지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
이용수
초록· 키워드
오류제보하기
It is recognized that the control surface fault is detected by monitoring the value of the coefficients due to the control surface deviation. It is found out the control surface stuck position by comparing the trim value with the reference value. To detect and isolate the fault, two mixed methods apply to the real-time parameter estimation and similarity measure. If the scatter of aerodynamic coefficients for the fault and normal are closing nearly, fault decision is difficult. Applying similarity measure to decide for fault or not, it makes a clear and easy distinction between fault and normal. Low power processor is applied to the real-time parameter estimator and computation of similarity measure.
목차
등록된 정보가 없습니다.
참고문헌 (22)
참고문헌 신청
김유단 / 2005 / 고장진단 및 다중화 기술개발
Napolitano, M. R. / 2001 / Online Parameter Estimation for Restructurable Flight Control Systems / Aircraft Design 4:19~50
Wook-Je Park / 2007 / A Study on the Real-Time Parameter Estimation of DURUMI-II for Control Surface Fault Using Flight Test Data (Longitudinal Motion) / International Journal of Control, Automation, and Systems 5(4):410~418
Wook-Je Park / 2006 / A Study on the Parameter Estimation of DURUMI-II for the Fixed Right Elevator Using Flight Test Data / Journal of Mechanical Science and Technology 20(8):1224~1231
M.S. Hwang / 2002 / Lateral Stability Improvement of a Canard Airplane Using a Vertical Panel / AIAA Atmospheric Flight Mechanics Conference and Exhibit, AIAA-2002-4625
Napolitano, M. R. / 2001 / Online Parameter Estimation for Restructurable Flight Control Systems / Aircraft Design 4:19~50
Wook-Je Park / 2007 / A Study on the Real-Time Parameter Estimation of DURUMI-II for Control Surface Fault Using Flight Test Data (Longitudinal Motion) / International Journal of Control, Automation, and Systems 5(4):410~418
Wook-Je Park / 2006 / A Study on the Parameter Estimation of DURUMI-II for the Fixed Right Elevator Using Flight Test Data / Journal of Mechanical Science and Technology 20(8):1224~1231
M.S. Hwang / 2002 / Lateral Stability Improvement of a Canard Airplane Using a Vertical Panel / AIAA Atmospheric Flight Mechanics Conference and Exhibit, AIAA-2002-4625
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