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• W2133583337 abstract "Design and synthesis of a nonlinear supersonic missile longitudinal dynamics control for angle-of-attack output tracking are presented. In addition a sliding mode observer is designed to estimate the angle-of-attack which is difficult to measure in practice. The employed method is simple to implement in practical applications and enables the sliding mode control design to exhibit the desired dynamic properties during the entire output-tracking process independent of perturbations. Results of simulations are presented to demonstrate the performance, robustness, and stability of the considered autopilot." @default.
• W2133583337 created "2016-06-24" @default.
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• W2133583337 date "2008-12-01" @default.
• W2133583337 modified "2023-09-26" @default.
• W2133583337 title "Sliding mode autopilot and observer design for a supersonic flight vehicle" @default.
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• W2133583337 doi "https://doi.org/10.1109/isscaa.2008.4776375" @default.
• W2133583337 hasPublicationYear "2008" @default.
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