Sample LRT GENPRO-I header
803-03 MONEX 6DEC78 02/26/50 FIRST TIME ON THIS FILE 2 26 49 THIS FILE I
S ALL OR PART OF TIME PERIOD 2 26 50 TO 10 18 25 DESCRIPTION OF RECORD -- 88 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 148 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 10 CYCLES OF 148 SAMP/CYC = 1480 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 494 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 INS/KNOLLENBERG UPDATE FLAGS IKFLG = (N/ 1.0) - 0.0
5) 1 FIXED ZERO INPUT (A/D CHECK) (VDC) FZV VDC = (N/ 1000.0) - 100.0
6) 1 D/A OUTPUT (CALIBRATION CHECK) (VDC) D2AOUT VDC = (N/ 1000.0) - 100.0
7) 1 EVENT MARKER WORD (16 BITS) EVMRKS = (N/ 1.0) - 0.0
8) 1 16MM CAMERA FRAME COUNT CAMFC = (N/ 1.0) - 0.0
9) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 200.0
10) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
11) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
12) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
13) 1 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
14) 1 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
15) 1 RAW AIRCRAFT (INS) GROUND SPEED (M/S) GSF1 M/S = (N/ 1000.0) - 0.0
16) 1 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 100.0) - 5000.0
17) 1 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
18) 1 AIRCRAFT ROLL ATTITUDE ANGLE (HR) (DEG) ROLL DEG = (N/ 1000.0) - 100.0
19) 1 AIRCRAFT TRUE HEADING (YAW) (HR) (DEG) THF DEG = (N/ 1000.0) - 0.0
20) 1 RAW DYNAMIC PRESSURE (BOOM) (MB) QCB1 MB = (N/ 1000.0) - 100.0
21) 1 RAW DYNAMIC PRESSURE (WINGTIP) (MB) QCW1 MB = (N/ 1000.0) - 100.0
22) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB1 MB = (N/ 500.0) - 0.0
23) 1 RAW STATIC PRESSURE (WINGTIP) (MB) PSW1 MB = (N/ 500.0) - 0.0
24) 1 CORRECTED STATIC PRESSURE (MB) PSXC1 MB = (N/ 500.0) - 0.0
25) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 100.0) - 100.0
26) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
27) 1 CABIN PRESSURE (MB) PCAB MB = (N/ 500.0) - 0.0
28) 1 TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C) TTB1 C = (N/ 1000.0) - 100.0
29) 1 TOTAL TEMP (FUSELAGE ROSEMOUNT) (C) TTF1 C = (N/ 1000.0) - 100.0
30) 1 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATX1 C = (N/ 1000.0) - 100.0
31) 1 AIRCRAFT TRUE AIRSPEED (M/S) TASX1 M/S = (N/ 1000.0) - 100.0
32) 1 DEW/FROST POINT TEMP (L THERMOELEC) (C) DPL C = (N/ 1000.0) - 100.0
33) 1 DEW/FROST POINT TEMP (R THERMOELEC) (C) DPR C = (N/ 1000.0) - 100.0
34) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPXC C = (N/ 1000.0) - 100.0
35) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
36) 1 RAW LYMAN-ALPHA HYGROMETER OUTPUT (VDC) LAV VDC = (N/ 1000.0) - 100.0
37) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (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 DOWNWARD SW/WG-7 IRRADIANCE (WATTS/M2) TPYR1 W/M2 = (N/ 500.0) - 100.0
40) 1 DOWNWARD SW/OG-1 IRRADIANCE (WATTS/M2) TPYR2 W/M2 = (N/ 500.0) - 100.0
41) 1 DOWNWARD SW/RG-8 IRRADIANCE (WATTS/M2) TPYR3 W/M2 = (N/ 500.0) - 100.0
42) 1 RAW DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRG W/M2 = (N/ 1000.0) - 100.0
43) 1 UPPER PYRGEOMETER DOME TEMP (C) TPGDT C = (N/ 1000.0) - 100.0
44) 1 UPPER PYRGEOMETER SINK TEMP (C) TPGST C = (N/ 1000.0) - 100.0
45) 1 UPWARD SW/WG-7 IRRADIANCE (WATTS/M2) BPYR1 W/M2 = (N/ 500.0) - 100.0
46) 1 UPWARD SW/OG-1 IRRADIANCE (WATTS/M2) BPYR2 W/M2 = (N/ 500.0) - 100.0
47) 1 UPWARD SW/RG-8 IRRADIANCE (WATTS/M2) BPYR3 W/M2 = (N/ 500.0) - 100.0
