Die Programme für ATARI ST Computer laufen mit dem ATARI STEmulator  (mit ARARI  TOS ROM 2.06) unter Windows 9x/ME (s. Abschnitt Kompatibilität). Kopieren Sie die ATARI ST Progr. aus dem Ordner GFA/GFA_PROG. und den GFA-BASIC-Interpreter auf das Festplatten-Laufwerk >C<.

REM ATARI ST GFA-BASIC46  ASTROGRAPH II FÜR GROSSMASSTÄBIGE FELDSTERNAUFNAHMEN
DEFFN gzb(x) = ATN(1 / (1 + 0.006739501819 * (6378140 / (6378140 + eh))) * TAN(x))
DEFFN ro(x) = 6356755.288157 / SQR(1 - 0.006694384999591 * COS(ATN(0.993305615 * TAN(x))) ^ 2) + eh
DEFFN r(x) = x - INT(x / (2 * PI)) * (2 * PI)
DIM ar(20),dek(20),ar1(20),dek1(20),x(20),y(20),x1(20),y1(20),ko(15),ko1(15),koo(15),p1(15,15),p(15,15),xo(20),yo(20),n(20),aa(20),dd(20),w1(20),w2(20),w3(20)
GOSUB astrograph
PROCEDURE astrograph
  REM -- ASTROGRAPH II - PHOTOGRAPHISCHE ORTSBESTIMMUNG AUF GROSSFELDAUFNAHMEN --
  k1 = RAD(20.49552 / 3600)
  neu:
  CLS
  PRINT AT(1,1);"- ASTRONOMISCHE ORTSBESTIMMUNG II -"
  PRINT AT(1,3);"DATUM (TT.MM.JJJJ)...........................: ";
  REM  INPUT "",a$
  a$="1.1.2000" !EINTRAG TESTDATEN-------------------
  a1 = ABS(LEN(a$) - 2)
  a2 = VAL(LEFT$(a$,2))
  a3 = VAL(MID$(a$,4 + (a2 < 10),2))
  a4 = VAL(RIGHT$(a$,a1 + (a2 < 10) + (a3 < 10) + (a2 > 9) * 2 + (a3 > 9) * 2))
  IF a2 = 0 OR a1 > 10 OR ABS(a2) > 31 OR ABS(a3) > 12 THEN
    GOTO neu
  ENDIF
  GOSUB jd
  PRINT AT(1,4);"UHRZEIT (UT AUFNAHMEMITTE h,m,s).............: ";
  REM  INPUT "",h,m,s
  h = 12
  m=0 !-------------------------
  s = 0
  ut = h + m / 60 + s / 3600
  PRINT AT(1,5);"KORREKTIONSWERT FÜR EPHEMERIDENZEIT (SEK)....: ";
  REM  INPUT "",ddt  !ddt=TDT-UT
  ddt=0 !---------------
  ddt = ddt / 3600
  PRINT AT(1,6);"HÖHE ÜBER N.N. (METER).......................: ";
  REM   INPUT "",eh
  eh = 0
  PRINT AT(1,7);"GEOGRAPHISCHE BREITE (o,','')................: ";
  REM   INPUT "",h$,m,s
  h$ = "50"
  m=0 !----------------------
  s = 0
  GOSUB grad        !KOORDINATEN BEOBACHTRUNGSSTATION
  br=FN gzb(g)      !FÜR TÄGL. ABERRATION
  p1 = FN ro(g) / 6378140
  PRINT AT(1,8);"GEOGRAPHISCHE L¥NGE (o,','').................: ";
  REM   INPUT "",h$,m,s
  h$ = "6"
  m=0 !---------------------
  s = 0
  GOSUB grad
  lgeo = DEG(g)
 jdbeo=jd+(ut+ddt)/24 !JULIAN. DATUM DER AUFNAHMEMITTE
  PRINT AT(1,9);"KATALOGEPOCHE REFERENZSTERNE (1950.0, 2000.0): ";
  REM  INPUT "",ep
  ep=2000 !-----------------
  PRINT AT(1,10);"BESSEL/FK4 ODER JULIAN./FK5  B,J.............: ";
  REM   INPUT "",ep$
  ep$="J" !------------------------
  ep$=UPPER$(ep$)
  IF ep$ = "B" THEN
    jdep = 2415020.31352 + 365.242198781 * (ep - 1900)
  ENDIF
  IF ep$ = "J" THEN
    jdep = 2451545 + 365.25 * (ep - 2000)
  ENDIF
  t1 = (jd - 2451545) / 36525
  t = (jdbeo - 2451545) / 36525
  GOSUB nut
  GOSUB osz
  jdd=(jdbeo-jdep)/365.25 !DIFFERENZ AUFNAHMENITTE-EPOCHE IN JULIAN. JAHREN
  PRINT AT(1,11);"PRIMÄRBRENNWEITE DER AUFNAHMEOBTIK (mm)......: ";  !IN;MILIIMETER
  REM  INPUT "",f
  fo=5000 !------------------
  PRINT AT(1,12);"ANZAHL REFERENZSTERNE........................: ";
  REM  INPUT "",anz
  anz=10 !---------------
  CLS
  i = 1
  PRINT AT(1,2);"KATALOG-REKTASZENSION STERN AUFNAHMEMITTE (h,m,s): ";  !AR;DER;OPTISCHEN;ACHSE
  REM  INPUT "",h$,m,s
  h$ = "0"
  m=20 !----------------------
  s = 0
  GOSUB grad
  ar(i) = g * 15
  REM EIGENBEWEGUNG BEZOGEN AUF DIESELBE EPOCHE WIE AR UND DEKLIN.
  PRINT AT(1,3);"EIGENBEWEGUNG STERN AR AUFNAHMEMITTE (ZEITSEK.)..: "; !FALLS STERN INMIITEN DER AUFNAHME SONST;pm = 0
  REM   INPUT "",pm
  pm=0 !--------------------
  ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
  PRINT AT(1,4);"KATALOG-DEKLINATION STERN AUFNAHMEMITTE (o,','').: ";  !DEKLIN. OPTISCHE ACHSE
  REM   INPUT "",h$,m,s
  h$ = "-15"
  m=40 !-----------------
  s = 0
  GOSUB grad
  dek(i) = g
  PRINT AT(1,5);"EIGENBEWEGUNG STERN DEKLIN. AUFNAHMEMITTE ('')...: ";
  REM   INPUT "",pm
  pm=0 !------------------
  dek(i) = dek(i) + RAD(pm / 3600) * jdd
  PRINT AT(1,6);"J¥HRL. PARALLAXE ('')............................: ";  !FALLS;STERN;INMITTEN;DER;AUFNAHME, SONST;p = 0
  REM   INPUT "",p
  p=0 !---------------------
  GOSUB appapos
  do = dek(i)
  aro = ar(i)
  CLS
  GOTO jump !----------------
  FOR i=1 TO anz  !EINGABE REFERENZSTERNE
  PRINT AT(1,2);i;") KATALOG-REKTASZENSION REFERENZSTERN (h,m,s): ";
  INPUT "",h$,m,s
  GOSUB grad
  ar(i) = g * 15
  REM EIGENBEWEGUNG BEZOGEN AUF DIESELBE EPOCHE WIE AR UND DEKLIN.
