DocumentCode
3412526
Title
Design combination in integrated flight control
Author
Liu, Hugh H T
Author_Institution
Inst. for Aerosp. Studies, Toronto, Ont., Canada
Volume
1
fYear
2001
fDate
2001
Firstpage
494
Abstract
Control integration makes engineering and business sense, to reduce cost and design cycling time, and to improve performance. We select two specific autopilot control channels, namely the pitch attitude and speed control, to investigate the special design challenges that one may face during system integration. Two integration approaches are proposed, and compared through an example of Boeing 747 transport. The simulation results justify the theoretical analysis
Keywords
aircraft control; attitude control; closed loop systems; control system synthesis; transfer functions; velocity control; Boeing 747 transport; autopilot control channels; control integration; design challenges; integrated flight control; pitch attitude control; speed control; Aerospace control; Aerospace engineering; Attitude control; Automatic control; Control design; Control systems; Design engineering; Elevators; Transfer functions; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.945593
Filename
945593
Link To Document