The comparative study of vibration control of flexible structure using smart materials.
Fei, Juntao, Fang, Yunmei, Yan, Chunyan (2010)
Mathematical Problems in Engineering
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Fei, Juntao, Fang, Yunmei, Yan, Chunyan (2010)
Mathematical Problems in Engineering
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Marian J. Błachuta, Valery D. Yurkevich, Konrad Wojciechowski (1999)
Kybernetika
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In the paper the design of an aircraft motion controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem for Euler angles, where the desired decoupled output transients are accomplished under assumption of high-level, high-frequency sensor noise and incomplete information about varying parameters of the system and external disturbances. The resulting controller has a simple form of a combination of a low-order linear dynamical...
Molter, Alexandre, Da Silveira, Otávio A.Alves, Fonseca, Jun S.Ono, Bottega, Valdecir (2010)
Mathematical Problems in Engineering
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Acosta, J.Á. (2010)
Mathematical Problems in Engineering
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Przemysław Gorczyca, Krystyn Hajduk (2004)
International Journal of Applied Mathematics and Computer Science
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The tracking control problem of a strongly nonlinear MIMO system is presented. The system shares some features with a helicopter, such as important interactions between the vertical and horizontal motions. The dedicated IO board allows for control, measurements and communication with a PC. The RTWT toolbox in the MATLAB environment is used to perform real-time experiments. The control task is to track a predefined reference trajectory. A mathematical model of the system, containing experimental...
Al-Muthairi, N.F., Zribi, M. (2004)
Mathematical Problems in Engineering
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Bueno, Douglas Domingues, Marqui, Clayton Rodrigo, Santos, Rodrigo Borges, Neto, Camilo Mesquita, Lopes, Vicente (2008)
Mathematical Problems in Engineering
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Bottega, Valdecir, Molter, Alexandre, Fonseca, Jun S.O., Pergher, Rejane (2009)
Mathematical Problems in Engineering
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Yong He, Chunjuan Li, Weiguo Zhang, Jingping Shi, Yongxi Lü (2016)
Kybernetika
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In flight control of a morphing aircraft, the design objective and the dynamics may be different in its various configurations. To accommodate different performance goals in different sweep wing configurations, a novel switching strategy, mode dependent average dwell time (MDADT), is adopted to investigate the flight control of a morphing aircraft in its morphing phase. The switching signal used in this note is more general than the average dwell time (ADT), in which each mode has its...
Oto Tezak (1999)
Mathware and Soft Computing
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Knowledge based controller for a balance control model is presented in this paper. The design of the controller was based on the human control of the same process. Developed controller is tested by means of simulation and operation on the laboratory balance control model. The simulation results of the controller as well as a statistical description of the experiments with developed controller and human control is presented in the paper. Verification is based on experiments with an intelligent...
Semba, Tetsuo, Furuta, Katsuhisa (1996)
Mathematical Problems in Engineering
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