Improved optimal steering law for SGCMG and adaptive attitude control of flexible spacecraft
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Institute of Electrical and Electronics Engineers (IEEE)
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Adaptive Spacecraft Attitude Control Using Single-Gimbal Control Moment Gyroscopes Without Singularity Avoidance;Journal of Guidance, Control, and Dynamics;2019-11
2. Vector Control-Based Singularity Avoidance/Escape Steering Law for Single Gimbal Control Moment Gyros;IEEE Access;2019
3. Attitude-Rate Measurement and Control Integration Using Magnetically Suspended Control and Sensitive Gyroscopes;IEEE Transactions on Industrial Electronics;2018-06
4. Robust adaptive attitude control for flexible spacecraft in the presence of SGCMG friction nonlinearity;International Journal of Robust and Nonlinear Control;2018-03-23
5. Spacecraft vibration suppression based on micro-gimbal moment of magnetically suspended flywheel with dynamic feedback and feedforward decoupling control;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2017-12-12
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