基于SO(3)鲁棒比例导数补偿力矩的四旋翼镇定

A. H. Ginting, O. Wahyunggoro, A. Cahyadi, Muhammad Faris
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引用次数: 1

摘要

针对四旋翼飞行器,提出了一种鲁棒PD控制器。针对四旋翼原点在重心位置不确定情况下的稳定问题,提出了该控制器。在动态控制系统中,采用指数坐标参数来表示姿态,避免了其他姿态表示如欧拉角或四元数所带来的复杂性和模糊性。仿真结果表明,通过对悬架位置不确定设计上界补偿器,该控制系统可以在不知道悬架位置的情况下稳定悬停状态。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Stabilization Of Quadrotor on SO(3) With Robust Proportional-Derivative to Compensate CoG
In this paper, a robust PD controller for a quadrotor is presented. This controller is proposed for stabilizing the quadrotor with uncertain position of center of gravity (CoG), when the origin of quadrotor is placed in CoG. The exponential coordinates parameter is used to represent the attitude in dynamic and proposed control system, to avoid complexities and ambiguities associated with other attitude representations such as Euler angles or quaternions. The simulation results indicate that by designing an upper bound compensator for the uncertain position of CoG, the proposed control system can stabilize the hovering condition without the knowledge of the position of CoG.
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