Add to ORKGThe problem of optimal state feedback controller design in terms of quadratic performance index is considered. The problem is formulated in the form of linear matrix inequalities (LMIs). The obtained solution guarantees stabilization of the aircraft during flight mission. During flight envelope the aircraft is subjected to the external stochastic disturbances. The efficiency of the proposed approach is illustrated by a case study of airplane longitudinal motion
Bibliography: leaf 27.NASA Grant NGL-22-009-124 and Grant AF-AFosr-72-2273.by Poh Kam Wong, Michael ...
International audienceThe problem of a state feedback design for control of a quadrotor system under...
In the last years, several control theories have been widely developed. They are generally applied t...
The problem of optimal state feedback controller design in terms of quadratic performance ind...
This study addresses the problem of designing a guaranteed cost controller for non-linear discrete q...
A set of guidance control laws is developed for application to a reduced order dynamic aircraft mode...
The automation of the operation of aircraft equipment lightens and diminishes the manipulation of th...
This paper presents the robust control design for aircraft autopilot. The controller provides a maxi...
This article proposes a modal approach to the synthesis of robust systems for optimal stabilization ...
A control system design approach for optimal stability augmentation, systems, using limited state fe...
This paper proposes a state feedback controller for the attitude stabilization problem of quadrotors...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
The paper presents an alternative approach of observer-based flight control system design. This ap...
The purpose of this paper is to provide a practical example to the Linear Quadratic Gaussian (LQG) c...
The standard results of linearised optimal control theory are explored and examined to see how they ...
Bibliography: leaf 27.NASA Grant NGL-22-009-124 and Grant AF-AFosr-72-2273.by Poh Kam Wong, Michael ...
International audienceThe problem of a state feedback design for control of a quadrotor system under...
In the last years, several control theories have been widely developed. They are generally applied t...
The problem of optimal state feedback controller design in terms of quadratic performance ind...
This study addresses the problem of designing a guaranteed cost controller for non-linear discrete q...
A set of guidance control laws is developed for application to a reduced order dynamic aircraft mode...
The automation of the operation of aircraft equipment lightens and diminishes the manipulation of th...
This paper presents the robust control design for aircraft autopilot. The controller provides a maxi...
This article proposes a modal approach to the synthesis of robust systems for optimal stabilization ...
A control system design approach for optimal stability augmentation, systems, using limited state fe...
This paper proposes a state feedback controller for the attitude stabilization problem of quadrotors...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
The paper presents an alternative approach of observer-based flight control system design. This ap...
The purpose of this paper is to provide a practical example to the Linear Quadratic Gaussian (LQG) c...
The standard results of linearised optimal control theory are explored and examined to see how they ...
Bibliography: leaf 27.NASA Grant NGL-22-009-124 and Grant AF-AFosr-72-2273.by Poh Kam Wong, Michael ...
International audienceThe problem of a state feedback design for control of a quadrotor system under...
In the last years, several control theories have been widely developed. They are generally applied t...