Add to ORKGIn this work, we provide details of the control design of a morphing UAV capable of variable wing sweep. This morphing capability is assumed to be superimposed on a GENMAV (Generic Micro Air Vehicle) configuration originally developed by the Air Force Research Laboratory (AFRL). The nonlinear aerodynamic model for this aircraft is obtained using the Athena-Vortex Lattice (AVL) method with a quasi-steady state assumption
Click on the IEEE link to access the article (may not be free)Aeroelastic wing micro aerial vehicle ...
The variable sweep morphing technology integrated on the newly designed unmanned aerial vehicle (UAV...
Thesis (Ph.D.)-- Wichita State University, College of Engineering, Dept. of Aerospace EngineeringThe...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace EngineeringThis ...
A morphing aircraft can adapt its configuration to suit different types of tasks, which is also an i...
Thesis (Master's)--University of Washington, 2012Air vehicle design is a study in compromises. Airc...
This paper reviews the various control algorithms and strategies used for fixed-wing morphing aircra...
Morphing wings have the potential to optimize UAV performance for a variety of flight conditions and...
This paper investigates the problems of modeling and control of the morphing aircraft. Henceforth, a...
In the present paper the initial review of morphing design methodologies is discussed and forms part...
Morphing aircraft are the flight vehicles that can reconfigure their shape during the flight in orde...
Morphing wings are the subject of intensive research interest today due to their potential to imp...
Morphing winglets are innovative aircraft devices capable to adaptively enhance aircraft lift distri...
This work develops a morphing decision strategy to optimize the cruising efficiency for a variable-s...
The morphing of an air vehicle is to change its shape and size substantially during flight. Thus, th...
Click on the IEEE link to access the article (may not be free)Aeroelastic wing micro aerial vehicle ...
The variable sweep morphing technology integrated on the newly designed unmanned aerial vehicle (UAV...
Thesis (Ph.D.)-- Wichita State University, College of Engineering, Dept. of Aerospace EngineeringThe...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace EngineeringThis ...
A morphing aircraft can adapt its configuration to suit different types of tasks, which is also an i...
Thesis (Master's)--University of Washington, 2012Air vehicle design is a study in compromises. Airc...
This paper reviews the various control algorithms and strategies used for fixed-wing morphing aircra...
Morphing wings have the potential to optimize UAV performance for a variety of flight conditions and...
This paper investigates the problems of modeling and control of the morphing aircraft. Henceforth, a...
In the present paper the initial review of morphing design methodologies is discussed and forms part...
Morphing aircraft are the flight vehicles that can reconfigure their shape during the flight in orde...
Morphing wings are the subject of intensive research interest today due to their potential to imp...
Morphing winglets are innovative aircraft devices capable to adaptively enhance aircraft lift distri...
This work develops a morphing decision strategy to optimize the cruising efficiency for a variable-s...
The morphing of an air vehicle is to change its shape and size substantially during flight. Thus, th...
Click on the IEEE link to access the article (may not be free)Aeroelastic wing micro aerial vehicle ...
The variable sweep morphing technology integrated on the newly designed unmanned aerial vehicle (UAV...
Thesis (Ph.D.)-- Wichita State University, College of Engineering, Dept. of Aerospace EngineeringThe...