Attitude Determination Using Ambiguous GNSS Phase Measurements and Absolute Angular Rate Measurements
- Autores: Zharkov M.V.1, Veremeenko K.K.1, Antonov D.A.1, Kuznetsov I.M.1
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Afiliações:
- Moscow Aviation Institute (MAI) (National Research University)
- Edição: Volume 9, Nº 4 (2018)
- Páginas: 277-286
- Seção: Article
- URL: https://journals.rcsi.science/2075-1087/article/view/204484
- DOI: https://doi.org/10.1134/S2075108718040090
- ID: 204484
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Resumo
Integration of a multiantenna GNSS receiver and inertial sensors (gyroscopes) is proposed to determine attitude parameters using GNSS phase measurements, containing integer ambiguity, and measurements of the absolute rotation rate of a moving vehicle. The potential accuracy of the proposed technology is estimated based on the simulation and full-scale tests. The implementation of the proposed approach is considered.
Sobre autores
M. Zharkov
Moscow Aviation Institute (MAI) (National Research University)
Autor responsável pela correspondência
Email: mv_zharkov@mai.ru
Rússia, Moscow, 125993
K. Veremeenko
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
Rússia, Moscow, 125993
D. Antonov
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
Rússia, Moscow, 125993
I. Kuznetsov
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
Rússia, Moscow, 125993
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