  PRINT AT(1,3);i;") EIGENBEWEGUNG AR REFERENZSTERN (ZEITSEK.)..: ";
  INPUT "",pm
  ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
  PRINT AT(1,4);i;") KATALOG-DEKLINATION REFERENZSTERN (o,','').: ";
  INPUT "",h$,m,s
  GOSUB grad
  dek(i) = g
  PRINT AT(1,5);i;") EIGENBEWEGUNG DEKLIN. REFERENZSTERN ('')...: ";
  INPUT "",pm
  dek(i) = dek(i) + RAD(pm / 3600) * jdd
  PRINT AT(1,6);i;") J¥HRL. PARALLAXE ('')......................: ";
  INPUT "",p
  GOSUB appapos
  PRINT AT(1,7);i;") x-,y-MESSUNG REFERENZSTERN (mm)............: "; !IN MILLIMETER
  INPUT "",x(i),y(i)
  REM STRENGE STANDARDKOORDINATEN X,Y
  j = SIN(dek(i)) * SIN(do) + COS(dek(i)) * SIN(do) * COS(ar(i) - aro)
  x1(i) = (COS(dek(i)) * SIN(ar(i) - AR)) / j
  y1(i) = (SIN(dek(i)) * COS(do) - COS(dek(i)) * SIN(do) * COS(ar(i) - aro)) / j
  CLS
NEXT i
jump: !------------------
REM EINGABE REFERENZSTERNE
REM (BEI VERWENDUNG OBIGER EINGABESCHLEIFE DIESEN TESTTEIL LÖSCHEN)--
i=1 !NR. 1
h$="0"  !REKTASZENSION STUNDEN
m=7     !MINUTEN
s=46.923 !SEKUNDEN
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$="-22" !DEKLINATION
m=30     !BOGENMINUTEN
s=30.96  !BOGENSEKUNDEN
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=2 !NR. 2
h$ = "0"
m = 6
s = 24.982
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-18"
m = 2
s = 17.81
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=3 !NR. 3
h$ = "0"
m = 17
s = 8.883
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-15"
m = 39
s = 27.94
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=4 ! NR. 4
h$ = "0"
m = 34
s = 45.931
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-24"
m = 31
s = 40.79
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=5 ! NR. 5
h$ = "0"
m = 30
s = 45.105
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-17"
m = 42
s = 54.03
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=6 ! NR. 6
h$ = "0"
m = 43
s = 35.372
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-17"
m = 59
s = 11.82
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ---------------------------
i = 7
h$ = "0"
m = 30
s = 22.661
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-23"
m = 47
s = 15.72
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i = 8
h$ = "0"
m = 24
s = 49.643
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-18"
m = 28
s = 18.66
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=9 !NR. 9
h$ = "0"
m = 18
s = 16.954
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-21"
m = 8
s = 18.22
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=10 ! NR. 10
h$ = "0"
m = 20
s = 2.973
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-17"
m = 42
s = 1.67
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=11 ! NR. 11
h$ = "0"
m = 15
s = 46
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-28"
m = 40
s = 0
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
i=12 ! NR. 12
h$ = "2"
m = 43
s = 35
GOSUB grad
ar(i) = g * 15
pm = 0
ar(i) = FN r(ar(i) + RAD((pm * 15) / 3600) * jdd)
h$ = "-5"
m = 59
s = 11.82
GOSUB grad
dek(i) = g
pm = 0
dek(i) = dek(i) + RAD(pm / 3600) * jdd
p = 0
GOSUB appapos
GOSUB messung
x(i) = x
y(i) = y
REM ----------------------------------------------
REM STRENGE STANDARDKOORDINATEN X,Y AUSGLEICHUNG BEOBACHTUNG MINUS RECHNUNG
FOR i = 1 TO anz
  j = SIN(dek(i)) * SIN(do) + COS(dek(i)) * COS(do) * COS(ar(i) - aro)
  x1(i) = (COS(dek(i)) * SIN(ar(i) - aro)) / j
  y1(i) = (SIN(dek(i)) * COS(do) - COS(dek(i)) * SIN(do) * COS(ar(i) - aro)) / j
