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압전작동기를 이용한 무인항공기 EO/IR 센서 마운트의 능동 진동 제어

Active Vibration Control of UAV EO/IR Sensor Mount Using Piezoelectric Actuator

  • 박동현 (인하대학교 대학원 기계공학과) ;
  • 최승복 (인하대학교 기계공학부)
  • 발행 : 2008.12.20

초록

This paper presents an inertia type of piezostack based active mount fur unmanned aero vehicle (UAV) camera system. After identifying the stiffness and damping properties of the rubber element and piezostack a mechanical model of the active mount system is established. The governing equation of mount is then derived and expressed in a state space form. Subsequently, a sliding mode controller which is robust to uncertain parameters is designed in order to reduce the vibration imposed according to the military specification associated with UAV camera mount system operation. Control performances such as acceleration and transmitted force are evaluated through both computer simulation and experimental implementation.

키워드

참고문헌

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