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

Research output: Contribution to journal › Article › peer-review

31 Citations (Scopus)

Abstract

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.

Original language	English
Article number	7444031
Pages (from-to)	49-59
Number of pages	11
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	52
Issue number	1
DOIs	https://doi.org/10.1109/TAES.2016.140472
Publication status	Published - Feb 2016
Externally published	Yes

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Shi, L., Kinkaid, N., & Katupitiya, J. (2016). Robust control for satellite attitude regulation during on-orbit assembly. IEEE Transactions on Aerospace and Electronic Systems, 52(1), 49-59. Article 7444031. https://doi.org/10.1109/TAES.2016.140472

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Robust control for satellite attitude regulation during on-orbit assembly

Abstract

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