control system design small de tun hla (6 résultats)

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

Taschenbuch. Etat : 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.

Taschenbuch. Etat : 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.

Etat : 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.

Taschenbuch. Etat : 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.

Taschenbuch. Etat : 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.