ryan/Apollo-11
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

checked pages 0658-0667

Browse Source
This commit is contained in:
Chyanne Haugen 2021-10-23 09:49:40 -07:00
parent 0ffa756930
commit 9be7b9a864
1 changed files with 29 additions and 30 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

59
Luminary099/P34-35_P74-75.agc
View File

@ -34,13 +34,13 @@
# TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74) # TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74)
# MOD NO -1 LOG SECTION -- P32-P35, P72-P75 # MOD NO -1 LOG SECTION -- P32-P35, P72-P75
# MOD BY WHITE, P. DATE: 1 JUNE 67 # MOD BY WHITE.P DATE 1JUNE67
# #
# PURPOSE # PURPOSE
# #
# (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS # (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS
# REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE TRANSFER # REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE TRANSFER
# PHASE INITITATION (TPI) MANEUVER, GIVEN -- # PHASE INITITATION (TPI) MANEUVER, GIVEN -
# (A) TIME OF IGNITION TIG (TPI) OR THE ELEVATION ANGLE (E) OF # (A) TIME OF IGNITION TIG (TPI) OR THE ELEVATION ANGLE (E) OF
# THE ACTIVE/PASSIVE VEHICLE LOS AT TIG (TPI). # THE ACTIVE/PASSIVE VEHICLE LOS AT TIG (TPI).
@ -62,9 +62,9 @@
# #
# ASSUMPTIONS # ASSUMPTIONS
# (1) LM ONLY -- THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF # (1) LM ONLY - THIS PROGRAM IS BASED UPON PREVIOUS COMPLETION OF
# THE CONSTANT DELTA ALTITUDE (CDH) PROGRAM (P33/P73). # THE CONSTANT DELTA ALTITUDE (CDH) PROGRAM (P33/P73).
# THEREFORE -- # THEREFORE -
# (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT # (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT
# BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE # BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE
@ -108,23 +108,23 @@
# (5) THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM. # (5) THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
# (6) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -- # (6) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -
# #
# ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS # ACTIVE VEHICLE FLAG - DESIGNATES THE VEHICLE WHICH IS
# DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH # DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF # CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
# EACH RENDEZVOUS PRE-THRUSTING PROGRAM. # EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
# #
# FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS # FINAL FLAG - SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
# SELECTED THE FINAL MANEUVER COMPUTATION CYCLE. # SELECTED THE FINAL MANEUVER COMPUTATION CYCLE.
# #
# EXTERNAL DELTA V FLAG -- DESIGNATES THE TYPE OF STEERING # EXTERNAL DELTA V FLAG - DESIGNATES THE TYPE OF STEERING
# REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE THRUSTING # REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE THRUSTING
# PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM. # PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM.
# #
# (7) ONCE THE PARAMETERS REQUIRED FOR COMPUTATION OF THE MANEUVER # (7) ONCE THE PARAMETWRS REQUIRED FOR COMPUTATION OF THE MANEUVER
# HAVE BEEN COMPLETELY SPECIFIED, THE VALUE OF THE ACTIVE # HAVE BEEN COMPLETELY SPECIFIED, THE VALUE OF THE ACTIVE
# VEHICLE CENTRAL ANGLE OF TRANSFER IS COMPUTED AND STURED. # VEHICLE CENTRAL ANGLE OF TRANSFER IS COMPUTED AND STORED.
# THIS NUMBER WILL BE AVAILABLE FOR DISPLAY TO THE ASTRONAUT # THIS NUMBER WILL BE AVAILABLE FOR DISPLAY TO THE ASTRONAUT
