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LMI-Based Fuzzy Optimal Variance Control of Airfoil Model Subject to Input Constraints
- Publication Year :
- 2017
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 2017.
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Abstract
- This paper presents a study of fuzzy optimal variance control problem for dynamical systems subject to actuator amplitude and rate constraints. Using Takagi-Sugeno fuzzy modeling and dynamic Parallel Distributed Compensation technique, the stability and the constraints can be cast as a multi-objective optimization problem in the form of Linear Matrix Inequalities. By utilizing the formulations and solutions for the input and output variance constraint problems, we develop a fuzzy full-state feedback controller. The stability and performance of the proposed controller is demonstrated through its application to the airfoil flutter suppression.
- Subjects :
- Theoretical Mathematics
Aircraft Stability And Control
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.20170006472
- Document Type :
- Report