Email this article To the Problem of Estimating the Angle of Attack of an Aircraft by the Kalman Filter
- Authors: Golovan A.A.1, Sharonov A.V.2
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Affiliations:
- Lomonosov Moscow State University
- Moscow Aviation Institute (National Research University)
- Issue: Vol 61, No 2 (2018)
- Pages: 311-315
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/230556
- DOI: https://doi.org/10.3103/S1068799818020241
- ID: 230556
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Abstract
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.
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About the authors
A. A. Golovan
Lomonosov Moscow State University
Author for correspondence.
Email: aagolovan@yandex.ru
Russian Federation, GSP-1, Leninskie Gory, Moscow, 119991
A. V. Sharonov
Moscow Aviation Institute (National Research University)
Email: aagolovan@yandex.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
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