Momentum Management of Chinese space station based on robust H∞

L. Yue, Jia Ying-min, Gao Ya-nan, Fan Song-tao
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Abstract

For the requirement of multi-structure architecture, a controller based on robust H_∞ is proposed for LVLH angular momentum Management control method. The method is characterized by a combination of robust control and classical pole placement, and gives the system more robustness of parameter variation. Numerical simulation based on accurate dynamic model is proposed. Simulation result shows that controller meets the requirement of different structure of Chinese space station, and do not need to change control rate of system.
基于鲁棒H∞的中国空间站动量管理
针对多结构体系结构的要求,提出了一种基于鲁棒H_∞的LVLH角动量管理控制方法。该方法将鲁棒控制与经典极点配置相结合,使系统对参数变化具有更强的鲁棒性。提出了基于精确动力学模型的数值模拟方法。仿真结果表明,该控制器能够满足我国空间站不同结构的要求,且不需要改变系统的控制速率。
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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