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
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