25   Artículos

 
en línea
Álvaro Muñoz and Pablo García-Fogeda    
This paper compares various procedures for determining the optimal control law for a wing section in compressible flow. The flow regime includes subsonic, sonic and supersonic flows. For the evolution of the system in the Laplace plane, the present metho... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Amalia Moutsopoulou, Markos Petousis, Georgios E. Stavroulakis, Anastasios Pouliezos and Nectarios Vidakis    
In this study, we created an accurate model for a homogenous smart structure. After modeling multiplicative uncertainty, an ideal robust controller was designed using µ-synthesis and a reduced-order H-infinity Feedback Optimal Output (Hifoo) controller, ... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Fredrik Fogh Sørensen, Malte von Benzon, Jesper Liniger and Simon Pedersen    
Offshore pipelines and structures require regular marine growth removal and inspection to ensure structural integrity. These operations are typically carried out by Remotely Operated Vehicles (ROVs) and demand reliable and accurate feedback signals for o... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Alexandr V. Efremov, Zoe Mbikayi and Eugene V. Efremov    
The modern trend of developing highly automated aircraft is characterized by a transition from traditional methods and technical solutions to innovative approaches in order to control the system, inceptor and display design. This paper deals with the dev... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Martin Goubej, Jana Königsmarková, Ronald Kampinga, Jakko Nieuwenkamp and Stéphane Paquay    
The paper deals with development of a methodology for mechatronic system design using state-of-the-art model-based system engineering methods. A simple flexible robotic arm is considered as a benchmark problem for the evaluation of various techniques use... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Kai Masuda and Kenji Uchiyama    
This paper describes the design method of a flight control system of a Quad Tilt-Wing (QTW) Unmanned Aerial Vehicle (UAV). A QTW-UAV is necessary to design a controller considering its nonlinear dynamics because of the appearance of the nonlinearity duri... ver más
Revista: Aerospace    Formato: Electrónico

 
usuarios registrados
McEneaney, William M     Pág. 379 - 412
Revista: SIAM JOURNAL ON CONTROL AND OPTIMIZATION    Formato: Impreso

 
usuarios registrados
Shi Lin Xie, Xi Nong Zhang, Jing Hui Zhang, and Lie Yu     Pág. 115 - 133
Revista: JOURNAL OF VIBRATION AND CONTROL    Formato: Impreso

 
usuarios registrados
Mei, S; Chen, J; Song, Y H; Goto, M; Yokoyama, A     Pág. 557 - 561
Revista: IET GENERATION, TRANSMISSION & DISTRIBUTION    Formato: Impreso

 
usuarios registrados
Chung, C Y; Tse, C T; David, A K; Rad, A B     Pág. 413 - 419
Revista: IET GENERATION, TRANSMISSION & DISTRIBUTION    Formato: Impreso

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