DOI QR코드

DOI QR Code

Development of Automatic flight Control System for Low Cost Unmanned Aerial Vehicle

저가형 무인 항공기의 자동비행시스템 개발

  • 유혁 (한국항공우주연구원 항법제어그룹) ;
  • 이장호 (한국항공우주연구원 항법제어그룹) ;
  • 김재은 (한국항공우주연구원 항법제어그룹) ;
  • 안이기 (한국항공우주연구원 항법제어그룹)
  • Published : 2004.02.01

Abstract

Automatic flight control system (AFCS) for a low-cost unmanned aerial vehicle is described in this paper. Development process and block diagram of the AFCS are introduced. The flight control law for longitudinal and lateral channel autopilot is designed using optimization process. In this procedure, the performance index is composed of desired location of closed loop system poles and H$_2$norm of the resultant flight control system. This procedure is applied to the autopilot design of an unmanned target vehicle. Performance of the AFCS is evaluated by processor-in-the-loop simulation test and flight test. These results show that the AFCS has acceptable performance fur low cost UAV.

Keywords

References

  1. 오재석, 유혁, 구삼옥, '소형 무인항공기용 저가형 자동 조종장비의 개발' 제어.자동화.시스템공학회지 제7권, 제5호, pp.37-45, 2001
  2. J. Roskam, Airplane Flight Dynamics and Automatic Flight Controls, Roskam Aviation and Engineering Corporation, 1979
  3. B. L. Stevens and F. L. Lewis, Aircraft Control and Simulation, John Wiley & Sons, Inc., 1992
  4. A. A. Tunik, H. Ryu, H.-C. Lee, 'Parametric optimization procedure for robust flight control system design,' KSAS International Journal, vol. 2, no. 2, pp. 95-107, 2001
  5. J. Doyle, K. Glover, P. Khargonekar, and B. Francis, 'State-space solution to standard $H_2$ and $H_{infty}$ control problems,' IEEE Trans. on Automatic Control, vol. 34, no. 8, pp. 831-847, 1989 https://doi.org/10.1109/9.29425
  6. 유혁, 이상혁, 박무혁, '자동비행시스템 검증을 위한 PILS 개발,' 2000년 한국항공우주학회 추계학술발표회 논문집, 울산대학교, pp. 71-74, 2000
  7. 유혁, 박무혁, 구삼옥, 김중옥, 안이기, '소형 무인항공기 비행시험과 교훈,' 2001년 한국항공우주학회 추계학술발표회 논문집, 세종대학교, pp. 337-341, 2001