Fly-by wire-controlled aircraft with a flexible and vibratable body

A gyrometer (7) is arranged at the vibration node of a fuselage (2). Each accelerometer (5,6) is arranged at the vibration antinode of the fuselage. The gyrometer and accelerometers are connected to a flight control computer (12) such that measurement signals from the gyrometer and accelerometers are used as flight control parameters.