Study of the intentional influence ultrashort electromagnetic pulses on electronic equipment aircraft

An approach based on the electromagnetic topology method for predicting immunity to disturbance of aircraft electronic equipment 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 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 intentional ultrashort electromagnetic pulses is discusses.