Full Description

Scope

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, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance.

Abstract

Corrigendum Standard - Active.Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.

Product Details

Published: 10/26/2017 ISBN(s): 9781504444804 Number of Pages: 12File Size: 1 file , 760 KB Product Code(s): STD22874