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

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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.<>