Optimal Control of Fully-Actuated Systems for Spacecraft Rendezvous

In this paper, the rigid spacecraft rendezvous problem is studied in the sense of fully-actuated system. According to the attitude and orbit dynamics, the fully-actuated system model is established. And the linear quadratic optimal controller of the fully-actuated system is designed for spacecraft r...

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Bibliographic Details
Main Authors: Duan, Guang-Quan, Liu, Guo-Ping
Format: Conference Proceeding
Language:English
Subjects:
Attitude control
Attitude Stabilization
Fully-Actuated System
Numerical models
Numerical simulation
Optimal control
Optimal Controller
Orbit Control
Orbits
Space vehicles
Spacecraft Rendezvous
Task analysis
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Description
Summary:In this paper, the rigid spacecraft rendezvous problem is studied in the sense of fully-actuated system. According to the attitude and orbit dynamics, the fully-actuated system model is established. And the linear quadratic optimal controller of the fully-actuated system is designed for spacecraft rendezvous task. Finally, numerical simulation and physical experiment are considered. Both simulation and experiment results indicate the effectiveness and practicability of the optimal controller.
ISSN:2161-2927
DOI:10.23919/CCC55666.2022.9902246