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Proof LAMBERT_AIMPOINT_GUIDANCE #601 (#731)

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Co-authored-by: Travis Wentz <twentz@avanleecare.com>
Co-authored-by: James Harris <wopian@wopian.me>
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travis8 2020-10-19 13:04:36 -06:00 committed by GitHub
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2 changed files with 40 additions and 41 deletions
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77
Luminary099/LAMBERT_AIMPOINT_GUIDANCE.agc
View File

@ -25,75 +25,75 @@
# Notations on the hardcopy document read, in part:
#
# Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
# 16:27 JULY 14, 1969
# 16:27 JULY 14,1969
# Page 651
# GENERAL LAMBERT AIMPOINT GUIDANCE **
# WRITTEN BY RAMA M AIYAWAR
# GENERAL LAMBERT AIMPOINT GUIDANCE **
# WRITTEN BY RAMA M AIYAWAR
# PROGRAM P-31 DESCRIPTION **
#
# 1. TO ACCEPT TARGETING PARAMETERS OBTAINED FROM A SOURCE EXTERNAL
# TO THE LEM AND COMPUTE THERE FROM THE REQUIRED-VELOCITY AND
# OTHER INITIAL CONDITIONS REQUIRED BY LM FOR DESIRED MANEUVER.
# THE TARGETING PARAMETERS ARE TIG (TIME OF IGNITION), TARGET
# VECTOR (RTARG), AND THE TIME FROM TIG UNTIL THE TARGET IS
# REACHED (DELLT4), DESIRED TIME OF FLIGHT FROM RINIT TO RTARG.
# 1. TO ACCEPT TARGETING PARAMETERS OBTAINED FROM A SOURCE EXTERNAL
# TO THE LEM AND COMPUTE THERE FROM THE REQUIRED-VELOCITY AND
# OTHER INITIAL CONDITIONS REQUIRED BY LM FOR DESIRED MANEUVER.
# THE TARGETING PARAMETERS ARE TIG (TIME OF IGNITION), TARGET
# VECTOR (RTARG), AND THE TIME FROM TIG UNTIL THE TARGET IS
# REACHED(DELLT4),DESIRED TIME OF FLIGHT FROM RINIT TO RTARG..
# ASSUMPTIONS **
#
# 1. THE TARGET PARAMETERS MAY HAVE BEEN LOADED PRIOR TO THE
# EXECUTION OF THIS PROGRAM.
# 2. THIS PROGRAM IS APPLICABLE IN EITHER EARTH OR LUNAR ORBIT.
# 3. THIS PROGRAM IS DESIGNED FOR ONE-MAN OPERATION, AND SHOULD
# BE SELECTED BY THE ASTRONAUT BY DSKY ENTRY V37 E31.
# 1. THE TARGET PARAMETERS MAY HAVE BEEN LOADED PRIOR TO THE
# EXECUTION OF THIS PROGRAM.
# 2. THIS PROGRAM IS APPLICABLE IN EITHER EARTH OR LUNAR ORBIT.
# 3. THIS PROGRAM IS DESIGNED FOR ONE-MAN OPERATION, AND SHOULD
# BE SELECTED BY THE ASTRONAUT BY DSKY ENTRY V37 E31.
# SUBROUTINES USED **
#
# MANUPARM, TTG/N35, R02BOTH, MIDGIM, DISPMGA, FLAGDOWN, BANKCALL,
# GOTOPOOH, ENDOFJOB, PHASCHNG, GOFLASHR, GOFLASH.
#
# MANUPARM CALCULATES APOGEE, PERIGEE ALTITUDES AND DELTAV DESIRED
# FOR THE MANEUVER.
# MANUPARM CALCULATES APOGEE, PERIGEE ALTITUDES AND DELTAV DESIRED
# FOR THE MANEUVER.
#
# TTG/N35 CLOCKTASK - UPDATES CLOCK.
# TTG/N35 CLOCKTASK - UPDATES CLOCK.
#
# MIDGIM CALCULATES MIDDLE GIMBAL ANGLE FOR DISPLAY.
# MIDGIM CALCULATES MIDDLE GIMBAL ANGLE FOR DISPLAY.
#
# R02BOTH IMU - STATUS CHECK ROUTINE.
# R02BOTH IMU - STATUS CHECK ROUTINE.
# DISPLAYS USED IN P-31LM **
#
# V06N33 DISPLAY SOTRED TIG (IN HRS. MINS. SECS.)
# V06N42 DISPLAY APOGEE, PERIGEE, DELTAV.
