Sample LRT GENPRO-I header
ELECTRA 583 GAMETAG 23JULY76 FIRST TIME ON THIS FILE 18 55 29 THIS FILE I
S ALL OR PART OF TIME PERIOD 18 55 30 TO 21 27 52 DESCRIPTION OF RECORD -- 82 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 221 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 6 CYCLES OF 221 SAMP/CYC = 1326 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 442 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 TIME TIME SECONDS = (N/ 1.0) - 0.0
2) 1 UNALTERED TAPE TIME (SECONDS) TPTIME SECONDS = (N/ 1.0) - 0.0
3) 1 CORRECTED STATIC PRESSURE (MB) PSXC (MB) = (N/ 500.0) - 0.0
4) 1 AMBIENT TEMPERATURE FUSELAGE (DEG C) ATX (C) = (N/ 1000.0) - 100.0
5) 1 CORRECTED DEWPOINT TEMPERATURE (C) DPXC (C) = (N/ 1000.0) - 100.0
6) 1 ABSOLUTE HUMIDITY (THERMOELEC) (GM/M3) RHOTD (GM/M3) = (N/ 1000.0) - 100.0
7) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEGS = (N/ 1000.0) - 0.0
8) 1 HORIZONTAL WIND SPEED (M/S) WSPD (M/S) = (N/ 1000.0) - 0.0
9) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 (M/S) = (N/ 1000.0) - 200.0
10) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 (M/S) = (N/ 1000.0) - 200.0
11) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 (M/S) = (N/ 1000.0) - 200.0
12) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 (M/S) = (N/ 1000.0) - 200.0
13) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
14) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
15) 1 NACA PRESSURE ALTITUDE (M) HP (M) = (N/ 100.0) - 100.0
16) 1 PRESSURE DAMPED INERTIAL ALTITUDE (M) HI31 (M) = (N/ 100.0) - 100.0
17) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM (M) = (N/ 1000.0) - 100.0
18) 1 AIRCRAFT GROUND SPEED (M/S) GS (M/S) = (N/ 1000.0) - 0.0
19) 1 AIRCRAFT GROUND SPD EAST COMP (M/S) VEW (M/S) = (N/ 1000.0) - 500.0
20) 1 AIRCRAFT GROUND SPD NORTH COMP (M/S) VNS (M/S) = (N/ 1000.0) - 500.0
21) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP31 (M/S) = (N/ 1000.0) - 100.0
22) 1 AIRCRAFT C.G. VERT ACCELERATION (M/S2) CGAC1 M/S2 = (N/ 1000.0) - 100.0
23) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 0.0
24) 1 ROLL (DEG) ROLL DEGS = (N/ 1000.0) - 100.0
25) 1 PITCH (DEG) PITCH DEGS = (N/ 1000.0) - 100.0
26) 1 TRUE AIR SPEED (M/SEC) TASX M/SEC = (N/ 1000.0) - 100.0
27) 1 CORCTD IR SURFACE TEMP (PRT-5) (C) PRT5C (C) = (N/ 1000.0) - 100.0
28) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
29) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
30) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
31) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
32) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
33) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
34) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
35) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
36) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
37) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
38) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
39) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
40) 1 NOSEBOOM TOTAL TEMP (ROSEMOUNT) (C) TTB5 (C) = (N/ 1000.0) - 100.0
41) 1 FUSELAGE TOTAL TEMP (ROSEMOUNT) (C) TTF (C) = (N/ 1000.0) - 100.0
42) 1 LHS DEW/FROSTPOINT TEMP (C) DPLH (C) = (N/ 1000.0) - 100.0
43) 1 RHS DEW/FROSTPOINT TEMP (C) DPRH (C) = (N/ 1000.0) - 100.0
44) 1 RAW WINGTIP STATIC PRESSURE (MB) PSW (MB) = (N/ 500.0) - 0.0
45) 1 RAW WINGTIP DYNAMIC PRESSURE (MB) QCW (MB) = (N/ 1000.0) - 100.0
46) 1 RAW NOSEBOOM STATIC PRESSURE (MB) PSB (MB) = (N/ 500.0) - 0.0
47) 1 RAW NOSEBOOM DYNAMIC PRESSURE (MB) QCB (MB) = (N/ 1000.0) - 100.0
48) 1 RAW INS LATITUDE (DEG) ALAT DEGS = (N/ 1000.0) - 200.0
49) 1 RAW INS LONGITUDE (DEG) ALONG DEGS = (N/ 1000.0) - 200.0
50) 1 RAW VLF LATITUDE (DEG) VLAT DEGS = (N/ 1000.0) - 200.0
51) 1 RAW VLF LONGITUDE (DEG) VLONG DEGS = (N/ 1000.0) - 200.0
52) 1 INS VERTICAL VELOCITY (M/S) VZI (M/S) = (N/ 100.0) - 5000.0
53) 1 INS WANDER ANGLE (DEG) ALPHA DEGS = (N/ 1000.0) - 100.0
54) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0
55) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
56) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
57) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
58) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
59) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
60) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
61) 1 PRT-5 IRTRAN WINDOW TEMP (C) PRTWT (C) = (N/ 1000.0) - 100.0
62) 1 RAW IR SURFACE TEMP(PRT-5) (C) PRT5 (C) = (N/ 1000.0) - 100.0
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 UNUSED UNUSED = (N/ 1.0) - 0.0
68) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
69) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
70) 1 16MM CAMERA FRAME COUNT CAMFC = (N/ 1.0) - 0.0
71) 1 EVENT MARKERS EVENT MARKS = (N/ 1.0) - 0.0
72) 1 INS/KNLBRG UPDATE FLAGS UPDATE = (N/ 1.0) - 0.0
73) 1 RAW INS GROUND SPD X COMPONENT (M/S) XVI (M/S) = (N/ 1000.0) - 100.0
74) 1 RAW INS GROUND SPD Y COMPONENT (M/S) YVI (M/S) = (N/ 1000.0) - 100.0
75) 1 UNUSED UNUSED = (N/ 1.0) - 0.0
76) 20 ACCELERATION AT C.G. M/S2 CGAC (M/S2) = (N/ 1000.0) - 100.0
77) 20 LEFT WING STRAIN GAGE M-IN/IN STRLW UIN/IN = (N/ 500.0) - 1000.0
78) 20 RIGHT WING STRAIN GAGE M-IN/IN STRRW UIN/IN = (N/ 500.0) - 1000.0
79) 64 KNOLLENBERG 64 WORDS KNLBG COUNTS = (N/ 1.0) - 0.0
80) 1 CCN OUTPUT CHANNEL 55 (VDC) (DRI) CCN(55) VDC = (N/ 1000.0) - 100.0
81) 1 CCN OUTPUT CHANNEL 56 (VDC) (DRI) CCN(56) VDC = (N/ 1000.0) - 100.0
82) 20 NEPHELOMETER BACKSCATTER(VDC) (NCAR) NEPHSK VDC = (N/ 1000.0) - 100.0
THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE
ELECTRA 583 GAMETAG 23JULY76
THIS FILE IS ALL OR PART OF THE TIME PERIOD 18 55 30 TO 21 27 52
DESCRIPTION OF TAPE:
HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
232 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
193024 BITS PER PHYSICAL HEADER RECORD
DATA FILE -- 4420 BITS PER LOGICAL DATA RECORD
6 LOGICAL DATA RECORDS PER PHYSICAL RECORD
26520 BITS PER PHYSICAL DATA RECORD