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529-1980  -  Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-Of-Freedom Rate-Integrating Gyros

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This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an inertial navigation system for an attitude reference unit in an aircraft or missile application. The characteristics of the external capture electronics are considered where necessary to define gyro performance.<>

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