Large Angle Super Agile Attitude Maneuver Control of Small Satellite using Reaction Wheels

被引：0
|
作者：
Fan Guowei [1 ]
Zhang Jiabao [1 ]
Zhao Huanyu [1 ]
Lv Xueying [1 ]
机构：
[1] Jilin Univ, Coll Instrumentat & Elect Engn, Changchun 130012, Peoples R China
来源：
2021 PROCEEDINGS OF THE 40TH CHINESE CONTROL CONFERENCE (CCC) | 2021年
基金：
中国国家自然科学基金;
关键词：
Super Agile Attitude Maneuver; Rigid Small Satellite; Attitude Planning; Tracking Control;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Super agile imaging mode can effectively solve the contradiction between short transit time and various imaging tasks, and can significantly improve the satellite observation efficiency. The premise of its on-orbit implementation is to geatly improve the attitude control ability of satellite platform. In order to satisfy the requirement of super agile attitude maneuver control for multi-target imaging task, an "attitude planning + moving horizon tracking" control scheme for rigid satellite using reaction wheels is designed. Based on the analysis of the performance requirement of attitude control for multi-target imaging task, two methods of attitude deterinination in the stages of attitude maneuver and stable control are proposed. The control model of the rigid satellite is established, and the super agile attitude maneuver trajectory is designed based on the three-stage planning method, then the moving horizon optimization tracking control method is proposed to realize the super agile attitude maneuver control. The effectiveness of the proposed control scheme is demonstrated by numerical simulation.
引用
收藏
页码：7557 / 7562
页数：6
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