Optimizing the Control Input Trajectory (Co-Planar Case)
Trajectory Optimization for Relative Transfer Around a Central Body
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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 (2026). Optimizing the Control Input Trajectory (Co-Planar Case) (https://in.mathworks.com/matlabcentral/fileexchange/64790-optimizing-the-control-input-trajectory-co-planar-case), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.0.0.0 (6.26 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0.0 |
