文件名称:fly_to_the_Mars
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Control optimisation. It is example of use BFGS algorithm to control satellite form Earth atmosphere to the Mars. Controled is engine power (bang-bang type) and angle of nozze.
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fly to the Mars
...............\bfgs_alg.asv
...............\bfgs_alg.m
...............\bfgs_f_celu.m
...............\bfgs_f_celu2.asv
...............\bfgs_f_celu2.m
...............\bfgs_f_celu_grad.asv
...............\bfgs_f_celu_grad.m
...............\bfgs_min_kier.m
...............\bfgs_u2_alg.asv
...............\bfgs_u2_alg.m
...............\bfgs_u2_f_celu_grad.asv
...............\bfgs_u2_f_celu_grad.m
...............\bfgs_u2_min_kier.m
...............\daj_q.m
...............\hs_err_pid3656.log
...............\main.m
...............\rhs.m
...............\rhs_adj.m
...............\rk4.asv
...............\rk4.m
...............\rk4_adj.asv
...............\rk4_adj.m
...............\wylicz_ffprzel.m
...............\wylicz_t.m
...............\wylicz_u1.m
...............\wylicz_u2.m
...............\zmien_u2.m
...............\bfgs_alg.asv
...............\bfgs_alg.m
...............\bfgs_f_celu.m
...............\bfgs_f_celu2.asv
...............\bfgs_f_celu2.m
...............\bfgs_f_celu_grad.asv
...............\bfgs_f_celu_grad.m
...............\bfgs_min_kier.m
...............\bfgs_u2_alg.asv
...............\bfgs_u2_alg.m
...............\bfgs_u2_f_celu_grad.asv
...............\bfgs_u2_f_celu_grad.m
...............\bfgs_u2_min_kier.m
...............\daj_q.m
...............\hs_err_pid3656.log
...............\main.m
...............\rhs.m
...............\rhs_adj.m
...............\rk4.asv
...............\rk4.m
...............\rk4_adj.asv
...............\rk4_adj.m
...............\wylicz_ffprzel.m
...............\wylicz_t.m
...............\wylicz_u1.m
...............\wylicz_u2.m
...............\zmien_u2.m