Two Reconfigurable Control Allocation Schemes for Unmanned Aerial Vehicle under Stuck Actuator Failures

Author:

Zhou Qing-Li1,Zhang Youmin1,Rabbath Camille-Alain2,Apkarian Jacob3

Affiliation:

1. Concordia University

2. Defence Research and Development Canada

3. Quanser, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. 1Earon, E. "Almost-Light-Than-Air-Vehicle Fleet Simulation," Technical Report, V.2.1,Quanser Inc., Toronto,Canada, 2005.

2. Bibliographical review on reconfigurable fault-tolerant control systems

3. Evaluation of Optimization Methods for Control Allocation

4. 4Bordignon, K. A. "Constrained Control Allocation for System with Redundant Control Effectors," Ph.D. Thesis,Virginia Polytechnic Institute and Sate University, 1996.

5. Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation

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