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
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