ARINC561-11: 561-11 Air Transport Inertial Navigation System (INS) - Characteristic

Issuing Committee: Airlines Electronic Engineering Committee

Scope

Content: This standard defines the requirements of an INS, which provides sensor and steering command outputs. The INS includes inertial sensing and provides outputs for aircraft attitude, present position, and steering signals suitable for operating the pilot's instruments. The basic INS provides complete self-contained horizontal navigation capability intended to serve as the sole means of navigation on a worldwide basis.

Meta Tags

Topics: Avionics

Details

Additional Details

Publisher: SAE Industry Technologies Consortia IA

Published: Jan 1, 1975

Product Code: ARINC561-11

Content Type: Characteristic

Status: Current

Language: English

ARINC561-11