Sample HRT GENPRO-I header
886-01 ARCTIC STRATUS 13JUN80 18 19 20 FIRST TIME ON THIS FILE 18 19 25 THIS FILE I
S ALL OR PART OF TIME PERIOD 18 19 20 TO 24 25 30 DESCRIPTION OF RECORD -- 113 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 615 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 2 CYCLES OF 615 SAMP/CYC = 1230 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 410 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(BOOM)(LR)(MB) PSBC1 MB = (N/ 500.0) - 0.0
4) 1 AMBIENT TEMPERATURE (BOOM)(LR) (C) ATB1 C = (N/ 1000.0) - 100.0
5) 1 DEWPOINT TEMPERATURE (THERM.)(TOP) (C) DPRTC C = (N/ 1000.0) - 100.0
6) 1 DEWPOINT TEMPERATURE (THERM.)(BOT.)(C) DPRBC C = (N/ 1000.0) - 100.0
7) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
8) 1 HORIZONTAL WIND DIRECTION (LR)(DEG) WDRCTN1 DEG = (N/ 1000.0) - 0.0
9) 1 HORIZONTAL WIND SPEED (LR)(M/S) WSPD1 M/S = (N/ 1000.0) - 0.0
10) 1 WIND VECTOR EAST COMPONENT (LR)(M/S) UI1 M/S = (N/ 1000.0) - 200.0
11) 1 WIND VECTOR NORTH COMPONENT(LR) (M/S) VI1 M/S = (N/ 1000.0) - 200.0
12) 1 WIND VECTOR VERTICAL GUST COMP(LR)(M/S) WI1 M/S = (N/ 1000.0) - 100.0
13) 1 WIND VECTOR LNGTDNL COMP.(LR)(M/S) UX1 M/S = (N/ 1000.0) - 200.0
14) 1 WIND VECTOR LATERAL COMP.(LR)1(M/S) VY1 M/S = (N/ 1000.0) - 200.0
15) 1 NACA PRESSURE ALTITUDE (LR) (M) HP1 M = (N/ 10.0) - 500.0
16) 1 PRESSURE-DAMPED INERTIAL ALTITUDE(LR)(M) HI31 M = (N/ 10.0) - 500.0
17) 1 COARSE ALTITUDE SYNCHRO (DEG) CHGME DEG = (N/ 1000.0) - 100.0
18) 1 FINE ALTITUDE SYNCHRO (DEG) HGME DEG = (N/ 1000.0) - 100.0
19) 1 ALTITUDE (M) (APN-159) ALT M = (N/ 10.0) - 500.0
20) 1 RAW INS GROUND SPD EAST COMP.(LR)(M/S) VEW1 M = (N/ 1000.0) - 500.0
21) 1 RAW INS GROUND SPD NORTH COMP.(LR)(M/S) VNS1 M = (N/ 1000.0) - 500.0
22) 1 DAMPED AIRCRAFT VERT VELOCITY(LR)(M/S) WP31 M/S = (N/ 1000.0) - 100.0
23) 1 AIRCRAFT C.G. ACCELERATION (LR)(M/S2) CGAC1 M/S2 = (N/ 1000.0) - 100.0
24) 1 AIRCRAFT TRUE HEADING (YAW)(LR) (DEG) THF1 DEG = (N/ 1000.0) - 0.0
25) 1 AIRCRAFT ROLL ATTITUDE ANGLE(LR) (DEG) ROLL1 DEG = (N/ 1000.0) - 100.0
26) 1 AIRCRAFT PITCH ATTITUDE ANGLE(LR)(DEG) PITCH1 DEG = (N/ 1000.0) - 100.0
27) 1 AIRCRAFT TRUE AIRSPEED (WING) (M/S) TASW1 M/S = (N/ 1000.0) - 100.0
28) 1 RAW RADIOMETRIC SURFACE TEMP (PRT-5) (C) PRT-5 C = (N/ 1000.0) - 100.0
29) 1 RAW BOTTOM PYRANOMETER OUTPUT (WG-7) (WA BPYR1 WATTS/M2 = (N/ 500.0) - 100.0
30) 1 RAW BOTTOM PYRANOMETER OUTPUT (OG-1) (WA BPYR2 WATTS/M2 = (N/ 500.0) - 100.0
31) 1 RAW BOTTOM PYRANOMETER OUTPUT (RG-8) (WA BPYR3 WATTS/M2 = (N/ 500.0) - 100.0
32) 1 RAW TOP PYRANOMETER OUTPUT (WG-7) (WAT TPYR1 WATTS/M2 = (N/ 500.0) - 100.0
33) 1 RAW TOP PYRANOMETER OUTPUT (RG-8) (WAT TPYR2 WATTS/M2 = (N/ 500.0) - 100.0
34) 1 RAW TOP PYRANOMETER OUTPUT (RG-8) (WAT TPYR3 WATTS/M2 = (N/ 500.0) - 100.0
