Study immunity to disturbance of electronic system aircraft by influences of intentional ultrashort electromagnetic pulses

摘要

An approach based on the electromagnetic topology method for predicting immunity to disturbance of electronic system aircraft at the influence of intentional ultrashort electromagnetic impulses is discussed. Aircraft for small aircraft a fuselage and tail, which are made of composite material, are considered. An example prediction of immunity to disturbance of electronic aircraft control system and recommendations to ensure immunity to disturbance at the influence of intentional ultrashort electromagnetic pulses is discusses.