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Nonlinear Disturbance Observer-Based Adaptive Sliding Mode Control for a Generic Hypersonic Vehicle

机译:通用高超音速飞行器基于非线性干扰观测器的自适应滑模控制

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In this paper, a new adaptive sliding mode control method is presented for the longitudinal model of a generic hypersonic vehicle subject to uncertainties and external disturbance. Firstly, an oriented-control model with mismatched uncertainties is built for a generic hypersonic vehicle. Secondly, the back-stepping technique is introduced to design a sliding mode controller with an adaptive law to adapt to the disturbance and uncertainty. Thirdly, a set of nonlinear disturbance observers are designed to estimate the lumped disturbance and compensate the sliding mode controller, and the stability of the proposed controller is analyzed by utilizing Lyapunov stability theory. Finally, simulation results show that the effectiveness of the proposed controller is validated by the nonlinear model and the proposed method exhibits promising robustness to mismatched uncertainties.
机译:本文提出了一种新的自适应滑模控制方法,该方法适用于具有不确定性和外部干扰的通用超音速飞行器的纵向模型。首先,为通用高超音速飞行器建立了具有不匹配不确定性的定向控制模型。其次,引入反步技术来设计具有自适应律的滑模控制器,以适应干扰和不确定性。第三,设计了一组非线性扰动观测器来估计集总扰动并补偿滑模控制器,并利用李雅普诺夫稳定性理论分析了所提出控制器的稳定性。最后,仿真结果表明,所提控制器的有效性通过非线性模型验证,所提方法对不匹配不确定性具有良好的鲁棒性。

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