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Proof ENTRY_LEXICON #203 (#381)

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* Proof FIXED_FIXED_CONSTANT_POOL (#207)

* wip(p838/843): Proof ENTRY_LEXICON #203

* wip(843/843: DONE): Proof ENTRY_LEXICON #203
This commit is contained in:
Glenn Dwiyatcita 2019-05-02 16:06:26 +02:00 committed by James Harris
parent 98faa4c43d
commit 2599c17241
1 changed files with 67 additions and 141 deletions
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134
Comanche055/ENTRY_LEXICON.agc
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@ -30,7 +30,8 @@
# Page 837 # Page 837
# VARIABLE DESCRIPTION MAXIMUM VALUE * COMPUTER NAME # VARIABLE DESCRIPTION MAXIMUM VALUE * COMPUTER NAME
# -------- ----------- --------------- ------------- # -------- ----------- ------- ------- -------- ----
#
# _ # _
# URT0 INITIAL TARGET VECTOR 2 (UNIT VECTOR) = RTINIT # URT0 INITIAL TARGET VECTOR 2 (UNIT VECTOR) = RTINIT
# _ # _
@ -55,139 +56,78 @@
# G GRAVITY VECTOR 128 M/CENTISEC = GDT/2 # G GRAVITY VECTOR 128 M/CENTISEC = GDT/2
# #
# A0 INITIAL DRAG FOR UPCONTRL 805 FPSS FPSS=FT/SEC/SEC # A0 INITIAL DRAG FOR UPCONTRL 805 FPSS FPSS=FT/SEC/SEC
#
# AHOOKDV TERM IN GAMMAL CALC. = AHOOK DVL 16 # AHOOKDV TERM IN GAMMAL CALC. = AHOOK DVL 16
#
# A1 DRAG VALUE IN FACTOR CALCULATION 805 FPSS # A1 DRAG VALUE IN FACTOR CALCULATION 805 FPSS
#
# ALP CONST FOR UPCONTRL 1 # ALP CONST FOR UPCONTRL 1
#
# ASKEP KEPLER RANGE 21600 NM NM = NAUTICAL MILE # ASKEP KEPLER RANGE 21600 NM NM = NAUTICAL MILE
#
# ASP1 FINAL PHASE RANGE 21600 NM # ASP1 FINAL PHASE RANGE 21600 NM
#
# ASPUP UP-RANGE 21600 NM # ASPUP UP-RANGE 21600 NM
#
# ASP3 GAMMA CORRECTION 21600 NM # ASP3 GAMMA CORRECTION 21600 NM
#
# ASPDWN RANGE DOWN TO PULL-UP 21600 NM # ASPDWN RANGE DOWN TO PULL-UP 21600 NM
#
# ASP PREDICTED