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- 1 ' Comet ephemeris
- 2 gosub 10000
- 20 ' LET PI=3.1.159267
- 30 LET CO$="COMET HALLEY"
- 40 LET PH=1986.11
- 50 LET PL = 170.011
- 60 LET AN = 58.1453
- 70 LET PY = 76.0081
- 80 LET SM = 17.9435
- 90 LET EO = 0.967267
- 100 LET IO = 162.239
- 110 REM -------------------------
- 120 PRINT TAB (10);CO$
- 130 PRINT "- - - - - - - - - - - - - - -"
- 140 PRINT " EPHEMERIS FOR DATES"
- 150 PRINT " BETWEEN 1946 AND 2026"
- 160 PRINT "By Roger Browne"
- 165 Print "Adapted for Amiga by Tim Holloway":print
- 170 REM ========================
- 180 ' INPUT THE DATE
- 190 '
- 200 PRN=0:PRINT "Input year";
- 210 INPUT Y
- 220 IF Y<1946 OR Y > 2026 THEN 200
- 230 PRINT "Input month";
- 240 INPUT M
- 250 IF M < 1 OR M > 12 THEN 230
- 260 PRINT "Input day";
- 270 INPUT D
- 280 PRINT
- 290 PRINT INVERSE (1);" Calculating ... "
- 300 ' CALCULATIONS FOR THE COMET
- 310 '
- 320 LET X = PH
- 330 IF Y >= 1986 THEN Z=1984
- 340 IF Y < 1986 THEN Z = 1988
- 350 IF Y >= 1986 THEN S=0
- 360 IF Y < 1986 THEN S = 1
- 370 GOSUB 1780
- 380 DS = N
- 390 B = (360/PY)*(N/365.25)
- 400 K=B
- 410 GOSUB 1930
- 420 B=(K*PI)/180
- 430 E=B
- 440 Y1=EO
- 450 Q=E-(Y1*SIN(E))-B
- 460 IF ABS(Q) <= 1.7E-05 THEN 500
- 470 U=Q/(1-(Y1*COS(E)))
- 480 E=E-U
- 490 GOTO 450
- 500 V=(SQR((1+Y1)/(1-Y1))*(SIN(E/2)/COS(E/2)))
- 510 V=2*ATN(V)
- 520 V1=(V*180)/PI
- 530 L=V1+PL
- 540 R=SM*(1-(Y1*Y1))/(1+Y1*COS(V))
- 550 F=L-AN
- 560 F2=IO
- 570 F1=F*PI/180
- 580 F2=F2*PI/180
- 590 I=SIN(F1)*SIN(F2)
- 600 I=ATN(I/SQR(-I*I+1))
- 610 P=ATN((SIN(F1)/COS(F1))*COS(F2))
- 620 P1=P*180/PI+AN
- 630 IF F>= 90 AND F<= 270 THEN P1=P1+180
- 640 IF P1 < 0 THEN P1=P1+360
- 650 P=P1*PI/180
- 660 R2=R*COS(I)
- 670 '===========================
- 680 ' Calculations for the Earth
- 690 '
- 700 X=1975
- 710 IF Y>= X THEN Z=1972
- 720 IF Y < X THEN Z=1976
- 730 IF Y>= X THEN S=0
- 740 IF Y<1976 THEN S=1
- 750 GOSUB 1780
- 760 T=(360/365.25)*(N/1.00004)
- 770 K=T
- 780 GOSUB 1930
- 790 T=K
- 800 T1=T*PI/180
- 810 C=0.01672
- 820 J=T+(360/PI)*C*SIN(T1-0.051943)
- 830 J=J+99.5343
- 840 IF J>360 THEN J=J-360
- 850 IF J<0 THEN J=J+360
- 860 h=((j-102.51044)*pi)/180
- 870 r1 = (1-c*c)/(1+c*cos(h))
- 880 REM ------------------------
- 890 REM Compute Ecliptic coordinates
- 900 REM ------------------------
- 910 U1=((P1-J)*PI)/180
- 920 U2=((J-P1)*PI)/180
- 930 IF (R2<R1) THEN 990
- 940 Q1=(R1*SIN(U1))
- 950 Q1=Q1/(R2-(R1*COS(U1)))
- 960 Q1=ATN(Q1)
- 970 Q2=(Q1*180)/PI+P1
- 980 GOTO 1030
- 990 Q3=R2*SIN(U2)
- 1000 Q3=Q3/(R1-(R2*COS(U2)))
- 1010 Q3=ATN(Q3)
- 1020 Q2=(Q3*180)/PI+J+180
- 1030 IF Q2>360 THEN Q2=Q2-360
- 1040 IF Q2<0 THEN Q2=Q2+360
- 1050 Q4=Q2*PI/180
- 1060 Q5=(R2*(SIN(I)/COS(I))*SIN(Q4-P))
- 1070 Q5=Q5/(R1*SIN(U1))
- 1080 Q5=ATN(Q5)
- 1090 REM ------------------------
