Neural Back-Stepping Control of Hypersonic Flight Vehicle with Actuator Fault

This paper addresses the fault-tolerant control of hypersonic flight vehicle. To estimate the unknown function in flight dynamics, neural networks are employed in controller design. Moreover, in order to compensate the actuator fault, an adaptive signal is introduced in the controller design to esti...

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Bibliographic Details
Main Authors: Qi Wu, Yuyan Guo
Format: Article
Language:English
Published: Wiley 2018-01-01
Series:Journal of Control Science and Engineering
Online Access:http://dx.doi.org/10.1155/2018/2198423
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