# Copyright: Public domain. # Filename: R31.agc # Purpose: Part of the source code for Luminary 1A build 099. # It is part of the source code for the Lunar Module's (LM) # Apollo Guidance Computer (AGC), for Apollo 11. # Assembler: yaYUL # Contact: Ron Burkey . # Website: www.ibiblio.org/apollo. # Pages: 703-708 # Mod history: 2009-05-19 RSB Adapted from the corresponding # Luminary131 file, using page # images from Luminary 1A. # # This source code has been transcribed or otherwise adapted from # digitized images of a hardcopy from the MIT Museum. The digitization # was performed by Paul Fjeld, and arranged for by Deborah Douglas of # the Museum. Many thanks to both. The images (with suitable reduction # in storage size and consequent reduction in image quality as well) are # available online at www.ibiblio.org/apollo. If for some reason you # find that the images are illegible, contact me at info@sandroid.org # about getting access to the (much) higher-quality images which Paul # actually created. # # Notations on the hardcopy document read, in part: # # Assemble revision 001 of AGC program LMY99 by NASA 2021112-061 # 16:27 JULY 14, 1969 # Page 703 BANK 40 SETLOC R31LOC BANK COUNT* $$/R31 R31CALL CAF PRIO3 TC FINDVAC EBANK= SUBEXIT 2CADR V83CALL DSPDELAY TC FIXDELAY DEC 100 CA EXTVBACT MASK BIT12 EXTEND BZF DSPDELAY CAF PRIO5 TC NOVAC EBANK= TSTRT 2CADR DISPN5X TCF TASKOVER BANK 37 SETLOC R31 BANK COUNT* $$/R31 DISPN5X CAF V16N54 TC BANKCALL CADR GOMARKF TC B5OFF TC B5OFF TCF DISPN5X V83CALL CS FLAGWRD7 # TEST AVERAGE G FLAG MASK AVEGFBIT EXTEND BZF MUNG? # ON - TEST MUNFLAG CS FLAGWRD8 MASK SURFFBIT EXTEND BZF ONEBASE # ON SURFACE - BYPASS LEMPREC TC INTPRET # EXTRAPOLATE BOTH STATE VECTORS RTB # Page 704 LOADTIME STCALL TDEC1 LEMPREC # PRECISION BASE VECTOR FOR LM VLOAD RATT1 STOVL BASETHP VATT1 STODL BASETHV TAT DOCMBASE STORE BASETIME # PRECISION BASE VECTOR FOR CM STCALL TDEC1 CSMPREC VLOAD RATT1 STOVL BASEOTP VATT1 STORE BASEOTV EXIT REV83 CS FLAGWRD7 MASK AVEGFBIT EXTEND BZF GETRVN # IF AVEGFLAG SET, USE RN,VN CS FLAGWRD8 MASK SURFFBIT EXTEND BZF R31SURF # IF ON SURFACE,USE LEMAREC TC INTPRET # DO CONIC EXTRAPOLATION FOR BOTH VEHICLES RTB LOADTIME STCALL TDEC1 INTSTALL VLOAD CLEAR BASETHP MOONFLAG STOVL RCV BASETHV STODL VCV BASETIME BOF SET # GET APPROPRIATE MOONFLAG SETTING MOONTHIS +2 MOONFLAG SET INTYPFLG # CONIC EXTRAP. STCALL TET INTEGRVS # INTEGRATION --- AT LAST--- OTHCONIC VLOAD # Page 705 RATT STOVL RONE VATT STCALL VONE # GET SET FOR CONIC EXTRAP.,OTHER. INTSTALL SET DLOAD INTYPFLG TAT OTHINT STORE TDEC1 VLOAD CLEAR BASEOTP MOONFLAG STOVL RCV BASEOTV STODL VCV BASETIME BOF SET MOONTHIS +2 MOONFLAG STCALL TET INTEGRVS COMPDISP VLOAD VSU RATT RONE RTB PDDL NORMUNX1 # UNIT(RANGE) TO PD 0-5 36D SL* # RESCALE AFTER NORMUNIT 0,1 STOVL RANGE # SCALED 2(29)M VATT VSU DOT # (VCM- VLM).UNIT(LOS). PD=0 VONE SL1 # SCALED 2(7)M/CS STOVL RRATE RONE UNIT PDVL # UNIT(R) TO PD 0-5 UNITZ CALL CDU*NBSM VXM PUSH # UNIT (Z)/4 TO PD 6-11 REFSMMAT VPROJ VSL2 # UNIT(P)=UNIT(UZ -(UZ)PROJ(UR)) 0D BVSU UNIT 6D PDVL VXV # UNIT(P) TO PD 12-17 0D # UNIT(RL) VONE # Page 706 VXV DOT # (UR * VL)*UR . U(P) 0D 12D PDVL # SIGN TO 12-13 , LOAD U(P) DOT SIGN 6D 12D SL2 ACOS # ARCCOS(UP.UZ(SIGN)) STOVL RTHETA 0D DOT BPL # IF UR.UZ NEG, 6D # RTHETA = 1 - RTHETA +5 DLOAD DSU DPPOSMAX RTHETA STORE RTHETA EXIT CA BIT5 MASK EXTVBACT EXTEND # IF ANSWERED, BZF ENDEXT # TERMINATE CS EXTVBACT MASK BIT12 ADS EXTVBACT # SET BIT 12 TCF REV83 # AND START AGAIN. GETRVN CA PRIO22 # INHIBIT SERVICER TC PRIOCHNG TC INTPRET VLOAD SETPD RN # LM STATE VECTOR IN RN,VN 0 STOVL RONE VN STOVL VONE # LOAD R(CSM),V(CSM) IN CASE MUNFLAG SET V(CSM) # (TO INSURE TIME COMPATABILITY) PDVL PDDL R(CSM) PIPTIME EXIT CA PRIO3 TC PRIOCHNG TC INTPRET BOFF VLOAD MUNFLAG GETRVN2 # IF MUNFLAG RESET, DO CM DELTA PRECISION # Page 707 VXM VSR4 # CHANGE TO REFERENCE SYSTEM AND RESCALE REFSMMAT PDVL # R TO PD 0-5 VXM VSL1 REFSMMAT PUSH SETPD # V TO PD 5-11 0 GOTO COMPDISP GETRVN2 CALL INTSTALL CLEAR GOTO INTYPFLG # PREC EXTRAP FOR OTHER OTHINT R31SURF TC INTPRET RTB # LM IS ON SURFACE, SO PRECISION LOADTIME # INTEGRATION USES PLANETARY INERTIAL STCALL TDEC1 # ORIENTATION SUBROUTINE LEMPREC GOTO # DO CSM CONIC OTHCONIC MUNG? CS FLAGWRD6 MASK MUNFLBIT EXTEND BZF GETRVN # IF MUNFLAG SET, CSM BASE NOT NEEDED ONEBASE TC INTPRET # GET CSM BASE VECTOR RTB GOTO LOADTIME DOCMBASE V16N54 VN 1654 # Page 708 (empty page)