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Hybrid non-fragile attitude takeover control of modular spacecraft with communication delay

Ziyu YANG Yibo DING Ran TAO Xiaokui YUE

Chinese Journal of Aeronautics2025，Vol.38Issue(11)：P.469-486,18.

Chinese Journal of Aeronautics2025，Vol.38Issue(11)：P.469-486,18.DOI:10.1016/j.cja.2025.103763

Hybrid non-fragile attitude takeover control of modular spacecraft with communication delay

Ziyu YANG ¹Yibo DING ¹Ran TAO ¹Xiaokui YUE¹

作者信息

1. Research&Development Institute of Northwestern Polytechnical University in Shenzhen,Shenzhen 518063,China School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China
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摘要

关键词

Attitude stabilization/Communication delay/Hybrid non-fragile/Modular spacecraft/Takeover control

分类

航空航天

引用本文复制引用

Ziyu YANG,Yibo DING,Ran TAO,Xiaokui YUE..Hybrid non-fragile attitude takeover control of modular spacecraft with communication delay[J].Chinese Journal of Aeronautics,2025,38(11):P.469-486,18.

基金项目

co-supported by the National Natural Science Foundation of China(No.12372048) （No.12372048）

the China Postdoctoral Science Foundation(No.2023M742835) （No.2023M742835）

the Guangdong Basic and Applied Basic Research Foundation,China(No.2023A1515011421) （No.2023A1515011421）

the Aeronautical Science Foundation of China(No.2022Z004053001) （No.2022Z004053001）

the Fundamental Research Funds for the Central Universities,China(No.D5000210833) （No.D5000210833）

the Young Talent Fund of Association for Science and Technology in Shaanxi,China(No.20220509)。（No.20220509）

Chinese Journal of Aeronautics

ISSN：1000-9361

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