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低低卫-卫跟踪重力测量物理模型及部分姿轨控技术需求
Physical model for SST-LL gravity measurement and some technical demand for attitude and orbit control
【摘要】 文章从低低卫 卫跟踪(SST LL)重力测量的基本物理思想出发,导出了SST LL重力测量的物理模型,并由此确定了SST LL重力测量所需要的观测量;从重力测量对低低孪星的编队要求出发,得出了孪星轨道的平均半长轴之差最低控制需求,导出了卫星姿态俯仰角控制与孪星到地心的距离、及与孪星沿迹相对距离的关系,并估算了孪星两次编队保持机动的时间间隔。
【Abstract】 Based on the essential physical thought,the paper builds up the physical model of gravity measurement by Low-Low Satellite-Satellite Tracing (SST-LL) technology,therefore,confirms the required observations for SST-LL gravity measurement.To meet the low-low twin satellites formation,the paper analyzes the requirement of the difference of the mean semi-major axes and the pitch control of the twin satellites.Finally,the time space between two formation keeping maneuvers is approximately calculated.
【关键词】 卫星重力测量;
SSTLL;
孪星编队;
姿轨控需求;
【Key words】 Space-borne gravity measurement; SST-LL; Twin satellites formation; Attitude and orbit control;
【Key words】 Space-borne gravity measurement; SST-LL; Twin satellites formation; Attitude and orbit control;
【基金】 "十五"863预研项目(编号2002AA74010)资助
- 【文献出处】 宇航学报 ,Journal of Astronautics , 编辑部邮箱 ,2004年05期
- 【分类号】V448
- 【被引频次】5
- 【下载频次】146