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1431-2004 - IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros | IEEE Standard | IEEE Xplore

1431-2004 - IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros

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Abstract:

Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring system...Show More
Scope:Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring system...Show More
Purpose:This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial a...Show More

Abstract:

Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A standard specification format guide for the preparation of a single-axis CVG is provided. A compilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.
Scope:
Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.
Purpose:
This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros.
Date of Publication: 20 December 2004
Electronic ISBN:978-0-7381-4006-3
Persistent Link: https://ieeexplore.ieee.org/servlet/opac?punumber=9606

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