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ARINC 704A

Inertial Reference System

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Organization: ARINC
Publication Date: 26 March 1999
Status: active
Page Count: 61
scope:

Purpose of This Document

This document sets forth the basic features for a 4 MCU Inertial Reference System (IRS), consisting of the necessary inertial measuring devices and associated electronics specifically designed for installation in commercial transport-type aircraft, that may be used in place of an in-service 10 MCU ARINC 704 Inertial Reference System.

The intent of this document is to provide general and specific design guidance for the development of an IRS for airline use. It describes the desired operational capability of the system and the standards necessary to ensure interchangeability.

Document History

ARINC 704A
March 26, 1999
Inertial Reference System
Purpose of This Document This document sets forth the basic features for a 4 MCU Inertial Reference System (IRS), consisting of the necessary inertial measuring devices and associated electronics...

References

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