Evaluation of orbit determination using dual ranging method

被引：0
|
作者：
Ibrahim, Mohamed [1 ]
Zahara, Mohamed [1 ]
Emam, Amr [1 ]
Elghany, Mohamed Abd [1 ]
机构：
[1] Al Azhar Univ, Dept Elect Engn, Fac Engn, Nasr City, Cairo, Egypt
来源：
PROCEEDINGS OF THE WSEAS INTERNATIONAL CONFERENCE ON CIRCUITS, SYSTEMS, ELECTRONICS, CONTROL & SIGNAL PROCESSING: SELECTED TOPICS ON CIRCUITS, SYSTEMS, ELECTRONICS, CONTROL & SIGNAL PROCESSING | 2007年
关键词：
orbit; coordinate systems; orbit determination; dual ranging;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The paper provides both the theoretical and practical results for Geo-stationary satellites orbit determination using both dual Ranging from Two separate earth station locations and Classical orbit determination from an earth station. The orbit determination is performed through a generated Matlab program and is compared with a flight proven software tool. The program takes into account the dynamic model [1],[5],[6] of the satellite which takes orbit perturbations due to non-spherical earth shape, the gravitational forces of the sun and moon, and the atmospheric drag. Acceptable results where foreseen in comparison to the flight proven software tool.
引用
收藏
页码：515 / 520
页数：6
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