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• W2899435019 abstract "The problem of designing the flight controller for a quad-tilt-wing UAV to achieve robust performance under constraints on the controller structure is considered. An approach based on $mu$ -synthesis is proposed: a non-parametric inverse multiplicative uncertainty description is employed to account for the uncertainties of the aircraft attitude dynamics at each operating condition. The resulting structured $mu$ -synthesis problem is reformulated as a structured $H_{infty}$ problem and solved by means of available MATLAB® software. Simulation results are presented in order to show the effectiveness of the approach." @default.
• W2899435019 created "2018-11-09" @default.
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• W2899435019 date "2018-08-01" @default.
• W2899435019 modified "2023-10-18" @default.
• W2899435019 title "Robust Attitude Control Design of Quad-Tilt-Wing UAV: A Structured <tex>$mu$</tex>-Synthesis Approach" @default.
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• W2899435019 doi "https://doi.org/10.1109/ccta.2018.8511407" @default.
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