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http://dx.doi.org/10.5302/J.ICROS.2005.11.3.193

Development of Simulation Program for Tilt Rotor Aircraft  

Yoo, Chang-Sun (한국항공우주연구원 스마트무인기술개발)
Choi, Hyung-Sik (한국항공우주연구원 항행체계그룹)
Park, Bum-Jin (충남대학교 항공우주공학과)
Ahn, Sung-Jun (한국항공우주연구원 스마트무인기술개발)
Kang, Young-Shin (한국항공우주연구원 스마트무인기술개발)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.11, no.3, 2005 , pp. 193-199 More about this Journal
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.
Keywords
unmanned aerial vehicle; tilt rotor; rotor drive; aircraft modelling; nonlinear simulation;
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