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

机译:超音速车辆纵向动力学对致动器饱和度扰动的自适应BackStepping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向控制策略,以解决对致动器饱和度和干扰的超音速车辆(HSV)的纵向控制问题。小扰动线性化将动力学转换为每个修剪点的借调系统,具有完全干扰,包括未拼件的动态,参数不确定度和外部干扰。通过扩展状态观察者(ESO)可以估计和补偿扰动,因此系统分离。为了处理执行器饱和度和宽飞行信封,设计了一种自适应的反向控制策略。提供了Lyapunov方法的严格有限时间收敛证明。在模拟中验证了所提出的控制方案的有效性。

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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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