Avionics function testing method for aircraft, involves simulating behavior of real element of aircraft, where real element is applied by function, activating another real element that is applied by function, and testing function

摘要

The method involves performing personalization of an aircraft (400), where the personalization allows simulation of behavior of a real element of the aircraft. The behavior of the real element of the aircraft is simulated (405), where the real element is applied by a function i.e. hydraulic function. Another real element of the aircraft is activated (410), where the latter real element is applied by the function. The function is tested (415). A step of disconnection of the former real element is performed by another function e.g. electric or electronic function.