Integrated Adaptive Fault-Tolerant H Infinity Output Feedback Control with Adaptive Fault Identification
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
2. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.55199
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5. Robust and reliable H∞ control for linear systems with parameter uncertainty and actuator failure
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