Aircraft frequency adaptive modal suppression system
AssigneeThe Boeing Company
InventorsChuong B. Tran, Stephen White
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Abstract
An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.
Claims1
An aircraft having a frequency adaptive modal suppression system including a yaw damper control path, said yaw damper control path including a variable yaw damper notch filter for compensating for weight change of the aircraft, said variable yaw damper notch filter having a frequency range determined by sweeping the rudder of the aircraft at the aircraft's heaviest and lightest gross weights.
Dependencies are inferred from the claim text.