Adaptation of pendulum correction of an aircraft strapdown gyrovertical to flight conditions
- 作者: Kachanov B.1, Grishin D.2, Akhmedova S.1, Tuktarev N.1, Kulabukhov V.1
-
隶属关系:
- Uspensky Avionica Moscow Research and Production Complex JSC
- Moscow Aviation Institute (National Research University)
- 期: 卷 8, 编号 2 (2017)
- 页面: 115-120
- 栏目: Article
- URL: https://journals.rcsi.science/2075-1087/article/view/204051
- DOI: https://doi.org/10.1134/S2075108717020067
- ID: 204051
如何引用文章
详细
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.
作者简介
B. Kachanov
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
俄罗斯联邦, Moscow
D. Grishin
Moscow Aviation Institute (National Research University)
Email: ms.akhmedova@gmail.com
俄罗斯联邦, Moscow
S. Akhmedova
Uspensky Avionica Moscow Research and Production Complex JSC
编辑信件的主要联系方式.
Email: ms.akhmedova@gmail.com
俄罗斯联邦, Moscow
N. Tuktarev
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
俄罗斯联邦, Moscow
V. Kulabukhov
Uspensky Avionica Moscow Research and Production Complex JSC
Email: ms.akhmedova@gmail.com
俄罗斯联邦, Moscow