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Sinopsis
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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Reseña del editor
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.
Biografía del autor
Prof. 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 from Yangon Technological University in 2003. He was awarded the Ph.D (Electronic Engineering) degree from M.T.U in 2008.
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Control System Design for Small Unmanned Aerial Vehicle
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LAP LAMBERT Academic Publishing Sep 2017, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
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Taschenbuch. Condición: 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. Nº de ref. del artículo: 9783659506062
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Control System Design for Small Unmanned Aerial Vehicle
Publicado por
LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
Nuevo
Taschenbuch
Librería: AHA-BUCH GmbH, Einbeck, Alemania
Calificación del vendedor: 5 de 5 estrellas
Taschenbuch. Condición: 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. Nº de ref. del artículo: 9783659506062
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Control System Design for Small Unmanned Aerial Vehicle
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LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Librería: moluna, Greven, Alemania
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Condición: 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. Nº de ref. del artículo: 173836886
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Control System Design for Small Unmanned Aerial Vehicle
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LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Librería: Revaluation Books, Exeter, Reino Unido
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Paperback. Condición: Brand New. 112 pages. 8.66x5.91x0.26 inches. In Stock. Nº de ref. del artículo: 3659506060
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Control System Design for Small Unmanned Aerial Vehicle
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LAP LAMBERT Academic Publishing Sep 2017, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
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Taschenbuch. Condición: 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. Nº de ref. del artículo: 9783659506062
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Control System Design for Small Unmanned Aerial Vehicle
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LAP LAMBERT Academic Publishing, 2017
ISBN 10: 3659506060
ISBN 13: 9783659506062
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Librería: preigu, Osnabrück, Alemania
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Taschenbuch. Condición: 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. Nº de ref. del artículo: 113179468
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