Inactive-Reserved Standard

IEEE 293-1969

IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros

Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.

Sponsor Committee
AES/GA - Gyro Accelerometer Panel
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Status
Inactive-Reserved Standard
Corrigendum
293-1969/Cor 1-2014
History
ANSI Approved:
1986-11-17
Published:
1968-11-30
Reaffirmed:
2010-06-17
Inactivated Date:
2021-03-25

Working Group Details

Society
IEEE Aerospace and Electronic Systems Society
Learn More About IEEE Aerospace and Electronic Systems Society
Sponsor Committee
AES/GA - Gyro Accelerometer Panel
Learn More About AES/GA - Gyro Accelerometer Panel
Working Group
SENSR_WG - Sensors Working Group
IEEE Program Manager
Malia Zaman
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Working Group Chair
Jason Bingham

Other Activities From This Working Group

Current projects that have been authorized by the IEEE SA Standards Board to develop a standard.


P1431
Standard for Specifying and Testing Coriolis Vibratory Gyros

This standard defines requirements and test procedures 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. Informative annexes cover CVG design features and theoretical principles of operation.

Learn More About P1431

P836
Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers

This recommended practice describes the conduct and analysis of precision tests for linear accelerometers using centrifuge techniques. The term “precision,” in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.

Learn More About P836

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