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Tracking control and robustness analysis for planar vertical takeoff and landing aircraft under bounded feedbacks

机译:有限反馈下飞机垂直起降飞机的跟踪控制和鲁棒性分析

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摘要

We study feedback tracking problems for the planar vertical takeoff and landing (PVTOL) aircraft dynamics, which is a benchmark model in aerospace engineering. We provide a survey of the literature on the model. Then we construct new feedback stabilizers for the PVTOL tracking dynamics. The novelty of our work is in the boundedness of our feedback controllers and their applicability to cases where the velocity measurements may not be available, coupled with the uniform global asymptotic stability and uniform local exponential stability of the closed-loop tracking dynamics and the input-to-state stable performance of the closed-loop tracking dynamics with respect to actuator errors. Our proofs are based on a new bounded backstepping result. We illustrate our work in a tracking problem along a circle.
机译:我们研究了用于飞机垂直起降(PVTOL)飞机动力学的反馈跟踪问题,这是航空工程中的基准模型。我们提供了有关该模型的文献调查。然后,我们为PVTOL跟踪动力学构造新的反馈稳定器。我们工作的新颖之处在于我们的反馈控制器的局限性,以及它们在无法进行速度测量的情况下的适用性,再加上闭环跟踪动力学的均匀全局渐近稳定性和均匀局部指数稳定性以及输入-闭环跟踪动力学相对于执行器误差的稳定状态。我们的证明是基于新的有界反推结果。我们围绕一个跟踪问题说明了我们的工作。

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