Vibration control of adaptive aircraft wings modeled as tapered thin-walled beams

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 4326, Issue , 2001, Pages 319-330

  Librescu, L ^a   Na, S ^a  

^a State University   (United States)

Author keywords

Bang bang control; Boundary moment control; Closed loop eigenfrequency dynamic response; Dynamic response control; Piezoactuator; Tapered beam; Thin walled beam

Indexed keywords

CANTILEVER BEAMS; COMPUTER SIMULATION; DYNAMIC RESPONSE; PIEZOELECTRIC DEVICES; PIEZOELECTRICITY; STRAIN MEASUREMENT; VIBRATION CONTROL; WINGS;

PIEZOACTUATORS;

THIN WALLED STRUCTURES;

EID: 0034767854     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.436486     Document Type: Conference Paper

References (18)

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