# THROUGH THE USE OF V06N52. # THROUGH THE USE OF V06N52.
# #
@ -132,10 +132,10 @@
# CENTRAL ANGLE OF TRANSFER OF THE ACTIVE VEHICLE IS NOT WITHIN # CENTRAL ANGLE OF TRANSFER OF THE ACTIVE VEHICLE IS NOT WITHIN
# Page 660 # Page 660
# 170 TO 190 DEGREES. IF THE ANGLE IS WITHIN THIS ZONE THE # 170 TO 190 DEGREES. IF THE ANGLE IS WITHIN THIS ZONE THE
# ASTRONAUT SHOULD REASSES THE INPUT TARGETING PARAMETERS BASED # ASTRONAUT SHOULD REASSESS THE INPUT TARGETING PARAMETERS BASED
# UPON DELTA V AND EXPECTED MANEUVER TIME. # UPON DELTA V AND EXPECTED MANEUVER TIME.
# #
# (8) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -- # (8) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -
# #
# P34 IF THIS VEHICLE IS ACTIVE VEHICLE. # P34 IF THIS VEHICLE IS ACTIVE VEHICLE.
# #
@ -159,8 +159,8 @@
# (5) POSTTPI PERIGEE ALTITUDE AFTER THE TPI MANEUVER # (5) POSTTPI PERIGEE ALTITUDE AFTER THE TPI MANEUVER
# (6) DELVTPI MAGNITUDE OF DELTA V AT TPI # (6) DELVTPI MAGNITUDE OF DELTA V AT TPI
# (7) DELVTPF MAGNITUDE OF DELTA V AT INTERCEPT # (7) DELVTPF MAGNITUDE OF DELTA V AT INTERCEPT
# (8) DVLOS DELTA VELOCITY AT TPI -- LINE OF SIGHT # (8) DVLOS DELTA VELOCITY AT TPI - LINE OF SIGHT
# (9) DELVLVC DELTA VELOCITY AT TPI -- LOCAL VERTICAL COORDINATES # (9) DELVLVC DELTA VELOCITY AT TPI - LOCAL VERTICAL COORDINATES
# #
# DOWNLINK # DOWNLINK
# #
@ -169,7 +169,7 @@
# (3) ELEV DESIRED LOS ANGLE AT TPI # (3) ELEV DESIRED LOS ANGLE AT TPI
# (4) CENTANG ORBITAL CENTRAL ANGLE OF THE PASSIVE VEHICLE DURING # (4) CENTANG ORBITAL CENTRAL ANGLE OF THE PASSIVE VEHICLE DURING
# TRANSFER FROM TPI TO TIME OF INTERCEPT # TRANSFER FROM TPI TO TIME OF INTERCEPT
# (5) DELVEET3 DELTA VELOCITY AT TPI -- REFERENCE COORDINATES # (5) DELVEET3 DELTA VELOCITY AT TPI - REFERENCE COORDINATES
# (6) TPASS4 TIME OF INTERCEPT # (6) TPASS4 TIME OF INTERCEPT
# #
# COMMUNICATION TO THRUSTING PROGRAMS # COMMUNICATION TO THRUSTING PROGRAMS
@ -323,14 +323,14 @@ P34/P74E TC INTPRET
# Page 664 # Page 664
# RENDEZVOUS MID-COURSE MANEUVER PROGRAMS (P35 AND P75) # RENDEZVOUS MID-COURSE MANEUVER PROGRAMS (P35 AND P75)
# MOD NO -1 LOG SECTION -- P32-P35, P72-P75 # MOD NO -1 LOG SECTION - P32-P35, P72-P75
# MOD BY WHITE, P. DATE: 1 JUNE 67 # MOD BY WHITE.P DATE 1JUNE67
# #
# PURPOSE # PURPOSE
# #
# (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS # (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS
# REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE NEXT # REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE NEXT
# MID-COURSE CORRECTION OF THE TRANSFER PHASE OF AN ACTIVE # MIDCOURSE CORRECTION OF THE TRANSFER PHASE OF AN ACTIVE
# VEHICLE RENDEZVOUS. # VEHICLE RENDEZVOUS.
# #
# (2) TO DISPLAY TO THE ASTRONAUT AND THE GROUND CERTAIN DEPENDENT # (2) TO DISPLAY TO THE ASTRONAUT AND THE GROUND CERTAIN DEPENDENT
@ -354,17 +354,17 @@ P34/P74E TC INTPRET
# RENDEZVOUS TRACKING MARK COUNTER IS ZEROED BY THE SELECTION OF # RENDEZVOUS TRACKING MARK COUNTER IS ZEROED BY THE SELECTION OF