35) 1 CORRECTED BOTTOM PYRGEOMETER OUTPUT (WAT BPYRGC WATTS/M2 = (N/ 1000.0) - 100.0
36) 1 CORRECTED TOP PYRGEOMETER OUTPUT (WATT TPYRGC WATTS/M2 = (N/ 1000.0) - 100.0
37) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0
38) 1 TOTAL TEMPERATURE(BOOM ROSMT)(LR)(C) TTB1 C = (N/ 1000.0) - 100.0
39) 1 DEW/FROSTPOINT TEMP (TOP) (C) DPRT C = (N/ 1000.0) - 100.0
40) 1 DEW/FROSTPOINT TEMP (BOT.) (C) DPRB C = (N/ 1000.0) - 100.0
41) 1 RAW DYNAMIC PRESSURE (WING)(LR)(MB) PSW1 MB = (N/ 500.0) - 0.0
42) 1 RAW DYNAMIC PRESSURE(WING)(LR)(MB) QCW1 MB = (N/ 1000.0) - 100.0
43) 1 RAW STATIC PRESSURE (BOOM)(LR) (MB) PSB1 MB = (N/ 500.0) - 0.0
44) 1 RAW DYNAMIC PRESSURE (LR) (BOOM) (MB) QCB1 MB = (N/ 1000.0) - 100.0
45) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
46) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
47) 1 INS WANDER ANGLE (DEG) (LR) ALPHA1 DEG = (N/ 1000.0) - 100.0
48) 1 AIRCRAFT TRUE HEADING (LR)(ARINC)(DEG) THI1 DEG = (N/ 1000.0) - 100.0
49) 1 RAW BOTTOM PYRGEOMETER OUTPUT (WATTS/M2) BPYRG WATTS/M2 = (N/ 100.0) - 1000.0
50) 1 RAW TOP PYRGEOMETER OUTPUT (WATTS/M2) TPYRG WATTS/M2 = (N/ 100.0) - 1000.0
51) 1 BOTTOM PYRGEOMETER DOME TEMPERATURE (C) BPGDT C = (N/ 1000.0) - 100.0
52) 1 BOTTOM PYRGEOMETER SINK TEMPERATURE (C) BPGST C = (N/ 1000.0) - 100.0
53) 1 TOP PYRGEOMETER DOME TEMPERATURE (C) TPGDT C = (N/ 1000.0) - 100.0
54) 1 TOP PYRGEOMETER SINK TEMPERATURE (C) TPGST C = (N/ 1000.0) - 100.0
55) 1 PRT-6 OVEN TEMP DEVIATION (VDC) P6OVNT VDC = (N/ 1000.0) - 100.0
56) 1 FMP MARK 1 VOLTAGE (VDC) MK1T VDC = (N/ 1000.0) - 100.0
57) 1 PRT-6 ROTATING MIRROR TEMP (VDC) P6RMT VDC = (N/ 1000.0) - 100.0
58) 1 PRT-6 FIXED MIRROR TEMP (VDC) P6FMT VDC = (N/ 1000.0) - 100.0
59) 1 PRT-6 CALIBRATION PLATE TEMP(VDC) P6CPT VDC = (N/ 1000.0) - 100.0
60) 1 FMP MARK 2 VOLTAGE MK2T VDC = (N/ 1000.0) - 100.0
61) 1 FMT MARK 1 VOLTAGE (VDC) MK1 VDC = (N/ 1000.0) - 100.0
62) 1 PRT-6 FILTER POSITION P6FP VDC = (N/ 1000.0) - 100.0
63) 1 PRT-6 MIRROR POSITION (VDC) P6MP VDC = (N/ 1000.0) - 100.0
64) 1 PRT-6 MODE INDICATOR P6MV VDC = (N/ 1000.0) - 100.0
65) 1 FMT MARK 2 VOLTAGE MK2 VDC = (N/ 1000.0) - 100.0
66) 1 PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC) P6RADV VDC = (N/ 1000.0) - 100.0
67) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0
68) 5 PRT-6 OVEN TEMP DEVIATION (VDC) P6OVNT VDC = (N/ 1000.0) - 100.0
69) 5 PRT-6 ALL MUX. TEMPERATURE (VDC) MUXTEMP VDC = (N/ 1000.0) - 100.0
70) 5 PRT-6 ALL MUX. POSITION (VDC) MUXPOS VDC = (N/ 1000.0) - 100.0
71) 5 PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC) P6RADV VDC = (N/ 1000.0) - 100.0
72) 20 AMBIENT TEMP. (COMP. BOOM) (C) ATBC C = (N/ 1000.0) - 100.0
73) 20 AMBIENT TEMPERATURE(FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
74) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
75) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
