挠性航天器动力学模型的非约束模态分析$^{\bf 1)}$
宋新宇,戈新生(
)
)
UNCONSTRAINED MODAL ANALYSIS OF DYNAMIC MODEL OF FLEXIBLE SPACECRAFT$^{\bf 1)}$
Song Xinyu,Ge Xinsheng()
)
图2. 挠性航天器模型及太阳帆板结构尺寸
Fig.2. Flexible spacecraft model and structure size of solar array
