Adaptive Fuzzy Sliding Mode Controller Design Using a High-Gain Observer for a Nonlinear Aeroelastic System under Unsteady Aerodynamics
Author:
Affiliation:
1. Lecturer A, Aeronautical Sciences Laboratory, Institute of Aeronautics and Space Studies, Univ. of Blida 1, B.P. 270, Route of Soumaa, C.P. 9000, Blida 09015, Algeria.
Publisher
American Society of Civil Engineers (ASCE)
Link
https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5504
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5. High-order sliding mode controller with backstepping design for aeroelastic systems
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