Browse Standards ARINC704-7
Current 1999-03-19

INERTIAL REFERENCE SYSTEM ARINC704-7

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.

ARINC704-7
1999-03-19
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