146 lines
		
	
	
		
			4.2 KiB
		
	
	
	
		
			Prolog
		
	
	
	
	
	
			
		
		
	
	
			146 lines
		
	
	
		
			4.2 KiB
		
	
	
	
		
			Prolog
		
	
	
	
	
	
% ----------------------------------------------------------------------
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% The Computer Language Benchmarks Game
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% http://shootout.alioth.debian.org/
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% Contributed by Anthony Borla
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% Modified to run with YAP by Glendon Holst
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% ----------------------------------------------------------------------
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:- yap_flag(unknown,error).
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:- initialization(main).
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main :-
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   unix( argv([H|_]) ), number_atom(N,H),
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   make_bodies(Bodies0),
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   energy(Bodies0, EnergyStart),
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   loop_advance(N, 0.01, Bodies0, Bodies),
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   energy(Bodies, EnergyAfter),
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   format('~9f~N~9f~N', [EnergyStart, EnergyAfter]),
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   statistics,
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   statistics_jit.
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% ------------------------------- %
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energy(Bodies, Energy) :- energy_(Bodies, 0.0, Energy).
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energy_([ _:B | Bs], Energy0, Energy) :-
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    !, B = [_X, _Y, _Z, VX, VY, VZ, Mass],
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    Energy1 is Energy0 + 0.5 * Mass * (VX * VX + VY * VY + VZ * VZ),
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   energy_diff_(B, Bs, Energy1, Energy2),
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   energy_(Bs, Energy2, Energy).
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energy_([], Energy, Energy).
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energy_diff_(Planet, [_:B | Bs], Energy0, Energy) :-
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   Planet = [X, Y, Z, _VX, _VY, _VZ, Mass],
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   B = [XT, YT, ZT, _VXT, _VYT, _VZT, MassT],
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   DX is X - XT, DY is Y - YT, DZ is Z - ZT,
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   DISTANCE is sqrt(DX * DX + DY * DY + DZ * DZ),
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   Energy1 is Energy0 - (Mass * MassT) / DISTANCE,
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   energy_diff_(Planet, Bs, Energy1, Energy).
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energy_diff_(_, [], Energy, Energy).
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% ------------------------------- %
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loop_advance(N, Dt, Bodies0, Bodies) :-
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   N > 0, !,
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   advance(Dt, Bodies0, Bodies1),
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   N1 is N - 1,
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   loop_advance(N1, Dt, Bodies1, Bodies).
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loop_advance(_, _, Bodies, Bodies).
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advance(Dt, Bodies0, Bodies) :-
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   Bodies0 = [B0 | B0s], !,
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   advance_(Dt, B0, B1, B0s, B1s),
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   advance(Dt, B1s, Bs),
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   B1 = E:[X, Y, Z, VX, VY, VZ, Mass],
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   X1 is X + Dt * VX,
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   Y1 is Y + Dt * VY,
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   Z1 is Z + Dt * VZ,
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   B = E:[X1, Y1, Z1, VX, VY, VZ, Mass],
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   Bodies = [ B | Bs].
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advance(_, Bodies, Bodies).
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advance_(Dt, Planet0, Planet, Bodies0, Bodies) :-
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   Bodies0 = [B0 | B0s], !,
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   Planet0 = E:[X, Y, Z, VX, VY, VZ, Mass],
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   B0 = ET:[XT, YT, ZT, VXT, VYT, VZT, MassT],
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   DX is X - XT, DY is Y - YT, DZ is Z - ZT,
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   DISTANCE is sqrt(DX * DX + DY * DY + DZ * DZ),
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   Mag is Dt / (DISTANCE * DISTANCE * DISTANCE),
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   VX1 is VX - DX * MassT * Mag,
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   VY1 is VY - DY * MassT * Mag,
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   VZ1 is VZ - DZ * MassT * Mag,
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   VXT1 is VXT + DX * Mass * Mag,
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   VYT1 is VYT + DY * Mass * Mag,
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   VZT1 is VZT + DZ * Mass * Mag,
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   Planet3 = E:[X, Y, Z, VX1, VY1, VZ1, Mass],
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   advance_(Dt, Planet3, Planet, B0s, Bs),
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   B = ET:[XT, YT, ZT, VXT1, VYT1, VZT1, MassT],
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   Bodies = [B | Bs].
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advance_(_, P, P, Bs, Bs).
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% ------------------------------- %
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make_bodies(Bodies) :-
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   SOLAR_MASS = 3.9478417604357432000e+01,
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   Bodies0 =
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   [
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      jupiter:[4.84143144246472090e+00, -1.16032004402742839e+00,
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         -1.03622044471123109e-01, 6.06326392995832020e-01,
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         2.811986844916260200e+00, -2.5218361659887636e-02,
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         3.7693674870389486e-02],
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      saturn:[8.34336671824457987e+00, 4.12479856412430479e+00,
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         -4.03523417114321381e-01, -1.010774346178792400e+00,
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         1.825662371230411900e+00, 8.415761376584154e-03,
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         1.1286326131968767e-02],
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      uranus:[1.28943695621391310e+01, -1.51111514016986312e+01,
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         -2.23307578892655734e-01, 1.082791006441535600e+00,
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         8.68713018169607890e-01, -1.0832637401363636e-02,
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         1.723724057059711e-03],
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      neptune:[1.53796971148509165e+01, -2.59193146099879641e+01,
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         1.79258772950371181e-01, 9.79090732243897980e-01,
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         5.94698998647676060e-01, -3.4755955504078104e-02,
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         2.033686869924631e-03]
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   ],
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   Sun0 = sun:[0.0, 0.0, 0.0, 0.0, 0.0, 0.0, SOLAR_MASS],
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   offset_momentum(Sun0, Sun, Bodies0, SOLAR_MASS),
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   Bodies = [Sun | Bodies0].
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% ------------- %
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offset_momentum(Sun0, Sun, Bodies, SOLAR_MASS) :-
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   offset_momentum_(Bodies, [0.0, 0.0, 0.0], [PX, PY, PZ]),
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   Sun0 = E:[X, Y, Z, VX, VY, VZ, Mass],
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   VX1 is -(PX / SOLAR_MASS),
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   VY1 is -(PY / SOLAR_MASS),
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   VZ1 is -(PZ / SOLAR_MASS),
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   Sun = E:[X, Y, Z, VX1, VY1, VZ1, Mass].
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offset_momentum_([_:E|Bs], Pt0, Pt) :-
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   E = [_X, _Y, _Z, VX, VY, VZ, Mass],
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   Pt0 = [PX, PY, PZ],
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   PX1 is PX + VX * Mass,
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   PY1 is PY + VY * Mass,
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   PZ1 is PZ + VZ * Mass,
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   offset_momentum_(Bs, [PX1, PY1, PZ1], Pt).
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offset_momentum_([], Pt, Pt).
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% ------------------------------- %
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