Method of controlling the integrity of a system according to the avionics and control device for implementing said method

摘要

The present invention relates to a method for monitoring the integrity of an avionics system (1) installed in an aircraft, said method consisting of checking the integrity in terms of electrical installation and acquisition and transmission of data, characterized in that it consists of: - use an ethernet network (4) connecting the avionics system (1) to a control computer (3), - generate with the aid of the computer (3) of the first control signals transmitted to the component and / or acquire the second control signals coming from the component, - the use of means for reading and writing of data of a computer of the avionics system (1) for generating the reference data relating to the component and transmitted to the control computer (3) via the ethernet network (4), - display the reference data and the control signals and to record in the case, the reference data and the control signals.