A numerical optimization approach for tuning fuzzy logic controllers

被引:15
作者
Woodard, SE [1 ]
Garg, DP
机构
[1] NASA, Langley Res Ctr, Hampton, VA 23681 USA
[2] Duke Univ, Dept Mech Engn & Mat Sci, Durham, NC 27708 USA
来源
IEEE TRANSACTIONS ON SYSTEMS MAN AND CYBERNETICS PART B-CYBERNETICS | 1999年 / 29卷 / 04期
关键词
attitude control; fuzzy logic controllers; numerical optimization; pointing control; spacecraft control;
D O I
10.1109/3477.775276
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper develops a method to tune fuzzy controllers using numerical optimization. The main attribute of this approach is that it allows fuzzy logic controllers to be tuned to achieve global performance requirements. Furthermore, this approach allows design constraints to be implemented during the tuning process. The method tunes the controller by parameterizing the membership functions for error, change-in-error, and control output. The resulting parameters form a design vector which is iteratively changed to minimize an objective function. The minimal objective function results in an optimal performance of the system. A spacecraft mounted science payload line-of-sight pointing control is used to demonstrate results.
引用
收藏
页码:565 / 569
页数:5
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