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A Robust Control Scheme for a PVTOL System Subject to Wind Disturbances

机译:一种鲁棒控制方案,适用于风扰动的PVTOL系统

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In this study, a control scheme that allows performing height position regulation and stabilization for an unmanned planar vertical take-off and landing aerial vehicle, in the presence of disturbance due to wind, is presented. To this end, the backstepping procedure together with nested saturation function method is used. Firstly, a convenient change of coordinates in the aerial vehicle model is carried out to dissociate the rotational dynamics from the translational one. Secondly, the backstepping procedure is applied to obtain the height position controller, allowing the reduction of the system and expressing it as an integrator chain with nonlinear disturbance. Therefore, the nested saturation function method is used to obtain a stabilizing controller for the horizontal position and roll angle. The corresponding stability analysis is conducted via the Lyapunov second method. In addition, to estimate the disturbance due to wind, an extended state observer is used. The effectiveness of the proposed control scheme is assessed through numerical simulations, from which convincing results have been obtained.
机译:在本研究中,呈现了一种控制方案,其允许在由于风引起的扰动存在下对无人平面垂直起飞和着陆航空车进行高度位置调节和稳定的控制方案。为此,使用与嵌套饱和函数方法一起的BackStepping过程。首先,进行空中车辆模型中的坐标的方便变化,以使旋转动力学来自翻译。其次,施加背击过程以获得高度位置控制器,允许减少系统并将其表示为具有非线性干扰的集成器链。因此,嵌套饱和函数方法用于获得水平位置和辊角的稳定控制器。相应的稳定性分析通过Lyapunov第二方法进行。另外,为了估计由于风引起的扰动,使用了扩展状态观察者。通过数值模拟评估所提出的控制方案的有效性,从中获得了令人信服的结果。

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