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IEEE 292

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

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Organization: IEEE
Publication Date: 1 January 1969
Status: active
Page Count: 29
scope:

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].

Document History

June 19, 2013
Errata to Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
A description is not available for this item.
April 26, 2010
Errata to Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
Foreword This Specification Format has been prepared as a guide for the preparation of a single-degree-of-freedom springrestrained rate gyro specification. Prepared by the Gyro and Accelerometer...
January 1, 1969
Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
A description is not available for this item.
January 1, 1969
Specification Format for Single- Degree-of-Freedom Spring-Restrained Rate Gyros
Foreword This Specification Format has been prepared as a guide for the preparation of a single-degree-of-freedom springrestrained rate gyro specification. Prepared by the Gyro and Accelerometer...
January 1, 1969
Specification Format for Single- Degree-of-Freedom Spring-Restrained Rate Gyros
Foreword This Specification Format has been prepared as a guide for the preparation of a single-degree-of-freedom springrestrained rate gyro specification. Prepared by the Gyro and Accelerometer...
IEEE 292
January 1, 1969
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...

References

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