A VARIABLE-UNIVERSE FUZZY PID CONTROLLER APPLIED FOR SATELLITE ATTITUDE MANEUVER

被引：0
作者：
Xu, Peng [1 ]
Zhang, Zilong [1 ]
Xu, Ziyao [1 ]
Sun, Jiandang [1 ]
机构：
[1] Shanghai Aerosp Control Technol Inst, Shanghai 201109, Peoples R China
来源：
FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III | 2018年 / 165卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The dynamic performance optimization of satellite maneuver is a research hotspot in satellite attitude control. A fuzzy PID controller based on the variable-universe algorithm is presented in this paper. Firstly, based on the requirements of maneuver task, the deficiency of traditional single set PID parameter control is analyzed. Then, the mathematical characteristics of maneuver process is analyzed thus, a variable-universe algorithm whose variable-universe coefficient is adaptively adjusted by fuzzy logic is proposed. Finally, the control algorithm simulation using the variable-universe algorithm and the traditional algorithm is given respectively. The results show that the variable universe algorithm improves the dynamic performance of the maneuver tracking process effectively compared with the traditional one.
引用
收藏
页码：851 / 859
页数：9
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