Relative Orbit Low-Thrust Trajectory Optimization
Version 1.0.0.0 (1.45 KB) by
Yajur Kumar
Program to calculate the optimized control input trajectory for relative orbital motion
This is the program for optimizing the control input trajectory for the co-planar relative motion using HCW (Hill-Clohessey-Wiltshire) model. The program uses bvp4c solver for solving the resulting state equations.
Cite As
Yajur Kumar (2024). Relative Orbit Low-Thrust Trajectory Optimization (https://www.mathworks.com/matlabcentral/fileexchange/64791-relative-orbit-low-thrust-trajectory-optimization), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Created with
R2015b
Compatible with any release
Platform Compatibility
Windows macOS LinuxCategories
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Version | Published | Release Notes | |
---|---|---|---|
1.0.0.0 | Bugs in plot title are corrected. |