Autonomous orbit determination study for space navigation satellite

被引：0

作者：

Wang D.-X. ^{[1
]}

Xin J. ^{[1
]}

Zhang Z.-X. ^{[1
]}

Tang T.-S. ^{[1
]}

Fu J.-Z. ^{[1
]}

机构：

[1] Beijing Satellite Navigation Center, Beijing

来源：

Journal of Beijing Institute of Technology (English Edition) | 2016年 / 25卷

基金：

中国国家自然科学基金;

关键词：

Autonomous orbit determination; Distributed; Inter-satellite links; Kalman filter;

D O I：

10.15918/j.jbit1004-0579.201625.S206

中图分类号：

学科分类号：

摘要：

In order to improve the ephemeris accuracy of space navigation satellite, an autonomous orbit determination method is proposed. This paper not only builds the bidirectional pseudo-range measurement model, but also designs the two-step Kalman filter method. The satellite position and covariance are obtained in the first step by single point positioning method, which is considered as the pseudo-range measurement in second step to update orbital and time parameters. Moreover, the orbit orientation parameters are used to constraint the constellation rotation, solving the problem of rank deficiency of autonomous orbit determination. The simulation and analysis results illustrate the feasibility the proposed algorithm. © 2016 Beijing Institute of Technology.

引用

页码：26 / 30

页数：4

共 10 条

[1]

Ananda M.P., Berstein H., Bruce R.W., Et al., Autonomous navigation of the global positioning system satellite, AIAA Guidance and Control Conference, (1984)

[2]

Codik A., Autonomous navigation of GPS satellites-A challenge for the future, The 8th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GNSS), (1985)

[3]

Ananda M.P., Bernstein H., Cunninggham W.A., Et al., Global positioning system (GPS) autonomous navigation, IEEE Position Location and Navigation Symposium, (1990)

[4]

Liu Y.C., Liu L., Wang C.B., On the orbit determination combined the satellite-satellite tracking and the ground based tracking, Publications of Purple Mountain Observatory, 19, 2, pp. 117-120, (2000)

[5]

Menn M.D., Berstein H., Ephemeris observability issues in the global positioning system autonomous navigation, IEEE Position Location and Navigation Symposium, (1994)

[6]

Li B., Research on long-term autonomous orbit determination for navigation constellation based on inter-satellite orientation observation, (2010)

[7]

Yang L., Guo F.X., Wen Y.L., Et al., Analysis of autonomous orbit determination for navigation constellation with one anchor station, Journal Spacecraft TT&C Technology, 32, pp. 444-448, (2013)

[8]

Shang L., Ren Q.Y., Zhang R., Et al., Eliminating constellation rotation error of autonomous orbit determination using differential anchor station, Geomatics and Information Science of Wuhan University, 38, pp. 920-924, (2013)

[9]

Liu L., Spacecraft Orbital Theory, (2000)

[10]

Song X.Y., Study on the orbit determination of COMPASS navigation satellite, (2009)

← 1 →