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http://dx.doi.org/10.5302/J.ICROS.2005.11.8.726

Design of Autolanding Guidance and Control Algorithm Using Singular Perturbation  

Ha, Cheol-Keun (울산대학교 항공우주공학과)
Choi, Hyoung-Sik (한국항공우주연구원)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.11, no.8, 2005 , pp. 726-732 More about this Journal
Abstract
This paper proposes an autolanding guidance and control algorithm with the lateral guidance law. This algorithm is basically formulated and designed in feedback linearization based on singular perturbation. Main features of this algorithm are two facts. One of those is that when a certain situation happens that airplane must realign to the runway suddenly assigned due to unexpected environment change around the landing site, the heading guidance in this algorithm is very valuable, and the other is the fact that the inner loop control of this algorithm is able to be designed directly based on the Handling Quality Requirements that most flight control systems must be satisfied with. To illustrate the potential of this algorithm, 6-DOF nonlinear simulation based on the nonlinear airplane model shown in Ref.[11] is carried out. The simulation results showed that the altitude response to the given landing trajectory is accurate, and the airplane heading alignment to the assigned runway from the lateral deviation is successful. It is noted that this algorithm is also applicable to unmanned aerial vehicle, which can be retrieved in autolanding technique, where the runway far retrieving the vehicle is in any direction for example at war field.
Keywords
lateral guidance far autolanding; singular perturbation; feedback linearization;
Citations & Related Records
Times Cited By KSCI : 3  (Citation Analysis)
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1 하철근, 임상수, 김병수, '항공기 CSAS 설계를 위한 고전적 Gain Scheduling 기법과 Dynamic Model Inversion 비선형 기법의 비교 연구,' 제어.자동화.시스템공학 논문지 vol. 7, no. 7, pp.574-581, July 2001   과학기술학회마을
2 T. Troudet, S. Garg, and W. C. Merill, 'Neural network application to aircraft control system design,' AIAA Paper 91-2715
3 G. J. Balas, J. Reiner, and W. L. Garrard, 'Design of a flight control system for a highly maneuverable aircraft using ${\mu}$-synthesis,' AIAA Paper 93-3774
4 Cheolkeun Ha and Sangwon Ahn, 'Longitudinal automatic landing in adaptive PID control law under wind shear turbulence,' KSAS International Journal, vol. 5, no. 1, pp.30-38, May 2004
5 A. Thurkral, and M. Innocenti, 'Control design challenge : a variable structure approach,' Journal of Guidance, Control and Dynamics, vol. 17, no. 5, pp.942-949, 1994   DOI   ScienceOn
6 L. Duke, 'Controls design challenge proposal,' Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA Washington DC, 1990
7 G. Meyer and L. Cicolani, 'Application of nonlinear systems inverses to automatic flight control design,' Theory and Application of Optimal Control in Aerospace Systems, AG251, pp.1-29, 1981
8 P. K. A. Menon and R. A. Walker, 'Aircraft flight test trajectory control,' NAS2-11877, March 1985
9 J. H. Blakelock, Automatic control of Aircraft and Missiles (2nd edition), John Willey & Sons, Inc, 1991
10 P. Riseborough, 'Automatic take-off and landing control for small UAV,' The 5th Asian Control Conference, pp.210-215, 2003
11 B. L. Stevens and F. L. Lewis, Aircraft control and Simulation, John Willey & Sons, Inc, 1992
12 W. T. Miller, R. S. Sutton, and P. J. Werbos, Neural Networks for Control, Bradford Book, MIT Press, Cambridge, MA. pp.403-426, 1992
13 J. H. Chow, and P. V. Kokotovic, 'Two-time scale feedback design of a class of nonlinear systems,' IEEE Transactions on Automatic Control, vol. AC-23, no. 3, pp.438-443, June 1978   DOI
14 하철근, 김병수, '모델역변환을 이용한 종운동 지동착륙 유도제어 알고리즘 설계,' 한국항공우주학회, 제32 권, 제2호, pp.66-73, 2004
15 하철근, 박영일, 윤석준, '종/횡운동 자동착륙 유도 및 제어시스템 설계 및 분석,' 11차 유도무기 학술대회, 국방과학연구소, pp.249-252, 10월 25일, 2001
16 김봉주, 하철근, '자동착륙을 위한 횡운동 설계기법 연구,' 한국항공우주학회 추계학술발표회, 보광휘닉스파크호텔, pp.1317-1320, 11월 8-9일, 2002
17 R. J. Niewoehner and I. I. Kaminer, 'Design of an autolanding controller for an F-14 aircraft using $H_{\infty}-synthesis$,' Journal of Guidance, Control, and Dynamics, vol. 19, no. 3, pp.656-663, 1996   DOI   ScienceOn
18 M. B. Subrahmanyam, 'H design of F/A-18A automatic carrier landing system,' Journal of Guidance, Control, and Dynamics, vol. 17, no. 1, pp.187-191, 1994   DOI   ScienceOn
19 M. R. Napolitano and M. Kincheloe, 'On-line learning neural-network controllers for autopilot systems,' Journal of Guidance, Control and Dynamics, vol. 33, no. 6, pp.1008-1015, 1995
20 M. Bodson, and J. E. Groszkiewicz, 'Multivariable adaptive algorithms for reconfigurable flight control,' IEEE Transactions Control Systems Technology, vol. 5, no. 2, Mar. pp.217-229, 1997   DOI   ScienceOn
21 D. J. Bugajski and D. F. Enns, 'Nonlinear control law with application to high angle-of-attack flight,' Journal of Guidance, Control, and Dynamics, vol. 15, no. 3, pp.761-767, 1992   DOI