Journal of Institute of Control, Robotics and Systems (제어로봇시스템학회논문지)

Institute of Control, Robotics and Systems (제어로봇시스템학회)
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Development of Simulation Program for Tilt Rotor Aircraft

틸트로터 항공기 비선형 시뮬레이션 프로그램 개발

  • 유창선 (한국항공우주연구원 스마트무인기술개발) ;
  • 최형식 (한국항공우주연구원 항행체계그룹) ;
  • 박범진 (충남대학교 항공우주공학과) ;
  • 안성준 (한국항공우주연구원 스마트무인기술개발) ;
  • 강영신 (한국항공우주연구원 스마트무인기술개발)
  • Published : 2005.03.01
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Abstract

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.

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References

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