Adaptation of pendulum correction of an aircraft strapdown gyrovertical to flight conditions

B. O. Kachanov; D. V. Grishin; S. K. Akhmedova; N. A. Tuktarev; V. S. Kulabukhov

doi:10.1134/S2075108717020067

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
Affiliations:
1. Uspensky Avionica Moscow Research and Production Complex JSC
2. Moscow Aviation Institute (National Research University)
Issue: Vol 8, No 2 (2017)
Pages: 115-120
Section: Article
URL: https://journals.rcsi.science/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.