Relative Orbit Low-Thrust Trajectory Optimization

Versione 1.0.0.0 (1,45 KB) da Yajur Kumar
Program to calculate the optimized control input trajectory for relative orbital motion
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Aggiornato 20 ott 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.

Cita come

Yajur Kumar (2025). Relative Orbit Low-Thrust Trajectory Optimization (https://it.mathworks.com/matlabcentral/fileexchange/64791-relative-orbit-low-thrust-trajectory-optimization), MATLAB Central File Exchange. Recuperato .

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Versione Pubblicato Note della release
1.0.0.0

Bugs in plot title are corrected.