We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter during landing, while stabilizing the lateral and longitudinal position and maintaining a constant attitude. The dynamics of the helicopter main and tail rotors are often neglected to simplify the control design, but this reduction has the disadvantage of an unreal choice of the control inputs. We have solved this contradiction by choosing the main controller required for performing the secure landing by neglecting the complex rotors dynamics, and then we have included these important dynamics in a closed loop model having real controls determined from an auxiliary controller. Simulation results show the effectiveness of the method to cope with uncertainties on the plant and actuator model. We apply a nonlinear controller which combines recent results on nonlinear adaptive output regulation and robust stabilization of systems in feed forward form by means of saturated controls. The added dynamics required the design of an auxiliary controller to force the states of the main and tail rotors systems to follow their reference values determined from the main controller.
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We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter during landing, while stabilizing the lateral and longitudinal position and maintaining a constant attitude. The dynamics of the helicopter main and tail rotors are often neglected to simplify the control design, but this reduction has the disadvantage of an unreal choice of the control inputs. We have solved this contradiction by choosing the main controller required for performing the secure landing by neglecting the complex rotors dynamics, and then we have included these important dynamics in a closed loop model having real controls determined from an auxiliary controller. Simulation results show the effectiveness of the method to cope with uncertainties on the plant and actuator model. We apply a nonlinear controller which combines recent results on nonlinear adaptive output regulation and robust stabilization of systems in feed forward form by means of saturated controls. The added dynamics required the design of an auxiliary controller to force the states of the main and tail rotors systems to follow their reference values determined from the main controller.
Hasan received B.Sc. and M.Sc. in electrical engineering from Benha University, Egypt, in 2001 and 2007 respectively. He obtained PhD in mechatronics and robotics engineering from Egypt-Japan University of Science and Technology (jointly with Osaka University, Japan) in 2013. His research interests include robotics, control and computer vision.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter during landing, while stabilizing the lateral and longitudinal position and maintaining a constant attitude. The dynamics of the helicopter main and tail rotors are often neglected to simplify the control design, but this reduction has the disadvantage of an unreal choice of the control inputs. We have solved this contradiction by choosing the main controller required for performing the secure landing by neglecting the complex rotors dynamics, and then we have included these important dynamics in a closed loop model having real controls determined from an auxiliary controller. Simulation results show the effectiveness of the method to cope with uncertainties on the plant and actuator model. We apply a nonlinear controller which combines recent results on nonlinear adaptive output regulation and robust stabilization of systems in feed forward form by means of saturated controls. The added dynamics required the design of an auxiliary controller to force the states of the main and tail rotors systems to follow their reference values determined from the main controller. 104 pp. Englisch. N° de réf. du vendeur 9783659696817
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Vendeur : moluna, Greven, Allemagne
Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Hasan MohamedHasan received B.Sc. and M.Sc. in electrical engineering from Benha University, Egypt, in 2001 and 2007 respectively. He obtained PhD in mechatronics and robotics engineering from Egypt-Japan University of Science and Te. N° de réf. du vendeur 159143872
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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter during landing, while stabilizing the lateral and longitudinal position and maintaining a constant attitude. The dynamics of the helicopter main and tail rotors are often neglected to simplify the control design, but this reduction has the disadvantage of an unreal choice of the control inputs. We have solved this contradiction by choosing the main controller required for performing the secure landing by neglecting the complex rotors dynamics, and then we have included these important dynamics in a closed loop model having real controls determined from an auxiliary controller. Simulation results show the effectiveness of the method to cope with uncertainties on the plant and actuator model. We apply a nonlinear controller which combines recent results on nonlinear adaptive output regulation and robust stabilization of systems in feed forward form by means of saturated controls. The added dynamics required the design of an auxiliary controller to force the states of the main and tail rotors systems to follow their reference values determined from the main controller. N° de réf. du vendeur 9783659696817
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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -We consider the problem of controlling the vertical motion of a nonlinear model of a helicopter during landing, while stabilizing the lateral and longitudinal position and maintaining a constant attitude. The dynamics of the helicopter main and tail rotors are often neglected to simplify the control design, but this reduction has the disadvantage of an unreal choice of the control inputs. We have solved this contradiction by choosing the main controller required for performing the secure landing by neglecting the complex rotors dynamics, and then we have included these important dynamics in a closed loop model having real controls determined from an auxiliary controller. Simulation results show the effectiveness of the method to cope with uncertainties on the plant and actuator model. We apply a nonlinear controller which combines recent results on nonlinear adaptive output regulation and robust stabilization of systems in feed forward form by means of saturated controls. The added dynamics required the design of an auxiliary controller to force the states of the main and tail rotors systems to follow their reference values determined from the main controller.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 104 pp. Englisch. N° de réf. du vendeur 9783659696817
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Vendeur : preigu, Osnabrück, Allemagne
Taschenbuch. Etat : Neu. Autonomous Helicopter Landing | Aviation Control System for a Flying Robot | Mohamed Hasan | Taschenbuch | 104 S. | Englisch | 2015 | LAP LAMBERT Academic Publishing | EAN 9783659696817 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 104660426
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Vendeur : Mispah books, Redhill, SURRE, Royaume-Uni
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