跟踪翻滚目标的鲁棒部分状态反馈姿态控制

Qi Li, Jinyuan Wei, Xueping Wang, Qiuxiong Gou, Zhiqi Niu
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引用次数: 0

摘要

研究了存在外部干扰和控制输入饱和情况下的不受控翻滚目标跟踪的部分状态反馈姿态控制问题。首先,建立了非线性相对姿态运动模型,并研究了基于死区算子的输入饱和模型。随后,建立了一种新的模型辅助扩展状态观测器来估计未测量状态和集总不确定性。然后,将扩展状态观测器技术与滑模方法相结合,提出了一种输出反馈抗饱和控制策略,消除了两个航天器之间全状态测量的需要。在Lyapunov框架下,所提出的控制策略能够保证相对姿态误差收敛到包含原点的小区域。最后,通过数值仿真验证了所提控制策略的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Robust Partial-state Feedback Attitude Control for Tracking Tumbling Target
This paper investigates the partial-state feedback attitude control problem of tracking an uncontrolled tumbling target in the presence of external disturbances and control input saturation. Firstly, a nonlinear relative attitude motion model is presented, and a dead-zone operator based model is investigated to describe the input saturation phenomenon. Subsequently, a novel model-assisted extended state observer is established to estimate the unmeasured states and the lumped uncertainties. Then, by combining the extended state observer technique with sliding mode methodology, an output-feedback anti-saturation control strategy that removes the need for full-state measurements between the two spacecrafts is proposed. Within the Lyapunov framework, the proposed control strategy is able to guarantee that the relative attitude errors can converge to small regions containing the origin. Finally, numerical simulations are performed to demonstrate the effectiveness of the presented control strategy.
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