Routing algorithms of satellite communication system with hybrid orbit are studied. The system consists of LEO and GEO satellites.
研究了混合轨道卫星通信系统的路由算法，系统由低轨道和静止轨道卫星构成。
After it reaches orbit, the craft will be dropped, and its hybrid motors will be used to adjust its orbit or dock it to a space station.
进入轨道之后，飞行器被剥离，并利用其混合动力发动机调整轨道进而与空间站对接。
In order to ensure structural reliability of deployable structures in orbit, the hybrid analysis of its mechanism motion and flexible deformation is required.
为了保证空间可展结构可靠运行，在展开过程分析中需同时考虑机构运动和弹性变形。
In order to ensure structural reliability of deployable structures in orbit, the hybrid analysis of its mechanism motion and flexible deformation is required.
为了保证空间可展结构可靠运行，在展开过程分析中需同时考虑机构运动和弹性变形。
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