Reconfigurable fault-tolerant attitude control for over-actuated hypersonic flight vehicle with actuator failures

This paper proposes a novel fast attitude fault-tolerant control (FTC) scheme for over-actuated hypersonic flight vehicles experiencing actuator failures, such as stuck faults and loss of effectiveness faults. The FTC scheme comprises two main components: a systematic algorithm in the control layer...

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Bibliografische Detailangaben

Hauptverfasser:	Ao Li, Xiaoxiang Hu, Kejun Dong, Hongzeng Li, Bing Xiao
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	Elsevier 2025-02-01
Schriftenreihe:	Alexandria Engineering Journal
Schlagworte:	Fault-tolerant control Control allocation Model predictive static programming Hypersonic flight vehicles
Online-Zugang:	http://www.sciencedirect.com/science/article/pii/S1110016824015606
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