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- W2326553108 abstract "1 Abstract This paper1 presents the development and experimental demonstration of a novel nonlinear approach to developing control laws for the lateral-directional dynamics of aircraft at high angle of attack using Forebody Tangential Blowing (FTB). The vortical flow over the forebody is modified with FTB which in turn creates roll and yaw moments for control. The blowing system is driven by nonlinear control laws based on combining High-Gain Control (HGC) and Lyapunov min-max techniques. This control design technique can handle the severe nonlinearities associated with FTB, and therefore, can exploit fully the FTB capabilities. Simulation and experimental results are provided that demonstrate the effectiveness of the approach." @default.
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- W2326553108 date "1998-08-10" @default.
- W2326553108 modified "2023-09-25" @default.
- W2326553108 title "Nonlinear control using forebody tangential blowing" @default.
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- W2326553108 doi "https://doi.org/10.2514/6.1998-4204" @default.
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