Attitude control of a spacecraft using an extended self-organizing fuzzy logic controller

Author:

Daley S1,Gill K F2

Affiliation:

1. Department of Electrical Engineering and Electronics, Brunel University

2. Department of Mechanical Engineering, University of Leeds

Abstract

A simple method for extending the range of sensitivity of the self-organizing fuzzy logic controller (SOC) is proposed. The performance of the resulting controller is studied through its application to the attitude control of a flexible satellite. It is found that the extended SOC can provide excellent control and also possesses a high degree of robustness.

Publisher

SAGE Publications

Subject

Mechanical Engineering

Cited by 18 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Dynamics modeling and attitude control of spacecraft flexible solar array considering the structure of the hinge rolling;Acta Astronautica;2018-12

2. Fuzzy-scored genetically-designed controller for the VLS-1 launcher;2008 IEEE International Conference on Fuzzy Systems (IEEE World Congress on Computational Intelligence);2008-06

3. Genetic-Based Fuzzy Logic Controller for Satellites Stabilized by Reaction Wheels and Gravity Gradient;AIAA Guidance, Navigation and Control Conference and Exhibit;2007-06-15

4. Design considerations for a Model Reference Fuzzy Adaptive Controller;Transactions of the Institute of Measurement and Control;2001-08

5. Fuzzy logic based attitude control of the spacecraft X-38 along a nominal re-entry trajectory;Control Engineering Practice;2001-07

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