NEXT i
REM ---------------------
GOSUB ausgleich
CLS
PRINT AT(1,1);"BESTIMMUNG DER PROJIZIERTEN/REPRODUZIERTEN NEGATIVVERGRÖSSERUNG
PRINT AT(1,2);"NR. ZWEIER REFERENZSTERNE GEMESS. WINKELDISTANZ A,B: ";
REM  INPUT "",nr1,nr2
nr1 = 2
nr2=4 !---------------
PRINT AT(1,3);"GEMESSENE WINKELDISTANZ STERN NR. ";nr1;" ZU ";nr2;" (mm)......: "; !MILLIMETER
REM  INPUT "",dis
dis=101.65 !--------------
d = ACOS(SIN(dek(nr1)) * SIN(dek(nr2)) + COS(dek(nr1)) * COS(dek(nr2)) * COS(ar(nr2) - ar(nr1)))
d=DEG(d)*3600 !DISTANZ DER ZWEI STERNE IN BOGENSEKUNDEN
f1=fo/206264.8062471 !1'' (BOGENSEK.) AM HIMMEL = f1 MILLIMETER AUF DEM NEGATIV
v=dis/(d*f1) !VERGRÖSSERUNG DER DIAPROJEKTION/KOPIE GEGENÜBER DEM NEGATIV
r=fo*v !EFFEKTIVE BRENNWEITE IN MILLIMETER
f2=r/206264.8062471 !MASSTAB 1'' AUF DER DIAPROJEKTION/KOPIE = f2 MILLIMETER
f3=1/f2 !1 mm DER DIAPROJEKTION/KOPIE = f3 BOGENSEKUNDEN
CLS
PRINT AT(1,1);"ANZAHL MESSUNGEN OBJEKT: ";  !GERADE MEHRFACH HIN UND ZURÜCK MESSEN
REM  INPUT "",ns
ns=1 !------------------
PRINT AT(1,2);SPC(50)
j = 0
GOTO ik !----------------
FOR i = 1 TO ns
  j = j + 1
  PRINT AT(1,j);j;") MESSUNG OBJEKT x,y (mm): ";  !EINGABE;MILLIMETER
  INPUT "",x(i),y(i)
NEXT i
ik: !-------
x(ns) = ROUND(x(1),1)
y(ns) = ROUND(y(1),1)
FOR i = 1 TO ns
  xo(i)=koo(1)+koo(2)*x(i)+koo(3)*y(i)+koo(4)*x(i)*y(i)+koo(5)*x(i)*x(i)+koo(6)*y(i)*y(i)+koo(7)*x(i)*y(i)*y(i)+koo(8)*x(i)*x(i)*y(i)+koo(9)*x(i)*x(i)*x(i)+k oo(10)*y(i)*y(i)*y(i)  !AUSGEGLICHENE STANDARDKOORDINATEN
  yo(i)=ko1(1)+ko1(2)*x(i)+ko1(3)*y(i)+ko1(4)*x(i)*y(i)+ko1(5)*x(i)*x(i)+ko1(6)*y(i)*y(i)+ko1(7)*x(i)*y(i)*y(i)+ko1(8)*x(i)*x(i)*y(i)+ko1(9)*x(i)*x(i)*x(i)+ko 1(10)*y(i)*y(i)*y(i)  !DES OBJEKTS
  j=COS(do)-yo(i)*SIN(do)
  ar1(i)=FN r(aro+ATN(xo(i)/j))  !REKTASZENSION OBJEKT
  dek1(i)=ATN((SIN(do)+yo(i)*COS(do))/SQR(xo(i)^2+j^2)) !DEKLINATION OBJEKT
NEXT i
FOR i=1 TO ns
  n(i)=xo(i)
NEXT i
GOSUB sig
PRINT AT(1,1);"AUSGEGLICHENE STANDARDKOORDINATEN DES OBJEKT:"
PRINT AT(1,2);USING "X: ##.######### ",mw;
PRINT "/ m.F. ";mf;"/ Streuung ";sig
FOR i=1 TO ns
  n(i)=yo(i)
NEXT i
GOSUB sig
PRINT AT(1,3);USING "Y: ##.######### ",mw;
PRINT "/ m.F. ";mf;"/ Streuung ";sig
FOR i=1 TO ns
  n(i)=DEG(ar1(i))/15
NEXT i
GOSUB sig
arap=RAD(mw)*15
GOSUB sexa
IF ep$="J" THEN
  PRINT AT(1,4);"SCHEINBARER ORT OBJEKT, WAHRES ÄQUINOKTIUM DES DATUM/FK5:"
ELSE
  PRINT AT(1,4);"SCHEINBARER ORT OBJEKT, WAHRES ÄQUINOKTIUM DES DATUM/FK4:"
ENDIF
PRINT AT(1,5);USING "AR.....: ## h ## m ##.### s",h,m,s;
PRINT "/ m.F. ";mf;"/ Streuung ";sig
FOR i=1 TO ns
  n(i)=DEG(dek1(i))
NEXT i
GOSUB sig
dekap=RAD(mw)
GOSUB sexa
PRINT AT(1,6);"DEKLIN.: ";z$;USING "## o ## ' ##.## ''",h,m,s;
PRINT "/ m.F. ";mf;"/ Streuung ";sig
GOSUB app  !SUBROUTINE MITTL. ORT
arj=ar !MITTL. AR
dj=d   !MITTL. DEKLIN.
mw=DEG(AR)/15
GOSUB sexa
IF ep$="J" THEN
  PRINT AT(1,7);"ASTROMETR. ORT OBJEKT, MITTL. ÄQUINOKTIUM J2000/FK5"
ELSE
  PRINT AT(1,7);"ASTROMETR. ORT OBJEKT, MITTL. ÄQUINOKTIUM B1950/FK4"
ENDIF
PRINT AT(1,8);USING "AR.....:  ## h ## m ##.### s",h,m,s
mw=DEG(d)
GOSUB sexa
PRINT AT(1,9);"DEKLIN.: ";z$;USING "## o ## ' ##.## ''",h,m,s
IF ep$="J" THEN
  GOSUB conv1
ELSE
  GOSUB conv
ENDIF
mw=DEG(AR)/15
GOSUB sexa
IF ep$="J" THEN
  PRINT AT(1,10);"ASTROMETR. ORT OBJEKT, MITTL. ÄQUINOKTIUM B1950/FK4"
ELSE
  PRINT AT(1,10);"ASTROMETR. ORT OBJEKT, MITTL. ÄQUINOKTIUM J2000/FK5"
ENDIF
PRINT AT(1,11);USING "AR.....: ## h ## m ##.### s",h,m,s
mw=DEG(d)
GOSUB sexa
