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Sliding mode disturbance observer-enhanced adaptive control for the air-breathing hypersonic flight vehicle

机译:呼吸高超声速飞行器的滑模干扰观测器增强自适应控制

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摘要

This paper presents a backstepping procedure to design an adaptive controller for the air-breathing hypersonic flight vehicle (AHFV) subject to external disturbances and actuator saturations. In each step, a sliding mode exact disturbance observer (SMEDO) is exploited to exactly estimate the lumped disturbance in finite time. Specific dynamics are introduced to handle the possible actuator saturations. Based on SMEDO and introduced dynamics, an adaptive control law is designed, along with the consideration on "explosion of complexity" in backstepping design. The developed controller is equipped with fast disturbance rejection and great capability to accommodate the saturated actuators, which also lead to a wider application scope. A simulation study is provided to show the effectiveness and superiority of the proposed controller.
机译:本文提出了一种反推程序,以设计一种适用于遭受外部干扰和执行器饱和的空气呼吸高超音速飞行器(AHFV)的自适应控制器。在每个步骤中,均采用滑模精确干扰观测器(SMEDO)来精确估计有限时间内的集总干扰。引入了特定的动力学特性来处理可能的执行器饱和。基于SMEDO并介绍了动力学,设计了自适应控制律,并在后推设计中考虑了“复杂性的爆炸”。所开发的控制器具有快速的抗干扰能力,并且能够容纳饱和的执行器,这也导致了更广泛的应用范围。仿真研究表明了所提出控制器的有效性和优越性。

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