Abstract: In this paper a Lyapunov control algorithm for a tandem rotor helicopter is obtained using backstepping techniques. A simple model dynamics for a behavior of a helicopter close to hover is obtained. Some simulation results are presented to illustrate the performance of such controller
International audienceThis paper proposes a design of a direct optimal control for a class of multi-...
Quadrotors have generated considerable interest in both the control community due to their simple dy...
International audienceThis paper presents the study of stabilization with motion planning of two mod...
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
This paper considers two-input, two-output nonlinear adaptive model following control of a 3-DOF (de...
This thesis is concerned with robust control theory and its application to the autonomous flight con...
Abstract- This paper considered the problem of stabilization of longitudinal and lateral dynamics of...
A helicopter is a highly nonlinear system. Its mathematical model is difficult to establish accurate...
ii This thesis investigates the use of an integrator backstepping controller for a standard helicopt...
AbstractIn this article, a nonlinear model of an underactuated six degrees of freedom (6 DOF) quadro...
In this paper, a novel nonlinear control strategy along with its simulation for a quadrotor helicopt...
This thesis investigates the use of an integrator backstepping controller for a standard helicopter....
ln this article the sliding mode controller is applied for a small unmanned helicopter called quadro...
The paper considers the problem of synthesizing a control law that stabilizes the spatial position o...
International audienceThis paper proposes a design of a direct optimal control for a class of multi-...
Quadrotors have generated considerable interest in both the control community due to their simple dy...
International audienceThis paper presents the study of stabilization with motion planning of two mod...
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
This paper considers two-input, two-output nonlinear adaptive model following control of a 3-DOF (de...
This thesis is concerned with robust control theory and its application to the autonomous flight con...
Abstract- This paper considered the problem of stabilization of longitudinal and lateral dynamics of...
A helicopter is a highly nonlinear system. Its mathematical model is difficult to establish accurate...
ii This thesis investigates the use of an integrator backstepping controller for a standard helicopt...
AbstractIn this article, a nonlinear model of an underactuated six degrees of freedom (6 DOF) quadro...
In this paper, a novel nonlinear control strategy along with its simulation for a quadrotor helicopt...
This thesis investigates the use of an integrator backstepping controller for a standard helicopter....
ln this article the sliding mode controller is applied for a small unmanned helicopter called quadro...
The paper considers the problem of synthesizing a control law that stabilizes the spatial position o...
International audienceThis paper proposes a design of a direct optimal control for a class of multi-...
Quadrotors have generated considerable interest in both the control community due to their simple dy...
International audienceThis paper presents the study of stabilization with motion planning of two mod...