Precise Orbit Determination for COMPASS IGSO Satellites During Yaw Maneuvers-Reference-Cited by-同舟云学术

Precise Orbit Determination for COMPASS IGSO Satellites During Yaw Maneuvers

Published:2013 Issue: Volume: Page:41-53
ISSN:1876-1100
Container-title:Lecture Notes in Electrical Engineering
language:
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Author:

Guo Jing,Zhao Qile,Geng Tao,Su Xing,Liu Jingnan

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-37407-4_4

Reference9 articles.

1. Bar-Sever Y (1996) A new model for GPS yaw attitude. J Geod 70:714–723. doi: 10.1007/BF00867149

2. Kouba J (2009) A simplified yaw-attitude model for eclipsing GPS satellites. GPS Sol 13:1–12. doi: 10.1007/s10291-008-0092-1

3. Dilssner F (2010) GPS IIF-1 satellite antenna phase center and attitude modeling. In: Inside GNSS. Gibbons Media and Research, LLC, Eugene, Orefon, U.S.A, pp 59–64

4. Dilssner F, Springer T, Gienger G, Dow J (2011) The GLONASS-M satellite yaw-attitude model. Adv Space Res 47:160–171. doi: 10.1016/j.asr.2010.09.007

5. Griffiths J, Ray J (2009) On the precision and accuracy of IGS orbits. J Geod 83:277–287. doi: 10.1007/s00190-008-0237-6

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