PRINT AT(1,12);"DEKLIN.: ";z$;USING "## o ## ' ##.## ''",h,m,s
PRINT AT(1,16);"PRIMÄRBRENNWEITE DER AUFNAHMEOPTIK: ";fo;" mm"
PRINT AT(1,17);"EFFEKTIVE BRENNWEITE: ";r;" mm"
PRINT AT(1,18);"VERGRÖSSERUNGSFAKTOR: ";v;"x"
PRINT AT(1,19);"MASSTAB: 1''  = ";f1;" mm AUF DEM NEGATIV"
PRINT AT(1,20);"MASSTAB: 1''  = ";f2;" mm AUF DER KOPIE/DIAPROJEKTION"
PRINT AT(1,21);"MASSTAB: 1 mm = ";f3;" '' AUF DER KOPIE/DIAPROJEKTION"
PRINT AT(1,23);"TASTE >1<"
PRINT AT(1,24);"TASTE >2<"
PRINT AT(1,25);"TASTE >S<"
DO
  w$=UPPER$(INKEY$)
  IF w$="1" THEN
    GOSUB tafel
    IF w$="1" THEN
      GOSUB tafel
    ENDIF
  ENDIF
  IF w$="2" THEN
    GOSUB astrographZ
  ENDIF
  EXIT IF w$="S"
LOOP
RETURN
PROCEDURE grad
  j=1
  IF LEFT$(h$,1)="-" THEN
    j=-1
  ENDIF
  g=RAD(ABS(VAL(h$))+m/60+s/3600)*j
RETURN
PROCEDURE sexa
  IF mw<0 THEN
    z$="-"
  ELSE
    z$="+"
  ENDIF
  g=ABS(mw)
  h=FIX(g)
  m=FIX((g-h)*60)
  s=((g-h)*60-m)*60
RETURN
PROCEDURE tafel
  CLS
  PRINT AT(15,1);"       EINMESSUNG EINES KOORDINATENKREUZES    "
  PRINT AT(15,2);"STRENGE STANDARDKOORDINATEN X,Y DER REFERENZSTERNE"
  PRINT AT(15,3);"           WAHRS ÄQUINOKTIUM DES DATUMS       "
  u=4
  FOR i=1 TO anz
    u=u+1
    PRINT AT(1,u);i;") X: ";-r*x1(i);" mm, Y: ";r*y1(i);" mm"
  NEXT i
  PRINT AT(1,24);"TASTE >W<"
  REPEAT
  UNTIL UPPER$(INKEY$)="W"
  CLS
  PRINT AT(15,1);"SCHEINBARE REKTASZENSION UND DEKLINATION"
  PRINT AT(15,2);"     WAHRES ÄQUINOKTIUM DES DATUMS"
  u=3
  FOR i=1 TO anz
    u=u+1
    mw=DEG(ar(i))/15
    GOSUB sexa
    PRINT AT(1,u);i;USING ") AR:  ## h ## m ##.### s",h,m,s;
    mw=DEG(dek(i))
    GOSUB sexa
    PRINT ",  DEKLIN.: ";z$;USING "## o ## ' ##.## ''",h,m,s
  NEXT i
  PRINT AT(1,23);"TASTE >1<"
  PRINT AT(1,24);"TASTE >2<"
  REPEAT
  UNTIL UPPER$(INKEY$)="1" OR UPPER$(INKEY$)="2"
  DO
    w$=UPPER$(INKEY$)
    IF w$="1" OR w$="2" THEN
      GOTO j
    ENDIF
  LOOP
  j:
RETURN
PROCEDURE jd
  jd=1720994.5+a2+FIX(30.6001*((a3-12*(a3<3))+1))+FIX(f*365.245*(a4+(a3<3)))
RETURN
PROCEDURE ausgleich
  REM AUSGLEICHSRECHNUNG NACH DER METHODE DER KLEINSTEN QUADRATE
  REM ----- NORMALGLEICHUNG MATRIX 10 X 10 ----------
  rr=0
  br=0
  cr=0
  dr=0
  er=0
  fr=0
  gr=0
  hr=0
  ir=0
  jr=0
  FOR i=1 TO anz
    rr=rr+x1(i)
    br=br+x(i)*x1(i)
    cr=cr+y(i)*x1(i)
    dr=dr+x(i)*y(i)*x1(i)
    er=er+x(i)*x(i)*x1(i)
    fr=fr+y(i)*y(i)*x1(i)
    gr=gr+x(i)*y(i)*y(i)*x1(i)
    hr=hr+x(i)*x(i)*y(i)*x1(i)
    ir=ir+x(i)*x(i)*x(i)*x1(i)
    jr=jr+y(i)*y(i)*y(i)*x1(i)
  NEXT i
  GOSUB mess
  m=10
  n=10
  FOR i=1 TO m
    FOR k=1 TO n+1
      p(i,k)=p1(i,k)
    NEXT k
  NEXT i
  GOSUB elim
  FOR i=1 TO m
    koo(i)=ko(i)
  NEXT i
  i=1
  GOSUB gl
  PRINT
  PRINT "TASTE >W<"
  REPEAT
  UNTIL UPPER$(INKEY$)="W"
  CLS
  rr=0
  br=0
  cr=0
  dr=0
  er=0
  fr=0
  gr=0
  hr=0
  ir=0
  jr=0
  FOR i=1 TO anz
    rr=rr+y1(i)
    br=br+x(i)*y1(i)
    cr=cr+y(i)*y1(i)
    dr=dr+x(i)*y(i)*y1(i)
    er=er+x(i)*x(i)*y1(i)
    fr=fr+y(i)*y(i)*y1(i)
    gr=gr+x(i)*y(i)*y(i)*y1(i)
    hr=hr+x(i)*x(i)*y(i)*y1(i)
    ir=ir+x(i)*x(i)*x(i)*y1(i)
    jr=jr+y(i)*y(i)*y(i)*y1(i)
  NEXT i
  GOSUB mess
  m=10
  n=10
  FOR i=1 TO m
    FOR k=1 TO n+1
      p(i,k)=p1(i,k)
    NEXT k
  NEXT i
  GOSUB elim
  FOR i=1 TO m
    ko1(i)=ko(i)
  NEXT i
  i=0
  GOSUB gl
  PRINT
  PRINT "TASTE >W<"
  REPEAT
  UNTIL UPPER$(INKEY$)="W"
RETURN
PROCEDURE elim
  FOR j=1 TO n-1     !GAUSS ELIMINATION
  nr=j
  no=ABS(p(j,j))
  FOR i=j+1 TO n    STEP !ZEILENPIVOT
    noo=ABS(p(i,j))
    EXIT IF (noo-no)<0
