Attitude controller designed based on pole assignment theory for combined spacecraft

Yan-ru Qin, Feng Wang, Xibin Cao
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引用次数: 1

Abstract

This paper investigates the attitude control problem of on-orbit servicing spacecraft which changes moment of inertia after the rendezvous and docking task. Considering in the small-angle circumstance and manipulating attitude dynamics model with linearization method, the attitude controller based on pole assignment is obtained. Finally, a numerical example is provided to illustrate the effectiveness of the proposed approach.
基于极点配置理论的组合航天器姿态控制器设计
研究了在轨服务航天器交会对接后转动惯量变化的姿态控制问题。考虑小角度环境,采用线性化方法控制姿态动力学模型,得到了基于极点配置的姿态控制器。最后,给出了一个数值算例来说明所提方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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