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Proof P34-35_P74-75 #615 (pg: 0658-0667) #834

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Proof P34-35_P74-75 #615 (pg: 0658-0667) #834

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b4ed0f9
Poof read and fixed minor typos
crhaugen Oct 5, 2020
aeaf66d
Poof read
crhaugen Oct 9, 2020
13e072e
updating in other branch
crhaugen Oct 9, 2020
7425246
Merge branch 'master' of https://github.com/crhaugen/Apollo-11
crhaugen Oct 9, 2020
d1683c4
updating in other branch
crhaugen Oct 9, 2020
35b8b18
updating in other branch
crhaugen Oct 9, 2020
309ad06
Review changes
wopian Oct 13, 2020
0ffa756
Merge branch 'chrislgarry:master' into master
crhaugen Oct 17, 2021
9be7b9a
checked pages 0658-0667
crhaugen Oct 23, 2021
aaec83b
Merge branch 'chrislgarry:master' into Proof-1
crhaugen Oct 26, 2021
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59 changes: 29 additions & 30 deletions Luminary099/P34-35_P74-75.agc
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Original file line number Diff line number Diff line change
Expand Up @@ -34,13 +34,13 @@
# TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74)

# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
# MOD BY WHITE, P. DATE: 1 JUNE 67
# MOD BY WHITE.P DATE 1JUNE67
#
# PURPOSE
#
# (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS
# 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
# THE ACTIVE/PASSIVE VEHICLE LOS AT TIG (TPI).
Expand All @@ -62,9 +62,9 @@
#
# 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).
# THEREFORE --
# THEREFORE -

# (A) AT A SELECTED TPI TIME (NOW IN STORAGE) THE LINE OF SIGHT
# BETWEEN THE ACTIVE AND PASSIVE VEHICLES WAS SELECTED TO BE
Expand Down Expand Up @@ -108,34 +108,34 @@

# (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
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
# 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.
#
# 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
# 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
# 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
# THROUGH THE USE OF V06N52.
#
# THE ASTRONAUT WILL CALL THIS DISPLAY TO VERIFY THAT THE
# CENTRAL ANGLE OF TRANSFER OF THE ACTIVE VEHICLE IS NOT WITHIN
# Page 660
# 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.
#
# (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.
#
Expand All @@ -159,8 +159,8 @@
# (5) POSTTPI PERIGEE ALTITUDE AFTER THE TPI MANEUVER
# (6) DELVTPI MAGNITUDE OF DELTA V AT TPI
# (7) DELVTPF MAGNITUDE OF DELTA V AT INTERCEPT
# (8) DVLOS DELTA VELOCITY AT TPI -- LINE OF SIGHT
# (9) DELVLVC DELTA VELOCITY AT TPI -- LOCAL VERTICAL COORDINATES
# (8) DVLOS DELTA VELOCITY AT TPI - LINE OF SIGHT
# (9) DELVLVC DELTA VELOCITY AT TPI - LOCAL VERTICAL COORDINATES
#
# DOWNLINK
#
Expand All @@ -169,7 +169,7 @@
# (3) ELEV DESIRED LOS ANGLE AT TPI
# (4) CENTANG ORBITAL CENTRAL ANGLE OF THE PASSIVE VEHICLE DURING
# 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
#
# COMMUNICATION TO THRUSTING PROGRAMS
Expand Down Expand Up @@ -323,14 +323,14 @@ P34/P74E TC INTPRET
# Page 664
# RENDEZVOUS MID-COURSE MANEUVER PROGRAMS (P35 AND P75)

# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
# MOD BY WHITE, P. DATE: 1 JUNE 67
# MOD NO -1 LOG SECTION - P32-P35, P72-P75
# MOD BY WHITE.P DATE 1JUNE67
#
# PURPOSE
#
# (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS
# 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.
#
# (2) TO DISPLAY TO THE ASTRONAUT AND THE GROUND CERTAIN DEPENDENT
Expand All @@ -354,17 +354,17 @@ P34/P74E TC INTPRET
# RENDEZVOUS TRACKING MARK COUNTER IS ZEROED BY THE SELECTION OF
# 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
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
# 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.
#
# 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
# PROGRAM SELECTED AFTER COMPLETION OF THIS PROGRAM.
#
Expand All @@ -385,36 +385,35 @@ P34/P74E TC INTPRET
# ASTRONAUT SHOULD REASSESS THE INPUT TARGETING PARAMETERS BASED
# 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.
#
# P75 IF THIS VEHICLE IS PASSIVE VEHICLE.
#
# INPUT
#
# (1) TPASS4 TIME OF INTERCEPT -- SAVED FROM P34/P74
# (1) TPASS4 TIME OF INTERCEPT - SAVED FROM P34/P74
#
# OUTPUT
#
# (1) TRKMKCNT NUMBER OF MARKS
# (2) TTOGO TIME TO GO
# (3) +MGA MIDOLF GIMBAL ANGLE
# (4) DVLOS DELTA VELOCITY AT MID -- LINE OF SIGHT
# (5) DELVLVC DELTA VELOCITY AT MID -- LOCAL VERTICAL COORDINATES
# (3) +MGA MIDDLE GIMBAL ANGLE
# (4) DVLOS DELTA VELOCITY AT MID - LINE OF SIGHT
# (5) DELVLVC DELTA VELOCITY AT MID - LOCAL VERTICAL COORDINATES
#
# DOWNLINK
#
# (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
#
# COMMUNICATION TO THRUSTING PROGRAMS
#
# (1) TIG TIME OF THE TPM MANEUVER
# (2) RTARG OFFSET TARGET POSITION
# (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
#
Expand Down