Please use this identifier to cite or link to this item:
Title: Piloted Sliding Mode FTC Simulator Evaluation for the ELAL Flight 1862 Incident
Authors: Alwi, Halim
Edwards, Christopher
Stroosma, Olaf
Mulder, J. A.
First Published: Aug-2008
Publisher: American Institute of Aeronautics and Astronautics (AIAA)
Citation: Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Honolulu, Hawaii, Aug. 18-21, 2008, 18 pp.
Abstract: This paper considers a model reference based sliding mode control allocation scheme for fault tolerant control. The scheme uses equal distribution of the control signals to all actuators even when a fault or failure occurs, and assumes no FDI is available. The paper analyzes the scheme and determines conditions under which closed-loop stability is retained for a certain class of faults and failures. It is shown that faults and even certain total actuator failures can be handled directly without reconfiguring the controller. The results obtained from implementing the controller on the SIMONA research flight simulator, configured to represent a large transport aircraft under the ELAL flight 1862 scenario, shows good performance in both nominal and failure scenarios.
ISBN: 1563479451
Type: Conference paper
Rights: Copyright © 2008 by the American Institute of Aeronautics and Astronautics, Inc.
Description: Metadata only entry
Appears in Collections:Conference Papers & Presentations, Dept. of Engineering

Files in This Item:
There are no files associated with this item.

Items in LRA are protected by copyright, with all rights reserved, unless otherwise indicated.