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• W2128513205 abstract "This paper develops a new state-space model for vortex-coupled 65-degree delta wing aircraft systems based on a modified nonlinear indicial response method combined with an internal state-space representation. Relationships between vortex breakdown location, rolling moment coefficient, and roll angle dynamics are determined. The state-space equations derived are subject to state delays and are also nonlinear in the vortex-coupled rolling moment coefficient Linear and nonlinear parameter identification methods are developed to empirically estimate the rolling moment coefficient as a function of the roll angle and primary vortex breakdown locations. A comparison between numerical simulations and experimental data indicates close agreement for a number of different initial conditions." @default.
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• W2128513205 date "2009-01-01" @default.
• W2128513205 modified "2023-09-26" @default.
• W2128513205 title "State-Space Modeling and Identification of Delta Wing Vortex-Coupled Roll Dynamics" @default.
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• W2128513205 doi "https://doi.org/10.2514/1.23596" @default.
• W2128513205 hasPublicationYear "2009" @default.
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