Adaptive Fault-Tolerant Control of a Hybrid Canard Rotor/Wing UAV Under Transition Flight Subject to Actuator Faults and Model Uncertainties
Author:
Affiliation:
1. School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
2. Department of Mechanical, Industrial and Aerospace Engineering, Concordia University, Montreal, QC, Canada
Funder
National Natural Science Foundation of China
Industry-University-Research Innovation Foundation for the Chinese Ministry of Education
Fundamental Research Funds for the Central Universities
Natural Sciences and Engineering Research Council of Canada
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/10213347/10041814.pdf?arnumber=10041814
Reference52 articles.
1. Canard Rotor/Wing: A Revolutionary High-speed Rotorcraft Concept
2. Flight dynamics characteristics of canard rotor/wing aircraft in helicopter flight mode
3. The Canard Rotor Wing (CRW) Aircraft - A New Way to Fly
4. Low-speed wind tunnel test results of the Canard Rotor/Wing concept
5. Dynamic Control Allocation Using Constrained Quadratic Programming
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