RANGE 21600 NM NOT STORED # ASP PREDICTED RANGE 21600 NM NOT STORED
#
# COSG COSINE(GAMMAL) 2 = COSG/2 # COSG COSINE(GAMMAL) 2 = COSG/2
#
# C/D0 RECIPROCAL DRAG, -4/D0 B-8 64/FPSS # C/D0 RECIPROCAL DRAG, -4/D0 B-8 64/FPSS
#
# D TOTAL ACCELERATION 805 FPSS # D TOTAL ACCELERATION 805 FPSS
#
# D0 CONTROLLED CONSTANT D 805 FPSS # D0 CONTROLLED CONSTANT D 805 FPSS
#
# DHOOK TERM IN GAMMAL COMPUTATION 805 FPSS # DHOOK TERM IN GAMMAL COMPUTATION 805 FPSS
#
# DIFF THETNM-ASP (RANGE DIFFERENCE) 21600 NM # DIFF THETNM-ASP (RANGE DIFFERENCE) 21600 NM
#
# DIFFOLD PREVIOUS VALUE OF DIFF 21600 NM # DIFFOLD PREVIOUS VALUE OF DIFF 21600 NM
#
# DLEWD CHANGE IN LEWD 1 # DLEWD CHANGE IN LEWD 1
#
# DR REFERENCE DRAG FOR DOWNCONTROL 805 FPSS NOT STORED # DR REFERENCE DRAG FOR DOWNCONTROL 805 FPSS NOT STORED
#
# DREFR REFERENCE DRAG 805 FPSS NOT STORED # DREFR REFERENCE DRAG 805 FPSS NOT STORED
#
# DVL VS1-VL 2 VSAT # DVL VS1-VL 2 VSAT
#
# E ECCENTRICITY 4 NOT STORED # E ECCENTRICITY 4 NOT STORED
#
# F1 DRANGE/D DRAG (FINAL PHASE) 2700/805 = FX +5 # F1 DRANGE/D DRAG (FINAL PHASE) 2700/805 = FX +5
#
# F2 DRANGE/D RDOT (FINAL PHASE) 2700/2VS NM/FPS = FX +4 # F2 DRANGE/D RDOT (FINAL PHASE) 2700/2VS NM/FPS = FX +4
# Page 838 # Page 838
#
# F3 DRANGE/D (L/D) 2700 NM = FX # F3 DRANGE/D (L/D) 2700 NM = FX
#
# FACT1 CONST FOR UPCONTRL 805 FPSS # FACT1 CONST FOR UPCONTRL 805 FPSS
#
# FACT2 CONST FOR UPCONTRL 1/805 FPSS # FACT2 CONST FOR UPCONTRL 1/805 FPSS
#
# FACTOR USED IN UPCONTRL 1 * MAXIMUM VALUE DENOTES UNSCALED # FACTOR USED IN UPCONTRL 1 * MAXIMUM VALUE DENOTES UNSCALED
# VARIABLE VALUE WHEN SCALED # GAMMAL FLIGHT PATH ANGLE AT VL 1 RADIAN VARIABLE VALUE WHEN SCALED
# GAMMAL FLIGHT PATH ANGLE AT VL 1 RADIAN VARIABLE HAS MAXIMUM VALUE OF ONE. # GAMMAL1 SIMPLE FORM OF GAMMAL 1 RADIAN VARIABLE HAS MAXIMUM VALUE OF ONE.
