INERTIAL REFERENCE SYSTEM

Standard:
:
  • 1999-03-19
 
  • CURRENT
Publisher:
  • SAE Industry Technologies Consortia
Pages:
88
Scope:

IRS characteristics are defined in this standard. It defines the desired performance of inertial measuring devices and associated electronics specifically designed for installation in commercial transport aircraft. This system provides the basic outputs for aircraft angular rate and acceleration, and computed outputs of altitude, true heading, velocity and present position in a 10 MCU form factor.

History:
Standard Published Revision Status
ARIC704-7 1999-03-19 Latest
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