틸트로터 항공기 비선형 시뮬레이션 프로그램 개발 = Development of Simulation Program for Tilt Rotor Aircraft

다국어 초록 (Multilingual 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.

참고문헌 (Reference)

1 "틸트로터 항공기 조종개념-X-15사례중심" 항공우주연구원 2004.6.

2 "틸트로터 항공기 비선형 시뮬레이션 프로그램 검증" 2004.4

3 "틸트로터 무인기 동특성 분석" 2004.4.

4 "틸트로타 TR301 시뮬레이션 프로그램 설명서" 항공우주연구원 2003.11

5 "V/STOL Tilt Rotor Aircraft Study Mathematical Model for a Real Time Simulation of a Tilt Rotor Aircraft 항공우주연구원" Boing Vertol Company me viii : 4-, 19732003.11.24.

6 "The history of the XV-15 Tilt Rotor Research Aircraft-From Concept to Flight" Government Reprinting Press 1998.

7 "Guidance Logis For Decelerating Spiral Approach of a Tilt Rotor Aircraft In the Presence of Wind" SUDAAR-506 Stanford University 1977.12.

8 "Flying Qualities of Piloted V/STOL Aircraft" 1991.9.

9 "Evaluation of XV-15 Rotor Aircraft for Flying Qualities Research Application" 1976.4.

10 "Bell eagle eye TR-911X tilt rotor UAV:recent developments, autoland integration, and flight test demonstrations" 2000.

11 "A Mathematical Model for Real Time Flight Simulation of The Bell 301 Tilt Rotor Research Aircraft" 1973.