Optimal Relative Coplanar Transfer in the Orbit

バージョン 1.0.0.0 (2.14 KB) 作成者: Yajur Kumar
Program for optimizing the control (specific thrust) for relative coplanar transfer in the orbit
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更新 2018/6/3

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The problem is to rendezvous the maneuvering spacecraft with the target spacecraft while optimizing the overall fuel consumption. Since, the transfer is coplanar, no out of plane terms are considered. This is a free final time optimal control problem with boundary conditions specified.

引用

Yajur Kumar (2025). Optimal Relative Coplanar Transfer in the Orbit (https://www.mathworks.com/matlabcentral/fileexchange/67607-optimal-relative-coplanar-transfer-in-the-orbit), MATLAB Central File Exchange. に取得済み.

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