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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.
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Control System Design for Small Unmanned Aerial Vehicle
Editore:
LAP LAMBERT Academic Publishing Sep 2017, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
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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. Codice articolo 9783659506062
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Control System Design for Small Unmanned Aerial Vehicle
Editore:
LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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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. Codice articolo 173836886
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Control System Design for Small Unmanned Aerial Vehicle
Editore:
LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Da: Revaluation Books, Exeter, Regno Unito
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Paperback. Condizione: Brand New. 112 pages. 8.66x5.91x0.26 inches. In Stock. Codice articolo 3659506060
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Control System Design for Small Unmanned Aerial Vehicle
Editore:
LAP LAMBERT Academic Publishing Sep 2017, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
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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.Books on Demand GmbH, Überseering 33, 22297 Hamburg 112 pp. Englisch. Codice articolo 9783659506062
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Control System Design for Small Unmanned Aerial Vehicle
Editore:
LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Taschenbuch
Da: AHA-BUCH GmbH, Einbeck, Germania
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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. Codice articolo 9783659506062
Quantità: 1 disponibili