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Sliding mode disturbance observer–based adaptive tracking control for hypersonic reentry vehicle:

机译:基于滑模干扰观测器的高超声速再入飞行器自适应跟踪控制:

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Aiming at attitude tracking control for hypersonic reentry vehicle, an adaptive backstepping controller based on sliding mode disturbance observer is proposed in this article. First, the strict-feedback nonlinear model with uncertain aerodynamic parameters and external disturbances for the hypersonic reentry vehicle is established. Then, a sliding mode disturbance observer is designed to estimate external disturbances for the proposed controller. In addition, the adaptive backstepping controller with the sliding mode disturbance observer is proposed, in which adaptive strategies are used to estimate the uncertain aerodynamic parameters online. Finally, according to the Lyapunov theorem, the tracking errors of the closed-loop attitude stabilization system are proved to be ultimately bounded. Simulation results show that the proposed controller can achieve adaptive tracking control under the influences of parameter perturbation and external disturbances.
机译:针对高超声速再入飞行器的姿态跟踪控制,提出了一种基于滑模扰动观测器的自适应反推控制器。首先,建立了具有不确定的空气动力学参数和外部干扰的高超声速再入飞行器的严格反馈非线性模型。然后,设计了一种滑模干扰观测器,以估算所提出控制器的外部干扰。此外,提出了一种具有滑模扰动观测器的自适应反推控制器,其中采用自适应策略在线估计不确定的空气动力学参数。最后,根据李雅普诺夫定理,证明了闭环姿态稳定系统的跟踪误差是最终有界的。仿真结果表明,所提出的控制器在参数摄动和外部干扰的影响下可以实现自适应跟踪控制。

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