#
# GAMMAL1 SIMPLE FORM OF GAMMAL 1 RADIAN
# Page 839 # Page 839
# #
# HEADSUP INDICATOR FOR INITIAL ROLL 1 # HEADSUP INDICATOR FOR INITIAL ROLL 1
#
# KA DRAG TO LIFT UP IF DOWN 805 FPSS = KAT # KA DRAG TO LIFT UP IF DOWN 805 FPSS = KAT
#
# KLAT LATERAL SWITCH GAIN 1 (NOM = .0125) # KLAT LATERAL SWITCH GAIN 1 (NOM = .0125)
#
# K2ROLL INDICATOR FOR ROLL SWITCH # K2ROLL INDICATOR FOR ROLL SWITCH
#
# LAD MAX L/D (MIN ACTUAL VEHICLE L/D) 1 # LAD MAX L/D (MIN ACTUAL VEHICLE L/D) 1
#
# LADPAD NOMINAL VEHICLE L/D, SP PAD LOAD 1 (NOM = 0.3) # LADPAD NOMINAL VEHICLE L/D, SP PAD LOAD 1 (NOM = 0.3)
#
# LATANG LATERAL RANGE 4 RADIANS # LATANG LATERAL RANGE 4 RADIANS
#
# LEQ EXCESS C.F. OVER GRAV=(VSQ-1)GS 128.8 FPSS # LEQ EXCESS C.F. OVER GRAV=(VSQ-1)GS 128.8 FPSS
#
# LEWD UPCONTROL REFERENCE L/D 1 # LEWD UPCONTROL REFERENCE L/D 1
#
# LOD FINAL PHASE L/D 1 (NOM = 0.18) # LOD FINAL PHASE L/D 1 (NOM = 0.18)
#
# LODPAD FINAL PHASE L/D, SP PAD LOAD 1 # LODPAD FINAL PHASE L/D, SP PAD LOAD 1
#
# L/D DESIRED LIFT TO DRAG RATIO 1 # L/D DESIRED LIFT TO DRAG RATIO 1
# (VERTICAL PLANE) # (VERTICAL PLANE)
#
# L/D1 TEMP STORAGE FOR L/D IN LATERAL 1 # L/D1 TEMP STORAGE FOR L/D IN LATERAL 1
#
# L/DCMINR LAD COS(15DEG) 1 (NOM = 0.2895) # L/DCMINR LAD COS(15DEG) 1 (NOM = 0.2895)
# # PREDANGL PREDICTED RANGE (FINAL PHASE) 2700 NM = PREDANG
# PREDANGLE PREDICTED RANGE (FINAL PHASE) 2700 NM = PREDANG
#
# Q2 FINAL PHASE RANGE -23500 Q3 21600 NM # Q2 FINAL PHASE RANGE -23500 Q3 21600 NM
# Q2 = FCN(LAD) # Q2 = FCN(LAD)
#
# Q7 MINIMUM DRAG FOR UPCONTROL 805 FPSS # Q7 MINIMUM DRAG FOR UPCONTROL 805 FPSS
#
# RDOT ALTITUDE RATE 2 VSAT # RDOT ALTITUDE RATE 2 VSAT
#
# RDOTREF REFERENCE RDOT FOR UPCONTROL 2 VSAT # RDOTREF REFERENCE RDOT FOR UPCONTROL 2 VSAT
#
# RDTR REFERENCE RDOT FOR DOWNCONT 2 VSAT NOT SAVED # RDTR REFERENCE RDOT FOR DOWNCONT 2 VSAT NOT SAVED
#
# ROLLC ROLL COMMAND 1 REVOLUTION # ROLLC ROLL COMMAND 1 REVOLUTION
#
# RTOGO RANGE TO GO (FINAL PHASE) 2700 NM = FX +2 # RTOGO RANGE TO GO (FINAL PHASE) 2700 NM = FX +2
#
# SL SINE OF LATITUDE 1 NOT SAVED # SL SINE OF LATITUDE 1 NOT SAVED
#
# T TIME B 28 CENTISEC = TIME2,TIME1 # T TIME B 28 CENTISEC = TIME2,TIME1
#
# THETA DESIRED RANGE (RADIANS) 2 PI RADIANS = THETAH # THETA DESIRED RANGE (RADIANS) 2 PI RADIANS = THETAH
#
# THETNM DESIRED RANGE (NM) 21600 NM NON EXISTENT # THETNM DESIRED RANGE (NM) 21600 NM NON EXISTENT
#
# V VELOCITY MAGNITUDE 2 VSAT # V VELOCITY MAGNITUDE 2 VSAT
#
# V1 INITIAL VELOCITY FOR UPCONTROL 2 VSAT # V1 INITIAL VELOCITY FOR UPCONTROL 2 VSAT
#
# VL EXIT VELOCITY FOR UPCONTROL 2 VSAT # VL EXIT VELOCITY FOR UPCONTROL 2 VSAT
#
# VREF