Robust control for satellite attitude regulation during on-orbit assembly

Lingling Shi; Nathan Kinkaid; Jayantha Katupitiya

doi:10.1109/TAES.2016.140472

Robust control for satellite attitude regulation during on-orbit assembly

Lingling Shi
, Nathan Kinkaid
, Jayantha Katupitiya

University of New South Wales

科研成果: 期刊稿件 › 文章 › 同行评审

35 引用（Scopus）

摘要

In the future, large satellites may be automatically assembled on-orbit in order to reduce weight and increase volume efficiency in launchers. During this process, it may be important to maintain satellite attitude. This paper presents a dynamic model, including reaction wheels and a twisting-algorithm-based sliding-mode controller, to maintain attitude during a simple self-assembly process. Simulation results of this controller are compared with results from other controllers found in the literature.

源语言	英语
期刊论文编号	7444031
页（从-至）	49-59
页数	11
期刊	IEEE Transactions on Aerospace and Electronic Systems
卷	52
期	1
DOI	https://doi.org/10.1109/TAES.2016.140472
出版状态	已出版 - 2月 2016
已对外发布	是

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10.1109/TAES.2016.140472

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Robust control for satellite attitude regulation during on-orbit assembly

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