International audienceThis paper deals with the comparison of robust control approaches for the level water control of coupled tanks system. A new ultra-local model control (ULMC) approach leading to adaptive controller is proposed. The parameter identification of the ultra-local model is based on the algebraic derivation techniques. The main advantages of this control strategy are its simplicity and robustness. A comparison study with the integral sliding mode control (ISMC) approach is carried out. The perfect knowledge of the output variable degree, which is a standard assumption for sliding modes, is assumed here. The comparison of the simulation results for the proposed adaptive controller with the ISMC controller and the classical PID...
AbstractThis paper builds up an accurate nonlinear mathematical model of an electro hydraulic force/...
International audienceThe heat equation with boundary control and observation can be described by me...
Transitioning vehicles experience three different flight phases during typical missions. The hoverin...
This paper deals with the comparison of robust control approaches for the level water control of cou...
This paper deals with the design of an ultra local model control. The proposed approach is based o...
AbstractBased on nominal model, a novel global sliding mode controller (GSMC) with a new control sch...
Chen, Yipin.Thesis (M.Phil.)--Chinese University of Hong Kong, 2009.Includes bibliographical referen...
AbstractThe application of μ theory in compliant force control system is studied. A compliant force ...
International audienceThe aim of this work is to design an adaptive augmentation of an optimal basel...
AbstractA MIMO hybrid model of structural response control, which combines adaptive feedforward cont...
Dimirovski, Georgi M. (Dogus Author)A new extended adaptive backstepping algorithm for general nonli...
International audienceThe aim of this paper is to recast the heat equation with boundary control and...
This dissertation presents techniques and methodologies for system design, mathematical modeling, an...
Control architecture sizing is a main challenge for new aircraft design like blended wing-body desig...
This paper presents a new integrated procedure to tune a control law for overactuated mechanical sys...
AbstractThis paper builds up an accurate nonlinear mathematical model of an electro hydraulic force/...
International audienceThe heat equation with boundary control and observation can be described by me...
Transitioning vehicles experience three different flight phases during typical missions. The hoverin...
This paper deals with the comparison of robust control approaches for the level water control of cou...
This paper deals with the design of an ultra local model control. The proposed approach is based o...
AbstractBased on nominal model, a novel global sliding mode controller (GSMC) with a new control sch...
Chen, Yipin.Thesis (M.Phil.)--Chinese University of Hong Kong, 2009.Includes bibliographical referen...
AbstractThe application of μ theory in compliant force control system is studied. A compliant force ...
International audienceThe aim of this work is to design an adaptive augmentation of an optimal basel...
AbstractA MIMO hybrid model of structural response control, which combines adaptive feedforward cont...
Dimirovski, Georgi M. (Dogus Author)A new extended adaptive backstepping algorithm for general nonli...
International audienceThe aim of this paper is to recast the heat equation with boundary control and...
This dissertation presents techniques and methodologies for system design, mathematical modeling, an...
Control architecture sizing is a main challenge for new aircraft design like blended wing-body desig...
This paper presents a new integrated procedure to tune a control law for overactuated mechanical sys...
AbstractThis paper builds up an accurate nonlinear mathematical model of an electro hydraulic force/...
International audienceThe heat equation with boundary control and observation can be described by me...
Transitioning vehicles experience three different flight phases during typical missions. The hoverin...