Description: Using the CW equation, use the minimum energy, the use of pulse thrust, to achieve in a day two spacecraft rendezvous and docking. Is essentially an intersection orbit optimization problem, by the given conditions to optimize the selection of design variables, so that the objective function to get the optimal value.
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File list (Check if you may need any files):
C-W\computedetaV.m
...\compute_r_v.m
...\C_W.m
...\main.m
...\R_V_aftersometime.m
...\test.m
C-W
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