关键词: 非线性飞行力学, 分支控制, 分支突变理论方法, 模糊逻辑控制

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