Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach

This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization...

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Bibliographic Details
Published inJournal of systems science and complexity Vol. 35; no. 2; pp. 623 - 640
Main Authors Duan, Guangquan, Liu, Guo-Ping
Format Journal Article
LanguageEnglish
Published Beijing Academy of Mathematics and Systems Science, Chinese Academy of Sciences 01.04.2022
Springer Nature B.V
Subjects
Attitudes
Complex Systems
Control
Controllers
Liapunov functions
Mathematics
Mathematics and Statistics
Mathematics of Computing
Operations Research/Decision Theory
Optimal control
Orbital stability
Simulation
Spacecraft
Spacecraft stability
Statistics
Systems Theory
orbit control
Attitude control
fully-actuated system
optimal controller
combined spacecraft
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Summary:This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization control of combined spacecraft. The stability of the system is proved by introducing Lyapunov function. Numerical simulation of the combined spacecraft and physical experiment based on the combined spacecraft simulator (CSS) are completed. Both simulation and experiment results demonstrate the effectiveness and practicability of the optimal controller of fully-actuated system.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
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ISSN:1009-6124
1559-7067
DOI:10.1007/s11424-022-1492-y