نتایج جستجو برای: active controller

تعداد نتایج: 498682  

2006
Laetitia Chapel Guillaume Deffuant

We use support vector machines (SVMs) to compute the actions which maintain a dynamical system within a defined subset of its state space. The principles of our method are inspired by the viability theory. We use SVMs to approximate the viability kernel which is the set of states from which it is possible to maintain the system. The actions to perform on the system can then be easily computed f...

Journal: :journal of optimization in industrial engineering 2015
ahmad fakharian amir abbasi

in this paper, a state feedback h¥ controller is proposed in order to design an active queue management (aqm) system based on congestion control algorithm for networks supporting tcp protocols. in this approach, the available link bandwidth is modeled as a time-variant disturbance. the purpose of this paper is to design a controller which is capable of achieving the queue size and can guarantee...

Journal: :International Journal of u- and e-Service, Science and Technology 2015

2014
Sushil Karvekar Swapnil Patil

In this paper control of Goertzel Algorithm based shunt active power filter with sliding mode controller is considered. Shunt active power filter involves harmonics mitigation due to three phase non linear loads under balanced and unbalanced load conditions. The sliding mode controller is used to regulate voltage of the capacitor used in inverter. The sliding mode controller improves the dynami...

Journal: :The Journal of the Acoustical Society of America 1986

Journal: :TNU Journal of Science and Technology 2020

In this article, the issue of attitude control and active vibration suppression of a nonlinear flexible spacecraft is assessed through piezoelectric patches as actuator and sensors. Two controller loops are applied: the inner loop, to make the panel vibration damped through piezoelectric patches; and the outer loop, to perform spacecraft maneuver using the reaction wheel acting on the hub. An o...

This paper deals with the study and comparison of passive and active landing gear system of  the aircraft and dynamic responses due to runway irregularities while the aircraft is taxying. The dynamic load and vibration caused by the unevenness of runway will result in airframe fatigue, discomfort of passengers and the reduction of the pilot’s ability to control the aircraft. One of the objectiv...

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