ACSR System for vibration suppression in coupled helicopter rotor/flexible fuselage model

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

Volumn , Issue , 1996, Pages 1972-1990

  Chiu, Thiem ^a   Friedmann, Peretz P ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; FUSELAGES; HELICOPTER ROTORS; MICROACTUATORS; STRUCTURAL DYNAMICS; VIBRATIONS (MECHANICAL); ACCELERATION; AERODYNAMICS; COMPUTER SIMULATION; EIGENVALUES AND EIGENFUNCTIONS; FORCE CONTROL; MATRIX ALGEBRA;

ACTIVE CONTROL; AEROELASTIC RESPONSE; HELICOPTER FUSELAGE; NON-ROTATING SYSTEM; STRUCTURAL RESPONSE; VIBRATION LEVEL; VIBRATION REDUCTIONS; VIBRATION SUPPRESSION;

VIBRATION ANALYSIS; VIBRATION CONTROL;

ACTIVE CONTROL OF STRUCTURAL RESPONSE; AEROELASTIC RESPONSE MODEL; COUPLED HELICOPTER ROTOR FLEXIBLE FUSELAGE MODEL; VIBRATION SUPPRESSION;

EID: 0029722589     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1547     Document Type: Conference Paper

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