DocumentCode
486901
Title
An Optimized Yaw Damper for Enhanced Passenger Ride Comfort
Author
Goslin, T.J. ; Ansari, F.H. ; Chakravarty, A.
Author_Institution
Boeing Commercial Airplane Company
fYear
1987
fDate
10-12 June 1987
Firstpage
395
Lastpage
396
Abstract
The primary purpose of any yaw damper is to suppress the dutch roll response of the airplane in turbulence. Large lateral accelerations at the aft end of the aircraft are especially degrading to ride quality. These lateral accelerations are due to higher frequency structural modes of the aircraft in addition to the low frequency dutch roll mode. Here we will present an optimized yaw damper to enhance passenger ride comfort. Because of the limited scope of this analysis, only the rigid body effects, or dutch roll mode, will be considered.
Keywords
Acceleration; Aircraft; Airplanes; Damping; Degradation; Delay; Feeds; Filters; Frequency; Shock absorbers;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1987
Conference_Location
Minneapolis, MN, USA
Type
conf
Filename
4789350
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