Constant thrust fuel-optimal control for spacecraft rendezvous

Author:

Qi Yongqiang,Jia Yingmin

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference29 articles.

1. Safe trajectories for autonomous rendezvous of spacecraft;Breger;J. Guid. Control Dynam.,2008

2. Optimal power-limited rendezvous with upper and lower bounds on thrust;Carter;J. Guid. Control Dynam.,1996

3. Drag-free and attitude control for the GOCE satellite;Enrico;Automatica,2008

4. Differentially flat systems with inequality constraints: an approach to real-time feasible trajectory generation;Faiz;J. Guid. Control Dynam.,2001

5. Automated Rendezvous and Docking of Spacecraft;Fehse,2003

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1. Feedback Control for Directional Rendezvous Using Constant-Magnitude Low Thrust;J GUID CONTROL DYNAM;2024

2. Spacecraft Rendezvous Using Constant-Magnitude Low Thrust;Journal of Guidance, Control, and Dynamics;2023-11

3. Impulsive guidance of optimal pursuit with conical imaging zone for the evader;Aerospace Science and Technology;2023-11

4. A feasible study on the model predictive control for docking approach of small spacecraft using thrusters and a control moment gyro;2023 IEEE/ASME International Conference on Advanced Intelligent Mechatronics (AIM);2023-06-28

5. An experimental maneuver control for rendezvous and autonomous docking of a small spacecraft;SICE Journal of Control, Measurement, and System Integration;2023-03-17

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