含间隙铰接的柔性航天器刚柔耦合动力学与控制研究1)
孙杰, 孙俊, 刘付成, 朱东方, 黄静

DYNAMICS AND CONTROL OF RIGID-FLEXIBLE COUPLING FLEXIBLE SPACECRAFT WITH JOINT CLEARANCE1)
Sun Jie, Sun Jun, Liu Fucheng, Zhu Dongfang, Huang Jing
图12 不同铰链数目时航天器的姿态角
Fig. 12 Attitude angle of the spacecraft with different number of joints