Abstract
This paper proposes a method for fault tolerant control. The design is based on an \(\mathcal{L}{}_{1}\) adaptive controller with a nominal reference model and a set of degraded reference models. In a degraded model the criteria of stability margins and performance bounds are reduced. The simulation results, for the altitude hold control of a small fixed-wing UAV, show good compromise between performance and robustness against faults and large uncertainties.
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Souanef, T., Fichter, W. (2015). Fault Tolerant \(\mathcal{L}{}_{1}\) Adaptive Control Based on Degraded Models. In: Bordeneuve-Guibé, J., Drouin, A., Roos, C. (eds) Advances in Aerospace Guidance, Navigation and Control. Springer, Cham. https://doi.org/10.1007/978-3-319-17518-8_9
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DOI: https://doi.org/10.1007/978-3-319-17518-8_9
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-17517-1
Online ISBN: 978-3-319-17518-8
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