    no=noo
    nr=i
  NEXT i
  IF nr=j THEN
    GOTO jum1
  ENDIF
  FOR i=j TO m+1
    no=p(nr,i)
    p(nr,i)=p(j,i)
    p(j,i)=no
  NEXT i
  jum1:
  FOR i=j+1 TO m+1   STEP !ELIMINATION
    p(j,i)=p(j,i)/p(j,j)
  NEXT i
  FOR i=j+1 TO n
    FOR k=j+1 TO m+1
      p(i,k)=p(i,k)-p(j,k)*p(i,j)
    NEXT k
  NEXT i
NEXT j
ko(n)=p(n,n+1)/p(n,n)  !RÜCKSUBSTITUTION
FOR j=n-1 TO 1 STEP -1
  ko(j)=p(j,n+1)
  FOR i=j+1 TO n
    ko(j)=ko(j)-p(j,i)*ko(i)
  NEXT i
NEXT j
RETURN
PROCEDURE nut
  REM DELAUNAY-ELEMENTE
  d = FN r(5.198468 + 7771.37714 * t)      !Mittl. Elongation Mond-Sonne
  ll = FN r(6.24006 + 628.3019555 * t)      !Mittl. Anomalie Sonne (Erde)
  l = FN r(2.3555482 + 8328.691422 * t)   !Mittl. Anomalie Mond
  f = FN r(1.627903 + 8433.46615813 * t) !Mittl. Länge Mond ab aufsteigenden Mondknoten
  af = FN r(2.182438 - 33.757045 * t)        !Mittl. Länge aufst. Mondknoten
  REM NUTATION IN LÄNGE
  nu = -172000 * SIN(af) + 2060 * SIN(2 * af)  - 1320 * SIN(2 * f - 2 * d + 2 * af) + 1430 * SIN(ll)
  nu = nu / 10000
  REM NUTATION IN SCHIEFE
  nu1 = 92000 * COS(af) - 895 * COS(2 * af) + 5740 * COS(2 * f - 2 * d + 2 * af) + 220 * COS(ll + 2 * f - 2 * d + 2 * af)
  nu1 = nu1 / 10000
   f7=0.409093-0.000227*t !MITTL. EKLIPTISCHIEFE
  ec=f7+RAD(nu1/3600) !WAHRE EKLIPTIKSCHIEFE
  REM lms,ms,ls = geometr. mittl. L„nge der Sonne. mittl. Anomalie der Sonne, geometr. wahre L„nge der Sonne
  lms=FN r(4.89506+628.33197*t)
  ms=FN r(6.24006+628.30196*t)
  c=0.03342*SIN(ms)+0.00035*SIN(2*ms)
  l=FN r(lms+c)
  v=FN r(ms+c)
  REM ds, ars = Deklin. und Rektaszension der Sonne Äquinoktium des Datums JD
  ds=ASIN(SIN(ec)*SIN(l))  !Deklin. Sonne
  ys=SIN(l)*COS(ec)
  xs=COS(l)
  r1=SQR(xs^2+ys^2)
  x1=xs/r1
  y1=ys/r1
  ars=FN r(ATN(y1/(1+x1))*2) !Rektaszension Sonne
  e=0.0167086
  pe=RAD(102.94+0.71953*t)
  rs = 10 ^ (((3040 - 15 * t) + (-727600 + 1810 * t) * COS(ms) + (-9090 + 50 * t) * COS(2 * ms)) / 100000000) //Radius Vektor Sonne
RETURN
PROCEDURE appapos
  d1=dek(i)
  a1=ar(i)
  t2=(jdbeo-jdep)/36525
  IF ep$="J" THEN
    GOSUB praez
  ELSE
    t2=(jdbeo-jdep)/36524.2198782
    GOSUB praez1
  ENDIF
  GOSUB reduk
  dek(i)=d+ded+dpa+dnu+dab+di
  ar(i)=FN r(AR+ard+apa+anu+aab+ai)
RETURN
PROCEDURE app
  d=dekap
  AR=arap
  p=0
  GOSUB reduk
  dekm=dekap-(dpa+ded+dnu+dab+di)
  arm=FN r(arap-(apa+ard+anu+aab+ai))
  REM ----- PRÄZESSION ----------
  t2=(jdep-jdbeo)/36525
  d1=dekm
  a1=arm
  IF ep$="J" THEN
    GOSUB praez
  ELSE
    t2=(jdep-jdbeo)/36524.2198782
    GOSUB praez1
  ENDIF
RETURN
PROCEDURE praez
  REM ----- PRÄZESSION FK5 ----------
  to=(jdep-2451545)/36525
  w1=RAD(((2306.218+1.4*to)*t2+0.3*t2*t2)/3600)
  w2=RAD(((2306.218+1.4*to)*t2+1.1*t2*t2)/3600)
  w3=RAD(((2004.311-0.85*to)*t2-0.43*t2*t2)/3600)
  d=ASIN(SIN(w3)*COS(d1)*COS(a1+w1)+COS(w3)*SIN(d1))
  x=(COS(w3)*COS(d1)*COS(a1+w1)-SIN(w3)*SIN(d1))/COS(d)
  y=(COS(d1)*SIN(a1+w1))/COS(d)
  AR=FN r(ATN(y/(1+x))*2+w2)
RETURN
PROCEDURE praez1
  REM ----- PRÄZESSION FK4----------
  to=(jdep-2433282.423459)/36524.2198781
  w1=RAD(((2304.952+1.4*to)*t2+0.3*t2*t2)/3600)
  w2=RAD(((2304.952+1.4*to)*t2+1.1*t2*t2)/3600)
  w3=RAD(((2004.259-0.85*to)*t2-0.43*t2*t2)/3600)
  d=ASIN(SIN(w3)*COS(d1)*COS(a1+w1)+COS(w3)*SIN(d1))
  x=(COS(w3)*COS(d1)*COS(a1+w1)-SIN(w3)*SIN(d1))/COS(d)
  y=(COS(d1)*SIN(a1+w1))/COS(d)
  AR=FN r(ATN(y/(1+x))*2+w2)
RETURN
PROCEDURE reduk
  REM -------- LICHTABLENKUNG ----------------
  REM elo = Elongationswinkel bzw. Winkeldistanz Stern-Sonne.