REFERENCE VELOCITY FOR UPCONTROL 2 VSAT # VREF REFERENCE VELOCITY FOR UPCONTROL 2 VSAT
#
# VS1 VSAT OR V1, WHICHEVER IS SMALLER 2 VSAT # VS1 VSAT OR V1, WHICHEVER IS SMALLER 2 VSAT
# 2 2 # 2 2
# VBARS VL /VSAT 4 # VBARS VL /VSAT 4
# 2 2 # 2 2
# VSQ NORMALIZED VEL. SQUARED = V /VSAT 4 = VSQUARE # VSQ NORMALISED VEL. SQUARED = V /VSAT 4 = VSQUARE
#
# WT EARTH RATE TIMES TIME 1 REVOLUTION NOT SAVED # WT EARTH RATE TIMES TIME 1 REVOLUTION NOT SAVED
# # = WIE (DTEAROT)
# X INTERMEDIATE VARIABLE IN G-LIMITER 2 VSAT NOT SAVED # X INTERMEDIATE VARIABLE IN G-LIMITER 2 VSAT NOT SAVED
#
# Y LATERAL MISS LIMIT 4 RADIANS NOT SAVED # Y LATERAL MISS LIMIT 4 RADIANS NOT SAVED
# Page 840 # Page 840
@ -198,45 +138,30 @@
# -------- ----------- ------------- # -------- ----------- -------------
# #
# GOTOADDR ADDRESS SELECTED BY SEQUENCER # GOTOADDR ADDRESS SELECTED BY SEQUENCER
#
# XPIPBUF BUFFER TO STORE X PIPA COUNTS # XPIPBUF BUFFER TO STORE X PIPA COUNTS
#
# YPIPBUF BUFFER TO STORE Y PIPA COUNTS # YPIPBUF BUFFER TO STORE Y PIPA COUNTS
#
# ZPIPBUF BUFFER TO STORE Z PIPA COUNTS # ZPIPBUF BUFFER TO STORE Z PIPA COUNTS
#
# PIPCTR COUNTS PASSES THRU PIPA READ ROUTINE # PIPCTR COUNTS PASSES THRU PIPA READ ROUTINE
#
# JJ INDEX IN FINAL PHASE TABLE LOOK-UP # JJ INDEX IN FINAL PHASE TABLE LOOK-UP
# # MM INDEX IN FINAL PHASE TABLE LOOK-UP
# MM INDEX IN FINAL PHASE TABLE LOOK-U
#
# GRAD INTERPOLATION FACTOR IN FINAL PHASE # GRAD INTERPOLATION FACTOR IN FINAL PHASE
#
# FX DRANGE/D L/D = F3 2700 NM # FX DRANGE/D L/D = F3 2700 NM
#
# FX +1 AREF 805 FPSS # FX +1 AREF 805 FPSS
#
# FX +2 RTOGO 2700 NM # FX +2 RTOGO 2700 NM
#
# FX +3 RDOTREF VSAT/4 # FX +3 RDOTREF VSAT/4
#
# FX +4 DRANGE/D RDOT = F2 21600/2VS NM/FPS # FX +4 DRANGE/D RDOT = F2 21600/2VS NM/FPS
#
# FX +5 DRANGE/D DRAG = F1 2700/805 NM/FPSS # FX +5 DRANGE/D DRAG = F1 2700/805 NM/FPSS
#
# TEM1B TEMPORARY LOCATION # TEM1B TEMPORARY LOCATION
#
# TIME/RTO TIME OF INITIAL TARGET RTINIT B 28 CENTISEC # TIME/RTO TIME OF INITIAL TARGET RTINIT B 28 CENTISEC
#
# DTEAROT EST TIME BETWEEN RTINIT AND RT B 28 CENTISEC # DTEAROT EST TIME BETWEEN RTINIT AND RT B 28 CENTISEC
#
# _ # _
# UNITV UNIT V VECTOR 2 # UNITV UNIT V VECTOR 2
# _ # _
# UNITR UNIT R VECTOR 2 # UNITR UNIT R VECTOR 2
# _ # _
# -VREL NEGATIVE VELOCITY REL TO ATMOSP 2 VSAT # -VREL NEGATIVE VELOCITY REL TO ATMOSP 2 VSAT
#
# COMPUTER SWITCHES INITIAL STATE CM/FLAGS = STATE +6 # COMPUTER SWITCHES INITIAL STATE CM/FLAGS = STATE +6
# ----------------- ------------- ------------------- # ----------------- ------------- -------------------
# #
@ -267,7 +192,7 @@
