• 学术论文 •

基于全球导航卫星系统的高轨卫星定轨理论研究及仿真实现

1. 装备指挥技术学院
• 收稿日期:2011-03-25 修回日期:1900-01-01 出版日期:2011-05-05 发布日期:2015-06-24
• 通讯作者: 王威

Research and Simulation of Orbit Determination for Geostationary Satellite Based on GNSS

• Received:2011-03-25 Revised:1900-01-01 Online:2011-05-05 Published:2015-06-24

Abstract: Abstract: As the limitations of ground orbit system, this paper presents a method of orbit determination of GEO satellite based on GNSS, and designs an orbit determination of GEO satellite software. Combination of orbit determination of GEO satellite characteristics and construction of GNSS, the satellite visibility algorithms and inter-satellite observation model are discussed, integral Filter method is proposed to determine the orbit of geostationary satellite to make use of the advantage of orbit integral and Kalman filter method. Simulation results show that orbit determination of GEO satellite based on GNSS can increase the satellite observations and improve the accuracy of orbit determination. Finally, the paper develops a space-based orbit determination of GEO satellite simulation platform with STK, MATLAB and Visual C++. The outcomes of this paper will provide theoretical reference and ideal simulation tool for the application of Compass on orbit determination of GEO satellite.