Autonomous Orbit Determination of HY2A and ZY3 Missions Using Space-borne GPS Measurements

GONG Xuewen; WANG Fuhong

doi:10.13203/j.whugis20140892

Volume 42 Issue 3

Mar. 2017

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Geomatics and Information Science of Wuhan University > 2017 > 42(3): 309-313. > DOI: 10.13203/j.whugis20140892

GONG Xuewen, WANG Fuhong. Autonomous Orbit Determination of HY2A and ZY3 Missions Using Space-borne GPS Measurements[J]. Geomatics and Information Science of Wuhan University, 2017, 42(3): 309-313. DOI: 10.13203/j.whugis20140892

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Autonomous Orbit Determination of HY2A and ZY3 Missions Using Space-borne GPS Measurements

GONG Xuewen^{1, 2,},
WANG Fuhong¹

1.
School of Geodesy and Geomatics, Wuhan University, Wuhan 430079, China
2.
Collaborative Innovation Center for Geospatial Technology, Wuhan University, Wuhan 430079, China

Funds:

The National Natural Science Foundation of China 41374035

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Author Bio:
GONG Xuewen, PhD candidate, specializes in GPS navigation. E-mail:gongxuewen@whu.edu.cn
Received Date: April 23, 2015
Published Date: March 04, 2017

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Abstract

Abstract

This paper studied the determination of autonomous orbits of HY2A and ZY3 missions using on-board GPS data. A simulative on-board processing of real-time orbit determination was carried out using the space-borne GPS dual frequency pseudo-range and phase measurements with the auto-developed software SATODS. The test demonstrates that, based on pseudo-rang data, the position and velocity error (3D RMS) of orbit results are up to 1.3 m and 1.2 mm/s respectively, but with phase data, they are reduced to 38cm and 0.36 mm/s for HY2A mission, where the radial accuracy is about 10 cm, and decreased to 54 cm and 0.54 mm/s for ZY3 mission. These contributions can be used for certain real-time service of continued low-earth orbiters (LEO) for earth observations.
- space-borne GPS,
- autonomous orbit determination,
- on-board real time processing

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References (16)

References

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Autonomous Orbit Determination of HY2A and ZY3 Missions Using Space-borne GPS Measurements

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