Fuzzy reaching law sliding mode controller for spacecraft attitude control

@article{Jie2014FuzzyRL,
  title={Fuzzy reaching law sliding mode controller for spacecraft attitude control},
  author={Ma Jie and Yang Xuebo},
  journal={2014 International Conference on Mechatronics and Control (ICMC)},
  year={2014},
  pages={1084-1089}
}
  • Ma Jie, Yang Xuebo
  • Published 2014 in
    2014 International Conference on Mechatronics and…
Aiming at attitude control of spacecraft, the method of fuzzy reaching law sliding mode is introduced. Firstly, the spacecraft dynamics equation based on angular velocity and kinematic equation based on error quaternion are introduced. Then according to the mathematical model of the satellite attitude control system, the sliding mode controller is designed… CONTINUE READING