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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.