Intelligent Fuzzy Control in Stabilizing Solar Sail with Individually Controllable Elements

作     者：Lin Chen Xiaoyu Fu Santos Ramil Ming Xu Lin Chen;Xiaoyu Fu;Santos Ramil;Ming Xu

作者机构：Beihang University100191 BeijingChina Surrey Space CentreThe University of SurreyGU27XH GuildfordUK 

出 版 物：《Space(Science & Technology)》 (空间科学与技术（英文）)

年 卷 期：2022年第2022卷第1期

页      面：274-285页

核心收录：

学科分类：07[理学] 0825[工学-航空宇航科学与技术] 0704[理学-天文学] 0701[理学-数学] 070101[理学-基础数学] 

基　　金：supported by the National Natural Science Foundation of China(11772024) 

主　　题：theory. overcome apply 

摘      要：Fuzzy logical control is a robust and effective control method in industrial fields,which renders it applicable to the attitude control of a solar ***,it is hard to apply in black-box and time-varying problem as real solar sail attitude *** the lack of a priori knowledge and the unacceptable manual workload in the design of the fuzzy logical controller(FLC),an intelligent FLC designer(IFLCD)is developed by introducing neural network modelling and automatic design ***,IFLCD also supports self-adaption for better control *** applying the proposed IFLCD in the attitude stabilization of a solar sail with individually controllable elements(SSICE),an effective solution of unmanned,time-varying,and complex system control method is offered without any mathematical model,which also overcomes the difficulties in FLC design Considering the performance degradation,accident,and distance problems faced by spacecraft,IFLCD can help with more practical problems that are hard be solved by traditional control theory.