摘要
分析了快速进入近地轨道特点及其星下点轨迹特性,并通过星下点轨迹特性反算快速进入近地轨道根参数。提出了J2摄动影响下快速进入近地轨道回归轨道设计方法。STK仿真验证了该设计方法的正确性。
The peculiarity of the fast access orbit and the speciality of subsatellite point track was analyzed in this paper.The orbital parameters of the fast access orbit was calculated according to the subsatellite point track.The design method of the fast access repeat orbit was proposed under J2 condition.The method＇s correctness was verified by the STK simulation.
出处
《上海航天》
2015年第3期12-15,46,共5页
Aerospace Shanghai
