Sample HRT GENPRO-I header
656-01 BAO SITE STUDY 17APR78 16/17/00 FIRST TIME ON THIS FILE 16 17 0 THIS FILE I
S ALL OR PART OF TIME PERIOD 16 17 0 TO 18 5 0 DESCRIPTION OF RECORD -- 76 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 1425 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 1 CYCLES OF1425 SAMP/CYC = 1425 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 475 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 ISIXP (VDC) SIXP VDC = (N/ 1000.0) - 100.0
4) 1 ISIXN (VDC) SIXN VDC = (N/ 1000.0) - 100.0
5) 1 PILOT MICROPHONE SWITCH (TRMT) (VDC) TRMT VDC = (N/ 1000.0) - 100.0
6) 20 CORRECTED STATIC PRESR (FUSELAGE) (MB) PSFC MB = (N/ 1000.0) - 0.0
7) 20 CORRECTED STATIC PRESSURE (BOOM) (MB) PSBC MB = (N/ 1000.0) - 0.0
8) 20 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATW C = (N/ 1000.0) - 100.0
9) 20 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0
10) 20 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPC C = (N/ 1000.0) - 100.0
11) 20 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0
12) 20 REFRACTIVE INDEX (N-UNITS) RFI N = (N/ 1000.0) - 100.0
13) 20 ABSOLUTE HUMIDITY (REFRACT) (G/M3) RHORF G/M3 = (N/ 1000.0) - 100.0
14) 20 RADIOMETRIC SURFACE TEMP (PRT-5) (C) PRT5 C = (N/ 1000.0) - 100.0
15) 20 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 100.0
16) 20 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 100.0
17) 20 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0
18) 20 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0
19) 20 WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI M/S = (N/ 1000.0) - 100.0
20) 20 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0
21) 20 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0
22) 20 RAW INS LATITUDE (DEG) ALAT1 DEG = (N/ 1000.0) - 100.0
23) 20 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0
24) 20 DME STATION STATN = (N/ 1000.0) - 100.0
25) 20 DME DISTANCE ( NMI ) DIST NMI = (N/ 1000.0) - 100.0
26) 20 AIRCRAFT LATITUDE (DME) (DEG) DMELAT DEG = (N/ 1000.0) - 100.0
27) 20 AIRCRAFT LONGITUDE (DME) (DEG) DMELON DEG = (N/ 1000.0) - 200.0
28) 20 DME LATITUDE - INS LATITUDE IN DEGS DIFLAT DEG = (N/ 1000.0) - 100.0
29) 20 DME LONGITUDE - INS LONGITUDE IN DEGS DIFLON DEG = (N/ 1000.0) - 100.0
30) 20 DME TRACK - INS TRACK IN METERS DIFTRK M = (N/ 100.0) - 0.0
31) 20 COMBINED DME AND INS LATITUDE (DEG) CDILAT DEG = (N/ 1000.0) - 100.0
32) 20 COMBINED DME AND INS LONGITUDE (DEG) CDILON DEG = (N/ 1000.0) - 200.0
33) 20 NACA PRESSURE ALTITUDE (M) HP M = (N/ 10.0) - 500.0
34) 20 PRESSURE-DAMPED INERTIAL ALTITUDE (M) HI3 M = (N/ 10.0) - 500.0
35) 20 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0
36) 20 RAW INS GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0
37) 20 RAW INS GROUND SPD EAST COMP (M/S) VEW M/S = (N/ 1000.0) - 500.0
38) 20 RAW INS GROUND SPD NORTH COMP (M/S) VNS M/S = (N/ 1000.0) - 500.0
39) 20 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0
40) 20 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0
41) 20 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
42) 20 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0
43) 20 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0
44) 20 AIRCRAFT TRUE AIRSPEED (WING) (M/S) TASW M/S = (N/ 1000.0) - 100.0
45) 20 AIRCRAFT TRUE AIRSPEED (GUST) (M/S) TASG M/S = (N/ 1000.0) - 100.0
46) 20 DISTANCE EAST OF BAO TOWER (KM) DEI KM = (N/ 100.0) - 1000.0
47) 20 DISTANCE NORTH OF BAO TOWER (KM) DNI KM = (N/ 100.0) - 1000.0
48) 20 TOTAL TEMPERATURE (WING ROSEMOUNT) (C) TTW C = (N/ 1000.0) - 100.0
49) 20 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0
50) 20 DEW/FROSTPOINT TEMP (THERMOELEC) (C) DP DEG C = (N/ 1000.0) - 100.0
51) 20 RAW DYNAMIC PRESSURE (WING) (MB) QCW MB = (N/ 1000.0) - 100.0
52) 20 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0
53) 20 RAW DYNAMIC PRESSURE (BOOM) (MB) QCB MB = (N/ 1000.0) - 100.0
54) 20 RAW STATIC PRESSURE (FUSELAGE) (MB) PSF MB = (N/ 1000.0) - 0.0
55) 20 RAW STATIC PRESSURE (BOOM) (MB) PSB MB = (N/ 1000.0) - 0.0
56) 20 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0
57) 20 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0
58) 20 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0
59) 20 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0
60) 20 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 1000.0) - 500.0
61) 20 ATTACK ANGLE (FIXED VANE) (DEG) AFIX DEG = (N/ 1000.0) - 100.0
62) 20 ATTACK ANGLE (ROTATING VANE) (DEG) AROT DEG = (N/ 1000.0) - 100.0
63) 20 SIDESLIP ANGLE (FIXED VANE) (DEG) BFIX DEG = (N/ 1000.0) - 100.0
64) 20 SIDESLIP ANGLE (ROTATING VANE) (DEG) BROT DEG = (N/ 1000.0) - 100.0
65) 20 GUST PROBE TIP VERT ACCEL (M/S2) VAC M/S2 = (N/ 1000.0) - 100.0
66) 20 GUST PROBE TIP LATERAL ACCEL (M/S2) LAC M/S2 = (N/ 1000.0) - 100.0
67) 20 POTENTIAL TEMPERATURE (K) THETA K = (N/ 1000.0) - 100.0
68) 20 EQUIVALENT POTENTIAL TEMPERATURE (K) ETHETA K = (N/ 1000.0) - 100.0
69) 20 VIRTUAL POTENTIAL TEMPERATURE (K) VTHETA K = (N/ 1000.0) - 100.0
70) 20 HOT WIRE VOLTAGE 1 (VDC) HWV1 VDC = (N/ 1000.0) - 100.0
71) 20 HOT WIRE VOLTAGE 2 (VDC) HWV2 VDC = (N/ 1000.0) - 100.0
72) 20 HOT WIRE RMS 1 (VDC) HWRMS1 VDC = (N/ 1000.0) - 100.0
73) 20 HOT WIRE RMS 2 (VDC) HWRMS2 VDC = (N/ 1000.0) - 100.0
74) 20 HOT WIRE RMS 3 (VDC) HWRMS3 VDC = (N/ 1000.0) - 100.0
75) 20 RAW OZONE (STEDMAN) (COUNTS) O3STR COUNTS = (N/ 1.0) - 0.0
76) 20 OZONE CONCENTRATION (STEDMAN) (CNTS/SEC) O3STC CNTS/SEC = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
656-01 BAO SITE STUDY 17APR78 16/17/00
THIS FILE IS ALL OR PART OF THE TIME PERIOD 16 17 0 TO 18 5 0
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
1436 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
****** BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 28500 BITS PER LOGICAL DATA RECORD
1 LOGICAL DATA RECORDS PER PHYSICAL RECORD
28500 BITS PER PHYSICAL DATA RECORD
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