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Super-twisting sliding mode control for aircraft at high angle of attack based on finite-time extended state observer
Authors:Liu  Junjie  Sun  Mingwei  Chen  Zengqiang  Sun  Qinglin
Affiliation:1.College of Artificial Intelligence, Nankai University, Tianjin, 300350, China
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Abstract:Nonlinear Dynamics - This paper proposes a finite-time decoupling control strategy for aircraft with thrust vector at high angle of attack maneuver. Firstly, the nonlinear mathematical model of the...
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