M -------------------- ASTR 1 /VZ 8504y * VARIABILI * . EC(9) = ECCENTRICITA' ORBITE G = GIORNI DI INTERVALLO  IX = FATTORE DI INGRANDIM.TO MA(9) = MASSE PIANETI\ N = NUMERO POSIZIONE ATT.LE NP = NUMERO MAX POSIZ.MEMOR.( P = NUMERO ORDINALE PIANETA PR(9) = PERIODI ROTAZ. PIANETI) P$(9) = NOMI PIANETI PR(9) = PERIODI ROTAZ. PIANETIJ2 R(9) = ANG.PREC.POSIZ.PIANETA R$ = RISPOSTA GENER.SU INPUT7 RG(9) = RAGGI MAX ORBITE PIAN. RP(9) = RAGGI MIN. ORBITE PIAN.F T(9,100,2) = POSIZIONI PIANETI " > 1:X 2:Y&G" > NUMERO POSIZIONE (N) > NUMERO PIANETAMK V = VELOCITA' CORPO ERRANTEP X = TABULAZ. ORIZZ. HR XC = TAB. ORIZZ. CORPO ERR.Q XV = VECCHIE COORD. CORPO ERU Y = TABULAZ. VERTIC, HR YC = TAB. VERT. CORPO ERR.TE<V YV = VECCHIE COORD. CORPO ERUZ I3 8: I,"": \ 1,"G 0: COL 0,1: COL 1,2: ? CHR$(142)"(13): 300 ------------- ORBITE SIST.SOLARE . MERCURY,57.9,88,7,0.206,4892, .053,,VENUS,108.2,224.7,3.4J 0.007,12112,0.815,0,EARTH,149.6 ,365.26,0,0.017,12756,1,1 MARS,227.9,687,1.9,.093,6787, .108,2,JUPITER,778,4331.98,1.3 .048,142800,317.9,15,SATURN, 1427,10760.55,2.5,.056,120000,95.22" 15,URANUS,2870,30685.49,0.8,.047 ,51800,14.6,5,NEPTUNE,4496k 60194.84,1.8,0.009,49500,17.2, 2,PLUTO,5946,90474.90,17.2,0.25 3000,0.0017,1,HALLEY COMETH, 2685,27772.85,162.1,0.9673,,, :, ------------------CARIC. VETTORI .. 0,1: 4,1: 1,2=1 1,1: ,160,100,30,,,,, 120: I0 2: 160,100{2 30;I120: 160,100: : ,14,16,"SVS SOFTWARE"3 T(9,100,2)6 P0 9: P$(P),RG(P),PR(P) ,IN(P),EC(P),DI(P),MA(P),SA(P): :8 ----------- CALC. SEMIASSI MIN. .<: P0 9: RP(P)(RG(P)2(EC( P)RG(P))2): F@ 0,1r ------------ MASTER VISUALIZZAZ. . 1,2: 5: 1,750,3 0,1: 4,1: 0,4,5: ,5,3,(14)"RG. 1" ,5,4,"": ,15,10,""N ,5,12,"1 - RBITS VIEWING": ,5,13,"2 - LANETS DIMENSIONS" ,5,14,"3 - RBITAL COURSES": ,5,15,"4 - LANETS DATA" ,5,16,"5 - OREIGN BODY ORBIT" : ,5,18,"6 - XIT"  ,5,22,"UN  1 - OFTWARE ESET": ,5,23,"TOP"2 R$: R$"1" R$"6" 500b (R$) 1000,1500,3000,2000, 3000,9000h: ----------------- ORBITE . 0,1: 1,2,4: 4,7,3 "": 2);"Ҡ͠Ӡ": 9 ,9,22,"( F2 = TANDARD DATA)" : ,0,6,""V 2,"30"(13)"1"(13): "CLIPTIC INCLINATION"; IE: IE90 IE0 1020 ,9,22," ": ,0,8,"": "OOM FACTOR";IX: IX0 IX1:  -------------- VISUALIZZAZIONE .4 1,1: 2,(0)n 1,8,5: ,310,8 270,8: 40;90IE: 270,8  ,270,8,30,,90,90IE1: IE0 1035: ,299,9  ,28,1,"INCL.": ,28,2, (IE): ,34,24,"X"(IX):SC(RG(8)RP(8))320IX: ,0,24 ,"SCALE= 1 :"(SC1000000)" KM."f8 --------------- VISUAL. ORBITE .9 ,160,101 160,100: 1,2 : 0,60: ,18,2,"SUN": I1 600: : 0,160,99 0,60: 0,18,2," "= P0 9: 1,8,5: ,0, 0,P$(P)" ": 1,2k?RY(((RG(P)RP(P))2)2((RG(P) RP(P))2)2)SCIE90: RY100 1100B ,160,100,(RG(P)RP(P))2SC, RY,,,IN(P)(90IE)90: 1,8,5L: ,0,0,"* SOLAR SYSTEM *", 1: (142): R$: 400! ------------ DIMENSIONI PIANETI .4 0,1: 4,7,3V 1,1: ,9,0,"PLANETS SIZES"SCDI(5)150: ,0,24,"SCALE= 1 : " (SC)" KM.": X0 P1 9: 1,P1,5: XX30 : ,31,22,P$(P)" "  ,30,24,(DI(P))" ": ,X,100,DI(P)2SC: M  ,31,22," ": ,30, 24," ": R$: 400S :  -------------- VISUALIZZ. DATI . : 0,1: 4,7,5: ,4,0,"ӠΒ"  (13);"( = EXT Œ = ND)"-! ,0,4,(27)"T": P0 9: 82);"AME:"; :Y! ----------- CONV. MIN.