Output feedback modular adaptive control of a nonlinear prototypical wing section

Nonlinear Dynamics

Volumn 37, Issue 4, 2004, Pages 357-373

  Bhoir, Nilesh ^a,b   Singh, Sahjendra N ^a  

^a UNIVERSITY OF NEVADA   (United States)

^b LTAS International   (United States)

Author keywords

Adaptive control; Limit cycle oscillation control; Nonlinear aeroelastic system

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; BENCHMARKING; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; MATHEMATICAL MODELS; OSCILLATIONS; PARAMETER ESTIMATION; WINGS;

ADAPTIVE CONTROL; FLAP DEFLECTION; LIMIT CYCLE OSCILLATION CONTROL; NONLINEAR AEROELASTIC SYSTEM;

AERODYNAMICS;

EID: 7544250802     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1023/B:NODY.0000045548.18838.72     Document Type: Article

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