48) 1 RAW UPWARD IR IRRADIANCE (WATTS/M2) BPYRG W/M2 = (N/ 1000.0) - 100.0
49) 1 LOWER PYRGEOMETER DOME TEMP (C) BPGDT C = (N/ 1000.0) - 100.0
50) 1 LOWER PYRGEOMETER SINK TEMP (C) BPGST C = (N/ 500.0) - 100.0
51) 1 CORCTD DOWNWARD IR IRRADIANCE (WATTS/M2) TPYRGC W/M2 = (N/ 500.0) - 100.0
52) 1 CORCTD UPWARD IR IRRADIANCE (WATTS/M2) BPYRGC W/M2 = (N/ 500.0) - 100.0
53) 1 BOTTOM PRT-5 IRTRAN WINDOW TEMP (C) BP5WT C = (N/ 1000.0) - 100.0
54) 1 BTM RAW RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5 C = (N/ 1000.0) - 100.0
55) 1 CORRCTD RADIOMTRC (SFC) TEMP (PRT-5) (C) BPRT5C C = (N/ 1000.0) - 100.0
56) 1 TOP PRT-5 IRTRAN WINDOW TEMPERATURE (C) TP5WT C = (N/ 1000.0) - 100.0
57) 1 TOP RAW RADIOMTRC (SKY) TEMP (PRT-5) (C) TPRT5 C = (N/ 1000.0) - 100.0
58) 1 CORRCTD RADIOMTRC (SKY) TEMP (PRT-5) (C) TPRT5C C = (N/ 1000.0) - 100.0
59) 1 AIRCRAFT C.G. VERT ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
60) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 0.0
61) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 0.0
62) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0
63) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0
64) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0
65) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0
66) 1 AIRCRAFT GROUND SPD EAST COMP (M/S) VEW1 M/S = (N/ 1000.0) - 500.0
67) 1 AIRCRAFT GROUND SPD NORTH COMP (M/S) VNS1 M/S = (N/ 1000.0) - 500.0
68) 1 DISTANCE EAST OF START (KM) DEI KM = (N/ 100.0) - 5000.0
69) 1 DISTANCE NORTH OF START (KM) DNI KM = (N/ 100.0) - 5000.0
70) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP31 M/S = (N/ 1000.0) - 100.0
71) 1 PRESSURE DAMPED INERTIAL ALTITUDE (M) HI31 M = (N/ 10.0) - 500.0
72) 1 TOP UV RADIOMETER (290-315NM) (VDC) TUVR3 VDC = (N/ 1000.0) - 100.0
73) 1 TOP UV RADIOMETER (290-380NM) (VDC) TUVR4 VDC = (N/ 1000.0) - 100.0
74) 1 BOTTOM UV RADIOMETER (290-315NM) (VDC) BUVR3 VDC = (N/ 1000.0) - 100.0
75) 1 BOTTOM UV RADIOMETER (290-380NM) (VDC) BUVR4 VDC = (N/ 1000.0) - 100.0
76) 1 ACTINOMETER PRESSURE (VDC) PACTN VDC = (N/ 1000.0) - 100.0
77) 1 NCAR DASIBI OZONE OUTPUT (DELANY) (VDC) NDO3 VDC = (N/ 1000.0) - 100.0
78) 1 NOX PRESSURE (DELANY) (VDC) PRNOX VDC = (N/ 1000.0) - 100.0
79) 1 NOX OUTPUT (DICKERSON) (VDC) NOXDN VDC = (N/ 1000.0) - 100.0
80) 1 NCAR CSI ETHYLENE OZONE OUTPUT (VDC) NEO3 VDC = (N/ 1000.0) - 100.0
81) 1 FIXED ANGLE NEPHELOMETER OUTPUT (VDC) FANEPH VDC = (N/ 1000.0) - 100.0
82) 1 NOX FLOW SIGNAL (DELANY) (VDC) FLNOX VDC = (N/ 1000.0) - 100.0
83) 1 HOT WIRE OUTPUT (LA RUE) (VDC) HWOLR VDC = (N/ 1000.0) - 100.0
84) 1 NOX OUTPUT (DELANY) (COUNTS) NOXDY COUNTS = (N/ 1.0) - 0.0
85) 16 P M S OAP-200X ACCUMS. (ID + 15 CELLS) OAP200X ACCUM = (N/ 1.0) - 0.0
86) 16 P M S OAP-200Y ACCUMS. (ID + 15 CELLS) OAP200Y ACCUM = (N/ 1.0) - 0.0
87) 16 P M S ASAS ACCUMULATIONS (ID + 15 CELLS) ASAS ACCUM = (N/ 1.0) - 0.0
88) 16 P M S FSSP ACCUMULATIONS (ID + 15 CELLS) FSSP ACCUM = (N/ 1.0) - 0.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
803-03 MONEX 6DEC78 02/26/50
THIS FILE IS ALL OR PART OF THE TIME PERIOD 2 26 50 TO 10 18 25
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
159 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
132288 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 2960 BITS PER LOGICAL DATA RECORD
10 LOGICAL DATA RECORDS PER PHYSICAL RECORD
29600 BITS PER PHYSICAL DATA RECORD
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