N306D Sample LRT GENPRO-I header


691A-1 CONVECTIVE STORMS - 78 1JUL78 FIRST TIME ON THIS FILE 13 41 37 THIS FILE I S ALL OR PART OF TIME PERIOD 13 41 35 TO 15 31 30 DESCRIPTION OF RECORD -- 103 PARAMETERS WERE SAVE D AT THEIR RESPECTIVE RATES. THIS REPRESENTS 103 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC THE 14 CYCLES OF 103 SAMP/CYC = 1442 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR D INTO 481 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 EVENT MARKER WORD EVMRKS = (N/ 1.0) - 0.0 5) 1 PILOT MICROPHONE SWITCH (XMIT) (VDC) XMIT VDC = (N/ 1000.0) - 100.0 6) 1 FIXED ZERO VOLTAGE (VDC) FZV VDC = (N/ 1000.0) - 100.0 7) 1 RAW INS LATITUDE (DEG) ALAT DEG = (N/ 1000.0) - 100.0 8) 1 RAW INS LONGITUDE (DEG) ALONG DEG = (N/ 1000.0) - 200.0 9) 1 AIRCRAFT TRUE HEADING (ARINC) (DEG) THI DEG = (N/ 1000.0) - 100.0 10) 1 INS WANDER ANGLE (DEG) ALPHA DEG = (N/ 1000.0) - 100.0 11) 1 RAW INS GROUND SPD X COMPONENT (M/S) XVI M/S = (N/ 1000.0) - 500.0 12) 1 RAW INS GROUND SPD Y COMPONENT (M/S) YVI M/S = (N/ 1000.0) - 500.0 13) 1 RAW INS GROUND SPEED (M/S) GSF M/S = (N/ 1000.0) - 100.0 14) 1 AIRCRAFT PITCH ATTITUDE ANGLE (DEG) PITCH DEG = (N/ 1000.0) - 100.0 15) 1 AIRCRAFT ROLL ATTITUDE ANGLE (DEG) ROLL DEG = (N/ 1000.0) - 100.0 16) 1 AIRCRAFT TRUE HEADING (YAW) (DEG) THF DEG = (N/ 1000.0) - 100.0 17) 1 RAW INS VERTICAL VELOCITY (M/S) VZI M/S = (N/ 1000.0) - 500.0 18) 1 RAW DYNAMIC PRESSURE (WING) (MB) QCW MB = (N/ 1000.0) - 100.0 19) 1 RAW DYNAMIC PRESSURE (GUST PROBE) (MB) QCG MB = (N/ 1000.0) - 100.0 20) 1 CORRECTED DYNAMIC PRESR (WING) (MB) QCWC MB = (N/ 1000.0) - 100.0 21) 1 CORRECTED DYNAMIC PRESR (GUST PROBE)(MB) QCGC MB = (N/ 1000.0) - 100.0 22) 1 RAW STATIC PRESSURE (FUSELAGE) (MB) PSF MB = (N/ 1000.0) - 0.0 23) 1 RAW STATIC PRESSURE (BOOM) (MB) PSB MB = (N/ 1000.0) - 0.0 24) 1 CORRECTED STATIC PRESR (FUSELAGE) (MB) PSFC MB = (N/ 1000.0) - 0.0 25) 1 CORRECTED STATIC PRESSURE (BOOM) (MB) PSBC MB = (N/ 1000.0) - 0.0 26) 1 NACA PRESSURE ALTITUDE (M) HP M = (N/ 10.0) - 500.0 27) 1 GEOMETRIC (RADIO) ALTITUDE (M) HGM M = (N/ 1000.0) - 100.0 28) 1 TOTAL TEMPERATURE (WING ROSEMOUNT) (C) TTW C = (N/ 1000.0) - 100.0 29) 1 TOTAL TEMPERATURE (REVERSE FLOW) (C) TTRF C = (N/ 1000.0) - 100.0 30) 1 TOTAL TEMPERATURE (FAST RESPONSE) (C) TTKP C = (N/ 1000.0) - 100.0 31) 1 AMBIENT TEMPERATURE (ROSEMOUNT) (C) ATW C = (N/ 1000.0) - 100.0 32) 1 AMBIENT TEMPERATURE (REVERSE-FLOW) (C) ATRF C = (N/ 1000.0) - 100.0 33) 1 AMBIENT TEMPERATURE (FAST RESPONSE) (C) ATKP C = (N/ 1000.0) - 100.0 34) 1 DEW/FROSTPOINT TEMP (THERMOELEC) (C) DP C = (N/ 1000.0) - 100.0 35) 1 DEWPOINT TEMPERATURE (THERMOELEC) (C) DPC C = (N/ 1000.0) - 100.0 36) 1 ABSOLUTE