Attitude Determination Using Ambiguous GNSS Phase Measurements and Absolute Angular Rate Measurements
- 作者: Zharkov M.V.1, Veremeenko K.K.1, Antonov D.A.1, Kuznetsov I.M.1
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隶属关系:
- Moscow Aviation Institute (MAI) (National Research University)
- 期: 卷 9, 编号 4 (2018)
- 页面: 277-286
- 栏目: Article
- URL: https://bakhtiniada.ru/2075-1087/article/view/204484
- DOI: https://doi.org/10.1134/S2075108718040090
- ID: 204484
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详细
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.
作者简介
M. Zharkov
Moscow Aviation Institute (MAI) (National Research University)
编辑信件的主要联系方式.
Email: mv_zharkov@mai.ru
俄罗斯联邦, Moscow, 125993
K. Veremeenko
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
俄罗斯联邦, Moscow, 125993
D. Antonov
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
俄罗斯联邦, Moscow, 125993
I. Kuznetsov
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
俄罗斯联邦, Moscow, 125993
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