  abl=RAD(0.00407/3600)
  elo=ACOS(SIN(ds)*SIN(d)+COS(ds)*COS(d)*COS(AR-ars))
  ard=abl*COS(ds)*SIN(AR-ars)/(1-COS(elo)*COS(d))
  ded=abl*(SIN(d)*COS(ds)*COS(AR-ars)-COS(d)*SIN(ds))/(1-COS(elo))
  REM ---------- JÄHRLICHE PARALLAXE  ----------
  apa=RAD((rs*p*(COS(AR)*COS(ec)*SIN(l)-SIN(AR)*COS(l))*(1/COS(d)))/3600)
  dpa=RAD((rs*p*(COS(d)*SIN(ec)*SIN(l)-COS(AR)*SIN(d)*COS(l)-SIN(AR)*SIN(d)*COS(ec)*SIN(l)))/3600)
  REM ---------- NUTATION --------------------
  anu=(COS(ec)+SIN(ec)*SIN(AR)*TAN(d))*RAD(nu/3600)-COS(AR)*TAN(d)*RAD(nu1/3600)
  dnu=(SIN(ec)*COS(AR)*RAD(nu/3600)+SIN(AR)*RAD(nu1/3600))
  REM --------- JÄHRL. ABERRATION (FIXSTERNABERRATION) ------
  aab=-k1*((COS(AR)*COS(l)*COS(ec)+SIN(AR)*SIN(l))/COS(d))+e*k1*((COS(AR)*COS(pe)*COS(ec)+SIN(AR)*SIN(pe))/ COS(d))
 dab=-k1*(COS(l)*COS(ec)*(TAN(ec)*COS(d)-SIN(AR)*SIN(d))+COS(AR)*SIN(d)*SIN(l))+e*k1*(COS(pe)*COS(ec)*(TA N(ec)*COS(d)-SIN(AR)*SIN(d))+COS(AR)*SIN(d)*SIN(pe))
  REM ------- TÄGL. ABERRATION -----
  di=RAD(-0.319/3600)*p1*COS(br)*SIN(osz-AR)*SIN(d)
  ai=RAD(-0.319/3600)*((p1*COS(br)*COS(osz-AR))/COS(d))
RETURN
PROCEDURE sig
  k=0
  vv=0
  FOR i=1 TO ns
    k=k+n(i)
  NEXT i
  mw=k/ns  !ARITHMERTISCHER MITTELWERT
  FOR i=1 TO ns
    vv=vv+(n(i)-mw)^2 !FEHLERQUADRATSUMME
  NEXT i
  IF ns>1 THEN
    sig=SQR(vv/(ns-1)) !STANDARDABWEICHUNG
    mf=SQR(vv/(ns*(ns-1))) !MITTL. FEHLER DES MITTELSWERTES
  ENDIF
RETURN
PROCEDURE osz
  REM ORTSSTERNZEIT
  sz=6.697374558333+0.05133690722222*t1
  sz1=2400*t1
  sz1=sz1-INT(sz1/24)*24
  sz=sz+sz1
  sz=sz-INT(sz/24)*24
  sz=sz+ut*1.002737909+lgeo/15+((nu*COS(ec))/15)/3600
  sz=sz-INT(sz/24)*24
  osz=RAD(sz*15)
RETURN
PROCEDURE conv
  REM astrometrisch B1950/FK4 zu astrometrisch J2000/FK5
  x=COS(dj)*COS(arj)
  y=COS(dj)*SIN(arj)
  z=SIN(dj)
  REM Subktraktion der E-Terme
  x1=x-(-1.6E-06)+(x*(-1.6E-06))*x
  y1=y-(-3.2E-07)+(y*(-3.3E-07))*y
  z1=z-(-1.4E-07)+(z*(-1.4E-07))*z
  xo=0.99993*x1-0.01118*y1-0.00486*z1
  yo=0.01118*x1+0.99994*y1-0.00003*z1
  zo=0.00486*x1-0.00003*y1+0.99999*z1
  t=(jdbeo-2433282.423459)/36525
  x=xo+((-0.00265*x1-1.154*y1+2.11114*z1)/1000000)*t
  y=yo+((1.1541*x1-0.0129*y1+0.0236*z1)/1000000)*t
  z=zo+((-2.1113*x1-0.0056*y1+0.01026*z1)/1000000)*t
  ro=SQR(x^2+y^2+z^2)
  d=ASIN(z/ro)
  x=x/(ro*COS(d))
  y=y/(ro*COS(d))
  AR=FN r(ATN(y/(1+x))*2)
RETURN
PROCEDURE conv1
  REM astrometrisch J2000/FK5 zu astrometrisch B1950/FK4
  x=COS(dj)*COS(arj)
  y=COS(dj)*SIN(arj)
  z=SIN(dj)
  xo=0.99993*x+0.01118*y+0.00486*z
  yo=-0.01118*x+0.99994*y-0.00003*z
  zo=-0.00486*x-0.00003*y+0.99999*z
  t=(jdbeo-2451545)/36525
  x=xo+((-0.00265*x-1.154*y+2.11114*z)/1000000)*t
  y=yo+((1.1541*x-0.0129*y+0.0236*z)/1000000)*t
  z=zo+((-2.1113*x-0.0056*y+0.01026*z)/1000000)*t
  REM Addition der E-Terme
  x1=x+(-1.6E-06)-(x*(-1.6E-06))*x
  y1=y+(-3.2E-07)-(y*(-3.3E-07))*y
  z1=z+(-1.4E-07)-(z*(-1.4E-07))*z
  ro=SQR(x1^2+y1^2+z1^2)
  d=ASIN(z1/ro)
  x1=x1/(ro*COS(d))
  y1=y1/(ro*COS(d))
  AR=FN r(ATN(y1/(1+x1))*2)
RETURN
PROCEDURE gl
  IF i=1 THEN
    PRINT "PLATTENKONSTANTEN x:"
  ELSE
    PRINT "PLATTENKONSTANTEN y:"
  ENDIF
  PRINT "A: ";ko(1);"; B: ";ko(2);"; C: ";ko(3)
  PRINT "D: ";ko(4);"; E: ";ko(5);"; F: ";ko(6)
  PRINT "G: ";ko(7);"; H: ";ko(8);"; I: ";ko(9)
  PRINT "J: ";ko(10)
  PRINT "LINKE UND RECHTE SEITE NORMALGLEICHUNG:"
  PRINT anz*ko(1)+b1*ko(2)+c1*ko(3)+d1*ko(4)+e1*ko(5)+f1*ko(6)+g1*ko(7)+h1*ko(8)+i1*ko(9)+j1*ko(10),rr
  PRINT b1*ko(1)+bb*ko(2)+cb*ko(3)+db*ko(4)+eb*ko(5)+fb*ko(6)+gb1*ko(7)+hb*ko(8)+ib*ko(9)+jb*ko(10),br
  PRINT c1*ko(1)+bc*ko(2)+cc*ko(3)+dc*ko(4)+ecc*ko(5)+fc*ko(6)+gc*ko(7)+hc*ko(8)+ic*ko(9)+jc*ko(10),cr
  PRINT d1*ko(1)+bd*ko(2)+cd*ko(3)+dd*ko(4)+ed*ko(5)+fd*ko(6)+gd*ko(7)+hd*ko(8)+id*ko(9)+jd*ko(10),dr
