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

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

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.

K F Gill | S Daley | S. Daley | K. Gill

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