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首页> 外文期刊>Aerospace science and technology >Flatness-based finite-time leader-follower formation control of multiple quadrotors with external disturbances
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Flatness-based finite-time leader-follower formation control of multiple quadrotors with external disturbances

机译:基于平面度的多扰动四旋翼有限时间前随从编队控制

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摘要

This study considers the leader-follower formation control problem for multiple quadrotors in the presence of external disturbances. Based on the differential flatness theory, the underactuated quadrotor system is transformed into a fully actuated one with four degrees of freedom and four control inputs. Based on this model, a distributed finite-time observer is developed to reconstruct the leader's states for each follower. Then, an observer-based finite-time controller is proposed based on an adaptive disturbance rejection approach, which is independent of the upper bounds of the disturbances, to address the formation control problem for multiple quadrotors. The stability analysis indicates that the closed-loop system theoretically achieves the finite-time stability and robustness against the disturbances. Finally, a numerical simulation is provided to verify the performance of the proposed formation control scheme. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:这项研究考虑了在存在外部干扰的情况下多个四旋翼飞机的前随从编队控制问题。根据差动平面度理论,将欠驱动四旋翼系统转换为具有四个自由度和四个控制输入的完全致动的四旋翼系统。基于此模型,开发了一个分布式的有限时间观察者,以重建每个跟随者的领导者状态。然后,基于一种独立于扰动上限的自适应扰动抑制方法,提出了一种基于观测器的有限时间控制器,以解决多四旋翼飞机的编队控制问题。稳定性分析表明,闭环系统在理论上达到了有限时稳定性和对干扰的鲁棒性。最后,提供了数值模拟,以验证所提出的编队控制方案的性能。 (C)2019 Elsevier Masson SAS。版权所有。

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