Enviar artigo por via de e-mail Adaptation of pendulum correction of an aircraft strapdown gyrovertical to flight conditions
- Autores: Kachanov B.1, Grishin D.2, Akhmedova S.1, Tuktarev N.1, Kulabukhov V.1
-
Afiliações:
- Uspensky Avionica Moscow Research and Production Complex JSC
- Moscow Aviation Institute (National Research University)
- Edição: Volume 8, Nº 2 (2017)
- Páginas: 115-120
- Seção: Article
- URL: https://journals.rcsi.science/2075-1087/article/view/204051
- DOI: https://doi.org/10.1134/S2075108717020067
- ID: 204051
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
An algorithm for a gyrovertical based on MEMS sensors for detecting pitch and roll angles of aircraft is considered. It is suggested to integrate inertial sensors with an air data system. A flight simulator is used to optimize the algorithm coefficients.
Sobre autores
B. Kachanov
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
Rússia, Moscow
D. Grishin
Moscow Aviation Institute (National Research University)
Email: ms.akhmedova@gmail.com
Rússia, Moscow
S. Akhmedova
Uspensky Avionica Moscow Research and Production Complex JSC
Autor responsável pela correspondência
Email: ms.akhmedova@gmail.com
Rússia, Moscow
N. Tuktarev
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
Rússia, Moscow
V. Kulabukhov
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
Rússia, Moscow
