Delta Wing Flutter Control Using Spatially Optimized Transducers

Journal of Intelligent Material Systems and Structures

Volumn 14, Issue 11, 2003, Pages 677-691

  Richard, Robert E ^a   Clark, Robert L ^b  

^a BOEING COMPANY   (United States)

^b DUKE UNIVERSITY   (United States)

Author keywords

Control; Delta wing; Flutter; Genetic optimization; Spatial optimization

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; APPROXIMATION THEORY; CONTROL SYSTEM ANALYSIS; DELTA WING AIRCRAFT; GENETIC ALGORITHMS; MATHEMATICAL MODELS; OSCILLATIONS; SENSORS; TRANSDUCERS;

LIMIT CYCLE OSCILLATIONS (LCO); SPATIAL COUPLING;

FLUTTER (AERODYNAMICS);

EID: 0345306787     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1177/1045389X03038584     Document Type: Article

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