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Attitude Determination Using Ambiguous GNSS Phase Measurements and Absolute Angular Rate Measurements

https://doi.org/10.17285/0869-7035.2018.26.3.054-068

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)
Russian Federation


K. K. Veremeenko
(Moscow Aviation Institute (MAI) (National Research University)
Russian Federation


D. A. Antonov
(Moscow Aviation Institute (MAI) (National Research University)
Russian Federation


I. M. Kuznetsov
(Moscow Aviation Institute (MAI) (National Research University)
Russian Federation


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Review

For citations:


Zharkov M.V., Veremeenko K.K., Antonov D.A., Kuznetsov I.M. Attitude Determination Using Ambiguous GNSS Phase Measurements and Absolute Angular Rate Measurements. Giroskopiya i Navigatsiya / Gyroscopy and Navigation. 2018;26(3):54-68. (In Russ.) https://doi.org/10.17285/0869-7035.2018.26.3.054-068

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ISSN 0869-7035 (Print)
ISSN 2075-0927 (Online)