HUMIDITY (THERMOELEC) (G/M3) RHOTD G/M3 = (N/ 1000.0) - 100.0 37) 1 AIRCRAFT TRUE AIRSPEED (WING) (M/S) TASW M/S = (N/ 1000.0) - 100.0 38) 1 AIRCRAFT TRUE AIRSPEED (GUST) (M/S) TASG M/S = (N/ 1000.0) - 100.0 39) 1 RAW J-W LIQUID WATER CONTENT (G/M3) LWC G/M3 = (N/ 1000.0) - 100.0 40) 1 CORRCTD J-W LIQUID WATER CONTENT (G/M3) LWCC G/M3 = (N/ 1000.0) - 100.0 41) 1 ATTACK ANGLE (FIXED VANE) (DEG) AFIX DEG = (N/ 1000.0) - 100.0 42) 1 ATTACK ANGLE (ROTATING VANE) (DEG) AROT DEG = (N/ 1000.0) - 100.0 43) 1 SIDESLIP ANGLE (FIXED VANE) (DEG) BFIX DEG = (N/ 1000.0) - 100.0 44) 1 SIDESLIP ANGLE (ROTATING VANE) (DEG) BROT DEG = (N/ 1000.0) - 100.0 45) 1 GUST PROBE TIP VERT ACCEL (M/S2) VAC M/S2 = (N/ 1000.0) - 100.0 46) 1 GUST PROBE TIP LATERAL ACCEL (M/S2) LAC M/S2 = (N/ 1000.0) - 100.0 47) 1 WIND VECTOR EAST GUST COMPONENT (M/S) UI M/S = (N/ 1000.0) - 200.0 48) 1 WIND VECTOR NORTH GUST COMPONENT (M/S) VI M/S = (N/ 1000.0) - 200.0 49) 1 WIND VECTOR VERTICAL GUST COMP (H) (M/S) WI M/S = (N/ 1000.0) - 100.0 50) 1 WIND VECTOR LNGTDNL GUST COMPONENT (M/S) UX M/S = (N/ 1000.0) - 200.0 51) 1 WIND VECTOR LATERAL GUST COMPONENT (M/S) VY M/S = (N/ 1000.0) - 200.0 52) 1 HORIZONTAL WIND DIRECTION (DEG) WDRCTN DEG = (N/ 1000.0) - 100.0 53) 1 HORIZONTAL WIND SPEED (M/S) WSPD M/S = (N/ 1000.0) - 100.0 54) 1 WIND VECTOR EAST COMPONENT (M/S) UI1 M/S = (N/ 1000.0) - 200.0 55) 1 WIND VECTOR NORTH COMPONENT (M/S) VI1 M/S = (N/ 1000.0) - 200.0 56) 1 WIND VECTOR VERTICAL GUST COMP (L) (M/S) WI1 M/S = (N/ 1000.0) - 100.0 57) 1 WIND VECTOR LNGTDNL COMPONENT (M/S) UX1 M/S = (N/ 1000.0) - 200.0 58) 1 WIND VECTOR LATERAL COMPONENT (M/S) VY1 M/S = (N/ 1000.0) - 200.0 59) 1 RAW INS GROUND SPD EAST COMP (M/S) VEW M/S = (N/ 1000.0) - 500.0 60) 1 RAW INS GROUND SPD NORTH COMP (M/S) VNS M/S = (N/ 1000.0) - 500.0 61) 1 DISTANCE EAST OF GROVER, COLORADO (KM) DEIG KM = (N/ 100.0) - 1000.0 62) 1 DISTANCE NORTH OF GROVER, COLORADO (KM) DNIG KM = (N/ 100.0) - 1000.0 63) 1 AIRCRAFT C.G. ACCELERATION (M/S2) CGAC M/S2 = (N/ 1000.0) - 100.0 64) 1 DAMPED AIRCRAFT VERT VELOCITY (M/S) WP3 M/S = (N/ 1000.0) - 100.0 65) 1 PRESSURE-DAMPED INERTIAL ALTITUDE (M) HI3 M = (N/ 10.0) - 500.0 66) 1 TEMPERATURE AT LIFTING COND. LEVEL (C) TLCL C = (N/ 1000.0) - 100.0 67) 1 PRESR AT LIFTING CONDENSATION LEVEL (MB) PLCL MB = (N/ 1000.0) - 0.0 68) 1 MIXING RATIO (G/KG) RM G/KG = (N/ 1000.0) - 100.0 69) 1 EQUIVALENT POTENTIAL TEMPERATURE (K) ETHETA K = (N/ 1000.0) - 100.0 70) 1 POTENTIAL TEMPERATURE (K) THETA K = (N/ 1000.0) - 100.0 71) 1 AIRCRAFT INDICATED AIRSPEED (M/S) IASX M/S = (N/ 1000.0) - 100.0 72) 1 VERTICAL AIR VELOCITY (CSD EQNS.) (M/S) VAVCSD M/S = (N/ 1000.0) - 100.0 73) 1 I D WORD--PMS OAP 