Input-to-state Stable Attitude Takeover Control for Combined Spacecraft

被引：0
|
作者：
Lv Y.-Y. [1 ]
Fang H. [2 ]
Qin T.-H. [1 ]
Guo Y.-N. [1 ]
机构：
[1] Department of Control Engineering, Harbin Institute of Technology, Harbin
[2] Shanghai Aerospace Control Technology Institute, Shanghai
来源：
Fang, Hui (fanghui_email@163.com) | 1600年 / China Spaceflight Society卷 / 42期
关键词：
Attitude takeover control; Combined spacecraft; Excitation-response model; Input-to-state stability; Non-cooperative target;
D O I：
10.3873/j.issn.1000-1328.2021.07.007
中图分类号：
学科分类号：
摘要：
In this paper, the attitude takeover control method based on input-to-state stability is studied for noncooperative target with counteraction torque. Firstly, the excitation-response model is established based on real-time computing of the counteraction torque, so that the attitude of the combined spacecraft is depicted precisely. Next, a model-independent attitude takeover control scheme is proposed based on input-to-state stability, meanwhile the parameter selection principle is also established. Finally, the effectiveness is verified by numerical simulation. © 2021, Editorial Dept. of JA. All right reserved.
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页码：873 / 880
页数：7
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