Aircraft Control System Immunity Study at the Direct Lightning Strike

Abstract

In this paper, an approach for predicting the noise immunity of electronic systems of an aircraft during at the direct lightning strike is proposed. Aircraft for small aviation a fuselage and tail, which are made of composite material, are considered. An example prediction of electromagnetic interference in coupling path of interface and coupling path of mains is discusses. Results prediction of immunity to disturbance of electronic control system and recommendations to ensure immunity to disturbance at the influence of direct lightning strike is discusses.