Chattering free sliding adaptive attitude control for quadrotor

Zhi Li, Xin Ma, Zhigang Xu, Yafang Wang, Yibin Li
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引用次数: 4

Abstract

This paper investigates the quadrotor attitude tracking control problem in the presence of external disturbance and inertia uncertainty. An error quaternion based adaptive sliding mode control scheme is proposed in this paper. Adaptive control theory is applied to estimate inertia parameters and the upper bound of external disturbance. Lyapunov stability theory is applied to prove the stability of the controller. Simulation results are presented to demonstrate the performance and robustness of the controller.
四旋翼飞行器颤振自由滑动自适应姿态控制
研究了存在外部干扰和惯性不确定性的四旋翼飞行器姿态跟踪控制问题。提出了一种基于误差四元数的自适应滑模控制方案。应用自适应控制理论估计系统的惯性参数和外部扰动的上界。利用李雅普诺夫稳定性理论证明了控制器的稳定性。仿真结果验证了该控制器的性能和鲁棒性。
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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