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Concise Neural Nonaffine Control of Air-Breathing Hypersonic Vehicles Subject to Parametric Uncertainties

机译:带有参数不确定性的气动超音速飞行器的精确神经非仿射控制

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摘要

In this paper, a novel simplified neural control strategy is proposed for the longitudinal dynamics of an air-breathing hypersonic vehicle (AHV) directly using nonaffine models instead of affine ones. For the velocity dynamics, an adaptive neural controller is devised based on a minimal-learning parameter (MLP) technique for the sake of decreasing computational loads. The altitude dynamics is rewritten as a pure feedback nonaffine formulation, for which a novel concise neural control approach is achieved without backstepping. The special contributions are that the control architecture is concise and the computational cost is low. Moreover, the exploited controller possesses good practicability since there is no need for affine models. The semiglobally uniformly ultimate boundedness of all the closed-loop system signals is guaranteed via Lyapunov stability theory. Finally, simulation results are presented to validate the effectiveness of the investigated control methodology in the presence of parametric uncertainties.
机译:在本文中,提出了一种新颖的简化神经控制策略,用于直接使用非仿射模型而不是仿射模型来对呼吸高超音速飞行器(AHV)的纵向动力学进行控制。对于速度动力学,为了减少计算量,基于最小学习参数(MLP)技术设计了一种自适应神经控制器。高度动态被重写为纯反馈非仿射公式,为此,可以实现一种新颖的简洁的神经控制方法而不会退步。特别的贡献是控制体系结构简洁,计算成本低。此外,由于不需要仿射模型,因此开发的控制器具有良好的实用性。通过Lyapunov稳定性理论可以保证所有闭环系统信号的半全局一致的极限极限。最后,提出了仿真结果以验证在存在参数不确定性的情况下所研究控制方法的有效性。

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  • 来源
    《International journal of aerospace engineering》 |2017年第2期|1374932.1-1374932.16|共16页
  • 作者单位

    Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China;

    Air Force Engn Univ, Sci Coll, Xian 710051, Shaanxi, Peoples R China;

    Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China;

    Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China;

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  • 正文语种 eng
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  • 入库时间 2022-08-18 00:05:38

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