在轨服务飞行器对共面圆轨道目标接近过程分析  

The Approaching Process Analysis of On-Orbit Service Vehicle to Circular Coplanarity Orbit Target

作　　者：李岩 姚静波 辛朝军 苏宪程 

机构地区：[1]装备学院航天装备系,北京101416 [2]装备学院训练部,北京101416

出　　处：《航天控制》2015年第4期56-61,共6页Aerospace Control

摘　　要：为了研究在轨服务飞行器(On-orbit Service Vehicle,OSV)针对共面圆轨道目标的大范围机动过程,利用经典二体动力学模型和霍曼转移轨道模型,分析了OSV转移过程中的相位调整和能量需求,比较了自然调相和速度调相的特点,提出了待机轨道、停泊轨道、初始相位差、变轨时机和交会时间等参数选择的一般规律,为选择OSV接近目标的机动策略提供了理论参考。In order to analyze the orbital transfer of on-orbit service vehicle （OSV） aiming at the circular coplanarity orbital target, the OSV orbital phasing and maneuvering process are analyzed by using the clas- sical two-body dynamics and Hochmann transfer model together. Then, the general law of choosing the pa- rameters for the orbital transfer, such as the parking orbit, the temporary orbit, the original phasic differ- ence , transfer window and period and so on, is presented after the comparison of natural phasing and veloc- ity phasing. The study can serve as a good reference for the OSV maneuvering strategy design.

关 键 词：在轨服务飞行器 轨道转移 相位调整 机动策略 

分 类 号：V412.4[航空宇航科学与技术—航空宇航推进理论与工程]