From 717a643fdd143c75189aa643a3f87fdca3911102 Mon Sep 17 00:00:00 2001 From: =?UTF-8?q?K=C3=B3kai=20P=C3=A9ter?= Date: Fri, 6 Nov 2020 19:03:32 +0000 Subject: [PATCH] =?UTF-8?q?Proof=20R30=20(#626)=20Page:=200712=E2=80=94072?= =?UTF-8?q?2=20(#706)?= MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit * Proof R30 (#626) Page: 0712—0722 Signed-off-by: Kokan * Review comments fixed Co-authored-by: James Harris Signed-off-by: Kokan Co-authored-by: James Harris --- Luminary099/R30.agc | 155 ++++++++++++++++++++++---------------------- 1 file changed, 77 insertions(+), 78 deletions(-) diff --git a/Luminary099/R30.agc b/Luminary099/R30.agc index fbc9f66..0240b5f 100644 --- a/Luminary099/R30.agc +++ b/Luminary099/R30.agc @@ -40,51 +40,51 @@ # USED THROUGHOUT. CALCULATE AND DISPLAY ORBITAL PARAMETERS # # 1. IF AVERAGE G IS OFF: -# FLASH DISPLAY V04N06. R2 INDICATES WHICH SHIP'S STATE VECTOR IS -# TO BE UPDATED. INITIAL CHOICE IS THIS SHIP (R2=1). ASTRONAUT -# CAN CHANGE TO OTHER SHIP BY V22E XE. WHERE X IS NOT EQ 1. +# FLASH DISPLAY V04N06. R2 INDICATES WHICH SHIP'S STATE VECTOR IS +# TO BE UPDATED. INITIAL CHOICE IS THIS SHIP (R2=1). ASTRONAUT +# CAN CHANGE TO OTHER SHIP BY V22EXE, WHERE X NOT EQ 1. # SELECTED STATE VECTOR UPDATED BY THISPREC (OTHPREC). # CALLS SR30.1 (WHICH CALLS TFFCONMU + TFFRP/RA) TO CALCULATE -# RPER (PERIGEE RADIUS), RAPO (APOGEE RADIUS), HPER (PERIGEE -# HEIGHT ABOVE LAUNCH PAD OR LUNAR LANDING SITE), HARD (APOGEE -# HEIGHT AS ABOVE), TPER (TIME TO PERIGEE), TFF (TIME TO -# INTERSECT 300 KFT ABOVE PAD OR 35KFT ABOVE LANDING SITE). -# FLASH MONITOR V16N44 (HAPO, HPER, TFF). TFF IS -59M59S IF IT WAS -# NOT COMPUTABLE, OTHERWISE IT INCREMENTS ONCE PER SECOND. -# ASTRONAUT HAS OPTION TO MONITOR TPER BY KEYING IN N 32 E. -# DISPLAY IS IN HMS, IS NEGATIVE (AS WAS TFF), AND INCREMENTS -# ONCE PER SECOND ONLY IF TFF DISPLAY WAS -59M59S. -# 2. IF AVERAGE G IS ON: -# CALLS SR30.1 APPROX EVERY TWO SECS. STATE VECTOR IS ALWAYS -# FOR THIS VEHICLE. V82 DOES NOT DISTURB STATE VECTOR. RESULTS -# OF SR30.1 ARE RAPO, RPER, HAPO, HPER, TPER, TFF. -# FLASH MONITOR V16N44 (HAPO, HPER, TFF). -# ADDENDUM: HAPO AND HPER SHOULD BE CHANGED TO READ HAPOX AND HPERX IN THE -# ABOVE REMARKS. +# RPER (PERIGEE RADIUS), RAPO (APOGEE RADIUS), HPER (PERIGEE +# HEIGHT ABOVE LAUNCH PAD OR LUNAR LANDING SITE), HARD (APOGEE +# HEIGHT AS ABOVE), TPER (TIME TO PERIGEE), TFF (TIME TO +# INTERSECT 300 KFT ABOVE PAD OR 35KFT ABOVE LANDING SITE). +# FLASH MONITOR V16N44 (HAPO, HPER, TFF).TFF IS -59M59S IF IT WAS +# NOT COMPUTABLE, OTHERWISE IT INCREMENTS ONCE PER SECOND. +# ASTRONAUT HAS OPTION TO MONITOR TPER BY KEYING IN N 32 E. +# DISPLAY IS IN HMS, IS NEGATIVE (AS WAS TFF), AND INCREMENTS +# ONCE PER SECOND ONLY IF TFF DISPLAY WAS -59M59S. # -# CALLING SEQUENCE: VERB 82 ENTER. +# 2. IF AVERAGE G IS ON: +# CALLS SR30.1 APPROX EVERY TWO SECS. STATE VECTOR IS ALWAYS +# FOR THIS VEHICLE. V82 DOES NOT DISTURB STATE VECTOR. RESULTS +# OF SR30.1 ARE RAPO, RPER, HAPO, HPER, TPER, TFF. +# FLASH MONITOR V16N44 (HAPO, HPER, TFF). +# ADDENDUM: HAPO AND HPER SHOULD BE CHANGED TO READ HAPOX AND HPERX IN THE +# ABOVE REMARKS. # -# SUBROUTINES CALLED: SR30.1, GOXDSPF -# MAYBE -- THISPREC, OTHPREC, LOADTIME, DELRSPL +# CALLING SEQUENCE: VERB 82 ENTER. # +# SUBROUTINES CALLED: SR30.1, GOXDSPF +# MAYBE - THISPREC , OTHPREC, LOADTIME, DELRSPL # NORMAL EXIT MODES: TC ENDEXT # # ALARMS: NONE # -# OUTPUT: HAPOX (-29) M -# HPERX (-29) M -# RAPO (-29) M EARTH +# OUTPUT: HAPOX (-29) M +# HPERX (-29) M +# RAPO (-29) M EARTH # (-27) M MOON -# RPER (-29) M EARTH +# RPER (-29) M EARTH # (-27) M MOON -# TFF (-28) CS CONTAINS NEGATIVE QUANTITY -# -TPER (-28) CS CONTAINS NEGATIVE QUANTITY -# +# TFF (-28) CS CONTAINS NEGATIVE QUANTITY +# -TPER (-28) CS CONTAINS NEGATIVE QUANTITY # Page 713 -# ERASABLE INITIALIZATION REQUIRED: STATE VECTOR. # -# DEBRIS: QPRET, RONE, VONE, TFF/RTMU, HPERMIN, RPADTEM, V82EMFLG. -# MAYBE: TSTART82, V82FLAGS, TDEC1. +# ERASABLE INITIALIZATION REQUIRED: STATE VECTOR. +# +# DEBRIS: QPRET, RONE, VONE,TFF/RTMU, HPERMIN, RPADTEM, V82EMFLG. +# MAYBE: TSTART82, V82FLAGS, TDEC1. EBANK= HAPOX BANK 31 @@ -108,8 +108,8 @@ V82GOFF EXIT # ALLOW ASTRONAUT TO SELECT VEHICLE CADR GOXDSPF TC ENDEXT # TERMINATE TC +2 # PROCEED - TC -5 # DATA IN. OPTION1+1 = 1 FOR THIS VEHICLE - # UNEQ 1 FOR OTHER VEHICLE + TC -5 # DATA IN. OPTION1+1 = 1 FOR THIS VEHICLE. + # UNEQ 1 FOR OTHER VEHICLE. CAF BIT4 # 80 MS TC WAITLIST EBANK= TFF @@ -140,9 +140,9 @@ V82STALL CAF THREE # STALL IN