# V16N35 DISPLAY TIME FROM TIG.
# V06N45 TIME FROM IGNITION AND MIDDLE GIMBAL ANGLE.
# V06N33 DISPLAY SOTRED TIG (IN HRS. MINS. SECS)
# V06N42 DISPLAY APOGEE, PERIGEE, DELTAV.
# V16N35 DISPLAY TIME FROM TIG.
# V06N45 TIME FROM IGNITION AND MIDDLE GIMBAL ANGLE.
# ERASABLE INITIALIZATION REQUIRED **
#
# TIG TIME OF IGNITION DP (B+28) CS.
# TIG TIME OF IGNITION DP (B+28) CS.
#
# DELLT4 DESIRED TIME OF FLIGHT DP (B+28) CS
# FROM RINIT TO RTARG.
# DELLT4 DESIRED TIME OF FLIGHT DP (B+28) CS
# FROM RINIT TO RTARG .
#
# RTARG RADIUS VECTOR OF TARGET POSITION VECTOR
# RADIUS VECTOR SCALED TO (B+29)METERS IF EARTH ORBIT
# RTARG RADIUS VECTOR OF TARGET POSITION VECTOR
# RADIUS VECTOR SCALED TO (B+29)METERS IF EARTH ORBIT
# Page 652
# RADIUS VECTOR SCALED TO (B+27)METERS IF MOON ORBIT
# RADIUS VECTOR SCALED TO (B+27)METERS IF MOON ORBIT
# OUTPUT **
#
# HAPO APOGEE ALTITUDE
# HPER PERIGEE ALTITUDE
# VGDISP MAG. OF DELTAV FOR DISPLAY, SCALING B+7 M/CS EARTH
# MAG. OF DELTAV FOR DISPLAY, SCALING B+5 M/CS MOON
# MIDGIM MIDDLE GIMBAL ANGLE
# XDELVFLG RESETS XDELVFLG FOR LAMBERT VG COMPUTATIONS
# HAPO APOGEE ALTITUDE
# HPER PERIGEE ALTITUDE
# VGDISP MAG.OF DELTAV FOR DISPLAY ,SCALING B+7 M/CS EARTH
# MAG.OF DELTAV FOR DISPLAY,SCALING B+5 M/CS MOON
# MIDGIM MIDDLE GIMBAL ANGLE
# XDELVFLG RESETS XDELVFLG FOR LAMBERT VG COMPUTATIONS
# ALARMS OR ABORTS NONE **
# ALARMS OR ABORTS NONE **
# RESTARTS ARE VIA GROUP 4 **
# RESTARTS ARE VIA GROUP 4 **
SETLOC GLM
BANK
@ -102,7 +102,7 @@
COUNT* $$/P31
P31 TC P20FLGON
CAF V06N33 # T16
CAF V06N33 # TIG
TC VNPOOH
TC INTPRET
CLEAR DLOAD
@ -166,4 +166,3 @@ REVN1645 SET CALL # TRKMKCNT, TTOGO, +MGA
# *** END OF LEMP30S .103 ***

4
Luminary099/README.md
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@ -67,7 +67,7 @@ What follows is simply a bunch of file-includes for the individual code chunks.
| [P20-P25.agc] | 492-614 |
| [P30_P37.agc] | 615-617 |
| [P32-P35_P72-P75.agc] | 618-650 |
| [LAMBERT_AIMPOINT_GUIDANCE.agc] | 651-653 |
| [GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc] | 651-653 |
| [GROUND_TRACKING_DETERMINATION_PROGRAM.agc] | 654-657 |
| [P34-35_P74-75.agc] | 658-702 |
| [R31.agc] | 703-708 |
@ -164,7 +164,7 @@ What follows is simply a bunch of file-includes for the individual code chunks.
[P20-P25.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P20-P25.agc
[P30_P37.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P30_P37.agc
[P32-P35_P72-P75.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P32-P35_P72-P75.agc
[LAMBERT_AIMPOINT_GUIDANCE.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.agc
[GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc
[GROUND_TRACKING_DETERMINATION_PROGRAM.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/GROUND_TRACKING_DETERMINATION_PROGRAM.agc
[P34-35_P74-75.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P34-35_P74-75.agc
[R31.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/R31.agc