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


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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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