• 한국산학기술학회논문지
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• 제9권3호
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• pp.632-637
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• 2008

군용 항공기 탑재 무장제어장치는 무장관리시스템의 핵심장비로 조종사의 무장선택, 항공기 상태 및 외부 장착물 장착 상태 등에 따라 선택투하, 비상 투하 및 로켓발사 신호를 생성하여 외부 장착물을 제어한다. 본 논문은 순차 제어회로 설계기법을 이용하여 개발된 무장제어장치의 설계과정 및 성능검증에 대해 기술한다.

• 한국군사과학기술학회지
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• 제10권4호
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• pp.81-87
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• 2007

In this study, analysis of structural design criteria for the canopy actuating device has been conducted considering the aerodynamic breakaway capabilities of jettisonable canopy system. Unsteady aerodynamic loads for the opened canopy configuration at passively controlled jettision mode were computed using CFD method. The general purpose multi-body finite element code, SAMCEF Mecano, is used in the implemented analyses for the passive jettision condition. The recommended altitude and speed of aircraft was suggested as design criteria of aerodynamic breakaway capability of jettisonable canopy system as a bakup egress method when normal canopy jettison sequence malfunctioned. Aerodynamic breakaway condition of jettisonable canopy was also simulated and the fracture load conditions of canopy actuator were investigated.