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최승기,문정호,고준수,Choi, Seung Kie,Moon, Jung Ho,Ko, Joon Soo 한국군사과학기술학회 2014 한국군사과학기술학회지 Vol.17 No.4
This paper presents the case study of the airworthiness certification for the flight control system of tactical UAV. Airworthiness regulations for flight characteristics and design and construction based on the STANAG 4671 are selected, and safety assessment is performed. Stall protection on wing level and turning flight criteria, and flap interconnection system failures were analyzed and applied to the flight control system design. The Hardware-in-the-loop simulation including math model, integrated system verification and validation test and failure mode and effects test were also performed and they are used to validate the means of compliance of the proposed airworthiness.
신성식(Shin Sung Sik),최승기(Choi Seung kie),국태승(Kuk Tae Sueng),문정호(Moon Jung Ho),조신제(Cho Shin Je),오정균(Oh Jung Kyun),황돈영(Hwang Don Young) 대한기계학회 2006 대한기계학회 춘추학술대회 Vol.2006 No.11
This paper presents the development of flight control system of the close range surveillance UAV. The developed flight control system is composed of hardware and software including flight control and guidance algorithm. It includes the essential functions of UAV such as autopilot, point navigation and preprogram mode. The results of flight and PILS test show that the flight control system possesses the performance suitable for the purpose of close range surveillance.