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
Link To Document :
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