- 1100 REM Convert to equatorial coordinates
- 1110 REM ------------------------
- 1120 E1=0.40893064
- 1130 L1=SIN(Q5)*COS(E1)
- 1140 L1=L1+COS(Q5)*SIN(E1)*SIN(Q4)
- 1150 M1=ATN(L1/SQR(-L1*L1+1))
- 1160 Y2=M1*180/PI
- 1170 B1=(SIN(Q4)/COS(Q4))*COS(E1)
- 1180 B1=B1-(((SIN(Q5)/COS(Q5))*SIN(E1))/COS(Q4))
- 1190 G=ATN(B1)
- 1200 H1=G*180/PI
- 1210 I1=INT(Q2/90)
- 1220 J1=INT(H1/90)
- 1230 IF (I1-J1)=4 OR (I1-J1)=1 THEN H1=H1+360
- 1240 IF (I1-J1)=2 OR (I1-J1)=3 THEN H1=H1+180
- 1250 IF (I1-J1)=-4 THEN H1=H1+360
- 1260 IF (I1-J1)=-2 THEN H1=H1-180
- 1270 LET N1=H1/15
- 1280 W=INT((N1-INT(N1))*60+0.5)
- 1290 IF W=60 THEN N1=N1+1
- 1300 IF W=60 THEN W=0
- 1310 K1=ABS(Y2)
- 1320 W1=INT((K1-INT(K1))*60+0.5)
- 1325 G1=INT(K1)
- 1330 IF W1=60 THEN G1=G1+1
- 1340 IF W1=60 THEN W1=0
- 1360 IF (Y2<0) AND (G1<1) THEN W1=-W1
- 1370 D1=R1*R1+R2*R2
- 1380 D1=D1-(2*R1*R2*COS(U1))
- 1390 D2=SQR(D1)
- 1400 R3=D2/COS(I)
- 1410 K9=R
- 1420 GOSUB 2040
- 1430 R=K9
- 1440 K9=R3/10
- 1450 GOSUB 2040
- 1460 R3=K9*10
- 1470 MO=4.1:N=3.1
- 1480 IF DS<0 THEN MO=5:N=4.44
- 1490 MA=MO+5*0.4343*LOG(R3)
- 1500 MA=MA+N*2.5*0.4343*LOG(R)
- 1510 MA=(INT(10*MA))/10
- 1520 IF Y2<0 THEN G1=-G1
- 1530 REM ------------------------
- 1540 REM Print ephemeris for date
- 1550 REM ------------------------
- 1560 PRINT "--------------------"
- 1570 PRINT "Data for ";CO$:PRINT
- 1575 gshape (200,150),pic%
- 1580 print "Date: ";M;"/";D;"/";Y
- 1590 print "Days to perihelion: ";int(ds)
- 1600 print
- 1610 print "Coordinates: epoch 1950"
- 1620 print "RA ..... ";INT(N1);" hrs ";W; " min"
- 1630 print "Dec .... ";G1;" deg ";w1;" min":print
- 1650 print "Distances:"
- 1660 print "Comet to sun: . ";R;" A.U."
- 1670 print "Comet to Earth: ";R3;" A.U."
- 1680 print
- 1690 print "Predicted mag. ";MA
- 1700 print "--------------------"
- 1710 INPUT "Run another date";DATE$
- 1730 IF (DATE$<>"Y") AND (DATE$<> "y") THEN STOP
- 1740 GOTO 200
- 1770 REM ------------------------
- 1780 ' DAYS TO PERIHELION
- 1785 A=(Y-Z)/4
- 1790 A1=INT(A+S)
- 1800 N=365*(Y-X+S)+A1
- 1810 IF INT(A)<> A THEN 1830
- 1820 IF (M=2) AND (D<29) OR (M=1) THEN N=N-1
- 1830 IF M>2 THEN 1870
- 1840 M2=M-1
- 1850 M2=31*M2
- 1860 GOTO 1890
- 1870 M2=M+1
- 1880 M2=INT(30.6*M2)-63
- 1890 N=N+M2+D-365*S
- 1900 RETURN
- 1910 REM ------------------------
- 1920 REM PLACE BETWEEN 0 AND 360 DEG
- 1930 IF K<0 THEN 1950
- 1940 IF K>360 THEN 1980
- 1950 K=K+360
- 1960 IF K>=0 THEN 2010
- 1970 GOTO 1950
- 1980 K=K-360
- 1990 IF K<= 360 THEN 2010
- 2000 GOTO 1980
- 2010 RETURN
- 2020 REM ------------------------
- 2030 REM ROUND OFF SUBROUTINE
- 2040 K9=K9*1000
- 2050 K9=INT(K9+0.5)
- 2060 K9=K9/1000
- 2070 RETURN
- 10000 ' AMIGA GRAPHICS - OPTIONAL (TFH)
- 10005 scnclr
- 10010 dim pic%(138):bload "HALLEY.PIC",varptr(pic%(0))
- 10020 gshape (220,20),pic%
- 10030 return
-