The technology of precise orbit determination for HY-2A satellite

Jiang Xingwei,Wang Xiaohui,Peng Hailong,Lin Mingsen

Strategic Study of CAE ›› 2013, Vol. 15 ›› Issue (7) : 19 -24.

PDF (1005KB)
Strategic Study of CAE ›› 2013, Vol. 15 ›› Issue (7) : 19 -24.

The technology of precise orbit determination for HY-2A satellite

Author information +
History +
PDF (1005KB)

Abstract

The HY-2A satellite, launched on October 16, 2011 is the first dynamic environments satellite in China, carrying the radar altimeter which continues the time series of centimeter lever ocean topography measurement. Orbit error is a major component in the overall error budge of all altimeter satellite missions. The HY-2A satellite carries DORIS deceiver, Dual frequency GPS receiver and Laser Retroreflector Array for Precise orbit determination (POD) to meet 10cm radial accuracy goal for the HY-2A satellite radar altimeter. First, the tracking system and method of POD for HY-2A satellite is introduced, then the solution strategy is showed, finally the results of the radial accuracy for HY-2A satellite are given in this paper.

Keywords

precise orbit determination / GPS / DORIS / SLR

Cite this article

Download citation ▾
Jiang Xingwei,Wang Xiaohui,Peng Hailong,Lin Mingsen. The technology of precise orbit determination for HY-2A satellite. Strategic Study of CAE, 2013, 15(7): 19-24 DOI:

登录浏览全文

4963

注册一个新账户 忘记密码

References

AI Summary AI Mindmap
PDF (1005KB)

290

Accesses

0

Citation

Detail

Sections
Recommended

AI思维导图

/