THIS LOOP AND WITHOLD V 16 N 44 FLAGGON CAF V16N44 # MONITOR HAPO,HPER,TFF. TC BANKCALL CADR GOXDSPF - TC B5OFF # TERM. THIS TELLS TICKTEST TO KILL ITSELF - TC B5OFF # PROCEED. DITTO - TC V82GOFLP # RECYCLE. RECOMPUTE STATE VECT + DISPLAY + TC B5OFF # TERM THIS TELLS TICKTEST TO KILL ITSELF + TC B5OFF # PROCEED DITTO + TC V82GOFLP # RECYCLE RECOMPUTE STATE VECT + DISPLAY OPTIONVN VN 412 V16N44 VN 1644 @@ -162,16 +162,16 @@ OTHSHIP TC INTPRET CALL # CALL STATE VECTOR UPDATE FOR OTHER SHIP. OTHPREC BOTHSHIP VLOAD # MOVE RESULTS INTO TFFCONIC STORAGE AREAS - RATT # TO BE CALLED BY SR30.1. - STOVL RONE # RATT AT (-29)M FOR EARTH OR MOON. + RATT # TO BE CALLED BY SR30.1. + STOVL RONE # RATT AT (-29)M FOR EARTH OR MOON VATT - STORE VONE # VATT AT (-7)M/CS FOR EARTH OR MOON + STORE VONE # VATT AT (-7)M/CS FOR EARTH OR MOON DLOAD* - 1/RTMUE,2 # X2 IS 0 FOR EARTH CENTERED STATE VEC - STORE TFF/RTMU # X2 IS 2 FOR MOON + 1/RTMUE,2 # X2 IS 0 FOR EARTH CENTERED STATE VEC + STORE TFF/RTMU # X2 IS 2 FOR MOON DLOAD* # AS LEFT BY THISPREC OR OTHPREC. MINPERE,2 - STORE HPERMIN # TFFRTMU, HPERMIN, AND RPADTEM ARE ALL + STORE HPERMIN # TFFRTMU, HPERMIN AND RPADTEM ARE ALL SLOAD BHIZ # EARTH/MOON PARAMETERS AS SET HERE. X2 EARTHPAD @@ -184,41 +184,41 @@ THISSHIP TC INTPRET GOTO BOTHSHIP -# THE FOLLOWING CONSTANTS ARE PAIRWISE INDEXED. DO NOT SEPARATE PAIRS. +# THE FOLLOWING CONSTANTS ARE PAIRWISE INDEXED. DO NOT SEPARATE PAIRS. MINPERM 2DEC 10668 B-27 # 35 KFT MIN PERIGEE HEIGHT FOR MOON(-27)M MINPERE 2DEC 91440 B-29 # 300 KFT (-29)M FOR EARTH -EARTHPAD DLOAD CLRGO # PAD 37-B RADIUS. SCALED AT (-29)M +EARTHPAD DLOAD CLRGO # PAD 37-B RADIUS. SCALED AT (-29)M. RPAD - V82EMFLG # INDICATE EARTH SCALING FOR SR30.1 + V82EMFLG # INDICATE EARTH SCALING FOR SR30.1 BOTHPAD MOONPAD VLOAD ABVAL # COMPUTE MOON PAD RADIUS FROM RLS VECTOR. - RLS # SCALED AT (-27)M + RLS # SCALED AT (-27)M. SET - V82EMFLG # INDICATE MOON SCALILNG FOR SR30.1 + V82EMFLG # INDICATE MOON SCALING FOR SR30.1 BOTHPAD STCALL RPADTEM SR30.1 # CALCULATE ORBITAL PARAMETERS RTB DSU LOADTIME - TSTART82 # PRESENT TIME -- TIME V82GOFF1 BEGAN - STORE TSTART82 # SAVE IT + TSTART82 # PRESENT TIME - TIME V82GOFF1 BEGAN + STORE TSTART82 # SAVE IT DLOAD BZE # SR30.1 SETS -TPER=0 IF HPER L/ - -TPER # HPERMIN (300 OR 35) KFT. + -TPER # HPERMIN (300 OR 35) KFT. TICKTIFF # (-TPER = 0) -TICKTPER DLOAD DAD # (-TPER NON ZERO) TFF WAS NOT COMPUTED. - -TPER # BUT WAS SET TO 59M59S. DON'T DICK TFF, DO - TSTART82 # TICK -TPER. DISPLAY BOTH. +TICKTPER DLOAD DAD # (-TPER NON ZERO) TFF WAS NOT COMPUTED. + -TPER # BUT WAS SET TO 59M59S.DONT TICK TFF, DO + TSTART82 # TICK -TPER. DISPLAY BOTH. STORE -TPER # -TPER CORRECTED FOR TIME SINCE V82GOFF1 - EXIT # BEGAN + EXIT # BEGAN. CAF BIT1 TS V82FLAGS # INFORMS TICKTEST TO INCREMENT ONLY -TPER TC ENDOFJOB -TICKTIFF DLOAD DAD # (-TPER=0) TFF WAS COMPUTED. TICK TFF. - TFF # DO NOT TICK -TPER. DISPLAY TFF, BUT NOT +TICKTIFF DLOAD DAD # (-TPER=0) TFF WAS COMPUTED.TICK TFF. + TFF # DO NOT TICK -TPER.DISPLAY TFF, BUT NOT TSTART82 # -TPER. STORE TFF # TFF CORRECTED FOR TIME SINCE V82GOFF1 EXIT # BEGAN. @@ -232,7 +232,7 @@ TICKTEST CAF BIT5 # THIS WAITLIST PROGRAM PERPETUATES ITSELF CCS A TC DOTICK CAF PRIO25 - TC NOVAC # TERMINATE V 82. CAN'T CALL ENDEXT IN RUPT. + TC NOVAC # TERMINATE V 82.CANT CALL ENDEXT IN RUPT. EBANK= EXTVBACT 2CADR ENDEXT @@ -246,10 +246,10 @@ DOTICK CAF 1SEC # RE-REQUEST TICKTEST. MASK V82FLAGS INDEX A TC +1 - TC TASKOVER # IF NO FLAGBITS SET DONT' CHANGE TFF OR + TC TASKOVER # IF NO FLAGBITS SET DONT CHANGE TFF OR # -TPER, BUT CONTINUE LOOP. - TC TPERTICK # ONLY BIT 1 SET. INCR -TPER BY 1 SEC. -TFFTICK CAF 1SEC # ONLY BIT 2 SET. INCR TFF BY 1 SEC. + TC TPERTICK # ONLY BIT 1 SET. INCR -TPER BY 1 SEC. +TFFTICK CAF 1SEC # ONLY BIT 2 SET. INCR TFF BY 1 SEC. TS L CAF ZERO DAS TFF @@ -261,7 +261,7 @@ TPERTICK CAF 1SEC TC TASKOVER # Page 717 -V82GON EXIT # AVERAGE G ON. USE CURRENT STATE VECTOR +V82GON EXIT # AVERAGE G ON. USE CURRENT STATE VECTOR # FOR ORBITAL PARAMETER CALCULATIONS. CAF PRIO7 # LESS THAN LAMBERT TC FINDVAC # V82GON1 WILL PERFORM ORBIT CALCULATIONS @@ -270,7 +270,7 @@ V82GON EXIT # AVERAGE G ON. USE CURRENT STATE VECTOR RELINT CCS NEWJOB # WITHOLD V16 N44 UNTIL FIRST ORBIT CALC - TC CHANG1 # IS DONE. NOTE: V82GON1 (PRIO7, FINDVAC + TC CHANG1 # IS DONE. NOTE: V82GON1 (PRIO7, FINDVAC # JOB) IS COMPLETED BEFORE V82GON (PRIO7, # NOVAC JOB). V82REDSP CAF V16N44 # MONITOR HAPO, HPER, TFF @@ -283,23 +283,23 @@ V82REDSP CAF V16N44 # MONITOR HAPO, HPER, TFF