A new setpoint control scheme is proposed for single-input systems, where a regulated output must be transferred between two setpoints, with the additional requirement that a set of limited outputs remain within prescribed bounds. The strategy is based on a max-min selector system frequently used in the process control and aerospace fields. The regulators used for the controlled and outputs are of the sliding mode type, where the sliding variable is defined as the difference between an output and its limit. The max and min arrangements enjoy many beneficial properties, including a separation principle allowing the independent design of the sliding regulators, with overall asymptotic stability guarantee. The paper details the stability proof...
The thesis considers the development of robust output feedback sliding mode controllers for linear t...
The paper presents the design of sliding mode control for the higher order system via reduced order ...
This paper proposes a scheme for limit protection in aero-engines with two control inputs and two re...
A new setpoint control scheme is proposed for single-input systems, where a regulated output must be...
This paper proposes a multi-regulator control scheme for single-input systems, where the setpoint of...
The problem of setpoint regulation of a main output with constraints in a set of secondary outputs i...
In this paper, robust stabilization for a class of systems with a non-linear disturbance is consider...
This thesis describes the development of robust discrete time sliding mode controllers where only ou...
This technical note introduces the design of sliding mode control algorithms for nonlinear systems i...
This technical note introduces the design of sliding mode control algorithms for nonlinear systems i...
Min–Max selector structure is widely employed in current aircraft engine control logic. And the stru...
International audienceIn this paper we consider a problem of sliding mode control design for LTI sys...
This paper generalized a new sliding mode control (SMC) without reaching phase to solve two importan...
In this paper, a method to design the reduced-order sliding-mode control is proposed for the robust ...
This Ph.D. thesis considers the development of new analysis and control techniques for special class...
The thesis considers the development of robust output feedback sliding mode controllers for linear t...
The paper presents the design of sliding mode control for the higher order system via reduced order ...
This paper proposes a scheme for limit protection in aero-engines with two control inputs and two re...
A new setpoint control scheme is proposed for single-input systems, where a regulated output must be...
This paper proposes a multi-regulator control scheme for single-input systems, where the setpoint of...
The problem of setpoint regulation of a main output with constraints in a set of secondary outputs i...
In this paper, robust stabilization for a class of systems with a non-linear disturbance is consider...
This thesis describes the development of robust discrete time sliding mode controllers where only ou...
This technical note introduces the design of sliding mode control algorithms for nonlinear systems i...
This technical note introduces the design of sliding mode control algorithms for nonlinear systems i...
Min–Max selector structure is widely employed in current aircraft engine control logic. And the stru...
International audienceIn this paper we consider a problem of sliding mode control design for LTI sys...
This paper generalized a new sliding mode control (SMC) without reaching phase to solve two importan...
In this paper, a method to design the reduced-order sliding-mode control is proposed for the robust ...
This Ph.D. thesis considers the development of new analysis and control techniques for special class...
The thesis considers the development of robust output feedback sliding mode controllers for linear t...
The paper presents the design of sliding mode control for the higher order system via reduced order ...
This paper proposes a scheme for limit protection in aero-engines with two control inputs and two re...