무인항공기용 고성능 비행제어시스템 개발

FCS(Flight Control System) is to achieve autonomous flight of UAS(Unmanned Aerial System) with various missions. One of the most important factors in designing FCS is how to guarantee the reliability of overall system, ensuring survivability of aircraft as well as mission completeness. In this paper, design requirements, H/W components, and on-board S/W of the FCS　recently developed by ACLS(Aerospace Control & System Lab.) in Inha University are introduced.