATE TEMP (C) P6CPT C = (N/ 1000.0) - 100.0
74) 1 PRT-6 MODE INDICATOR P6MV = (N/ 1.0) - 0.0
75) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
76) 1 16MM CAMERA FRAME COUNT CAMFC = (N/ 1.0) - 0.0
77) 1 EVENT MARKER WORD (16 BITS) EVMRKS = (N/ 1.0) - 0.0
78) 1 INS/KNOLLENBERG UPDATE FLAGS UPDATE = (N/ 1.0) - 0.0
79) 1 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
80) 20 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
81) 20 AMBIENT TEMP (COMPNSTD BOOM ROSMNT) (C) ATBC C = (N/ 1000.0) - 100.0
82) 20 TOTAL TEMP (COMPENSATED BOOM ROSMNT) (C) TTBC C = (N/ 1000.0) - 100.0
83) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
84) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
85) 20 WIND VECTOR VERT GUST COMPONENT(HR)(M/S) WI M/S = (N/ 1000.0) - 100.0
86) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
87) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
88) 20 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
89) 20 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
90) 20 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
91) 20 *** UNUSED *** UNUSED = (N/ 1.0) - 0.0
92) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0
93) 20 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB C = (N/ 1000.0) - 100.0
94) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
95) 20 ATTACK ANGLE (ROTATING VANE) (DEG) AROT DEG = (N/ 1000.0) - 100.0
96) 20 ATTACK ANGLE (FIXED VANE) (DEG) AFIX DEG = (N/ 1000.0) - 100.0
97) 20 SIDESLIP ANGLE (ROTATING VANE) (DEG) BROT DEG = (N/ 1000.0) - 100.0
98) 20 SIDESLIP ANGLE (FIXED VANE) (DEG) BFIX DEG = (N/ 1000.0) - 100.0
99) 20 GUST PROBE TIP VERT ACCELERATION (M/S2) VAC M/S2 = (N/ 1000.0) - 100.0
100) 20 GUST PROBE TIP LATERAL ACCEL. (M/S2) LAC M/S2 = (N/ 1000.0) - 100.0
101) 20 AIRCRAFT C.G. VERT ACCEL. (HR) (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
102) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
103) 20 AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG) ROLL DEG = (N/ 1000.0) - 100.0
104) 20 AIRCRAFT PITCH ATTITUDE ANGLE (HR) (DEG) PITCH DEG = (N/ 1000.0) - 100.0
105) 20 AIRCRAFT TRUE HEADING (YAW) (HR) (DEG) THF DEG = (N/ 1000.0) - 100.0
106) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
107) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
108) 20 LEFT WING STRAIN (HR) (MICRO-IN/IN) STRLW UIN/IN = (N/ 500.0) - 1000.0
109) 20 RIGHT WING STRAIN (HR) (MICRO-IN/IN) STRRW UIN/IN = (N/ 500.0) - 1000.0
110) 64 KNOLLENBERG 64 WORDS KNLBG COUNTS = (N/ 1.0) - 0.0
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