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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2006, Vol. 27 ›› Issue (1): 5-9.
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CHEN Yong-liang, SHEN Hong-liang, LIU Chang
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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
CLC Number:
V212
CHEN Yong-liang;SHEN Hong-liang;LIU Chang. Roll Manoeuvre Bifurcation Analysis and Control of Aircraft Using EBA-FLC Method[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(1): 5-9.
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