V82GON1 TC INTPRET # THIS EXEC PROGRAM PERPETUATES ITSELF # ONCE A SEC UNTIL BIT 5 OF EXTVBACT =0. VLOAD GOTO # HOLDS OFF CCS NEWJOB BETWEEN RN AND - RN # VN FETCH SO RN, VN ARE FROM SAME - NEXTLINE # STATE VECTOR UPDATE. -NEXTLINE STOVL RONE # RN AT (-29)M FOR EARTH OR MOON + RN # VN FETCH SO RN , VN ARE FROM SAME + NEXTLINE # STATE VECTOR UPDATE. +NEXTLINE STOVL RONE # RN AT (-29)M FOR EARTH OR MOON VN STORE VONE # VN AT (-7)M/CS FOR EARTH OR MOON BON GOTO MOONTHIS # FLAG INDICATES BODY ABOUT WHICH ORBITAL - MOONGON # CALCULATIONS ARE TO BE PERFORMED. - EARTHGON # IF SET -- MOON, IF RESET --EARTH. + MOONGON # CALCULATIONS ARE TO BE PERFORMED. + EARTHGON # IF SET - MOON , IF RESET - EARTH. MOONGON SET DLOAD - V82EMFLG # FLAG MOON SCALING FOR SR30.1 + V82EMFLG # INDICATE MOON SCALING FOR SR30.1 1/RTMUM # LUNAR PARAMETERS LOADED HERE FOR SR30.1 STODL TFF/RTMU MINPERM STOVL HPERMIN - RLS # SCALED AT (-27)M + RLS # SCALED AT (-27)M. ABVAL GOTO V82GON2 EARTHGON CLEAR DLOAD @@ -319,7 +319,7 @@ V82GON3 CAF BIT5 BZF ENDEXT # YES, TERMINATE VB 82 LOOP CAF 1SEC TC BANKCALL # WAIT ONE SECOND BEFORE REPEATING - CADR DELAYJOB # ORBITAL PARAMETER COMPUTATION. + CADR DELAYJOB # ORBITAL PARAMETER COMPUTATION. TC V82GON1 SPLRET = V82GON3 @@ -433,9 +433,9 @@ STORHAPO STODL HAPOX STORHPER STODL HPERX # STORE (RPER - RPADTEM) INTO HPERX. MPAC +4 DSU BPL # HPERMIN AT (-29)M FOR EARTH, (-27)M MOON - HPERMIN # IF HPER L/ HPERMIN (300 OR 35) KFT, - DOTPER # THEN ZERO INTO -TPER. - DLOAD GOTO # OTHERWISE CALCULATE TPER. + HPERMIN # IF HPER L/ HPERMIN (300 OR 35)KFT, + DOTPER # THEN ZERO INTO -TPER. + DLOAD GOTO # OTHERWISE CALCULATE TPER. HI6ZEROS SKIPTPER DOTPER DLOAD CALL @@ -447,19 +447,18 @@ SKIPTPER STODL -TPER DAD CALL RPADTEM # RPADTEM AT (-29)M FOR EARTH, (-27)M MOON CALCTFF # GIVES 59M59S FOR TFF IF HPER G/ - DCOMP # HPERMIN + RPADTEM. (TPER WAS NON ZERO) + DCOMP # HPERMIN + RPADTEM. (TPER WAS NON ZERO) STCALL TFF # OTHERWISE COMPUTES TFF. (GOTO) S2 MAXCHK DSU BPL # IF C(MPAC) > 9999.9 NM. MPAC = 9999.9 NM. MAXNM - +3 # OTHERWISE C(MPAC) - B(MPAC). + +3 # OTHERWISE C(MPAC) = B(MPAC). DAD RVQ MAXNM - +3 DLOAD RVQ # (USED BY P30 -- P37 ALSO) + +3 DLOAD RVQ # (USED BY P30 - P37 ALSO) MAXNM MAXNM 2OCT 0106505603 # Page 722 (empty page) -