초록 ▼

Method for compensating structural vibrations of an aircraft caused by wind blasts and buffeting in an aircraft in flight includes the steps of: detecting the structural vibrations by measurement technology using roll rates determined in an inertial sensing system, supplying the determined disturbin

Method for compensating structural vibrations of an aircraft caused by wind blasts and buffeting in an aircraft in flight includes the steps of: detecting the structural vibrations by measurement technology using roll rates determined in an inertial sensing system, supplying the determined disturbing values to a flight control system, producing phase- and amplitude-correct control flap movements by generating appropriate control signals in respective control drives to counteract the phases and amplitudes of the excited vibrations.

대표청구항 ▼

1. A method for compensating structural vibrations of an aircraft caused by external disturbances acting on the aircraft in flight, the method comprising the acts of:detecting the structural vibrations via measurement technology using roll rates determined essentially by an inertial sensing system o

1. A method for compensating structural vibrations of an aircraft caused by external disturbances acting on the aircraft in flight, the method comprising the acts of:detecting the structural vibrations via measurement technology using roll rates determined essentially by an inertial sensing system of the aircraft without requiring additional sensors; feeding disturbing parameters of the detected structural vibrations to a flight control system of the aircraft; and producing phase- and amplitude-correct control flap movements of the aircraft by generating appropriate control signals at respective drives to counteract phases and amplitudes of excited structural vibrations.