# DLEWD0 INITIAL VARIATION IN LEWD -.05 # DLEWD0 INITIAL VARIATION IN LEWD -.05
# D2 DRAG TO CHANGE LEWD 175 FPSS # D2 DRAG TO CHANGE LEWD 175 FPSS
# DT COMPUTATION CYCLE TIME INTERVAL 2 SEC. # DT COMPUTATION CYCLE TIME INTERVAL 2 SEC.
# GMAX MAXIMUM ACCELERATION 257.6 FPSS (8 G'S) # GMAX MAXIMUM ACCELERATION 257.6 FPSS (8 G-S)
# KA1 FACTOR IN KA CALC 1.3 GS # KA1 FACTOR IN KA CALC 1.3 GS
# KA2 FACTOR IN KA CALC .2 GS # KA2 FACTOR IN KA CALC .2 GS
# KA3 FACTOR IN D0 CALC 90 FPSS # KA3 FACTOR IN D0 CALC 90 FPSS
@ -286,10 +211,10 @@
# Q5 FINAL PHASE DRANGE/D GAMMA 7050 NM/RAD # Q5 FINAL PHASE DRANGE/D GAMMA 7050 NM/RAD
# Q6 FINAL PHASE INITIAL FLIGHT PATH ANGLE .0349 RAD # Q6 FINAL PHASE INITIAL FLIGHT PATH ANGLE .0349 RAD
# Q7F MIN DRAG FOR UPCONTROL 6 FPSS # Q7F MIN DRAG FOR UPCONTROL 6 FPSS
# Q7MIN IN VALUE FOR Q7 IN FACTOR CALCULATION 40 FPSS # Q7MIN MIN VALUE FOR Q7 IN FACTOR CALCULATION 40 FPSS
# Q19 FACTOR IN GAMMAL1 CALCULATION .5 # Q19 FACTOR IN GAMMAL1 CALCULATION .5
# Q21 FACTOR IN Q2 CALCULATION 1000 NM # Q21 FACTOR IN Q2 CALCULATION. 1000 NM
# Q22 FACTOR IN Q2 CALCULATION -1302 NM # Q22 FACTOR IN Q2 CALCULATION. -1302 NM
# VFINAL1 VELOCITY TO START FINAL PHASE ON INITIAL ENTRY 27000 FPS # VFINAL1 VELOCITY TO START FINAL PHASE ON INITIAL ENTRY 27000 FPS
# VFINAL FACTOR IN INITIAL UP-DOWN CALC 26600 FPS # VFINAL FACTOR IN INITIAL UP-DOWN CALC 26600 FPS
# VLMIN MINIMUM VL 18000 FPS # VLMIN MINIMUM VL 18000 FPS
@ -301,21 +226,22 @@
# Page 842 # Page 842
# CONVERSION FACTORS AND SCALING CONSTANTS # CONVERSION FACTORS AND SCALING CONSTANTS
# ---------------------------------------- # ---------- ------- --- ------- ---------
# #
# ATK ANGLE IN RAD TO NM 3437.7468 NM/RAD # ATK ANGLE IN RAD TO NM 3437.7468 NM/RAD
# G5 NOMINAL G VALUE FOR SCALING 32.2 FPSS # G5 NOMINAL G VALUE FOR SCALING 32.2 FPSS
# H5 ATMOSPHERE SCALE HEIGHT 28500 FT # H5 ATMOSPHERE SCALE HEIGHT 28500 FT
# J GRAVITY HARMONIC COEFFICIENT .00162346 # J GRAVITY HARMONIC COEFFICIENT .00162346
# KWE EQUATORIAL EARTH RATE 1546.10168 FPS # KWE EQUATORIAL EARTH RATE 1546.70168 FPS
# MUE EARTH GRAVITATIONAL CONSTANT 3.986032233 E 14 CUBIC M/ SEC SEC # MUE EARTH GRAVITATIONAL CONSTANT 3.986032233 E 14 CUBIC M/ SEC SEC
# RE EARTH RADIUS 21202900 FT # RE EARTH RADIUS 21202900 FT
# REQ EARTH EQUATORIAL RADIUS 20925738.2 FT # REQ EARTH EQUATORIAL RADIUS 20925738.2 FT
# VSAT SATELLITE VELOCITY AT RE 25766.1973 FPS # VSAT SATELLITE VELOCITY AT RE 25766.1973 FPS
# WIE EARTH RATE .0000729211505 RAD/SEC # WIE EARTH RATE .0000729211505 RAD/SEC
#
# (END GSOP AS-278, VOL 1, FIG. 5.6-3 CONSTANTS,GAINS, ETC.) # (END GSOP AS-278, VOL 1, FIG. 5.6-3 CONSTANTS,GAINS, ETC.)