->MAIUSC. .!P$"": K1 (P$(P)): P0$ (P$(P),K,1): P$P$((P0$ )32)! P0$(65) P0$(90) (P$,K,1)P0$!: 39(P$(P)));""; P$-": 2);"RBIT' GREATER RAY (M):",RG(P): F"K(((RP(P)),2,6))o" 2);"RBIT' LOWER RAY (M):",K: " 2);"EVOLUTION TIME (GG):",PR(P): "  2);"RBIT INCLINATION (DEG):",IN(P): " 2);"RBIT EXCENTRICITY:",EC(P): #  2);"QUATOR DIAMETER (M):",DI(P): J#* 2);"ASS (ARTH=1):",, MA(P): w#/ 2);"UMBER OF SATELLITS:", SA(P)#4 R$: R$"E" P10: I1 4: : I,P#> (27)"N": 400# ------------ MOVIMENTI ORBITALI .$ 0,1: 1,2,4: 4,7,3?$ "": 1);"Ҡ͠Ӡ"}$ R$"3" 2,"90"(13)"3"(13)"20"(13)"15"(13)$ R$"5" K2$"90"(13)"6"(13)"20"(13)"40"(13) % R$"5" 2,K2$"130,120"(13)(13)".5"(13)"80"(13)"270"(13)>% ,9,23,"( 2 = EFAULT DATA)" : ,0,4,""z% "CLIPTIC INCLINATION";IE: IE90 IE0 3020% ,9,23," " : ,0,6,""% "OOM FACTOR";IX : IX0 IX1& : "AYS OF INTERVAL";G : G1 3027: Z& "UMBER OF POSITIONS TO BE SHOWN";NP: NP2 NP100 3028 :& ------------- MASCHERA VIDEO .& 4,1: ,12,22, "POSTONS PROCESS": 2,(0)& 1,8,5: ,155,8 135,8.' IE0 3036: ,135 ,8,15,,90,90IE: X2015((0) 135)g' Y2015((1)8): ,135,8 X135,Y8: ,149,9' ,28,1,"NCL.": ,28,2, (IE): ,34,24,"X"(IX)' SCRG(8)160IX: ,0,24,"SCALE= 1 :"(SC)" MKM."( ,0,1,"NTERVAL": ,0,2, (G)" DAYS"5( R$"5" 4000: 3a( ------------- CALCOLO POSIZIONI .z( P0 9: R(P)0: ( ,80,101 80,100: 1,2: 2 0,60: ,18,2,"SUN"( I1 600: : 0,80,99 0,60: ,18,2," ") 1,2: 2,2,1: 3,8,5H) N1 NP: P1 9: R(P)R (P)G365PR(P)w) R(P)359 R(P)R(P)359: 3085) RY(((RG(P)RP(P))2)2((RG(P) RP(P))2)2)SC2IE90) RY100 3090: T(P,N,1) 80: T(P,N,2)0: 3105H* 2,80,100,(RG(P)RP(P))2SC, RY,359R(P)1,359R(P),IN(P)(90IE )90* T(P,N,1)(0): T(P,N,2)(1): N1 T(P,N,2)0 3105* 2,T(P,N1,1),T(P,N1,2) T(P,N,1),T(P,N,2)* ,T(P,N,1),T(P,N,2)*! P+& ,30,22,(NP1N)" ": R$ "5" 4100V++ N: 4: 1,750,5: 1,650,5: R$"5" R$: 400+/ ----------- ANIMAZIONE ORBITE .+0 ,10,22," " : N1 NP: CO1 2+: P0 9: CO,T(P,N,1),T(P, N,2): P,CO,NB,D ,10,22,"REPEAT ANMATON (Y/N)?": R$: R$"Y" 3120: 400n, ------------ DATI CORPO ERRANTE ., 4: " Π٠": , "OORDINATES (X,Y):";XC,YC: XC159 XC0 YC159 YC0 40101- XC155 4015: : "K ? (Β=OT ETURN=ES)": z- ,XC4,YC8," ": ,XC4,YC 81," ": A$: A$(13) 4015- A$"N" 4010: I1 200: : ,XC4,YC8,"",1: ,XC41,YC8,""- ,XC4,YC81,"߸": I1 200: : 4012 .XVXC: YVYC=. "ASS (ARTH=1): ";MC: MC 0 4020. "PEED (M/S): ";F: V 0 4030: FF360024GSC 106. "IRECTION DEGREE: ";A: A0 A359 4040. 3: . ----------- CALCOLI X SCELTA 5 .)/ P0 9: T(P,N,1)0 T(P, N,2)0 4150`/FPMCMA(P)((T(P,N,1)XC)2(T(P,N ,2)YC)2)/ T(P,N,1)XC T(P,N,2)YC 4122/AP(((T(P,N,1)XC)(T(P,N,2) YC)))180/ T(P,N,1)XC T(P,N,2)YC AP180AP: 4130I0 T(P,N,1)XC T(P,N,2)YC AP180AP: T(P,N,1)XC T(P,N,2)YC AP360AP0" FSC;A: FPSC;AP: F (((0)XC)2((1)YC)2)0,A((((0)XC)((1)YC)))180: XC(0) YC(1) A180A: 415011 (0)XC YC(1) A 180A: 4150)13 (0)XC (1)YC A 360Am16 P: ,XV,YV FSC;A: XV (0): YV(1): XCXV: YCYV: s1'#:1(# -------------------------- END .12# (142): 0: : I