摘要
An adaptive neural control scheme is proposed for a class of generic hypersonic flight vehicles. The main advantages of the proposed scheme include the following: (1) a new constraint variable is defined to generate the virtual control that forces the tracking error to fall within prescribed boundaries; (2) RBF NNs are employed to compensate for complex and uncertain terms to solve the problem of controller complexity; (3) only one parameter needs to be updated online at each design step, which significantly reduces the computational burden. It is proved that all signals of the closed-loop system are uniformly ultimately bounded. Simulation results are presented to illustrate the effectiveness of the proposed scheme.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 591789 |
| 期刊 | Mathematical Problems in Engineering |
| 卷 | 2015 |
| DOI | |
| 出版状态 | 已出版 - 2015 |
指纹
探究 'Neural Network-Based Adaptive Backstepping Control for Hypersonic Flight Vehicles with Prescribed Tracking Performance' 的科研主题。它们共同构成独一无二的指纹。引用此
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