基于扰动观测器的伸缩四旋翼飞行器建模与控制

A. Baldini, R. Felicetti, A. Freddi, S. Longhi, A. Monteriù
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引用次数: 1

摘要

变形多旋翼的特点是能够在飞行过程中修改其形状,以便在不需要小型化的情况下谈判狭窄的间隙,从而保留飞行时间和有效载荷。本文提出了一种以伸缩臂为特征的变形四旋翼飞行器的数学模型:随着伸缩臂的运动,飞行器的质心位置会发生变化,同时飞行器的惯性也会发生变化。然后,采用基于扰动观测器的控制方法,研究了在外部加性扰动(如风)下伸缩四旋翼飞行器的跟踪控制问题。控制方案由内/外环结构组成,其中两个环与非线性扰动观测器相互作用。分析了闭环性能,并通过仿真验证了控制方案的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling and Control of a Telescopic Quadrotor Using Disturbance Observer Based Control
Morphing multirotors are characterized by the capability to modify their shape during the flight, in order to negotiate narrow gaps without the need for miniaturization, thus preserving flight time and payload. In this paper, we propose a mathematical model for a morphing quadrotor characterized by telescopic arms: as extendable arms move, the center of mass position changes, as well as the inertia of the vehicle. Then, we address the tracking control problem of the telescopic quadrotor under external additive disturbances (e.g., wind), following the disturbance observer based control approach. The control scheme consists in an inner/outer loop structure, where both loops interact with a nonlinear disturbance observer. Closed loop performances are analyzed and the control scheme is validated through a realistic numerical simulation.
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