Multi-input/multi-output adaptive active flutter suppression for a wing model

Journal of Aircraft

Volumn 35, Issue 3, 1998, Pages 462-469

  Andrighettoni, M ^a,b   Mantegazza, P ^a,b  

^a POLITECNICO DI MILANO   (Italy)

^b Dipto di Ingegneria Aerospaziale   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DISCRETE TIME CONTROL SYSTEMS; EIGENVALUES AND EIGENFUNCTIONS; IDENTIFICATION (CONTROL SYSTEMS); LEAST SQUARES APPROXIMATIONS; MATHEMATICAL MODELS; RECURSIVE FUNCTIONS; SYSTEM STABILITY; WINGS;

ADAPTIVE ACTIVE FLUTTER SUPPRESSION SYSTEM;

FLUTTER (AERODYNAMICS);

EID: 0032072394     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2319     Document Type: Article

References (10)

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