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http://dx.doi.org/10.5302/J.ICROS.2005.11.3.246

Flight Control Experiment of High-Speed Aero-Levitation Electric Vehicle Scale-Model in Wind-Tunnel  

Park, Young-Geun (항공대학교 항공우주및기계공학부)
Choi, Seung-Kie (항공대학교 항공우주및기계공학부)
Cho, Jin-Soo (한양대학교 기계공학부)
Song, Yong-Kyu (항공대학교 항공우주및기계공학부)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.11, no.3, 2005 , pp. 246-253 More about this Journal
Abstract
An experimenal study on flight control of high-speed AEV(Aero-levitation Electric Vehicle) scale model in wind-tunnel is conducted. The AEV is to fly at very low altitude in predesigned track so that it is always under the wing-in-ground effect. The experiment is intended to fly the scale model to follow the predesigned altitude schedule while holding its attitude (pitch, roll, and yaw). Especially, the altitude changes for climb, cruise, and descent with constant pitch angle are most important maneuvers. The experiment shows that the required mission flights can be performed with appropriate sensors, processors, and actuators.
Keywords
flight control experiment; scale-model; wind-tunnel; wing-in-ground effect;
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1 최동수, '채널 내를 운행하는 초고속 지상 운행체의 공력특성에 관한 실험적 연구', 석사학위논문, 한양대학교 2003
2 K. Nitta, 'Design and examination of $H{\infty}$ robust controller for ground effect problem', Journal of Guidance, Control and Dynamics, vol. 18. no. 4. 1995
3 H. Kawazoe, T. Yorikane and Y. Tone, 'A study on dynamic characteristics of delta wing in rolling motion near Ground', 39th AIAA Aerospace Sciences Meeting & Exhibit Report, 2001
4 R. W. Staufenbiel, U. J. Schlichting, 'Stability of airplane in ground effect', AIAA, 1988
5 I. Hall. 'An investigation into the flight dynamic of wing in ground effect aircraft operating in aerodynamic flight', Cranfield College of Aeronautics, sep 1994
6 J. B. Barlow, W. H. Rae and Jr. Alan Pope, 'Low-speed wind tunnel testing', John Wiley & Sons 1999
7 'Assessment of experiment uncertainty with application to wind tunnel testing', AIAA, 1999, ISBN 1-56347-363-1
8 Stauart Bennet, 'Real-time computer', Prentice Hall 1988
9 R. C. Nelson, 'Flight stability and automatic control', McGraw Hill 1998
10 M. D. Chawal, L. C. Edwards, M. E. Franke, 'Wind-tunnel investigatio of wing-in-ground effects', Journal of Aircraft, vol. 27. no. 4. 1990
11 A. O. Nuhait, M. F. Zedan, 'Stability derivatives of flapped plate in unsteady ground effect', Journal of Aircraft, vol. 32. no. 1 1995
12 송용규, '지면효과익기의 비행제어 방식에 관한 연구', 한국항공우주학회 춘계 학술대회 2002
13 R. D. Toles, 'Design methodology, implementation, and flight test of closed loop decoupling for the AFTI/F-16 aircraft', .AIAA Guidance and Control Conference, Aug 1983
14 J. Gera, 'Stability and control of win-in-ground effect vehicles or wingship', AIAA 95-0339, 1995
15 J. Roskam, 'Airplane flight dynamics and automatic flight controls : part I', DARcorpration, 1995
16 K. Hwang 'Advanced computer architecture: parallelism, stability, programmability', Mc Graw Hill, 1993
17 T. Kono, Y. Kohama and N. Matsui, 'Stability of guide way type wing in ground effect vehicle', Proceedings of the Third JSME-KSEM Fluid Engineering Conference, July 25-27, 19941, Sendai, Japan
18 C.-H. Han, 'Aerodynamic analysis and design of an aero-livitation vehicle for a high-speed ground transportation systems', P.H. D Thesis, Hanyang Univ 2002
19 J. Cho, Y. Yoon, and Y. Song, 'Multidisplinary studies for the development of an AEV-HGTS', .AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002, Technical Forum Los Angeles, California, Oct 2002
20 H. Delhaye, 'An investigation into the longitudinal stability of wing in ground effect vehicle', Master Thesis, Cranfield Univ, 1997
21 S. Ando, 'Prediction of static height stability for some types of WIG.'
22 R. W. Staufenbiel and U. J. Schlichting, 'Stability of airplanes in ground effect', AIAA 1988
23 M. D. Chawlla and L. C. Edwards and M. E. Franke, 'Wind-tunnel investigation of wing in ground effects', AIAA 1989