Spacecraft attitude fault tolerant control based on multi-objective optimization

• Autorzy: Moradi Rouzbeh , Alikhani Alireza , Fathi Jegarkandi Mohsen

Identyfikatory

DOI

10.15632/jtam-pl/125008

• Języki publikacji: EN

Abstrakty

EN

An active fault tolerant controller is designed for the attitude control of a faulty spacecraft. Feedback linearization and Lyapunov’s direct method are used to solve angular velocity equations and to ensure convergence of the system outputs to reference inputs, respectively. In order to ensure finite time convergence, final time constraints are proposed. Three con- structive objective functions are considered as performance measures and optimized using multi-objective optimization. The results show that the outputs converge to the reference attitudes, even for severe actuator faults/failures.

Słowa kluczowe

EN

active fault-tolerant control; spacecraft attitude control; finite time convergence; Pareto-optimal set

• Wydawca: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
• Czasopismo: Journal of Theoretical and Applied Mechanics
• Rocznik: 2020
• Tom: Vol. 58 nr 4
• Strony: 983--996
• Opis fizyczny: Bibliogr. 22 poz., rys., tab.

Twórcy

autor

Moradi Rouzbeh

• Aerospace Research Institute, Ministry of Science, Research and Technology, Tehran, Iran

autor

Alikhani Alireza

• Aerospace Research Institute, Ministry of Science, Research and Technology, Tehran, Iran

autor

Fathi Jegarkandi Mohsen

• Sharif University of Technology, Department of Aerospace Engineering, Tehran, Iran

Bibliografia

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Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).