共置卫星轨道及星间距确定  

Orbit and Relative Separation Determination for Colocated Geostationary Satellites

作　　者：王福润[1] 邹广瑞[1] 余四祥[1] 

机构地区：[1]北京控制工程研究所,100080

出　　处：《航天控制》1997年第1期24-28,共5页Aerospace Control

摘　　要：共置卫星的遥测遥控，离不开对其每一卫星的轨道及星间距的确定。本文通过地面站顺序测量确定和交替测量确定两种方法来完成三颗共置卫星的轨道参数及星间距的确定。It is very essential to determine the orbit elements and relative separation of cola-cated geostationary satellites. This paper puts puts forward two methods to solve this problem, oneis sequential observation determination method, and the other is alternate observation determination method. Compared with inter- satellite tracking, those methods are simple in engi-nerrign implementation.

关 键 词：星间距 卫星轨道 轨道确定 遥测 

分 类 号：V556.3[航空宇航科学与技术—人机与环境工程]