📄 g3plan.m
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function ans=g3plan (J)
% Generic program to accumulate sum of trigonometric series for 3 variables
% Use to calculate heliocentric ecliptic polar coordinates of earth-moon barycenter (J2000)
% input: TDT Julian date
% return : heliocentric ecliptic polar coordinates of earth-moon barycenter(J2000)
plan=ear404;
objnum=3;
header ; % common constant
mean_elements ;
T = (J - J2000) / plan.timescale;
n = plan.maxargs;
% Calculate sin( i*MM ),cos(i*MM), etc. for needed multiple angles.
for i =1:n
if plan.max_harmonic(i)>0
for j =1: plan.max_harmonic(i)
ss(i,j)=sin(j*Args(i));
cc(i,j)=cos(j*Args(i));
end
end
end
% Point to start of table of arguments.
p = plan.arg_tbl;
ip=1; % array index
%Point to tabulated cosine and sine amplitudes.
pl = plan.lon_tbl;
ipl=1; % array index
pb = plan.lat_tbl;
ipb=1; % array index
pr = plan.rad_tbl;
ipr=1; % array index
sl = 0.0;
sb = 0.0;
sr = 0.0;
while 1==1
% argument of sine and cosine
% Number of periodic arguments.
np = p(ip);
ip=ip+1;
if (np < 0)
break;
end
if np == 0 % It is a polynomial term.
nt = p(ip);
ip=ip+1;
%"Longitude" polynomial (phi).
cu = pl(ipl);
ipl=ipl+1;
for i = 1:nt
cu = cu * T + pl(ipl);
ipl=ipl+1;
end
sl =sl+ cu;
% "Latitude" polynomial (theta).
cu = pb(ipb);
ipb=ipb+1;
for i =1:nt
cu = cu * T + pb(ipb);
ipb=ipb+1;
end
sb =sb+ cu;
% Radius polynomial (psi).
cu = pr(ipr);
ipr=ipr+1;
for i=1:nt
cu = cu * T + pr(ipr);
ipr=ipr+1;
end
sr =sr+ cu;
else
k1 = 0;
cv = 0.0;
sv = 0.0;
for i=1:np
% What harmonic.
j = p(ip);
ip=ip+1;
% Which planet.
m = p(ip) - 1;
ip=ip+1;
if (j~=0)
k = abs (j)-1 ;
su = ss(m+1,k+1); % sin(k*angle)
if (j < 0)
su = -su;
end
cu = cc(m+1,k+1);
if (k1 == 0)
% set first angle
sv = su;
cv = cu;
k1 = 1;
else
% combine angles
t = su * cv + cu * sv;
cv = cu * cv - su * sv;
sv = t;
end %if
end
end % end of for
% Highest power of T.
nt =p(ip);
ip=ip+1;
% Longitude.
cu = pl(ipl);
ipl=ipl+1;
su = pl(ipl);
ipl=ipl+1;
for i= 1:nt
cu = cu * T + pl(ipl);
ipl=ipl+1;
su = su * T + pl(ipl);
ipl=ipl+1;
end
sl =sl+ cu * cv + su * sv;
% Latitiude.
cu = pb(ipb);
ipb=ipb+1;
su = pb(ipb);
ipb=ipb+1;
for i= 1:nt
cu = cu * T + pb(ipb);
ipb=ipb+1;
su = su * T + pb(ipb);
ipb=ipb+1;
end
sb =sb+ cu * cv + su * sv;
% Radius.
cu = pr(ipr);
ipr=ipr+1;
su = pr(ipr);
ipr=ipr+1;
for i= 1:nt
cu = cu * T + pr(ipr);
ipr=ipr+1;
su = su * T + pr(ipr);
ipr=ipr+1;
end
sr =sr+ cu * cv + su * sv;
end % end if np>0
end % end while
t = plan.trunclvl;
pobj(1) = Args(objnum) + STR * t * sl;
pobj(2) = STR * t * sb;
pobj(3) = plan.distance * (1.0+ STR * t * sr);
ans=pobj;
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