292-1969 IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros

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Organization: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 20 June 1969
Status: active
Page Count: 15
Page(s): 1 - 16
ICS Code (On-board equipment and instruments): 49.090
ISBN (Online): 978-0-7381-0542-0
DOI: 10.1109/IEEESTD.1969.80213

Abstracts

Standard

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]. An errata is available at http://standards.ieee.org/findstds/errata/292-1969.pdf

Document History

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292-1969 - IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
June 20, 1969 - IEEE - Institute of Electrical and Electronics Engineers, Inc.

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 ...

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