Fuzzy attitude control for a nanosatellite in low Earth orbit

作者：

Highlights：

• We design a PID and an adaptive fuzzy controller for the same satellite mission.

• This is the first time the performances and cost of operation of a PID and an adaptive fuzzy controllers are compared.

• The fuzzy controller is more efficient than the PID for single manoeuvres with similar accuracy.

摘要

•We design a PID and an adaptive fuzzy controller for the same satellite mission.•This is the first time the performances and cost of operation of a PID and an adaptive fuzzy controllers are compared.•The fuzzy controller is more efficient than the PID for single manoeuvres with similar accuracy.

论文关键词：Satellite attitude,Fuzzy logic,PID

论文评审过程：Received 9 July 2015, Revised 2 April 2016, Accepted 3 April 2016, Available online 5 April 2016, Version of Record 17 April 2016.

论文官网地址：https://doi.org/10.1016/j.eswa.2016.04.004