76) 20 WIND VECTOR VERTICAL GUST COMP. (M/S) WI M/S = (N/ 1000.0) - 100.0
77) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
78) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
79) 20 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0
80) 20 FIXED PATH LYMAN-ALPHA (VDC) VLAFP VDC = (N/ 1000.0) - 100.0
81) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0
82) 20 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB C = (N/ 1000.0) - 100.0
83) 20 TOTAL TEMP. (COMP. BOOM ROSEMOUNT) (C) TTBC C = (N/ 1000.0) - 100.0
84) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
85) 20 ATTACK ANGLE (FIXED VANE 1) (DEG) AFIX DEG = (N/ 1000.0) - 100.0
86) 20 SIDE SLIP ANGLE (FIXED VANE 1) (DEG) BFIX DEG = (N/ 1000.0) - 100.0
87) 20 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
88) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
89) 20 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0
90) 20 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
91) 20 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
92) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
93) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
94) 20 AIRCRAFT GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0
95) 20 AIRCRAFT TRUE AIRSPEED (GUST PROBE)(M/S) TASGB M/S = (N/ 1000.0) - 100.0
96) 16 PMS PROBE 1 FSSP (ID AND ACC.) PMSPB1 FSSP = (N/ 1.0) - 0.0
97) 16 PMS PROBE 2 200X (ID AND ACC.) PMSPB2 200X = (N/ 1.0) - 0.0
98) 1 EVENT MARKER WORD EVMRKS = (N/ 1000.0) - 100.0
99) 1 HRMN 01 (VDC) HRMN1 VDC = (N/ 1000.0) - 100.0
100) 1 HRMN 02 (VDC) HRMN2 VDC = (N/ 1000.0) - 100.0
101) 1 HRMN 03 (VDC) HRMN3 VDC = (N/ 1000.0) - 100.0
102) 1 HRMN 04 (VDC) HRMN4 VDC = (N/ 1000.0) - 100.0
103) 1 HRMN 05 (VDC) HRMN5 VDC = (N/ 1000.0) - 100.0
104) 1 HRMN 06 (VDC) HRMN6 VDC = (N/ 1000.0) - 100.0
105) 1 HRMN 07 (VDC) HRMN7 VDC = (N/ 1000.0) - 100.0
106) 1 HRMN 08 (VDC) HRMN8 VDC = (N/ 1000.0) - 100.0
107) 1 HRMN 09 (VDC) HRMN9 VDC = (N/ 1000.0) - 100.0
108) 1 HRMN 10 (VDC) HRMN10 VDC = (N/ 1000.0) - 100.0
109) 1 HRMN 11 (VDC) HRMN11 VDC = (N/ 1000.0) - 100.0
110) 1 HRMN 12 (VDC) HRMN12 VDC = (N/ 1000.0) - 100.0
111) 1 HRMN 13 (VDC) HRMN13 VDC = (N/ 1000.0) - 100.0
112) 1 HRMN 14 (VDC) HRMN14 VDC = (N/ 1000.0) - 100.0
113) 1 HRMN 15 (VDC) HRMN15 VDC = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
886-01 ARCTIC STRATUS 13JUN80 18 19 20
THIS FILE IS ALL OR PART OF THE TIME PERIOD 18 19 20 TO 24 25 30
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
626 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
520832 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 12300 BITS PER LOGICAL DATA RECORD
2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
24600 BITS PER PHYSICAL DATA RECORD
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