Sample HRT GENPRO-I header
803-12 24JUN79 SUMMER MONEX DRT FIRST TIME ON THIS FILE 3 49 31 THIS FILE I
S ALL OR PART OF TIME PERIOD 3 49 31 TO 10 50 30 DESCRIPTION OF RECORD -- 101 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 644 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 2 CYCLES OF 644 SAMP/CYC = 1288 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 430 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 TEMPERATURE (ROSEMOUNT) (C) ATX1 C = (N/ 1000.0) - 100.0
5) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPXC C = (N/ 1000.0) - 100.0
6) 1 DEWPOINT TEMPERATURE (LYMAN-ALPHA) (C) DPLAC1 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 (DEG) WDRCTN DEG = (N/ 1000.0) - 0.0
9) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 0.0
10) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0
11) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0
12) 1 WIND VECTOR VERT GUST COMPONENT (M/S) WI1 M/S = (N/ 1000.0) - 100.0
13) 1 WIND VECTOR LONGITUDINAL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0
14) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0
15) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
16) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
17) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 100.0) - 100.0
18) 1 PRESSURE DAMPED INERTIAL ALTITUDE (M) HI31 M = (N/ 100.0) - 100.0
19) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
20) 1 RAW AIRCRAFT (INS) GROUND SPEED (M/S) GSF1 M/S = (N/ 1000.0) - 0.0
21) 1 AIRCRAFT GROUND SPD EAST COMP (M/S) VEW1 M/S = (N/ 1000.0) - 500.0
22) 1 AIRCRAFT GROUND SPD NORTH COMP (M/S) VNS1 M/S = (N/ 1000.0) - 500.0
23) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP31 M/S = (N/ 1000.0) - 100.0
24) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF1 DEG = (N/ 1000.0) - 0.0
25) 1 AIRCRFT PITCH1 ATTITUDE ANGLE (HR) (DEG) PITCH1 DEG = (N/ 1000.0) - 100.0
26) 1 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL1 DEG = (N/ 1000.0) - 100.0
27) 1 AIRCRAFT TRUE AIRSPEED (M/S) TASX1 M/S = (N/ 1000.0) - 100.0
28) 1 CORRCTD RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5C C = (N/ 1000.0) - 100.0
29) 1 CORRCTD RADIOMTRC (SKY) TEMP (PRT-6) (C) TPRT6C C = (N/ 1000.0) - 100.0
30) 1 DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2) TPYR1 W/M2 = (N/ 500.0) - 100.0
31) 1 DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2) TPYR2 W/M2 = (N/ 500.0) - 100.0
32) 1 DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2) TPYR3 W/M2 = (N/ 500.0) - 100.0
33) 1 UPWARD SW/WG-7 IRRADIANCE (WATTS/M2) BPYR1 W/M2 = (N/ 500.0) - 100.0
34) 1 UPWARD SW/OG-1 IRRADIANCE (WATTS/M2) BPYR2 W/M2 = (N/ 500.0) - 100.0
35) 1 UPWARD SW/RG-8 IRRADIANCE (WATTS/M2) BPYR3 W/M2 = (N/ 500.0) - 100.0
36) 1 CORCTD UPWARD IR IRRADIANCE (WATTS/M2) TPYRGC W/M2 = (N/ 1000.0) - 100.0
37) 1 CORCTD DOWNWARD IR IRRADIANCE (WATTS/M2) BPYRGC W/M2 = (N/ 1000.0) - 100.0
38) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0
39) 1 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB1 C = (N/ 1000.0) - 100.0
40) 1 TOTAL TEMP (FUSELAGE ROSEMOUNT) (C)1/SEC TTF1 C = (N/ 1000.0) - 100.0
41) 1 DEW/FROST POINT TEMP (L THERMOELEC) (C) DPL C = (N/ 1000.0) - 100.0
42) 1 DEW/FROST POINT TEMP (R THERMOELEC) (C) DPR C = (N/ 1000.0) - 100.0
43) 1 RAW STATIC PRESSURE (WINGTIP) (MB) PSW1 MB = (N/ 500.0) - 0.0
44) 1 RAW DYNAMIC PRESSURE (WINGTIP) (MB) QCW1 MB = (N/ 1000.0) - 100.0
45) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB1 MB = (N/ 500.0) - 0.0
46) 1 RAW DYNAMIC PRESSURE (BOOM) (MB) QCB1 MB = (N/ 1000.0) - 100.0
47) 1 DISTANCE EAST OF START (KM) DEI KM = (N/ 100.0) - 5000.0
48) 1 DISTANCE NORTH OF START (KM) DNI KM = (N/ 100.0) - 5000.0
49) 1 LTN-51 ARINC TIME LAG (SEC) TMLAG SEC = (N/ 1000.0) - 100.0
50) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
51) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
52) 1 RAW DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRG W/M2 = (N/ 100.0) - 1000.0
