SST-LL重力测量卫星轨道分析  

Analysis of SST-LL Gravity Exploring Satellite Orbit

作　　者：覃政[1] 张立华[1] 丁延卫[1] 

机构地区：[1]航天东方红卫星有限公司,北京100094

出　　处：《航天器工程》2012年第3期23-27,共5页Spacecraft Engineering

基　　金：国家重大航天工程

摘　　要：论述了SST-LL重力测量卫星科学任务对轨道寿命、地面覆盖性能、轨道高度单圈波动、星间距离变化范围的需求。根据需求,计算了轨道的自然衰减情况,得出轨道初始高度为500km;综合考虑地面覆盖要求及运载火箭能力,得出了最佳轨道倾角为89°;得出了0.002 0偏心率下轨道高度波动范围不超过50km;分析得出星间距离的长周期变化主要受大气阻力影响,初步确定了轨道控制方案,即定期对受大气阻力较大的卫星进行轨道机动。The needs of scientific targets of the low-low satellite-to-satellite tracing （SST-LL） gravity exploring satellite for the orbit life, ground-coverage, altitude variation range in one circle and distance between two satellites are considered. According to the needs, the aerodynamic loss and the optimal in- clinations are computed. As a result, the initial altitude should be 500kin and inclination of 89°would be the best choice for the ground-coverage and launch vehicle. The altitude variation range is less than 50km with the eccentricity 0. 0020. The main cause of the distance variation between two satellites is aerody- namic drag, and the control strategy of the distance variation is analyzed, such as periodic orbit maneuver for the satellite which sufferes higher aerodynamic drag.

关 键 词：重力测量卫星 低-低卫星跟踪卫星 轨道参数 地面覆盖 星间距离 

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]