Please use this identifier to cite or link to this item:
|Title:||Fault Tolerant Sliding Mode Control Design with Piloted Simulator Evaluation|
|Publisher:||American Institute of Aeronautics and Astronautics (AIAA)|
|Citation:||Journal of Guidance, Control, and Dynamics, 2008, 31 (5), pp. 1186-1201.|
|Abstract:||This paper considers sliding mode allocation schemes for fault tolerant control. The schemes allow redistribution of the control signals to the remaining functioning actuators when a fault or failure occurs. The paper analyzes the schemes 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 controllers on a research flight simulator, configured to represent a B747 aircraft, show good performance in both nominal and failure scenarios, even in wind and gust conditions.|
|Rights:||Copyright © 2008 by the American Institute of Aeronautics and Astronautics, Inc.|
|Description:||Metadata only entry|
|Appears in Collections:||Published Articles, 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.