Email this article Adaptation of pendulum correction of an aircraft strapdown gyrovertical to flight conditions
- Authors: Kachanov B.O.1, Grishin D.V.2, Akhmedova S.K.1, Tuktarev N.A.1, Kulabukhov V.S.1
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Affiliations:
- Uspensky Avionica Moscow Research and Production Complex JSC
- Moscow Aviation Institute (National Research University)
- Issue: Vol 8, No 2 (2017)
- Pages: 115-120
- Section: Article
- URL: https://journal-vniispk.ru/2075-1087/article/view/204051
- DOI: https://doi.org/10.1134/S2075108717020067
- ID: 204051
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Abstract
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.
About the authors
B. O. Kachanov
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
Russian Federation, Moscow
D. V. Grishin
Moscow Aviation Institute (National Research University)
Email: ms.akhmedova@gmail.com
Russian Federation, Moscow
S. K. Akhmedova
Uspensky Avionica Moscow Research and Production Complex JSC
Author for correspondence.
Email: ms.akhmedova@gmail.com
Russian Federation, Moscow
N. A. Tuktarev
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
Russian Federation, Moscow
V. S. Kulabukhov
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
Russian Federation, Moscow
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