An empirical model for the attitude mode switch maneuvers of QZS-1 satellite

Author:

Yuan Yongqiang,Li Xingxing,Huang Jiande,Li Jie,Huang Shi,Liu Chengbo,Zhang Keke

Publisher

Springer Science and Business Media LLC

Subject

General Earth and Planetary Sciences

Reference32 articles.

1. Bar-Sever YE (1996) A new model for GPS yaw attitude. J Geod 70(11):714–723. https://doi.org/10.1007/BF00867149

2. Beutler G, Brockmann E, Gurtner W, Hugentobler U, Mervart L, Rothacher M, Verdun A (1994) Extended orbit modeling techniques at the CODE processing center of the international GPS service for geodynamics (IGS): theory and initial results. Manuscr Geod 19(6):367–386

3. Bury G, Sośnica K, Zajdel R, Strugarek D (2020) Toward the 1-cm Galileo orbits: challenges in modeling of perturbing forces. J Geod 94(2):16. https://doi.org/10.1007/s00190-020-01342-2

4. CAO (2021a) QZSS satellite property information. Cabinet Office, Government of Japan. https://qzss.go.jp/en/technical/qzssinfo/

5. CAO (2021b) The history information of QZS-1 operation. Cabinet Office, Government of Japan. https://qzss.go.jp/en/technical/qzssinfo/khp0mf0000000wuf-att/ohi-qzs1_20180630.pdf?t=1619697688071; and https://qzss.go.jp/en/technical/qzssinfo/khp0mf0000000wuf-att/ohi-qzs1_210328.pdf?t=1619697688071

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