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Adaptive Exponential Time-Varying Sliding mode Control for Hypersonic Cruise Vehicles

机译:高超音速巡航飞行器的自适应指数时变滑模控制

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This paper describes the design of an adaptive exponential time-varying sliding mode control (AETVSMC) with strong robustness for hypersonic cruise vehicles subject to parametric uncertainties on the inertial and aerodynamic coefficients. An adaptation scheme is adopted to deal with unknown but bounded system uncertainties. Thus, the selection of switching gains can be obtained on-line and the upper bounds of the model uncertainties are not required to be known in advance. Stability analysis of the closed-loop system is derived based on the Lyapunov theory. Finally, simulation results demonstrate the effectiveness and robustness of the proposed approach.
机译:本文描述了具有惯性和空气动力系数参数不确定性的高超音速巡航飞行器具有强健壮性的自适应指数时变滑模控制(AETVSMC)的设计。采用自适应方案来处理未知但有界的系统不确定性。因此,可以在线获得切换增益的选择,并且不需要预先知道模型不确定性的上限。基于李雅普诺夫理论推导了闭环系统的稳定性。最后,仿真结果证明了该方法的有效性和鲁棒性。

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