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Performance Evaluation on an Active Camera Mount System for UAV via Hardware-in-the-loop-simulation

HILS를 통한 무인항공기 카메라 지지 능동 마운트 시스템의 진동제어 성능 평가

  • 오종석 (인하대학교 대학원 기계공학과) ;
  • 최승복 (인하대학교 기계공학부) ;
  • 조한준 (인하대학교 대학원 기계공학과) ;
  • 이철희 (인하대학교 기계공학부) ;
  • 조명우 (인하대학교 기계공학부)
  • Received : 2010.06.10
  • Accepted : 2010.07.28
  • Published : 2010.08.20

Abstract

In the present work, vibration control performance of piezoactuator-based active mount system for unmanned aero vehicle(UAV) equipment is evaluated via hardware in the loop simulation(HILS). At first, the vibration level of UAV is measured and from this vibration data, the proper piezostack actuator is selected. Then, the dynamic model of active mount system including four active mounts and UAV camera equipment is derived. In order to evaluate vibration control performance, the HILS system is constructed. The proposed mount is prepared as hardware part and the other mounts are considered in software part. A sliding mode controller is designed and implemented to the HILS system. Effective vibration control results are presented in both time and frequency domains.

Keywords

References

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Cited by

  1. Active Vibration Control Experiment on Automobile Using Active Vibration Absorber vol.21, pp.8, 2011, https://doi.org/10.5050/KSNVE.2011.21.8.741