状态约束下四旋翼无人飞行器的快速有限时间反步进控制器

Nguyen Mung Xuan, Lanh Le Thanh, The Mich Nguyen
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引用次数: 0

摘要

四旋翼飞行器已在广泛的应用中得到普及。本文提出了一种解决具有全状态约束的四旋翼飞行器跟踪控制问题的新方法。所提出的方法涉及一种集成了快速有限时间滤波器的反步进控制方案。首先,进行必要的状态变换以支持有限时间滤波器和控制器的设计。然后,根据反步进技术制定控制器。控制器考虑了所有的状态约束。然而,众所周知,在计算某些非线性函数的时间导数时,反步法控制设计会导致 "复杂性爆炸"。因此,所提出的滤波器提供了一种估算时间导数的解决方案,估算误差在有限时间内趋于零。尽管存在状态约束,但利用 Lyapunov 理论严格证明了闭环系统的有限时间稳定性。仿真结果证明了所提方法的可行性和有效性。
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Fast finite-time backstepping controller for a quadrotor UAV under state constraints
Quadrotors have gained popularity in a wide range of applications. In this paper, a new approach for solving the tracking control problem of quadrotors with full-state constraints is presented. The proposed method involves a backstepping control scheme integrated with a fast finite-time filter. First, necessary state transformations are performed to support the design of the finite-time filter and controller. Next, the controller is formulated based on the backstepping technique. All the state constraints are taken into consideration in the controller. However, it is well-known that the backstepping control design can lead to the “explosion of complexity” when calculating time derivatives of certain nonlinear functions. Therefore, the proposed filter comes to provide a solution for estimating the time derivatives with the estimation errors converging to zero in finite time. The closed-loop system's finite-time stability is rigorously proved using the Lyapunov theory, despite the state constraints. Simulation results demonstrate the feasibility and efficacy of the proposed method.
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