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유창선,최형식,박범진,안성준,강영신,Yoo, Chang-Sun,Choi, Hyung-Sik,Park, Bum-Jin,Ahn, Sung-Jun,Kang, Young-Shin 제어로봇시스템학회 2005 제어·로봇·시스템학회 논문지 Vol.11 No.3
VTOL(Vertical Take-Off and Landing) aircraft is attractive due to the reason that it is not necessary to have long runway. However a rotorcraft has a definite limitation to fly at the high speed due to the stall at the tip of rotor. To solve this problem, tilt rotor, tilt wing and lift fan were researched and developed. It was verified that the tilt rotor aircraft among them was more effective in disk loading. On this basis, the tilt rotor aircraft has been made into XV-15, V-22, BA-609 and Eagle Eye. This paper shows a nonlinear simulation program for general tilt rotor aircraft that was developed in order to validate the flight characteristics of tilt rotor aircraft and verified through the simulation analysis.