摘要
提出了对中低高度卫星进行轨道调整的简化动力学模型。算例表明：可以通过选择发动机点火点的位置，满足卫星在可测控弧段进行轨道调整的要求。
The simplified dynamics model is prefered to modulate the orbits of satellites with medium or low altitude. The calculation example evinces that the request of the satellites to modulate the orbits in the controllable are part can be met through the selecting of the position of the retrofire point of the engine.
出处
《上海航天》
1999年第1期16-20,共5页
Aerospace Shanghai
