Inactive-Reserved Standard

IEEE 292-1969

IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros

This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].

Sponsor Committee
AES/GA - Gyro Accelerometer Panel
Learn More About AES/GA - Gyro Accelerometer Panel
Status
Inactive-Reserved Standard
History
ANSI Approved:
1986-11-17
Published:
1968-11-30
Reaffirmed:
2010-06-17
Inactivated Date:
2021-03-25

Additional Resources

Erratas
292-1969_errata.pdf

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
Contact Malia Zaman
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 u201cprecision,u201d 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

Standards approved by the IEEE SA Standards Board that are within the 10-year lifecycle.


No Active Standards

These standards have been replaced with a revised version of the standard, or by a compilation of the original active standard and all its existing amendments, corrigenda, and errata.


No Superseded Standards

These standards have been removed from active status through a ballot where the standard is made inactive as a consensus decision of a balloting group.


No Inactive-Withdrawn Standards

These standards are removed from active status through an administrative process for standards that have not undergone a revision process within 10 years.


No Inactive-Reserved Standards
Subscribe

Sign up for our monthly newsletter to learn about new developments, including resources, insights and more.