Математическое моделирование, компьютерный и натурный эксперимент в естественных науках
Электронный научный журнал

Технические науки
Method of research of inertial MEMS-type sensors, intended for operating on helicopter type under exposure to synusoidal vibration
Kondratov D.V. 2, Kalikhman D.M. 3, Lvov A.A. 1, Seranova A.A. 1, Ermakov R.V. 1

1.
2.
3. Branch of the Federal State Unitary Enterprise “Academician Pilyugin Scientific-production Center of Automatics and Instrument-making” - Production Association “Korpus”

Abstract:

The features of the use of micromechanical sensors of angular velocity and linear acceleration for building blocks of sensors of primary information used in automatic control systems for helicopter-type aircraft are considered. The difficulties arising from the replacement of previously used inertial sensors with sensors of a different type are described. The proposed methodology for the design of the sensor unit and its subsequent tests, allowing to take into account and eliminate the arising difficulties.

Keywords: frequency response of the sensor, micromechanical sensors, inertial sensors, tests

Сайт работает на RAE Editorial System