Decentralized formation control of quadcopters using feedback linearization

A. Mahmood, Yoonsoo Kim
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引用次数: 10

Abstract

This paper proposes a decentralized formation control scheme for a group of quadcopters using feedback linearization. Unlike most of the existing works that involve a complex design of nonlinear formation control laws, this work simplifies the design to yield an almost linear control law for under-actuated nonlinear quadcopters. In fact, a singularity-free dynamic inversion scheme is utilized such that the quadcopter dynamics can be treated as a linear system. Consequently, a linear formation control law can be designed for the resulting linear system to achieve desired positions and an identical heading angle through local information exchanges only. Although the present work considers quadcopter dynamics only, the proposed methodology can also be directly applied to attitude synchronization problems arising in space and robotic applications.
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基于反馈线性化的四轴飞行器分散编队控制
提出了一种基于反馈线性化的四轴飞行器分散编队控制方案。与大多数涉及非线性编队控制律复杂设计的现有工作不同,这项工作简化了设计,为欠驱动非线性四轴飞行器提供了几乎线性的控制律。实际上,利用无奇点动态反演方案,使四轴飞行器动力学可以视为线性系统。因此,可以设计线性编队控制律,使线性系统仅通过局部信息交换即可获得期望位置和相同航向角。虽然目前的工作只考虑四轴飞行器动力学,但所提出的方法也可以直接应用于空间和机器人应用中出现的姿态同步问题。
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