近圆太阳同步卫星轨道倾角偏差的影响和调整  

Impact Analysis and Adjustment of Nearly Round Sun-Synchronous Orbit Satellite Injection Inclination Deviation

作　　者：张国云[1,2] 蔡立锋[2] 黄晓峰[2] 杨钊[2] 

机构地区：[1]宇航动力学国家重点实验室,陕西西安710043 [2]中国西安卫星测控中心,陕西西安710043

出　　处：《上海航天》2014年第2期37-41,共5页Aerospace Shanghai

摘　　要：以某近圆太阳同步轨道卫星为例,分析了倾角偏差引起的降交点地方时的漂移规律及影响。为将降交点地方时漂移限制在允许的范围内,给出了轨道倾角调整方案,仿真实验结果表明控制方案有效。The local time of descending node shift characteristics and effect of inclination deviation were analyzed for nearly round sun-synchronous orbit satellite served as an example in this paper. To keep the local time shift of descending node with an allowable range, an orbital inclination maneuver scheme was given out. The simulation experiment results showed that the effectiveness of this control scheme.

关 键 词：太阳同步卫星 降交点地方时 倾角偏差 漂移 摄动因素 

分 类 号：V412.41[航空宇航科学与技术—航空宇航推进理论与工程]