Hybrid fuzzy sliding-mode control of an aeroelastic system

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 4, 2002, Pages 829-832

  Lin, Chih Min ^a   Hsu, Chun Fei ^a  

^a YUAN ZE UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; COMPUTER SIMULATION; FUZZY CONTROL; INFERENCE ENGINES; NONLINEAR CONTROL SYSTEMS; OSCILLATIONS;

LIMIT-CYCLE OSCILLATIONS (LCO);

SLIDING MODE CONTROL;

EID: 0036642265     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4955     Document Type: Article

References (8)

1. Experimental and analytical investigation of transonic limit-cycle oscillations of a flaperon
2. Identification and control of limit cycle oscillations in aeroelastic systems
3. Transonic flutter suppression control law design and wind-tunnel test results
4. Active control of flutter in compressible flow and its aeroelastic scaling
5. Adaptive output feedback control of an aeroelastic system with unstructured uncertainties
6. Fuzzy logic in control systems: Fuzzy logic controller-part I/II
7. Design of a single-input fuzzy logic controller and its properties
8. Guidance law design by adaptive fuzzy sliding-mode control