Study of Procedure Errors of the Vortex Air Data System of a Subsonic Aircraft
- Авторы: Efremova E.1, Soldatkin V.1
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Учреждения:
- Tupolev Kazan National Research Technical University
- Выпуск: Том 61, № 4 (2018)
- Страницы: 613-619
- Раздел: Aircraft Instruments and Instrumentation Computer Complexes
- URL: https://journals.rcsi.science/1068-7998/article/view/230733
- DOI: https://doi.org/10.3103/S1068799818040165
- ID: 230733
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Аннотация
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.
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Об авторах
E. Efremova
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: w-soldatkin@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111