Russian Aeronautics

, Volume 61, Issue 2, pp 311–315 | Cite as

To the Problem of Estimating the Angle of Attack of an Aircraft by the Kalman Filter

  • A. A. GolovanEmail author
  • A. V. Sharonov
Flight Dynamics and Control of Flight Vehicles


The paper considers the problem of estimating the angle of attack of an aircraft only by indications of accelerometers that are rigidly set on its fuselage. This task is posed as a task of “realization”, when the structure and the order of linearized model of the estimation problem is unknown. The possibility of solving this problem is analyzed.


angle of attack Hankel matrix Ho–Kalman algorithm 


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© Allerton Press, Inc. 2018

Authors and Affiliations

  1. 1.Lomonosov Moscow State UniversityMoscowRussia
  2. 2.Moscow Aviation Institute (National Research University)MoscowRussia

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