Design and Flight Testing of a Convertible Quadcopter for Maximum Flight Speed

[1]  R. Siegwart,et al.  Full Attitude Control of a VTOL tailsitter UAV , 2016, 2016 IEEE International Conference on Robotics and Automation (ICRA).

[2]  Jean-Marc Moschetta,et al.  Longitudinal study of a tilt-body vehicle: Modeling, control and stability analysis , 2015, 2015 International Conference on Unmanned Aircraft Systems (ICUAS).

[3]  Irene M. Gregory,et al.  NASA Langley Distributed Propulsion VTOL Tilt-Wing Aircraft Testing, Modeling, Simulation, Control, and Flight Test Development , 2014 .

[4]  George N. Barakos,et al.  Optimizing Rotor Blades with Approximate British Experimental Rotor Programme Tips , 2014 .

[5]  George N. Barakos,et al.  A review of helicopter rotor blade tip shapes , 2013 .

[6]  Simon Newman,et al.  Basic Helicopter Aerodynamics: Seddon/Basic Helicopter Aerodynamics , 2011 .

[7]  Peter W. Gibbens,et al.  Flight Testing of the T-Wing Tail-Sitter Unmanned Air Vehicle , 2008 .

[8]  R. H. Stone,et al.  Aerodynamic Modeling of the Wing-Propeller Interaction for a Tail-Sitter Unmanned Air Vehicle , 2008 .

[9]  R H Stone,et al.  The T-wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle , 2004 .

[10]  R Hugh Stone,et al.  Aerodynamic Modelling of a Wing-in-Slipstream Tail-Sitter UAV , 2002 .

[11]  R Hugh Stone,et al.  The T-Wing Tail-Sitter Research UAV , 2002 .

[12]  Ronald Gerdes,et al.  Lift-fan aircraft - Lessons learned from XV-5 flight experience , 1993 .

[13]  Henry Borst,et al.  The Curtiss-Wright X-19 experimental aircraft - Lessons learned , 1990 .

[14]  H. V. Borst,et al.  DESIGN AND DEVELOPMENT CONSIDERATIONS OF THE X‐19 VTOL AIRCRAFT , 1963 .