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Robust output tracking control of a class of non-minimum phase systems and application to VTOL aircraft

机译:一类非最小相位系统的鲁棒输出跟踪控制及其在垂直起降飞机上的应用

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摘要

In this article, we study the output tracking control of a class of MIMO nonlinear non-minimum phase systems in the presence of input disturbances. In order to attenuate the effects of disturbances, the method of uncertainty and disturbance estimator (UDE) is extended to the controller design for non-minimum phase systems. Due to the fact that the accumulated disturbances is composed of internal states and external disturbances, a different stability analysis is given, and the overall closed-loop system is proved to be semi-globally stable. The proposed state-feedback controller not only forces system outputs to asymptotically track desired trajectories, but also drives the unstable internal dynamics to follow bounded and causal ideal internal dynamics (IID) solved via stable system centre (SSC) method. Simulation results demonstrate that the proposed controller achieves excellent tracking and disturbance rejection performance via the example of VTOL aircraft which has been the benchmark of nonlinear non-minimum phase systems.
机译:在本文中,我们研究存在输入干扰的情况下一类MIMO非线性非最小相位系统的输出跟踪控制。为了减弱干扰的影响,不确定性和干扰估计器(UDE)的方法已扩展到非最小相位系统的控制器设计。由于累积的扰动由内部状态和外部扰动组成,因此进行了不同的稳定性分析,并且证明了整个闭环系统是半全局稳定的。提出的状态反馈控制器不仅迫使系统输出渐近跟踪所需的轨迹,而且驱动不稳定的内部动力学遵循通过稳定系统中心(SSC)方法解决的有界和因果理想内部动力学(IID)。仿真结果表明,以非线性非最小相位系统为基准的VTOL飞机为例,所提出的控制器具有出色的跟踪和干扰抑制性能。

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