```  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```