Abstract
This paper proposes a fault-tolerant back-stepping control method for the hypersonic flight vehicle. An adaptive law is proposed to make sure that the normal actuators could compensate the ineffective actuators while failure exists. Meanwhile, the RBF NN is employed to estimate the unknown nonlinearity of the model. The simulation results verify the effectiveness of the proposed approach.
This work was supported by National Natural Science Foundation of China (61622308), Aeronautical Science Foundation of China (2015ZA53003), Natural Science Basic Research Plan in Shaanxi Province (2016KJXX-86), Fundamental Research Funds of Shenzhen Science and Technology Project (JCYJ20160229172341417).
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Guo, Y., Wang, Q., Xu, B. (2017). Robust Adaptive Neural Fault-Tolerant Control of Hypersonic Flight Vehicle. In: Sun, F., Liu, H., Hu, D. (eds) Cognitive Systems and Signal Processing. ICCSIP 2016. Communications in Computer and Information Science, vol 710. Springer, Singapore. https://doi.org/10.1007/978-981-10-5230-9_5
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DOI: https://doi.org/10.1007/978-981-10-5230-9_5
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