Gyroscopy and Navigation

, Volume 9, Issue 4, pp 277–286 | Cite as

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

  • M. V. ZharkovEmail author
  • K. K. Veremeenko
  • D. A. Antonov
  • I. M. Kuznetsov


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.


GNSS integrated navigation system resolution of the integer ambiguity of phase measurements determination of attitude parameters 


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Copyright information

© Pleiades Publishing, Ltd. 2018

Authors and Affiliations

  • M. V. Zharkov
    • 1
    Email author
  • K. K. Veremeenko
    • 1
  • D. A. Antonov
    • 1
  • I. M. Kuznetsov
    • 1
  1. 1.Moscow Aviation Institute (MAI) (National Research University)MoscowRussia

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