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Real-Time Hovering Control of Unmanned Aerial Vehicles

机译:Real-Time Hovering Control of Unmanned Aerial Vehicles

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In this paper, the design of a controller for the altitude and rotational dynamics is presented. In particular, the control problem is to maintain a desired altitude in a fixed position. The unmanned aerial vehicle dynamics are described by nonlinear equations, derived using the Newton-Euler approach. The control problem is solved imposing the stability of the error dynamics with respect to desired position and angular references. The performance and effectiveness of the proposed control are tested, first, via numerical simulations, using the Pixhawk Pilot Support Package simulator provided by Mathworks. Then, the controller is tested via a real-time implementation, using a quadrotor Aircraft F-450.

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    Univ Guadalajara, La Cienega Univ Ctr, Technol Sci Dept, Av Univ 1115, Ocotlan 47820, Jalisco, Mexico|Univ Aquila, Ctr Excellence DEWS Design Methodol Embedded Cont, Via Vetoio, I-67100 Laquila, Italy;

    Univ Guadalajara, La Cienega Univ Ctr, Technol Sci Dept, Av Univ 1115, Ocotlan 47820, Jalisco, Mexico;

    Univ Aquila, Ctr Excellence DEWS Design Methodol Embedded Cont, Via Vetoio, I-67100 Laquila, Italy|Univ Aquila, Dept Informat Engn Comp Sci & Math, Via Vetoio, I-67100 Laquila, ItalyUniv Aquila, Ctr Excellence DEWS Design Methodol Embedded Cont, Via Vetoio, I-67100 Laquila, Italy|Ctr Res & Adv Studies, Campus Guadalajara,Av Bosque 1145, El Bajio 45019, Zapopan, Mexico;

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