Titlebook: EuCoMeS 2018; Proceedings of the 7 Burkhard Corves,Philippe Wenger,Mathias Hüsing Conference proceedings 2019 Springer Nature Switzerland A

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Alan D. Wilson,Havard J. Prossere mathematical model is introduced to define the dynamics of an aircraft. To inspect the performance of the controllers, the PID (Proportional-Integral-Derivative) and FLC (Fuzzy Logic Controller) is proposed for controlling the pitch angle of an aircraft. Simulation results are illustrated in the t

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Developments in Islamic Bankingories. Due to the statically indeterminate suspension, the stiffness of the payload has to be taken into account. The actuator coordinates can be algebraically calculated from the desired trajectory of the plate at the position, velocity and acceleration levels exploiting the flatness property of th

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Mechanisms and Machine Sciencehttp://image.papertrans.cn/e/image/316415.jpg