Email this article Attitude Determination Using Ambiguous GNSS Phase Measurements and Absolute Angular Rate Measurements
- Authors: Zharkov M.V.1, Veremeenko K.K.1, Antonov D.A.1, Kuznetsov I.M.1
-
Affiliations:
- Moscow Aviation Institute (MAI) (National Research University)
- Issue: Vol 9, No 4 (2018)
- Pages: 277-286
- Section: Article
- URL: https://journal-vniispk.ru/2075-1087/article/view/204484
- DOI: https://doi.org/10.1134/S2075108718040090
- ID: 204484
Cite item
Open Access
Access granted
Subscription Access
Abstract
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.
About the authors
M. V. Zharkov
Moscow Aviation Institute (MAI) (National Research University)
Author for correspondence.
Email: mv_zharkov@mai.ru
Russian Federation, Moscow, 125993
K. K. Veremeenko
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
Russian Federation, Moscow, 125993
D. A. Antonov
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
Russian Federation, Moscow, 125993
I. M. Kuznetsov
Moscow Aviation Institute (MAI) (National Research University)
Email: mv_zharkov@mai.ru
Russian Federation, Moscow, 125993
Supplementary files
