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• W2017218233 abstract "This paper proposes a high-level underactuated nonlinear controller capable to guide a RUAV during a 3D flight. First, it presents a dynamic model to represent the dynamics of the aircraft, explicitly showing its underactuated character. Following, a suitable controller based on partial feedback linearization is designed for stabilizing the rotorcraft dynamics. A proof of the stability of the closed-loop control system in the sense of Lyapunov, including modeled disturbances and parametric errors, is also presented, as well as experimental results obtained with a quadrotor, which validate the proposed model and controller." @default.
• W2017218233 created "2016-06-24" @default.
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• W2017218233 date "2013-02-01" @default.
• W2017218233 modified "2023-10-16" @default.
• W2017218233 title "High-level underactuated nonlinear control for rotorcraft machines" @default.
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• W2017218233 doi "https://doi.org/10.1109/icmech.2013.6518549" @default.
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