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Adaptive Backstepping Control for Longitudinal Dynamics of Hypersonic Vehicle Subject to Actuator Saturation and Disturbance

机译:高超声速飞行器纵向动态特性的自适应反演控制

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摘要

In this paper, an adaptive backstepping control strategy is presented to solve the longitudinal control problem for a hypersonic vehicle (HSV) subject to actuator saturation and disturbances. Small perturbation linearization transforms the dynamics to a seconded-order system at each trimming point, with total disturbance including unmodeled dynamics, parametric uncertainties, and external disturbances. The disturbance can be estimated and compensated for by an extended state observer (ESO), and thus the system is decoupled. To deal with the actuator saturation and wide flight envelope, an adaptive backstepping control strategy is designed. A rigorous proof of finite-time convergence is provided applying Lyapunov method. The effectiveness of the proposed control scheme is verified in simulations.
机译:在本文中,提出了一种自适应反步控制策略,以解决高超声速飞行器(HSV)在执行器饱和和干扰情况下的纵向控制问题。小扰动线性化可在每个微调点将动力学转换为二阶系统,总扰动包括未建模的动力学,参数不确定性和外部扰动。干扰可以通过扩展状态观察器(ESO)进行估计和补偿,从而使系统解耦。为了应对执行器饱和和较大的飞行范围,设计了一种自适应反推控制策略。利用Lyapunov方法提供了严格的有限时间收敛性证明。仿真结果验证了所提控制方案的有效性。

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  • 来源
    《Mathematical Problems in Engineering》 |2019年第5期|1019621.1-1019621.10|共10页
  • 作者单位

    Beijing Inst Technol, Sch Automat, Beijing, Peoples R China|Beijing Aerosp Automat Control Inst, Beijing, Peoples R China;

    Beijing Aerosp Automat Control Inst, Beijing, Peoples R China;

    Beijing Aerosp Automat Control Inst, Beijing, Peoples R China;

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