Measurement of Phase Difference for Micromachined Gyros Driven by Rotating Aircraft

This paper presents an approach for realizing a phase difference measurement of a new gyro. A silicon micromachined gyro was mounted on rotating aircraft for aircraft attitude control. Aircraft spin drives the silicon pendulum of a gyro rotating at a high speed so that it can sense the transverse an...

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Bibliographic Details

Published in:	Sensors
Main Authors:	Wei Zhang, Zengping Zhang, Fuxue Zhang
Format:	Article
Language:	English
Published:	MDPI AG 2013-08-01
Subjects:	micromachined gyro silicon pendulum phase difference rotating aircraft
Online Access:	http://www.mdpi.com/1424-8220/13/8/11051