This article investigates the control of a two-dimensional aeroelastic system with a torsional stiffness nonlinearity. The dynamics are transformed into a Linear Fractional Representation (LFR) such that the airspeed nonlinearity acts as a gain feedback to the nominal system. A controller in LFR, which allows it to schedule with airspeed, is then synthesised using Linear Matrix Inequalities (LMIs). The performance objectives of the controller are the minimisation of the H2 norm from a gust input to the pitch and plunge outputs, and the minimisation of an H1 norm that corresponds to the systematic method of H1 loop-shaping. This method has a rigorous mathematical background that allows upper limits on these criteria to be established. The no...
The design and assessment of a two degree of freedom gust load alleviation control system for a busi...
The paper presents the design of a symmetric, active, gust load alleviation system for a regional tr...
This paper demonstrates the implementation of an adaptive feedforward controller to reduce structura...
The development of a control system for the suppression of aeroelastic vibration of a two-dimensiona...
This paper deals with mixed H2infinty H1 state feedback control applied to mechanical systems. The H...
The development of an adaptive control system for the control of an uncertain aeroelastic system, in...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Two linear parameter-varying gain-scheduled controllers for active utter suppression of the NASA La...
The dynamic responses to aeroelastic gusts/manoeuvres play an important partacross much of the desig...
Systems which vary significantly over an operating envelope, such as fighter aircraft, generally can...
For flexible aircraft, it is often required to control individual aeroelastic modes which are lightl...
This paper describes a framework for an active control technique applied to gust load alleviation (G...
Traditional methods for gust alleviation of aircraft are mostly proposed based on a specific flight ...
A lateral flight control design for a flexible aircraft is presented. It is based on a standard two-...
The design and assessment of a two degree of freedom gust load alleviation control system for a busi...
The paper presents the design of a symmetric, active, gust load alleviation system for a regional tr...
This paper demonstrates the implementation of an adaptive feedforward controller to reduce structura...
The development of a control system for the suppression of aeroelastic vibration of a two-dimensiona...
This paper deals with mixed H2infinty H1 state feedback control applied to mechanical systems. The H...
The development of an adaptive control system for the control of an uncertain aeroelastic system, in...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Two linear parameter-varying gain-scheduled controllers for active utter suppression of the NASA La...
The dynamic responses to aeroelastic gusts/manoeuvres play an important partacross much of the desig...
Systems which vary significantly over an operating envelope, such as fighter aircraft, generally can...
For flexible aircraft, it is often required to control individual aeroelastic modes which are lightl...
This paper describes a framework for an active control technique applied to gust load alleviation (G...
Traditional methods for gust alleviation of aircraft are mostly proposed based on a specific flight ...
A lateral flight control design for a flexible aircraft is presented. It is based on a standard two-...
The design and assessment of a two degree of freedom gust load alleviation control system for a busi...
The paper presents the design of a symmetric, active, gust load alleviation system for a regional tr...
This paper demonstrates the implementation of an adaptive feedforward controller to reduce structura...