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2016 | OriginalPaper | Buchkapitel

26. Sliding Mode Fault-Tolerant Control for Air-Breathing Hypersonic Vehicles with External Disturbances

verfasst von : Wei Huang, Yingmin Jia

Erschienen in: Proceedings of the 2015 Chinese Intelligent Systems Conference

Verlag: Springer Berlin Heidelberg

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Abstract

This paper studies the fault-tolerant control for air-breathing hypersonic flight vehicles(AHFVs) subject to both actuator faults and external disturbances. The overall procedure includes the feedback linearization of the model and the adaptive sliding mode control design. Specifically, a feedback linearized model of AHFVs is firstly obtained with the actuator faults and external disturbances. Then, two adaptive laws are designed to approximately estimate their unknown bounds. Based on the Lyapunov analysis method, it is proved that adaptive sliding mode control law can achieve the asymptotic tracking of all commands signals and guarantee the stability of the system. Simulations are conducted to confirm the efficacy of the proposed control method.

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Metadaten
Titel
Sliding Mode Fault-Tolerant Control for Air-Breathing Hypersonic Vehicles with External Disturbances
verfasst von
Wei Huang
Yingmin Jia
Copyright-Jahr
2016
Verlag
Springer Berlin Heidelberg
DOI
https://doi.org/10.1007/978-3-662-48386-2_26