  PRINT e1*ko(1)+be*ko(2)+ce*ko(3)+de*ko(4)+ee*ko(5)+fe*ko(6)+ge*ko(7)+he*ko(8)+ie*ko(9)+je*ko(10),er
  PRINT f1*ko(1)+bf*ko(2)+cf*ko(3)+df*ko(4)+ef*ko(5)+ff*ko(6)+gf*ko(7)+hf*ko(8)+if*ko(9)+jf*ko(10),fr
  PRINT g1*ko(1)+bg*ko(2)+cg*ko(3)+dg*ko(4)+eg*ko(5)+fg*ko(6)+gg*ko(7)+hg*ko(8)+ig*ko(9)+jg*ko(10),gr
  PRINT h1*ko(1)+bh*ko(2)+ch*ko(3)+dh*ko(4)+eh*ko(5)+fh*ko(6)+gh*ko(7)+hh*ko(8)+ih*ko(9)+jh*ko(10),hr
  PRINT i1*ko(1)+bi*ko(2)+ci*ko(3)+di*ko(4)+ei*ko(5)+fi*ko(6)+gi*ko(7)+hi*ko(8)+ii*ko(9)+ji*ko(10),ir
  PRINT j1*ko(1)+bj*ko(2)+cj*ko(3)+dj*ko(4)+ej*ko(5)+fj*ko(6)+gj*ko(7)+hj*ko(8)+ij*ko(9)+jj*ko(10),jr
RETURN
PROCEDURE mess
  b1=0  !PARAMETER AUF NULL SETZEN
  c1=0
  d1=0
  e1=0
  f1=0
  g1=0
  h1=0
  i1=0
  j1=0
  REM ----------
  bb=0
  cb=0
  db=0
  eb=0
  fb=0
  gb=0
  hb=0
  ib=0
  jb=0
  REM ------------
  bc=0
  cc=0
  dc=0
  ecc=0
  fc=0
  gc=0
  hc=0
  ic=0
  jc=0
  REM ------------
  bd=0
  cd=0
  dd=0
  ed=0
  fd=0
  gd=0
  hd=0
  id=0
  jd=0
  REM ------------
  be=0
  ce=0
  de=0
  ee=0
  fe=0
  ge=0
  he=0
  ie=0
  je=0
  REM ------------
  bf=0
  cf=0
  df=0
  ef=0
  ff=0
  gf=0
  hf=0
  if=0
  jf=0
  REM ------------
  bg=0
  cg=0
  dg=0
  eg=0
  fg=0
  gg=0
  hg=0
  ig=0
  jg=0
  REM ------------
  bh=0
  ch=0
  dh=0
  eh=0
  fh=0
  gh=0
  hh=0
  ih=0
  jh=0
  REM ------------
  bi=0
  ci=0
  di=0
  ei=0
  fi=0
  gi=0
  hi=0
  ii=0
  ji=0
  REM ------------
  bj=0
  cj=0
  dj=0
  ej=0
  fj=0
gj = 0
hj = 0
ij = 0
jj = 0
FOR i=1 TO anz  !AUFSUMMIERUNG PARAMETER
b1 = b1 + x(i)
c1 = c1 + y(i)
d1 = d1 + x(i) * y(i)
e1 = e1 + x(i) * x(i)
f1 = f1 + y(i) * y(i)
g1 = g1 + x(i) * y(i) * y(i)
h1 = h1 + x(i) * x(i) * y(i)
i1 = i1 + x(i) * x(i) * x(i)
j1 = j1 + y(i) * y(i) * y(i)
REM -------------
bb = bb + x(i) * x(i)
cb = cb + y(i) * x(i)
db = db + x(i) * y(i) * x(i)
eb = eb + x(i) * x(i) * x(i)
fb = fb + y(i) * y(i) * x(i)
gb1 = gb1 + x(i) * y(i) * y(i) * x(i)
hb = hb + x(i) * x(i) * y(i) * x(i)
ib = ib + x(i) * x(i) * x(i) * x(i)
jb = jb + y(i) * y(i) * y(i) * x(i)
REM -------------
bc = bc + x(i) * y(i)
cc = cc + y(i) * y(i)
dc = dc + x(i) * y(i) * y(i)
ecc = ecc + x(i) * x(i) * y(i)
fc = fc + y(i) * y(i) * y(i)
gc = gc + x(i) * y(i) * y(i) * y(i)
hc = hc + x(i) * x(i) * y(i) * y(i)
ic = ic + x(i) * x(i) * x(i) * y(i)
jc = jc + y(i) * y(i) * y(i) * y(i)
REM -------------
bd = bd + x(i) * x(i) * y(i)
cd = cd + y(i) * x(i) * y(i)
dd = dd + x(i) * y(i) * x(i) * y(i)
ed = ed + x(i) * x(i) * x(i) * y(i)
fd = fd + y(i) * y(i) * x(i) * y(i)
gd = gd + x(i) * y(i) * y(i) * x(i) * y(i)
hd = hd + x(i) * x(i) * y(i) * x(i) * y(i)
id = id + x(i) * x(i) * x(i) * x(i) * y(i)
jd = jd + y(i) * y(i) * y(i) * x(i) * y(i)
REM -------------
be = be + x(i) * x(i) * x(i)
ce = ce + y(i) * x(i) * x(i)
de = de + x(i) * y(i) * x(i) * x(i)
ee = ee + x(i) * x(i) * x(i) * x(i)
fe = fe + y(i) * y(i) * x(i) * x(i)
ge = ge + x(i) * y(i) * y(i) * x(i) * x(i)
he = he + x(i) * x(i) * y(i) * x(i) * x(i)
ie = ie + x(i) * x(i) * x(i) * x(i) * x(i)
je = je + y(i) * y(i) * y(i) * x(i) * x(i)
REM -------------
bf = bf + x(i) * y(i) * y(i)
cf = cf + y(i) * y(i) * y(i)
df = df + x(i) * y(i) * y(i) * y(i)
ef = ef + x(i) * x(i) * y(i) * y(i)
ff = ff + y(i) * y(i) * y(i) * y(i)
gf = gf + x(i) * y(i) * y(i) * y(i) * y(i)
hf = hf + x(i) * x(i) * y(i) * y(i) * y(i)
if = if + x(i) * x(i) * x(i) * y(i) * y(i)
jf = jf + y(i) * y(i) * y(i) * y(i) * y(i)
REM -------------
bg = bg + x(i) * x(i) * y(i) * y(i)
cg = cg + y(i) * x(i) * y(i) * y(i)
dg = dg + x(i) * y(i) * x(i) * y(i) * y(i)
eg = eg + x(i) * x(i) * x(i) * y(i) * y(i)
fg = fg + y(i) * y(i) * x(i) * y(i) * y(i)
gg = gg + x(i) * y(i) * y(i) * x(i) * y(i) * y(i)
