Singularity-Free Model Predictive Spacecraft Attitude Regulation Using a Variable-Speed Control Moment Gyroscope Model

Yaguang Yang. Singularity-Free Model Predictive Spacecraft Attitude Regulation Using a Variable-Speed Control Moment Gyroscope Model. IEEE Trans. Aerospace and Electronic Systems, 54(3):1511-1518, 2018. [doi]

Authors

Yaguang Yang

This author has not been identified. Look up 'Yaguang Yang' in Google