机译:Enhancing Flight Envelope for a Nonlinear Aeroelastic Wing-Section Using Adaptive Fuzzy Sliding Mode Control Law
Univ Blida 1, Aeronaut Sci Lab, Inst Aeronaut & Space Studies, BP 270 Soumaa Rd, Blida 9068, Algeria;
Flutter control; Aeroservoelasticity; Sliding mode control; Fuzzy logic; Adaptive control;