DocumentCode
2382526
Title
Reconfigurable control allocation applied to an aircraft benchmark model
Author
Zhang, Youmin ; Rabbath, Camille A. ; Su, Chun-Yi
Author_Institution
Dept. of Mech. & Ind. Eng., Concordia Univ., Montreal, QC
fYear
2008
fDate
11-13 June 2008
Firstpage
1052
Lastpage
1057
Abstract
In this paper, a study of reconfigurable control allocation applied to a realistic and nonlinear aircraft model is presented. A pseudo-inverse based method for reconfigurable control allocation has been investigated in an ADMIRE (aero-data model in research environment) aircraft benchmark model. Partial loss of control effectiveness type faults have been implemented. Simulation results show satisfactory performance for accommodating the partial loss of control effectiveness in control effectors.
Keywords
aircraft control; nonlinear control systems; control effector; nonlinear aircraft model; pseudoinverse based method; reconfigurable control allocation; Actuators; Aerospace control; Aircraft propulsion; Control systems; Elevators; Fault tolerant systems; Industrial engineering; Mathematical model; Performance loss; Research and development;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2008
Conference_Location
Seattle, WA
ISSN
0743-1619
Print_ISBN
978-1-4244-2078-0
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2008.4586631
Filename
4586631
Link To Document