# P20 AND AFTER EACH THRUSTING MANEUVER. # P20 AND AFTER EACH THRUSTING MANEUVER.
# #
# (4) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -- # (4) THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -
# #
# THE ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS # ACTIVE VEHICLE FLAG - DESIGNATES THE VEHICLE WHICH IS
# DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH # DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF # CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
# EACH RENDEZVOUS PRE-THRUSTING PROGRAM. # EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
# #
# FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS # FINAL FLAG - SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
# SELECTED THE FINAL MANEUVER COMPUTATION CYCLE. # SELECTED THE FINAL MANEUVER COMPUTATION CYCLE.
# #
# EXTERNAL DELTA V FLAG -- DESIGNATES THE TYPE OF STEERING # EXTERNAL DELTA V FLAG - DESIGNATES THE TYPE OF STEERING
# REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE THRUSTING # REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE THRUSTING
# PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM. # PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM.
# #
@ -385,7 +385,7 @@ P34/P74E TC INTPRET
# ASTRONAUT SHOULD REASSESS THE INPUT TARGETING PARAMETERS BASED # ASTRONAUT SHOULD REASSESS THE INPUT TARGETING PARAMETERS BASED
# UPON DELTA V AND EXPECTED MANEUVER TIME. # UPON DELTA V AND EXPECTED MANEUVER TIME.
# #
# (7) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -- # (7) THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -
# #
# P35 IF THIS VEHICLE IS ACTIVE VEHICLE. # P35 IF THIS VEHICLE IS ACTIVE VEHICLE.
# #
@ -393,28 +393,27 @@ P34/P74E TC INTPRET
# #
# INPUT # INPUT
# #
# (1) TPASS4 TIME OF INTERCEPT -- SAVED FROM P34/P74 # (1) TPASS4 TIME OF INTERCEPT - SAVED FROM P34/P74
# #
# OUTPUT # OUTPUT
# #
# (1) TRKMKCNT NUMBER OF MARKS # (1) TRKMKCNT NUMBER OF MARKS
# (2) TTOGO TIME TO GO # (2) TTOGO TIME TO GO
# (3) +MGA MIDOLF GIMBAL ANGLE # (3) +MGA MIDDLE GIMBAL ANGLE
# (4) DVLOS DELTA VELOCITY AT MID -- LINE OF SIGHT # (4) DVLOS DELTA VELOCITY AT MID - LINE OF SIGHT
# (5) DELVLVC DELTA VELOCITY AT MID -- LOCAL VERTICAL COORDINATES # (5) DELVLVC DELTA VELOCITY AT MID - LOCAL VERTICAL COORDINATES
# #
# DOWNLINK # DOWNLINK
# #
# (1) TIG TIME OF THE TPM MANEUVER # (1) TIG TIME OF THE TPM MANEUVER
# (2) DELVEET3 DELTA VELOCITY AT TPM -- REFERENCE COORDINATES # (2) DELVEET3 DELTA VELOCITY AT TPM - REFERENCE COORDINATES
# (3) TPASS4 TIME OF INTERCEPT # (3) TPASS4 TIME OF INTERCEPT
#
# COMMUNICATION TO THRUSTING PROGRAMS # COMMUNICATION TO THRUSTING PROGRAMS
# #
# (1) TIG TIME OF THE TPM MANEUVER # (1) TIG TIME OF THE TPM MANEUVER
# (2) RTARG OFFSET TARGET POSITION # (2) RTARG OFFSET TARGET POSITION
# (3) TPASS4 TIME OF INTERCEPT # (3) TPASS4 TIME OF INTERCEPT
# (4) XDELVFLG RESET TO INDICATE LAMBERT (AIMPOINT) VG COMPUTATION. # (4) XDELVFLG RESET TO INDICATE LAMBERT (AIMPOINT) VG COMPUTATION
# #
# SUBROUTINES USED # SUBROUTINES USED
# #