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Control System Design Small by Tun Hla (6 results)

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  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

    • Softcover

    Seller: Revaluation Books, Exeter, United KingdomRevaluation Books

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    £ 61.93

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

  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

    • Softcover

    Seller: preigu, Osnabrück, Germanypreigu

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    Taschenbuch. Condition: 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. …

  • Language: English

    Published by LAP LAMBERT Academic Publishing Sep 2017, 2017

    3659506060 / 9783659506062

    • Softcover
    • Print on Demand

    Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermanyBuchWeltWeit Ludwig Meier e.K.

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    Taschenbuch. Condition: 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.…

  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

    • Softcover
    • Print on Demand

    Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH

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    Taschenbuch. Condition: 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.…

  • Language: English

    Published by LAP LAMBERT Academic Publishing, 2017

    3659506060 / 9783659506062

    • Softcover
    • Print on Demand

    Seller: moluna, Greven, Germanymoluna

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    Condition: 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.…

  • Language: English

    Published by LAP LAMBERT Academic Publishing Sep 2017, 2017

    3659506060 / 9783659506062

    • Softcover
    • Print on Demand

    Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germanybuchversandmimpf2000

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    Taschenbuch. Condition: 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.…