In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substantially in terms of control stabilization and navigation strategies. However, the energy available on board is finite and this is a limiting factor that prevents engineers from coming up with the best aerial solution in many situations. In this paper the path following control of a helicopter UAV based on the kinematic model is proposed using a feedback linearization technique. The helicopter speed is adjusted according to direction changes of the desired path. Thus, the aircraft should holds its own weight in the air for the shortest possible time, aiming to save energy without neglecting the position control errors which can accumulate when it...
The trajectory control problem, defined as making a vehicle follow a pre-established path in space, ...
International audienceThis paper addresses the problem of time optimal path planning for a quadrotor...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...
A substantial interest in aerial robots has grown in recent years. However, the energetic cost of fl...
This paper considers the path following of unmanned helicopters based on dynamic optimization. We as...
This paper develops a trajectory tracking control design algorithm to be applied in unmanned aerial ...
This paper presents an optimization-based approach to let an unmanned helicopter follow a geometrica...
This paper presents an optimization-based approach to let an unmanned helicopter follow a geometrica...
There has been a great deal of interest in the dynamics and control of unmanned helicopter robots si...
Abstract — A path following controller is presented for a quadrotor helicopter model. The controller...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
This paper addresses the problem of energy-optimal waypoint-following guidance for an Unmanned Aeria...
This work proposes a kinematic nonlinear controller for an autonomous miniature helicopter that gene...
International audiencePath following is a basic autonomous navigation capability for UAV’s and in th...
The trajectory control problem, defined as making a vehicle follow a pre-established path in space, ...
International audienceThis paper addresses the problem of time optimal path planning for a quadrotor...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...
A substantial interest in aerial robots has grown in recent years. However, the energetic cost of fl...
This paper considers the path following of unmanned helicopters based on dynamic optimization. We as...
This paper develops a trajectory tracking control design algorithm to be applied in unmanned aerial ...
This paper presents an optimization-based approach to let an unmanned helicopter follow a geometrica...
This paper presents an optimization-based approach to let an unmanned helicopter follow a geometrica...
There has been a great deal of interest in the dynamics and control of unmanned helicopter robots si...
Abstract — A path following controller is presented for a quadrotor helicopter model. The controller...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
This paper addresses the problem of energy-optimal waypoint-following guidance for an Unmanned Aeria...
This work proposes a kinematic nonlinear controller for an autonomous miniature helicopter that gene...
International audiencePath following is a basic autonomous navigation capability for UAV’s and in th...
The trajectory control problem, defined as making a vehicle follow a pre-established path in space, ...
International audienceThis paper addresses the problem of time optimal path planning for a quadrotor...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...