Relative clock estimation method between two LEO satellites with a double-difference solution constraint

Author:

Liu Junhong,Gu Defeng,Ju Bing,Lai Yuwang,Yi Dongyun

Funder

National Natural Science Foundation of China

Program for New Century Excellent Talents in University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. W. Bertiger, Y. Bar-Sever, S. Bettadpur, S. Desai, C. Dunn, B. Haines, et al., GRACE: millimeters and microns in orbit, in: Proceedings of the 15th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS 2002), 2002, pp. 2022–2029.

2. C. Dunn, W. Bertiger, G. Franklin, I. Harris, D. Nguyen, T. Meehan, et al., The Instrument on NASA׳s GRACE mission: augmentation of GPS to achieve unprecedented gravity field measurements, in: Proceedings of the15th Technical Meeting of the Satellite Division of the Institute of Navigation, 2002.

3. An Earth gravity field model complete to degree and order150 from GRACE: EIGEN-GRACE02S;Reigber;J. Geodyn.,2005

4. GGM02 – an improved Earth gravity field model from GRACE;Tapley;J. Geod.,2005

5. W. Bertiger, C. Dunn, I. Harris, G. Kruizinga, L. Romans, M. Watkins, et al., Relative time and frequency alignment between two low Earth orbiters, GRACE, in: Proceedings of the IEEE International Frequency Control Symposium and PDA Exhibition Jointly with the 17th European Frequency and Time Forum, 2003, pp. 273–279.

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