Optimal Relative Coplanar Transfer in the Orbit

Version 1.0.0.0 (2.14 KB) by Yajur Kumar
Program for optimizing the control (specific thrust) for relative coplanar transfer in the orbit
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Updated 3 Jun 2018

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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.

Cite As

Yajur Kumar (2024). 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. Retrieved .

MATLAB Release Compatibility
Created with R2018a
Compatible with any release
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Version Published Release Notes
1.0.0.0