Force control of semi‐active valve lag dampers for vibration reduction in helicopters

Author:

Morales Rafael Mauricio1,Turner Matthew C.1,Court Peter2,Hilditch Ross3,Postlethwaite Ian4

Affiliation:

1. Control and Instrumentation Research Group, Department of EngineeringUniversity of LeicesterUniversity RoadLeicesterLE1 7RHUK

2. AgustaWestland (a Finmeccanica company), Engineering, Westland WorksLysander RoadYeovilBA20 2YBUK

3. MBDAFiltonBristolBS34 7QQUK

4. University of NorthumbriaUK

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Reference32 articles.

1. Semi‐active damping of ground resonance in helicopters using magnetorheological dampers;Zhao Y.;J. Am. Helicopter Soc.,2004

2. PandaB.MychalowyczE.KothmanB. andBlackwellR.: ‘Active controller for comanche air resonance stability augmentation’.Proc. 55th American Helicopter Society Annual Forum 1999

3. Load reduction in lead‐lag dampers by speed‐scheduled aperture and modulated control of a bypass valve;Bottasso C.L.;J. Am. Helicopter Soc.,2012

4. Control evaluations of semi‐active fluid‐elastomeric helicopter lag damper;Kothare C.S.;AIAA J. Guid. Control Dyn.,2004

5. Magnetorheological fluid damper feedback linearization control for helicopter rotor application;Gandhi F.;Smart Mater. Struct.,2001

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