813-1988 IEEE Specification Format Guide and Test Procedure for Two-Degree-Of-Freedom Dynamically Tuned Gyros

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Organization: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 January 1989
Status: active
Page Count: 65
ICS Code (On-board equipment and instruments): 49.090
ISBN (Online): 0-7381-0552-X
DOI: 10.1109/IEEESTD.1989.94579

Abstracts

Standard

This specification defines the requirements for a two-degree-of-freedom dynamically tuned gyro to be used as a sensor in a strapdown, gimballed inertial navigation system (attitude reference units) for use in an aircraft, a missile, a spacecraft or similar applications. The characteristics of the external capture electronics are considered where necessary to define gyro performance.<>

Document History

813-1988 - IEEE Specification Format Guide and Test Procedure for Two-Degree-Of-Freedom Dynamically Tuned Gyros
January 1, 1989 - IEEE - Institute of Electrical and Electronics Engineers, Inc.

This specification defines the requirements for a two-degree-of-freedom dynamically tuned gyro to be used as a sensor in a strapdown, gimballed inertial navigation system (attitude reference units) for use in an aircraft, a missile, a spacecraft or similar applications. The characteristics of the ex...

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