200Y (PRECIP) (.2-3NM) IDPR1 OAP200Y = (N/ 1.0) - 0.0 74) 1 PROBE 1/ CELL 1 RAW ACCUMULATIONS ACC 1/ 1 RAW = (N/ 1.0) - 0.0 75) 1 PROBE 1/ CELL 2 RAW ACCUMULATIONS ACC 1/ 2 RAW = (N/ 1.0) - 0.0 76) 1 PROBE 1/ CELL 3 RAW ACCUMULATIONS ACC 1/ 3 RAW = (N/ 1.0) - 0.0 77) 1 PROBE 1/ CELL 4 RAW ACCUMULATIONS ACC 1/ 4 RAW = (N/ 1.0) - 0.0 78) 1 PROBE 1/ CELL 5 RAW ACCUMULATIONS ACC 1/ 5 RAW = (N/ 1.0) - 0.0 79) 1 PROBE 1/ CELL 6 RAW ACCUMULATIONS ACC 1/ 6 RAW = (N/ 1.0) - 0.0 80) 1 PROBE 1/ CELL 7 RAW ACCUMULATIONS ACC 1/ 7 RAW = (N/ 1.0) - 0.0 81) 1 PROBE 1/ CELL 8 RAW ACCUMULATIONS ACC 1/ 8 RAW = (N/ 1.0) - 0.0 82) 1 PROBE 1/ CELL 9 RAW ACCUMULATIONS ACC 1/ 9 RAW = (N/ 1.0) - 0.0 83) 1 PROBE 1/ CELL 10 RAW ACCUMULATIONS ACC 1/10 RAW = (N/ 1.0) - 0.0 84) 1 PROBE 1/ CELL 11 RAW ACCUMULATIONS ACC 1/11 RAW = (N/ 1.0) - 0.0 85) 1 PROBE 1/ CELL 12 RAW ACCUMULATIONS ACC 1/12 RAW = (N/ 1.0) - 0.0 86) 1 PROBE 1/ CELL 13 RAW ACCUMULATIONS ACC 1/13 RAW = (N/ 1.0) - 0.0 87) 1 PROBE 1/ CELL 14 RAW ACCUMULATIONS ACC 1/14 RAW = (N/ 1.0) - 0.0 88) 1 PROBE 1/ CELL 15 RAW ACCUMULATIONS ACC 1/15 RAW = (N/ 1.0) - 0.0 89) 1 PROBE 1/ CELL 1 CONCENTRATIONS (N/M3) CON 1/ 1 N/M3 = (N/ .1) - 0.0 90) 1 PROBE 1/ CELL 2 CONCENTRATIONS (N/M3) CON 1/ 2 N/M3 = (N/ .1) - 0.0 91) 1 PROBE 1/ CELL 3 CONCENTRATIONS (N/M3) CON 1/ 3 N/M3 = (N/ .1) - 0.0 92) 1 PROBE 1/ CELL 4 CONCENTRATIONS (N/M3) CON 1/ 4 N/M3 = (N/ .1) - 0.0 93) 1 PROBE 1/ CELL 5 CONCENTRATIONS (N/M3) CON 1/ 5 N/M3 = (N/ .1) - 0.0 94) 1 PROBE 1/ CELL 6 CONCENTRATIONS (N/M3) CON 1/ 6 N/M3 = (N/ .1) - 0.0 95) 1 PROBE 1/ CELL 7 CONCENTRATIONS (N/M3) CON 1/ 7 N/M3 = (N/ .1) - 0.0 96) 1 PROBE 1/ CELL 8 CONCENTRATIONS (N/M3) CON 1/ 8 N/M3 = (N/ .1) - 0.0 97) 1 PROBE 1/ CELL 9 CONCENTRATIONS (N/M3) CON 1/ 9 N/M3 = (N/ .1) - 0.0 98) 1 PROBE 1/ CELL 10 CONCENTRATIONS (N/M3) CON 1/10 N/M3 = (N/ .1) - 0.0 99) 1 PROBE 1/ CELL 11 CONCENTRATIONS (N/M3) CON 1/11 N/M3 = (N/ .1) - 0.0 100) 1 PROBE 1/ CELL 12 CONCENTRATIONS (N/M3) CON 1/12 N/M3 = (N/ .1) - 0.0 101) 1 PROBE 1/ CELL 13 CONCENTRATIONS (N/M3) CON 1/13 N/M3 = (N/ .1) - 0.0 102) 1 PROBE 1/ CELL 14 CONCENTRATIONS (N/M3) CON 1/14 N/M3 = (N/ .1) - 0.0 103) 1 PROBE 1/ CELL 15 CONCENTRATIONS (N/M3) CON 1/15 N/M3 = (N/ .1) - 0.0 THERE ARE 1 PHYSICAL RECORDS IN THE HEADER FILE 691A-1 CONVECTIVE STORMS - 78 1JUL78 THIS FILE IS ALL OR PART OF THE TIME PERIOD 13 41 35 TO 15 31 30 DESCRIPTION OF TAPE: HEADER FILE -- 832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD 114 LOGICAL HEADER RECORDS PER PHYSICAL RECORD 94848 BITS PER PHYSICAL HEADER RECORD DATA FILE -- 2060 BITS PER LOGICAL DATA RECORD 14 LOGICAL DATA RECORDS PER PHYSICAL RECORD 28840 BITS PER PHYSICAL DATA RECORD