Method for controlling the integrity of an avionics system and control device for implementing said method

摘要

The method involves utilizing data reading and writing units of a controller of an avionics system (1) to generate reference data relating to a component, where the reference data is transmitted to a control computer (3) via Ethernet network (4). The reference data and control signals are displayed on a screen of the control computer for purposes of monitoring and/or comparison by an operator. The reference data and the control signals are recorded in a memory of the control computer. An independent claim is also included for a system for controlling integrity of a component of an avionics system installed in an aircraft.