hg = hg + x(i) * x(i) * y(i) * x(i) * y(i) * y(i)
ig = ig + x(i) * x(i) * x(i) * x(i) * y(i) * y(i)
jg = jg + y(i) * y(i) * y(i) * x(i) * y(i) * y(i)
REM -------------
bh = bh + x(i) * x(i) * x(i) * y(i)
ch = ch + y(i) * x(i) * x(i) * y(i)
dh = dh + x(i) * y(i) * x(i) * x(i) * y(i)
eh = eh + x(i) * x(i) * x(i) * x(i) * y(i)
fh = fh + y(i) * y(i) * x(i) * x(i) * y(i)
gh = gh + x(i) * y(i) * y(i) * x(i) * x(i) * y(i)
hh = hh + x(i) * x(i) * y(i) * x(i) * x(i) * y(i)
ih = ih + x(i) * x(i) * x(i) * x(i) * x(i) * y(i)
jh = jh + y(i) * y(i) * y(i) * x(i) * x(i) * y(i)
REM -------------
bi = bi + x(i) * x(i) * x(i) * x(i)
ci = ci + y(i) * x(i) * x(i) * x(i)
di = di + x(i) * y(i) * x(i) * x(i) * x(i)
ei = ei + x(i) * x(i) * x(i) * x(i) * x(i)
fi = fi + y(i) * y(i) * x(i) * x(i) * x(i)
gi = gi + x(i) * y(i) * y(i) * x(i) * x(i) * x(i)
hi = hi + x(i) * x(i) * y(i) * x(i) * x(i) * x(i)
ii = ii + x(i) * x(i) * x(i) * x(i) * x(i) * x(i)
ji = ji + y(i) * y(i) * y(i) * x(i) * x(i) * x(i)
REM -------------
bj = bj + x(i) * y(i) * y(i) * y(i)
cj = cj + y(i) * y(i) * y(i) * y(i)
dj = dj + x(i) * y(i) * y(i) * y(i) * y(i)
ej = ej + x(i) * x(i) * y(i) * y(i) * y(i)
fj = fj + y(i) * y(i) * y(i) * y(i) * y(i)
gj = gj + x(i) * y(i) * y(i) * y(i) * y(i) * y(i)
hj = hj + x(i) * x(i) * y(i) * y(i) * y(i) * y(i)
ij = ij + x(i) * x(i) * x(i) * y(i) * y(i) * y(i)
jj = jj + y(i) * y(i) * y(i) * y(i) * y(i) * y(i)
REM ----------------
NEXT i
m=10  !EINTRAG ANZAHL GLEICHUNGEN
n=10  !EINTRAG ANZAHL UNBEKANNTE
p1(1,1)=anz  !anz=ANZAHL DER MESSUNGEN BZW. REFERENZPUNKTE
p1(1,2)=b1   !p(m,n)=m=ZEILEN,n+1=SPALTEN; n+1=UNBEKANNTE+RESIDUUM
p1(1,3) = c1
p1(1,4) = d1
p1(1,5) = e1
p1(1,6) = f1
p1(1,7) = g1
p1(1,8) = h1
p1(1,9) = i1
p1(1,10) = j1
p1(1,11) = rr
REM -------------------------
p1(2,1) = b1
p1(2,2) = bb
p1(2,3) = cb
p1(2,4) = db
p1(2,5) = eb
p1(2,6) = fb
p1(2,7) = gb1
p1(2,8) = hb
p1(2,9) = ib
p1(2,10) = jb
p1(2,11) = br
REM -------------------------
p1(3,1) = c1
p1(3,2) = bc
p1(3,3) = cc
p1(3,4) = dc
p1(3,5) = ecc
p1(3,6) = fc
p1(3,7) = gc
p1(3,8) = hc
p1(3,9) = ic
p1(3,10) = jc
p1(3,11) = cr
REM -------------------------
p1(4,1) = d1
p1(4,2) = bd
p1(4,3) = cd
p1(4,4) = dd
p1(4,5) = ed
p1(4,6) = fd
p1(4,7) = gd
p1(4,8) = hd
p1(4,9) = id
p1(4,10) = jd
p1(4,11) = dr
REM -------------------------
p1(5,1) = e1
p1(5,2) = be
p1(5,3) = ce
p1(5,4) = de
p1(5,5) = ee
p1(5,6) = fe
p1(5,7) = ge
p1(5,8) = he
p1(5,9) = ie
p1(5,10) = je
p1(5,11) = er
REM -------------------------
p1(6,1) = f1
p1(6,2) = bf
p1(6,3) = cf
p1(6,4) = df
p1(6,5) = ef
p1(6,6) = ff
p1(6,7) = gf
p1(6,8) = hf
p1(6,9) = if
p1(6,10) = jf
p1(6,11) = fr
REM -------------------------
p1(7,1) = g1
p1(7,2) = bg
p1(7,3) = cg
p1(7,4) = dg
p1(7,5) = eg
p1(7,6) = fg
p1(7,7) = gg
p1(7,8) = hg
p1(7,9) = ig
p1(7,10) = jg
p1(7,11) = gr
REM -------------------------
p1(8,1) = h1
p1(8,2) = bh
p1(8,3) = ch
p1(8,4) = dh
p1(8,5) = eh
p1(8,6) = fh
p1(8,7) = gh
p1(8,8) = hh
p1(8,9) = ih
p1(8,10) = jh
p1(8,11) = hr
REM -------------------------
p1(9,1) = i1
p1(9,2) = bi
p1(9,3) = ci
p1(9,4) = di
p1(9,5) = ei
p1(9,6) = fi
p1(9,7) = gi
p1(9,8) = hi
p1(9,9) = ii
p1(9,10) = ji
p1(9,11) = ir
REM -------------------------
p1(10,1) = j1
p1(10,2) = bj
p1(10,3) = cj
p1(10,4) = dj
p1(10,5) = ej
p1(10,6) = fj
p1(10,7) = gj
p1(10,8) = hj
p1(10,9) = ij
p1(10,10) = jj
p1(10,11) = jr
RETURN
PROCEDURE messung
  r = 5000 !EFFEKTIVE KAMERABRENNWEITE
  z = ATN(TAN(dek(i)) * COS(ar(i) - aro)) 
  x = -r * COS(z) * TAN(ar(i) - aro) / COS(z - do)  //x-Wert Paßpunktstern der Aufnahme
  y = r * TAN(z - do)      !y-Wert Paßpunktsterrn
RETURN
 

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