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