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Published on: August 15, 2014
A New MEMS Gyroscope Used for Single-Channel Damping
Zengping Zhang1, Wei Zhang2, Fuxue Zhang3
1School of Computer and Information Management, Inner Mongolia University of Finance and Economics, Hohhot 010070, China. 100002170@imufe.edu.cn.
This novel silicon microelectromechanical systems (MEMS) gyroscope uses aircraft spin for sensing angular velocity. Its unique design enables automatic carrier frequency adjustment, ideal for rotating aircraft control systems.
Area of Science:
- Mechanical Engineering
- Aerospace Engineering
- Electrical Engineering
Background:
- Traditional MEMS gyroscopes often require a dedicated drive structure.
- Rotating aircraft present unique challenges for attitude and motion sensing.
Purpose of the Study:
- To introduce a novel MEMS gyroscope concept that utilizes the inherent spin of a rotating aircraft.
- To demonstrate its suitability for single-channel control systems in rotating aircraft.
Main Methods:
- Derivation of the MEMS gyroscope's motion equation.
- Analysis to solve the motion equation and determine dynamic parameters.
- Experimental validation using a precision three-axis rate table.
Main Results:
- The novel MEMS gyroscope operates without a drive structure, relying solely on its sense structure.
- It generates an amplitude-modulation signal where the envelope is proportional to angular velocity.
- Experimental results showed high correlation (0.9969, 0.9872, 0.9842) between theoretical and tested values.
Conclusions:
- The proposed MEMS gyroscope design and sensing mechanism are validated.
- Its ability to sense transverse angular rotation and adapt carrier frequency makes it suitable for rotating aircraft control systems.
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