A simplified yaw-attitude model for eclipsing GPS satellites
作者： J. Kouba
DOI: 10.1007/S10291-008-0092-1
关键词:
摘要: … possible to model yaw-attitude control during eclipsing periods by using the constant hardware yaw rate of 0.20/s. The Block IIR satellites maintain the nominal yaw attitude even during …
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igs.org 参考文章(5)
E. Brockmann, G. Beutler, U. Hugentobler, A. Verdun, W. Gurtner, L. Mervart, M. Rothacher, Extended orbit modeling techniques at the CODE processing center of the international GPS service for geodynamics (IGS): theory and initial results. manuscripta geodaetica. ,vol. 19, pp. 367- 386 ,(1994)
P. Héroux, J. Kouba, GPS precise point positioning using IGS orbit products Physics and Chemistry of the Earth, Part A: Solid Earth and Geodesy. ,vol. 26, pp. 573- 578 ,(2001) , 10.1016/S1464-1895(01)00103-X
J.M. Dow, R.E. Neilan, G. Gendt, The International GPS Service: Celebrating the 10th anniversary and looking to the next decade Advances in Space Research. ,vol. 36, pp. 320- 326 ,(2005) , 10.1016/J.ASR.2005.05.125
W. I. Bertiger, G. A. Hajj, J. T. Wu, S. M. Lichten, S. C. Wu, Effects of antenna orientation on GPS carrier phase Astrodynamics 1991. pp. 1647- 1660 ,(1992)
Yoaz E. Bar-Sever, A new model for GPS yaw attitude Journal of Geodesy. ,vol. 70, pp. 714- 723 ,(1996) , 10.1007/BF00867149