Adaptive control of arm-equipped quadrotors. Theory and simulations

G. Antonelli, E. Cataldi
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引用次数: 18

Abstract

The paper presents an adaptive control for an aerial vehicle equipped with a manipulator, the latter is assumed to be already driven by a joint-based controller. The proposed control generates the vehicle thrusts by properly taking into account the physical interaction with the arm. Being adaptive, it estimates and then compensates the dynamics of the whole system. Moreover, the proposed approach is based on the Newton-Euler formulation, i.e., it is recursive. A stability analysis is provided to analytically support the developed controller. A reduced version is proposed to greatly simplify the controller by taking into account only the gravitational terms. Numerical simulations confirm the controller performance as compared with the effort and error of a benchmark controller.
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武装四旋翼机的自适应控制。理论与仿真
本文提出了一种飞行器的自适应控制方法,该方法假定飞行器已由基于关节的控制器驱动。所提出的控制通过适当地考虑与手臂的物理相互作用来产生飞行器推力。由于具有自适应性,它可以估计并补偿整个系统的动态。此外,所提出的方法基于牛顿-欧拉公式,即是递归的。稳定性分析提供了分析支持所开发的控制器。提出了一个简化版本,通过只考虑引力项来极大地简化控制器。通过数值仿真验证了该控制器的性能,并与基准控制器进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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