#
#
# DISPLAY QUANTITIES # DISPLAY QUANTITIES
# ------------------ # ------------------
# #
@ -324,36 +250,37 @@
# VARIABLE DESCRIPTION MAXIMUM VALUE # VARIABLE DESCRIPTION MAXIMUM VALUE
# -------- ----------- ------------- # -------- ----------- -------------
# #
# QMAX PREDICTED MAXIMUM ENTRY ACCEL 163.84 GS N 60 # GMAX PREDICTED MAXIMUM ENTRY ACCEL 163.84 GS N 60
# VPRED PREDICTED VELOCITY AT ALTITUDE 128 M/CENTISEC N 60 # VPRED PREDICTED VELOCITY AT ALTITUDE 128 M/CENTISEC N 60
# 400K FT ABOVE FISCHER RADIUS. # 400K FT ABOVE FISCHER RADIUS.
# GAMMAEI PREDICTED GAMMA AT ALTITUDE 1 REVOLUTION N 60 # GAMMAEI PREDICTED GAMMA AT ALTITUDE 1 REVOLUTION N 60
# 400K FT ABOVE FISCHER RADIUS # 400K FT ABOVE FISCHER RADIUS.
# D DRAG ACCELERATION 805 FPSS N 64 # D DRAG ACCELERATION 805 FPSS N 64
# VMAGI INERTIAL VELOCITY MAGNITUDE 128 M/CENTISEC N 64, N 68 # VMAGI INERTIAL VELOCITY MAGNITUDE 128 M/CENTISEC N 64, N 68
# THETAH DESIRED RANGE ANGLE NM 1 REVOLUTION N 64, N 67 # THETAH DESIRED RANGE ANGLE NM 1 REVOLUTION N 64, N 67
# LAT PRESENT LATITUDE 1 REVOLUTION N 67 # LAT PRESENT LATITUDE 1 REVOLUTION N 67
# LONG PRESENT LONGITUDE 1 REVOLUTION N 67 # LONG PRESENT LONGITUDE 1 REVOLUTION N 67
# RTOGO RANGE ANGLE TO SPLASH FROM 1 REVOLUTION N 67 # RTOGO RANGE ANGLE TO SPLASH FROM 1 REVOLUTION N 63
# EMSALT FT ABOVE FISCHER RADIUS (IN NM) # EMSALT FT ABOVE FISCHER RADIUS. (IN NM)
# VIO PREDICTED VELOCITY AT ALTITUDE 128 M/CENTISEC N 63 # VIO PREDICTED VELOCITY AT ALTITUDE 128 M/CENTISEC N 63
# EMSALT FT ABOVE FISCHER RADIUS. # EMSALT FT ABOVE FISCHER RADIUS.
# TTE TIME OF FREE FALL TO ALT B 28 CENTISEC N 63 # TTE TIME OF FREE FALL TO ALT B 28 CENTISEC N 63
# EMSALT FT ABOVE FISCHER RADIUS # EMSALT FT ABOVE FISCHER RADIUS.
# ROLLC ROLL COMMAND 1 REVOLUTION N 68, N 68, N 69 # ROLLC ROLL COMMAND 1 REVOLUTION N 66, N 68, N 69
# LATANG CROSS-RANGE ERROR (XRNGERR) 4 RADIANS N 66 # LATANG CROSS-RANGE ERROR (XRNGERR) 4 RADIANS N 66
# DNRNGERR DOWN RANGE ERROR 1 REVOLUTION N 66 # DNRNGERR DOWN RANGE ERROR 1 REVOLUTION N 66
# (PREDANG - THETAH IN NM) # (PREDANG - THETAH IN NM)
# HDOT ALTITUDE RATE 128 M/CENTISEC N 68 # HDOT ALTITUDE RATE 128 M/CENTISEC N 68
# QT MINIMUM DRAG FOR UPCONTROL 805 FPSS N 69 # Q7 MINIMUM DRAG FOR UPCONTROL 805 FPSS N 69
# VL EXIT VELOCITY FOR UP-CONTROL 2 VSAT N 69 # VL EXIT VELOCITY FOR UP-CONTROL 2 VSAT N 69
# Page 843 # Page 843
# BODY ATTITUDE QUANTITIES (CM/POSE) # BODY ATTITUDE QUANTITIES (CM/POSE)
# ---------------------------------- # ----------------------------------
# #
# VARIABLE DECRIPTION MAXIMUM VALUE # VARIABLE DESCRIPTION MAXIMUM VALUE
# -------- ---------- ------------- # -------- ---------- ------- -----
#
# _ # _
# -VREL NEGATIVE VELOCITY REL TO ATMOS. 2 VSAT # -VREL NEGATIVE VELOCITY REL TO ATMOS. 2 VSAT
# _ # _
@ -363,11 +290,10 @@
# _ # _
# UYA/2 BASED ON 2 # UYA/2 BASED ON 2
# _ # _
# UZA/2 THE TRAJECTORY 2 # UZA/2 THE TRAJECTORY. 2
# _ # _
# UBX/2 UNIT VECTOR 2 # UBX/2 UNIT VECTOR 2
# _ # _
# UBY/2 BODY TRIAD 2 # UBY/2 BODY TRIAD 2
# _ # _
# UBZ/2 FOR CM. 2 # UBZ/2 FOR CM. 2