Abstract
An innovative three-dimensional model of flexible wing is built, which is counted as a distributed parameter system. For the parameter uncertainty and unknown actuator fault of this system, an adaptive fault-tolerant control method combined with boundary control is designed to maintain stability. By using the Lyapunov-based method, the uniform boundedness is theoretically proved in this closed-loop system. The efficacy and feasibility of the strategy can be demonstrated by numerical simulation.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
