ISBN: 9783659506062 - control system design for small unmanned aerial vehicle (6 risultati)

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  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

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    Da: Revaluation Books, Exeter, Regno UnitoRevaluation Books

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    EUR 76,40

    EUR 11,98 spedizione 
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    Quantità: 1 disponibile

    Paperback. Condizione: Brand New. 112 pages. 8.66x5.91x0.26 inches. In Stock.

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

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    Da: preigu, Osnabrück, Germaniapreigu

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    EUR 36,60

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    Taschenbuch. Condizione: Neu. Control System Design for Small Unmanned Aerial Vehicle | Hla Myo Tun | Taschenbuch | Englisch | 2017 | LAP LAMBERT Academic Publishing | EAN 9783659506062 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. …

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing Sep 2017, 2017

    3659506060 / 9783659506062

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    Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermaniaBuchWeltWeit Ludwig Meier e.K.

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    EUR 39,90

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    Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The first component includes development of a physical, inertial and aerodynamic model representing an existing UAV in research. Second is the development and implementation of six degrees of freedom simulation, employing the developed model. The third component is the comparison between open loop flight and the UAV dynamics with the MATLAB simulation results. The simulation results show that the responses of the altitude control for small UAV are oscillated because of the wind disturbances in level flight condition. To apply the UAV system, the feedback control design is of linear quadratic regulator (LQR) and proportional, integral, derivative (PID) architectures. 112 pp. Englisch.…

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

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    Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH

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    EUR 39,90

    EUR 35,00 spedizione 
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    Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The first component includes development of a physical, inertial and aerodynamic model representing an existing UAV in research. Second is the development and implementation of six degrees of freedom simulation, employing the developed model. The third component is the comparison between open loop flight and the UAV dynamics with the MATLAB simulation results. The simulation results show that the responses of the altitude control for small UAV are oscillated because of the wind disturbances in level flight condition. To apply the UAV system, the feedback control design is of linear quadratic regulator (LQR) and proportional, integral, derivative (PID) architectures.…

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

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    Da: moluna, Greven, Germaniamoluna

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    EUR 34,25

    EUR 48,99 spedizione 
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    Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Tun Hla MyoProf. Dr. Hla Myo Tun who is a Professor and Head of the Department of Electronic Engineering of Y.T.U received his B.E(Electronics) degree from Mandalay Technological University in 2002. He got his M.E(Electronics) degree.…

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing Sep 2017, 2017

    3659506060 / 9783659506062

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    Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germaniabuchversandmimpf2000

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    EUR 39,90

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    Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The first component includes development of a physical, inertial and aerodynamic model representing an existing UAV in research. Second is the development and implementation of six degrees of freedom simulation, employing the developed model. The third component is the comparison between open loop flight and the UAV dynamics with the MATLAB simulation results. The simulation results show that the responses of the altitude control for small UAV are oscillated because of the wind disturbances in level flight condition. To apply the UAV system, the feedback control design is of linear quadratic regulator (LQR) and proportional, integral, derivative (PID) architectures.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 112 pp. Englisch.…