A distributed actuator approach for active control of helicopter airframe vibrations
40th Structures, Structural Dynamics, and Materials Conference and Exhibit ; 1999 ; St. Louis , MO , U.S.A.
01.01.1999
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A Distributed Actuator Approach for Active Control of Helicopter Airframe Vibrations
British Library Conference Proceedings | 1999
|An Optimal Actuator Placement Methodology for Active Control of Helicopter Airframe Vibrations
Online Contents | 2001
|OPTIMAL ACTUATOR PLACEMENT AND ACTIVE STRUCTURE DESIGN FOR CONTROL OF HELICOPTER AIRFRAME VIBRATIONS
British Library Conference Proceedings | 2002
|