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
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Updated 20 Oct 2017

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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 (2026). 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 Linux
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Version Published Release Notes
1.0.0.0

Bugs in plot title are corrected.