Purpose of This Document
This document sets forth the basic features for a 4 MCU InertialReference System (IRS), consisting of the necessary inertialmeasuring devices and associated electronics specifically designedfor installation in commercial transport-type aircraft, that may beused in place of an in-service 10 MCU ARINC 704 Inertial ReferenceSystem.
The intent of this document is to provide general and specificdesign guidance for the development of an IRS for airline use. Itdescribes the desired operational capability of the system and thestandards necessary to ensure interchangeability.
- Edition:
- 99
- Published:
- 03/26/1999
- Number of Pages:
- 61
- File Size:
- 1 file , 450 KB
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