구동장치 연동된 조종날개 혼합동강성 실험 및 특성보정

Experiments of Mixed Dynamic Stiffness of a Control Fin and Actuator and Correction of Experiment Results

  • 발행 : 2004.12.01

초록

In order to model a connection part between a control fin and actuator, the related characteristics of a dynamic stiffness were extracted from experiments. These characteristics include the static stiffness of a control fin and the dynamic stiffness of an actuator, so they are called the mixed dynamic stiffness here. This mixed dynamic stiffness is used as the boundary condition of a control fin connected to an actuator when the flutter characteristics are analyzed. The simulated stiffness of an actuator is corrected from the experiment results and the mixed dynamic is finally formulated in the domain of frequencies.

키워드

참고문헌

  1. 신영석 외 3명, '휴대용 대공유도탄의 전기체 및 구동장치 연동 플러터 특성연구', 제 10회 지상무 기체계 발전세미나, 2002, 10
  2. Stephen. C. Cayson, Roger P. Berry, 'Analysis of The Flutter Characteristics of the Advanced Kinematic Energy Missile Control Surface', Technical Report RD-GC-90-10, 1990, August
  3. 신영석 외 2명, 'M0206 조종날개 구동장치 통강성 연동 플러터 특성 연구', ADD보고서, 2003. 12