Parameterized fuzzy-logic controllers for the attitude control of nanosatellites in low earth orbits. A comparative studio with PID controllers

作者:

Highlights:

• Simple step based design for nanosatellite attitude controllers in LEO.

• Optimization process of LEO nanosatellite attitude controllers.

• Fuzzy controllers are more suitable for multiple operational situations.

• Fuzzy control converges to Boolean control far away from the targeted state.

• Intelligent controllers have great advantages over the classical ones.

摘要

•Simple step based design for nanosatellite attitude controllers in LEO.•Optimization process of LEO nanosatellite attitude controllers.•Fuzzy controllers are more suitable for multiple operational situations.•Fuzzy control converges to Boolean control far away from the targeted state.•Intelligent controllers have great advantages over the classical ones.

论文关键词:Satellite attitude,Fuzzy control,Multi-objective optimization,Genetic algorithms

论文评审过程:Received 23 October 2020, Revised 26 December 2020, Accepted 31 January 2021, Available online 9 February 2021, Version of Record 9 March 2021.

论文官网地址:https://doi.org/10.1016/j.eswa.2021.114679