Enviar artigo por via de e-mail To the Problem of Estimating the Angle of Attack of an Aircraft by the Kalman Filter
- Autores: Golovan A.A.1, Sharonov A.V.2
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Afiliações:
- Lomonosov Moscow State University
- Moscow Aviation Institute (National Research University)
- Edição: Volume 61, Nº 2 (2018)
- Páginas: 311-315
- Seção: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230556
- DOI: https://doi.org/10.3103/S1068799818020241
- ID: 230556
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Resumo
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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Sobre autores
A. Golovan
Lomonosov Moscow State University
Autor responsável pela correspondência
Email: aagolovan@yandex.ru
Rússia, GSP-1, Leninskie Gory, Moscow, 119991
A. Sharonov
Moscow Aviation Institute (National Research University)
Email: aagolovan@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
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