Post-stall flight dynamics of commercial transport aircraft configuration: A nonlinear bifurcation analysis and validation:
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Zhitao Liu | Jiang Yong | Fei Cen | Lei Zhang | Li Qing
[1] M. Lowenberg. Bifurcation analysis of multiple–attractor flight dynamics , 1998, Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences.
[2] Qing Wang,et al. Unsteady aerodynamic modeling at high angles of attack using support vector machines , 2015 .
[3] Mark H Lowenberg,et al. Experimental investigation of aerodynamic hysteresis using a 5-DoF wind tunnel manoeuvre rig , 2019 .
[4] Jean-Etienne T. Dongmo,et al. Nonlinear Analysis of Aircraft Loss of Control , 2013 .
[5] Chengwen Zhong,et al. Initial virtual flight test for a dynamically similar aircraft model with control augmentation system , 2017 .
[6] Mikhail Goman,et al. Application of bifurcation methods to nonlinear flight dynamics problems , 1997 .
[7] Bei Lu,et al. Linear Parameter-Varying Antiwindup Compensation for Enhanced Flight Control Performance , 2005 .
[8] Simon A Neild,et al. Upset Dynamics of an Airliner Model: A Nonlinear Bifurcation Analysis , 2013 .
[9] Luis G. Crespo,et al. Nonlinear Dynamics of Aircraft Controller Characteristics Outside the Standard Flight Envelope , 2015 .