Email this article Study of Procedure Errors of the Vortex Air Data System of a Subsonic Aircraft
- Authors: Efremova E.S.1, Soldatkin V.V.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 4 (2018)
- Pages: 613-619
- Section: Aircraft Instruments and Instrumentation Computer Complexes
- URL: https://journal-vniispk.ru/1068-7998/article/view/230733
- DOI: https://doi.org/10.3103/S1068799818040165
- ID: 230733
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Abstract
The features of design and structural-functional scheme of the vortex air data system for a subsonic aircraft are considered. Mathematical models are revealed and procedure aerodynamic errors of the system measuring channels are quantitatively estimated.
About the authors
E. S. Efremova
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
V. V. Soldatkin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: w-soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
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