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

Institute of Control, Robotics and Systems (제어로봇시스템학회)
권호 표지
DOI QR코드

DOI QR Code

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

공기부상 초고속 운행체 축소모델의 풍동내 비행제어 실험

  • 박영근 (항공대학교 항공우주및기계공학부) ;
  • 최승기 (항공대학교 항공우주및기계공학부) ;
  • 조진수 (한양대학교 기계공학부) ;
  • 송용규 (항공대학교 항공우주및기계공학부)
  • Published : 2005.03.01
Download PDF
⟨ Previous Next ⟩

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

References

  1. R. W. Staufenbiel and U. J. Schlichting, 'Stability of airplanes in ground effect', AIAA 1988
  2. M. D. Chawlla and L. C. Edwards and M. E. Franke, 'Wind-tunnel investigation of wing in ground effects', AIAA 1989
  3. S. Ando, 'Prediction of static height stability for some types of WIG.'
  4. Stauart Bennet, 'Real-time computer', Prentice Hall 1988
  5. R. C. Nelson, 'Flight stability and automatic control', McGraw Hill 1998
  6. 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
  7. 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
  8. 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
  9. K. Hwang 'Advanced computer architecture: parallelism, stability, programmability', Mc Graw Hill, 1993
  10. H. Delhaye, 'An investigation into the longitudinal stability of wing in ground effect vehicle', Master Thesis, Cranfield Univ, 1997
  11. 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
  12. J. Gera, 'Stability and control of win-in-ground effect vehicles or wingship', AIAA 95-0339, 1995
  13. J. Roskam, 'Airplane flight dynamics and automatic flight controls : part I', DARcorpration, 1995
  14. R. W. Staufenbiel, U. J. Schlichting, 'Stability of airplane in ground effect', AIAA, 1988
  15. I. Hall. 'An investigation into the flight dynamic of wing in ground effect aircraft operating in aerodynamic flight', Cranfield College of Aeronautics, sep 1994
  16. J. B. Barlow, W. H. Rae and Jr. Alan Pope, 'Low-speed wind tunnel testing', John Wiley & Sons 1999
  17. 'Assessment of experiment uncertainty with application to wind tunnel testing', AIAA, 1999, ISBN 1-56347-363-1
  18. 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
  19. 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
  20. 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
  21. A. O. Nuhait, M. F. Zedan, 'Stability derivatives of flapped plate in unsteady ground effect', Journal of Aircraft, vol. 32. no. 1 1995
  22. 송용규, '지면효과익기의 비행제어 방식에 관한 연구', 한국항공우주학회 춘계 학술대회 2002
  23. 최동수, '채널 내를 운행하는 초고속 지상 운행체의 공력특성에 관한 실험적 연구', 석사학위논문, 한양대학교 2003