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.
CITATION STYLE
Guo, Y., Wang, Q., & Xu, B. (2017). Robust adaptive neural fault-tolerant control of hypersonic flight vehicle. In Communications in Computer and Information Science (Vol. 710, pp. 44–51). Springer Verlag. https://doi.org/10.1007/978-981-10-5230-9_5
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