MODULAR CONTROL MOMENT GYROSCOPE (CMG) SYSTEM FOR SPACECRAFT ATTITUDE CONTROL

• 1. 一种用于控制力矩陀螺奇异规避的航天器姿态控制方法 [P] . 中国专利： CN105223961B . 2018.04.13
• 2. 一种用于控制力矩陀螺奇异规避的航天器姿态控制方法 [P] . 中国专利： CN105223961A . 2016-01-06
• 3. Method and system for controlling sets of collinear control moment gyroscopes with offset determination without attitude trajectory of spacecraft [P] . 美国专利： US7693619B2 . 2010-04-06

  机译： 在没有航天器姿态轨迹的情况下用偏移确定控制共线控制力矩陀螺仪组的方法和系统

• 4. Method and apparatus for singularity avoidance for control moment gyroscope (CMG) systems without using null motion [P] . 美国专利： US9567112B1 . 2017-02-14

  机译： 在不使用零运动的情况下避免控制矩陀螺仪（CMG）系统出现奇异性的方法和装置

• 5. DEVICE FOR CONTROLLING ATTITUDE OF SPACECRAFT AND METHOD FOR CALCULATING CMG GIMBAL ANGLE [P] . 美国专利： US2019061978A1 . 2019-02-28

  机译： 控制航天器姿态的装置和计算cmg陀螺角的方法

• 1. Review:A Survey of Single Gimbal Control Moment Gyroscope for Agile Spacecraft Attitude Control [J] . Yunhua Wu, Feng Han, Bing Hua, 哈尔滨工业大学学报（英文版） . 2018,第006期
• 2. Model predictive control of rigid spacecraft with two variable speed control moment gyroscopes [J] . Pengcheng WU, Hao WEN, Ti CHEN, 应用数学和力学（英文版） . 2017,第011期
• 3. Attitude control of a rigid spacecraft with one variable-speed control moment gyro [J] . Hai-Chao Gui, Lei Jin, Shi-Jie Xu 力学学报：英文版 . 2013,第005期
• 4. Underactuated spacecraft angular velocity stabilization and three-axis attitude stabilization using two single gimbal control moment gyros [J] . Lei Jin, Shijie Xu 力学学报：英文版 . 2010,第002期
• 5. Application of Ultrasonic Motor to Control of Moment Gyroscope Gimbal Servo System [J] . Wu Jintao, Pan Song, Zhao Lei, 南京航空航天大学学报（英文版） . 2017,第001期
• 6. Control Moment Gyroscopes for Spacecraft Attitude Control Systems: Current Status and Prospects [J] . A. R. Mkrtychyan, N. I. Bashkeev, D. O. Yakimovskii, Gyroscopy and navigation . 2015,第3期
• 7. Extended harmonic disturbance observer-based attitude control for flexible spacecraft with control moment gyroscopes [J] . Huang Liya, Wu Zhong Proceedings of the Institution of Mechanical Engineers . 2019,第14期
• 8. Adaptive Spacecraft Attitude Control Using Single-Gimbal Control Moment Gyroscopes Without Singularity Avoidance [J] . Zhao Zhanzhan, Cruz Gerardo, Bernstein Dennis S. Journal of guidance, control, and dynamics . 2019,第11期
• 9. Controllability of spacecraft attitude using control moment gyroscopes [C] . Bhat S.P. American Control Conference . 2006
• 10. A novel integrated spacecraft attitude control system using variable speed control moment gyroscopes: A Lyapunov-based approach [D] . Kim, Dohee. 2011
• 11. Design and Simulation of a MEMS Control Moment Gyroscope for the Sub-Kilogram Spacecraft [O] . Honglong Chang, Wenlong Jiao, Qianyan Fu, 2010
• 12. Controllability of spacecraft attitude using Control Moment Gyroscopes [O] . BHAT SP, TIWARI PK 2009
• 13. Minimum-time attitude maneuvers of spacecraft with Control Moment Gyroscopes /CMG/ [R] . Kranton, J. 1969

• 1. 双框架控制力矩陀螺在航天器姿态控制系统中的应用 [C] . 徐洪亮 ,战兴群 ,张炎华 . 2008年全国博士生学术论坛（航空宇航科学与技术） . 2008
• 2. 双框架控制力矩陀螺在航天器姿态控制系统中的应用 [A] . 徐洪亮 . 2008