This paper presents an autonomous path-following control architecture for a tilt-wing, distributed electric propulsion, vertical take-off and landing unmanned aerial system in hover mode and presents indoor flight test results. The test-bed vehicle is a subscale model with the same configuration as the NASA GL-10 aircraft. The control architecture consists of an inner-loop attitude controller, outer-loop trajectory controller, and a trajectory generation scheme. The flight test results show that the vehicle can satisfactorily follow a path prescribed by a list of waypoints around the indoor flight room
An aerial robot is a system capable of sustained flight with no direct human control and able to per...
In this work, control techniques for the autonomous navigation and landing of an Unmanned Aerial Veh...
Unmanned Aerial Vehicles are self-piloted or remotely piloted aircrafts that have the capacity to fl...
This paper presents vehicle models and test flight results for an autonomous fixed-wing airplane tha...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...
The ability of airships to fly in hover is a major plus of this category of flying vehicles. However...
Increasing endurance is a major challenge for battery-powered aerial vehicles. A method is presented...
The purpose of this thesis is to develop fly-by-wire pilot controls for a transport category airship...
The present work describes the development of an automatic control system and the investigation of t...
A novel, tiltrotor, unmanned aerial vehicle configuration has been designed, and a preliminary dynam...
This thesis presents an approach for a vertical infrastructure inspection using a vertical take-off ...
In recent years, Vertical Take-off and Landing vehicles (VTOL) have gained popularity among research...
Path planning for small unmanned aerial vehicle (SUAV) has been researched for its high potential in...
In this study, the design and analysis of hovering controller of an UAV which is capable of doing ve...
Control of complex Vertical Take-Off and Landing (VTOL) aircraft traversing from hovering to wing bo...
An aerial robot is a system capable of sustained flight with no direct human control and able to per...
In this work, control techniques for the autonomous navigation and landing of an Unmanned Aerial Veh...
Unmanned Aerial Vehicles are self-piloted or remotely piloted aircrafts that have the capacity to fl...
This paper presents vehicle models and test flight results for an autonomous fixed-wing airplane tha...
The article of record as published may be located at http://dx.doi.org/10.2514/1.42056The paper pres...
The ability of airships to fly in hover is a major plus of this category of flying vehicles. However...
Increasing endurance is a major challenge for battery-powered aerial vehicles. A method is presented...
The purpose of this thesis is to develop fly-by-wire pilot controls for a transport category airship...
The present work describes the development of an automatic control system and the investigation of t...
A novel, tiltrotor, unmanned aerial vehicle configuration has been designed, and a preliminary dynam...
This thesis presents an approach for a vertical infrastructure inspection using a vertical take-off ...
In recent years, Vertical Take-off and Landing vehicles (VTOL) have gained popularity among research...
Path planning for small unmanned aerial vehicle (SUAV) has been researched for its high potential in...
In this study, the design and analysis of hovering controller of an UAV which is capable of doing ve...
Control of complex Vertical Take-Off and Landing (VTOL) aircraft traversing from hovering to wing bo...
An aerial robot is a system capable of sustained flight with no direct human control and able to per...
In this work, control techniques for the autonomous navigation and landing of an Unmanned Aerial Veh...
Unmanned Aerial Vehicles are self-piloted or remotely piloted aircrafts that have the capacity to fl...