Feedback Error Learning Control of Magnetic Satellites Using Type-2 Fuzzy Neural Networks With Elliptic Membership Functions

被引:52
作者
Khanesar, Mojtaba Ahmadieh [1 ]
Kayacan, Erdal [2 ]
Reyhanoglu, Mahmut [3 ]
Kaynak, Okyay [4 ,5 ]
机构
[1] Semnan Univ, Fac Elect & Comp Engn, Dept Elect & Control Engn, Semnan 35131, Iran
[2] Nanyang Technol Univ, Sch Mech & Aerosp Engn, Singapore 639798, Singapore
[3] Embry Riddle Aeronaut Univ, Dept Phys Sci, Daytona Beach, FL 32114 USA
[4] Bogazici Univ, Dept Elect & Elect Engn, TR-34342 Istanbul, Turkey
[5] Harbin Inst Technol, Harbin 150080, Peoples R China
关键词
Fuzzy control; fuzzy neural networks; nonlinear control systems; stability analysis; CHAOTIC ATTITUDE MOTION; SPACECRAFT; LOGIC;
D O I
10.1109/TCYB.2015.2388758
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A novel type-2 fuzzy membership function (MF) in the form of an ellipse has recently been proposed in literature, the parameters of which that represent uncertainties are de-coupled from its parameters that determine the center and the support. This property has enabled the proposers to make an analytical comparison of the noise rejection capabilities of type-1 fuzzy logic systems with its type-2 counterparts. In this paper, a sliding mode control theory-based learning algorithm is proposed for an interval type-2 fuzzy logic system which benefits from elliptic type-2 fuzzy MFs. The learning is based on the feedback error learning method and not only the stability of the learning is proved but also the stability of the overall system is shown by adding an additional component to the control scheme to ensure robustness. In order to test the efficiency and efficacy of the proposed learning and the control algorithm, the trajectory tracking problem of a magnetic rigid spacecraft is studied. The simulations results show that the proposed control algorithm gives better performance results in terms of a smaller steady state error and a faster transient response as compared to conventional control algorithms.
引用
收藏
页码:858 / 868
页数:11
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