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Fractional Order Sliding Mode based Attitude-Orbit Integrated Control for Rigid-Flexible Coupled Spacecraft

Published Online: 2025-10-30

Published Print: 2025-12

Authors

Ma, Songjing

Wang, Dian

Wu, Xiande

Wu, Yunhua https://orcid.org/0000-0002-7012-1559
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (61973153)
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Text and Data Mining valid from 2025-10-30

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Article History

Received: 5 March 2025

Revised: 30 June 2025

Accepted: 12 August 2025

First Online: 30 October 2025

Declarations

:

: The authors have no competing interests to declare that are relevant to the content of this article.

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