Adaptive backstepping control for electrically driven unmanned helicopter

Control Engineering Practice

Volumn 17, Issue 8, 2009, Pages 903-913

  Yang, Jung Hua ^a   Hsu, Wen Chun ^a  

^a NATIONAL PINGTUNG UNIVERSITY OF SCIENCE AND TECHNOLOGY   (Taiwan)

Author keywords

Adaptive control; Backstepping; Helicopter; Twin rotor

Indexed keywords

ADAPTIVE BACKSTEPPING CONTROL; ADAPTIVE CONTROL; ASYMPTOTICALLY STABLE; CONTROL OBJECTIVES; CONTROL PROBLEMS; CONTROL SCHEMES; CONTROLLER DESIGNS; LYAPUNOV THEOREMS; NONLINEAR COUPLING; TWIN ROTOR; TWIN-ROTORS; UNMANNED HELICOPTER; YAW ANGLES;

ADAPTIVE CONTROL SYSTEMS; CONTROLLERS; DC MOTORS; HELICOPTER ROTORS; PROBLEM SOLVING;

BACKSTEPPING;

EID: 67349240207     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.conengprac.2009.02.012     Document Type: Article

References (20)

1. Ahmad, S. M., Shaheed, M. H., & Chipperfield, A. J. (2000). Nonlinear modeling of a twin rotor MIMO system using radial basis function networks. In Proceedings of the IEEE national aerospace and electronics conference (October, pp. 313-320).
2. Buskey, G., Roberts, J., & Wyeth, G. (2002). Online learning of autonomous helicopter control. In: Proceedings of Australasian conference on robotics and automation (pp. 19-24), Auckland, November 27-29.
3. Feng G. An approach to adaptive control of fuzzy dynamic systems. IEEE Transactions on Fuzzy Systems 10 2 (2002)
4. Goléa N., Goléa A., and Benmahammed K. Fuzzy model reference adaptive control. IEEE Transactions on Fuzzy Systems 10 4 (2002)
5. Huang Y.J., Kuo T.C., and Way H.K. Robust vertical takeoff and landing aircraft control via integral sliding mode. IEE Proceedings-Control Theory and Applications 150 4 (2003)
6. Islam, B., Ahmed, N., Bhatti, D. L., & Khan, S. (2003). Controller design using fuzzy logic for a twin rotor MIMO system. In Proceedings of the IEEE international conference on nonlinear modeling, identification, and control (pp. 264-268).
7. Liu C.C., Yang R.F., Yang C.D., and Chang Y.H. Helicopter H∞ control design with robust flying quality. Aerospace Science and Technology 7 2 (2003) 159-169
8. Lu, W. J. (2000). Composite sliding mode control with an application to a twin-rotor MIMO system. Master thesis, National Yunlin University of Science and Technology, Taiwan, ROC.
9. Mclean D., and Matsuda H. Helicopter station-keeping: Comparing LQR, fuzzy-logic and neural-net controllers. Engineering Applications of Artificial Intelligence 11 (1998) 411-418
10. Padfield G.D. Helicopter flight dynamics: The theory and application of flying qualities and simulation modeling (1996), AIAA and Blackwell Science Ltd., UK
11. Rahideh A., Shaeed M.H., and Huijberts H.J.C. Dynamic modeling of a TRMS using analytical and empirical approaches. Control Engineering Practice 16 (2008) 241-259
12. Saeki, M., & Sakaue, Y. (2001). Flight control design for a nonlinear non-minimum phase VTOL aircraft via two-step linearization. In Proceedings of the 40th IEEE conference of decision and control (December, pp. 217-222), Orlando, FL, USA.
13. Sastry S., and Marc B. Adaptive control stability, convergence, and robustness. 1st ed. (1989), Prentice-Hall, New York
14. Su J.P., Liang C.Y., and Chen H.M. Robust control of a class of nonlinear systems and its application to a twin rotor MIMO system. IEEE International Conference on Industrial Technology 2 (2002) 1272-1277
15. Su J.P., and Lu W.J. Composite sliding mode control and its application to a twin-rotor multi-input multi-output system. AASRC Transactions of the Aeronautical and Astronautical Society of the R.O.C 33 4 (2001) 275-282
16. Twin Rotor MIMO System (1998). Reference Manual, Feedback Instruments Ltd., UK.
17. Wey, W. E. (2000). Fuzzy sliding mode control with backstepping and its application to a twin rotor MIMO system. Master thesis, National Yunlin University of Science & Technology, Taiwan.
18. Yan, L., Sundararajan, N., & Saratchandean P. (2000). Dynamically structured radial basis function neural networks for robust aircraft flight control. In Proceedings of the American control conference (pp. 3501-3505), Chicago, IL.
19. Yang, C. D., & Liu, W. H. (2002). Robust nonlinear H∞ decoupling control of flight vehicle in hovering. In Proceedings of the 41st IEEE conference of decision and control (pp. 4486-4491), Las Vegas, NV, USA.
20. Yang, C. D., & Liu W. H. (2003). Nonlinear H∞ decoupling hover control of helicopter with parameter uncertainties. In Proceedings of the American control conference, June 4-6, Denver, CO.