Robust Attitude Control Design of Quad-Tilt-Wing UAV: A Structured $\mu$-Synthesis Approach - researchr publication authors

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Simone Panza, Masayuki Sato 0003, Marco Lovera, Koji Muraoka. Robust Attitude Control Design of Quad-Tilt-Wing UAV: A Structured $\mu$-Synthesis Approach. In IEEE Conference on Control Technology and Applications, CCTA 2018, Copenhagen, Denmark, August 21-24, 2018. pages 781-786, IEEE, 2018. [doi]

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