GIURGIUTIU V.Review of smart-materials actuation solutions for aeroelastic and vibration control[J].Journal of Intelligent Material Systems and Structures 2000,11:525?44.
[2]
ROTH D,ENENKL B,DIETERICH O.Active rotor control by flaps for vibration reduction―full scale demonstrator and first flight test results[C]//32nd European Rotorcraft Forum.Moscow:Russian Helicopter,JSC,2006:801-814.
[3]
BARRETT R,GROSS R S,BROZOSKI F.Missile flight control using active flexspar actuators[J].Smart Materials and Structures,1996,5(2):121.
[4]
BARRETT R,VOS R.Design,development and testing of a transonic missile fin employing PBP/DEAS actuators[C]//The 15th International Symposium on:Smart Structures and Materials & Nondestructive Evaluation and Health Monitoring.California,USA:International Society for Optics and Photonics,2008:693011-693011-11.
[5]
ROGET B,CHOPRA I.Wind-tunnel testing of rotor with individually controlled trailing-edge flaps for vibration reduction[J].Journal of Aircraft,2008,45(3):868-879.
[6]
STRAUB F K,KENNEDY D K,DOMZALSKI D B,et al.Smart material-actuated rotor technology?SMART[J].Journal of Intelligent Material Systems and Structures,2004,15(4):249-260.
[7]
DIETERICH O,ENENKL B,ROTH D.Trailing edge flaps for active rotor control-aeroelastic characteristics of the ADASYS rotor system[C]//Annual Forum Proceedings-American Helicopter Society.Phoenix,USA:American Helicopter Society,INC,2006,62(2):965.
[8]
J(¨overA)NKER P,HERMLE F,FRIEDL S,et al.Advanced piezoelectric servo flap system for rotor active control[C]//32nd European Rotorcraft Forum.Moscow:Russian Helicopter,JSC,2006:237-247.
[9]
GLAZ B,FRIEDMANN P P,LIU L.Vibration reduction and performance enhancement of helicopter rotors using an active/passive approach[C]//Proceedings of the 49th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.Schaumburg,IL,USA:AIAA,2008:338-350.