Active vibration control of rotorcraft driveshaft-airframe dynamics

Annual Forum Proceedings - American Helicopter Society

Volumn 1, Issue , 1998, Pages 472-488

  DeSmidt, Hans A ^a   Wang, K W ^a   Smith, E C ^a  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; AIRFRAMES; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; FREQUENCY AGILITY; FUSELAGES; OPTIMAL CONTROL SYSTEMS; VEHICLE TRANSMISSIONS; VIBRATION CONTROL;

COUPLED FUSELAGE TAILROTOR DRIVETRAIN STRUCTURES; FLEXIBLE COUPLING MISALIGNMENTS; MULTI FREQUENCY AERODYNAMIC LOADING;

HELICOPTERS;

EID: 0031677992     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)