Active flutter suppression using MIMO adaptive LMS control

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 237-247

  Eversman, Walter ^a   Danda Roy, Indranil ^a  

^a Architectural and Environmental Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ADAPTIVE SYSTEMS; AERODYNAMICS; CONTROLLERS; DEGREES OF FREEDOM (MECHANICS); FEEDFORWARD CONTROL; FLUTTER (AERODYNAMICS); RIGID WINGS; STRUCTURAL DYNAMICS; TIME VARYING CONTROL SYSTEMS; ULTRASONIC DEVICES; AIRFOILS; ALGORITHMS; COMPUTER SIMULATION; FINITE ELEMENT METHOD; IDENTIFICATION (CONTROL SYSTEMS); LEAST SQUARES APPROXIMATIONS; MATHEMATICAL MODELS; SYSTEM STABILITY; WINGS;

ACTIVE FLUTTER SUPPRESSION; FILTERED X LEAST MEAN SQUARES; FINITE-ELEMENT REPRESENTATION; MULTI-INPUT MULTI-OUTPUT; QUASI-STEADY AERODYNAMICS; SINGLE INPUT SINGLE OUTPUT; THREE DEGREE OF FREEDOMS; TRACKING TIME-VARYING PARAMETERS;

FLEXIBLE WINGS; ADAPTIVE CONTROL SYSTEMS;

ACTIVE FLUTTER SUPPRESSION; FEEDFORWARD CONTROLLER; FLEXIBLE WINGS; LEAST MEAN SQUARE; MULTI INPUT MULTI OUTPUT CONTROL; SINGLE INPUT SINGLE OUTPUT CONTROL; TIME DOMAIN UNSTEADY AERODYNAMICS; TWO DIMENSIONAL QUASI STEADY AERODYNAMICS;

EID: 0029719108     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1345     Document Type: Conference Paper

References (13)

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