Attitude stabilization control of an aerial manipulator using a quaternion-based backstepping approach

S. D. Lucia, Gian Diego Tipaldi, Wolfram Burgard
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引用次数: 34

Abstract

Aerial manipulation is a new research area that extends the potential of aerial vehicles, allowing them to physically interact with the environment. Modeling and control of such a system is not a trivial problem due to the coupled dynamics of the aerial vehicle and the robotic manipulator. This paper presents a robust and non linear control system for a Hexacopter equipped with a two-degrees-of-freedom robotic arm. The proposed mathematical model, which is based on a quaternion representation, takes into account the changing inertia and the mass distribution, depending on the arm configuration. We show how the attitude control, using a quaternion-based backstepping, is able to react to the disturbances caused by the arm. In the backstepping design, we introduce a command filter, which contributes to reduce the computational complexity of the algorithm. Finally, we present simulation results that demonstrate the stability of our approach and provide a comparison to a standard PD control.
基于四元数的航空机械臂姿态稳定控制
空中操纵是一个新的研究领域,它扩展了飞行器的潜力,使它们能够与环境进行物理交互。由于飞行器和机械臂的耦合动力学,该系统的建模和控制不是一个简单的问题。提出了一种具有二自由度机械臂的六旋翼机鲁棒非线性控制系统。所提出的数学模型基于四元数表示,考虑了随臂形变化的惯性和质量分布。我们展示了姿态控制,使用基于四元数的后退,能够对手臂引起的干扰做出反应。在回溯设计中,我们引入了命令滤波器,这有助于降低算法的计算复杂度。最后,我们给出了仿真结果,证明了我们方法的稳定性,并提供了与标准PD控制的比较。
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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