Add to ORKGInternational audienceThis paper presents recent advances in the project: development of a convertible unmanned aerial vehicle (UAV). This aircraft is able to change its flight configuration from hover to level flight and vice versa by means of a transition maneuver, while maintaining the aircraft in flight. For this purpose a nonlinear control strategy based on Lyapunov design is given. Numerical results are presented showing the effectiveness of the proposed approach
The last decade has seen significant advances in the development of Vertical takeoff and landing (VT...
With the goal of extending capabilities of multi-rotor unmanned aerial vehicles (UAVs) for wetland c...
The objective of this work was to develop a variety of control systems for a Stop-Rotor Unmanned Aer...
International audience— This paper presents a particular class of a convertible micro aerial vehicle...
A novel, tiltrotor, unmanned aerial vehicle configuration has been designed, and a preliminary dynam...
This paper presents the control system design process of a novel tilt-rotor unmanned aerial vehicle ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
We present our ongoing work on the development of a new quadrotor aerial vehicle which has a tilt-wi...
This paper concentrates on the flight control of a novel tiltrotor aircraft with fixed wings. This k...
International audienceIn this paper a nonlinear suboptimal stabilizing control strategy based on Con...
This paper describes the design method of a flight control system of a Quad Tilt-Wing (QTW) Unmanned...
The design of Flight Control Systems for tilt-rotor UAVs can be challenging for the management of th...
Quadcopter unmanned aerial vehicles continue to play important roles in several applications and the...
Abstract — We present our ongoing work on the development of a new quadrotor aerial vehicle which ha...
The last decade has seen significant advances in the development of Vertical takeoff and landing (VT...
With the goal of extending capabilities of multi-rotor unmanned aerial vehicles (UAVs) for wetland c...
The objective of this work was to develop a variety of control systems for a Stop-Rotor Unmanned Aer...
International audience— This paper presents a particular class of a convertible micro aerial vehicle...
A novel, tiltrotor, unmanned aerial vehicle configuration has been designed, and a preliminary dynam...
This paper presents the control system design process of a novel tilt-rotor unmanned aerial vehicle ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
A flight control system for a tilt rotor UAV has been synthesized based on an incremental nonlinear ...
We present our ongoing work on the development of a new quadrotor aerial vehicle which has a tilt-wi...
This paper concentrates on the flight control of a novel tiltrotor aircraft with fixed wings. This k...
International audienceIn this paper a nonlinear suboptimal stabilizing control strategy based on Con...
This paper describes the design method of a flight control system of a Quad Tilt-Wing (QTW) Unmanned...
The design of Flight Control Systems for tilt-rotor UAVs can be challenging for the management of th...
Quadcopter unmanned aerial vehicles continue to play important roles in several applications and the...
Abstract — We present our ongoing work on the development of a new quadrotor aerial vehicle which ha...
The last decade has seen significant advances in the development of Vertical takeoff and landing (VT...
With the goal of extending capabilities of multi-rotor unmanned aerial vehicles (UAVs) for wetland c...
The objective of this work was to develop a variety of control systems for a Stop-Rotor Unmanned Aer...