Optimizing the Control Input Trajectory (Co-Planar Case)

Version 1.0.0.0 (6.26 KB) by Yajur Kumar
Trajectory Optimization for Relative Transfer Around a Central Body
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Updated 20 Oct 2017

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This program uses the MATLAB Symbolic Toolbox and Value Presicion Arithmatic Operations to optimize the control input trajectory of a maneuvering spacecraft relative to a target spacecraft around a central body using the co-planar Clohessey-Wiltshire model.

Cite As

Yajur Kumar (2025). Optimizing the Control Input Trajectory (Co-Planar Case) (https://www.mathworks.com/matlabcentral/fileexchange/64790-optimizing-the-control-input-trajectory-co-planar-case), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2016b
Compatible with any release
Platform Compatibility
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Version Published Release Notes
1.0.0.0