53) 1 RAW UPWARD IR IRRADIANCE (WATTS/M2) BPYRG W/M2 = (N/ 100.0) - 1000.0
54) 1 TOP PYRGEOMETER DOME TEMPERATURE (C) TPGDT C = (N/ 1000.0) - 100.0
55) 1 TOP PYRGEOMETER SINK TEMPERATURE (C) TPGST C = (N/ 1000.0) - 100.0
56) 1 BOTTOM PYRGEOMETER DOME TEMPERATURE (C) BPGDT C = (N/ 1000.0) - 100.0
57) 1 BOTTOM PYRGEOMETER SINK TEMPERATURE (C) BPGST C = (N/ 1000.0) - 100.0
58) 1 PRT-5 IRTRAN WINDOW TEMPERATURE (C) BP5WT C = (N/ 1000.0) - 100.0
59) 1 RAW RADIOMETRIC (SFC) TEMP (PRT-5) (C) BPRT5 C = (N/ 1000.0) - 100.0
60) 1 TOP PRT-6 IRTRAN WINDOW TEMPERATURE (C) TP6WT C = (N/ 1000.0) - 100.0
61) 1 RAW RADIOMETRIC (SKY) TEMP (PRT-6) (C) TPRT6 C = (N/ 1000.0) - 100.0
62) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0
63) 1 16MM CAMERA FRAME COUNT CAMFC = (N/ 1.0) - 0.0
64) 1 EVENT MARKER WORD (16 BITS) EVMRKS = (N/ 1.0) - 0.0
65) 1 INS/KNOLLENBERG UPDATE FLAGS IKFLG = (N/ 1.0) - 0.0
66) 20 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
67) 20 AMBIENT TEMP (COMPNSTD BOOM ROSMNT) (C) ATBC C = (N/ 1000.0) - 100.0
68) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
69) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
70) 20 WIND VECTOR VERT GUST COMPONENT(HR)(M/S) WI M/S = (N/ 1000.0) - 100.0
71) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
72) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
73) 20 ABSOLUTE HUMIDITY (LYMN-ALPHA HR) (G/M3) RHOLA G/M3 = (N/ 1000.0) - 100.0
74) 20 RAW LYMAN-ALPHA HYGROMETER OUTPUT (VDC) LAV VDC = (N/ 1000.0) - 100.0
75) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) R TTKPR C = (N/ 1000.0) - 100.0
76) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) L TTKPL C = (N/ 1000.0) - 100.0
77) 20 TOTAL TEMP (COMPENSATED BOOM ROSMNT) (C) TTBC C = (N/ 1000.0) - 100.0
78) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
79) 20 ATTACK ANGLE (FIXED VANE,LEFT) (DEG) AFIX1 DEG = (N/ 1000.0) - 100.0
80) 20 ATTACK ANGLE (FIXED VANE,RIGHT) (DEG) AFIX2 DEG = (N/ 1000.0) - 100.0
81) 20 SIDESLIP ANGLE (FIXED TOP VANE) (DEG) BFIX1 DEG = (N/ 1000.0) - 100.0
82) 20 SIDESLIP ANGLE (FIXED VANE,BOTTOM) (DEG) BFIX2 DEG = (N/ 1000.0) - 100.0
83) 20 AIRCRAFT C.G. VERT ACCEL. (HR) (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
84) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
85) 20 AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG) ROLL DEG = (N/ 1000.0) - 100.0
86) 20 AIRCRAFT PITCH ATTITUDE ANGLE (HR) (DEG) PITCH DEG = (N/ 1000.0) - 100.0
87) 20 AIRCRAFT TRUE HEADING (YAW) (HR) (DEG) THF DEG = (N/ 1000.0) - 100.0
88) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
89) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
90) 20 GEOMETRIC (RADAR) ALTITUDE (APN-159) (M) HGME M = (N/ 100.0) - 100.0
91) 16 P M S OAP-200X ACCUMS. (ID + 15 CELLS) OAP200X ACCUM = (N/ 1.0) - 0.0
92) 16 P M S OAP-200Y ACCUMS. (ID + 15 CELLS) OAP200Y ACCUM = (N/ 1.0) - 0.0
93) 16 P M S ASAS ACCUMULATIONS (ID + 15 CELLS) ASAS ACCUM = (N/ 1000.0) - 100.0
94) 16 P M S FSSP ACCUMULATIONS (ID + 15 CELLS) FSSP ACCUM = (N/ 1.0) - 0.0
95) 5 PRT6 MULTIPLEXED TEMP VOLTAGE (VDC) P6MUX1 VDC = (N/ 1000.0) - 100.0
96) 5 PRT6 MULTIPLEXED POSITION VOLTAGE (VDC) P6MUX2 VDC = (N/ 1000.0) - 100.0
97) 1 PRT-6 RADIOMETER OUTPUT VOLTAGE (VDC) P6RADV VDC = (N/ 1000.0) - 100.0
98) 1 PRT-6 RADIOMETER TEMPERATURE (C) P6RADC C = (N/ 1000.0) - 100.0
99) 1 PRT-6 OVEN TEMP DEVIATION (C) P6OVNT C = (N/ 1000.0) - 100.0
100) 1 CCN OUTPUT (SAXENA) (VCD) CCNO VDC = (N/ 1000.0) - 100.0
101) 1 INTEGRATING NEPHELOMETER OUTPUT (VDC) NEPH VDC = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
1 803-12 24JUN79 SUMMER MONEX DRT
THIS FILE IS ALL OR PART OF THE TIME PERIOD 3 49 31 TO 10 50 30
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
655 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
544960 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 12880 BITS PER LOGICAL DATA RECORD
2 LOGICAL DATA RECORDS PER PHYSICAL RECORD
25760 BITS PER PHYSICAL DATA RECORD
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