DocumentCode
3091869
Title
Aircraft fore and aft model suppression system
Author
Tran, C.B. ; Goslin, T. ; Ho, J.K. ; Chakravarty, A.
Author_Institution
Boeing Commercial Airplane Company, Seattle, Washington
Volume
26
fYear
1987
fDate
9-11 Dec. 1987
Firstpage
2337
Lastpage
2340
Abstract
This paper will address the design procedure of a modal suppression system that can control fore and aft body oscillation of an aircraft in the presence of turbulence. Power spectral density (PSD) plots will be shown comparing the performance of the airplane with the modal suppression system on and off. Substantial benefits are derived in terms of ride quality improvement when this modal suppression system is used in place of a conventional yaw damper.
Keywords
Acceleration; Actuators; Aerospace control; Aircraft; Airplanes; Control systems; Damping; Power system modeling; Servomechanisms; Shock absorbers;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1987. 26th IEEE Conference on
Conference_Location
Los Angeles, California, USA
Type
conf
DOI
10.1109/CDC.1987.272960
Filename
4049725
Link To Document