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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2006, Vol. 27 ›› Issue (1): 5-9.

• 论文 • Previous Articles     Next Articles

Roll Manoeuvre Bifurcation Analysis and Control of Aircraft Using EBA-FLC Method

CHEN Yong-liang, SHEN Hong-liang, LIU Chang   

  1. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2004-09-20 Revised:2005-09-26 Online:2006-02-25 Published:2006-02-25

Abstract: The EBA-FLC technique, which is developed by integrating the extended bifurcation analysis with fuzzy logic control in this article, is a new close-loop bifurcation control method. The EBA-FLC technique is used to investigate the global nonlinear behavior of a maneuverable aircraft in zero sideslip roll maneuver. It turns out that the controlled aircraft has a desired dynamic behavior in wide range of the bifurcation parameter, and that the dynamic and static characteristics of the zero sideslip roll maneuver are both improved.

Key words: nonlinear flight dynamics, bifurcation control, BACTM, FLC

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