[5] A R MKRTYCHYAN, N I BASHKEEV, D O YAKIMOVSKII et al. Control moment gyroscopes for spacecraft attitude control systems：current status and prospects. Gyroscopy and Navigation, 6, 236-240(2015).

[6] H SCHAUB, S R VADALI, J L JUNKINS. Feedback control law for variable speed control moment gyros. The Journal of the Astronautical Sciences, 46, 307-328(1998).

[11] H KUROKAWA. Survey of theory and steering laws of single-gimbal control moment gyros. Journal of Guidance，Control，and Dynamics, 30, 1331-1340(2007).

[13] L VALK, A BERRY, H VALLERY. Directional singularity escape and avoidance for single-gimbal control moment gyroscopes. Journal of Guidance，Control，and Dynamics, 41, 1095-1107(2018).

[25] S P BHAT, P K TIWARI. Controllability of spacecraft attitude using control moment gyroscopes. IEEE Transactions on Automatic Control, 54, 585-590(2009).

[28] L YU. CMGs-based steering law design for high attitude stability and quick attitude maneuver agile satellite, 2553(2016).

[29] C CHEN, X LIU, B CONG et al. Dynamical sliding mode control of spacecraft attitude using SGCMG systems, 2240-2244(2010).

[31] L GRNE, J PANNEK. Nonlinear model predictive control：theory and algorithms, 1-11(2013).

[33] L GRNE, J PANNEK. Nonlinear model predictive control：theory and algorithms, 107-126(2013).

[34] M SCHWENZER, T BERGS et al. Review on model predictive control：an engineering perspective. The International Journal of Advanced Manufacturing Technology, 117, 1327-1349(2021).

[35] H CHEN, F ALLGÖWER. A quasi-infinite horizon nonlinear model predictive control scheme with guaranteed stability. Automatica, 34, 1205-1217(1998).