D. Aleksandrov and I. Penkov, Energy consumption of mini UAV helicopters with different number of rotors, 11th International Symposium "Topical Problems in the Field of Electrical and Power Engineering, pp.259-262, 2012.

C. Bhanja, A. Kulhare, A. Raina, and G. , A generalized control method for a tilt-rotor UAV stabilization, 2012 IEEE International Conference on Cyber Technology in Automation, Control, and Intelligent Systems (CYBER), pp.309-314, 2012.

A. R. Bramwell, G. T. Done, and D. Balmford, Bramwell's Helicopter Dynamics, 2001.

J. B. Brandt and M. S. Selig, Propeller Performance Data at Low Reynolds Numbers, 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011.
DOI : 10.2514/6.2011-1255

J. B. Brandt and M. S. Selig, UIUC pro- peller data site, 2012.

M. Drela, XFoil subsonic airfoil development system, 2008.

N. Guenard, Optimisation et implementation de lois de commande embarquees pour la teleoperation de micro drones aeriens "X4-flyer, 2007.

T. Hamel, R. Mahony, R. Lozano, and J. Ostrowski, DYNAMIC MODELLING AND CONFIGURATION STABILIZATION FOR AN X4-FLYER., 15th Triennial World Congress, 2002.
DOI : 10.3182/20020721-6-ES-1901.00848

G. M. Hoffmann, H. Huang, S. L. Waslander, and C. J. Tomlin, Quadrotor Helicopter Flight Dynamics and Control: Theory and Experiment, AIAA Guidance, Navigation and Control Conference and Exhibit, p.44, 2007.
DOI : 10.2514/6.2007-6461

URL : http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.77.9015

B. Moffitt, T. Bradley, D. E. Parekh, and D. Mavris, Validation of Vortex Propeller Theory for UAV Design with Uncertainty Analysis, 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008.
DOI : 10.2514/6.2008-406

R. Naldi and L. Marconi, On robust transition maneuvers for a class of tail-sitter vehicles, 49th IEEE Conference on Decision and Control (CDC), pp.358-363, 2010.
DOI : 10.1109/CDC.2010.5717170

S. Newman, Foundations of Helicopter Flight, 1994.

J. M. Pflimlin, Commande d'un minidrone à hélice carénée : De la stabilisation dans le vent à la navigation autonome, pp.LAAS-CNRS, 2006.

P. Pounds, R. Mahony, and P. Corke, Modelling and control of a large quadrotor robot, Control Engineering Practice, vol.18, issue.7, pp.691-699, 2010.
DOI : 10.1016/j.conengprac.2010.02.008

D. Pucci, Flight dynamics and control in relation to stall, 2012 American Control Conference (ACC), pp.118-124, 2012.
DOI : 10.1109/ACC.2012.6315035

D. Pucci, Toward a unified approach for the control of aerial vehicles, 2013.

D. Pucci, T. Hamel, P. Morin, and C. Samson, Nonlinear control of PVTOL vehicles subjected to drag and lift, IEEE Conference on Decision and Control and European Control Conference, pp.6177-6183, 2011.
DOI : 10.1109/CDC.2011.6160712

URL : https://hal.archives-ouvertes.fr/hal-01342420

H. Schenk, PropCalc -propeller calculator software, 2012.

W. Z. Stepniewski and C. N. Keys, Rotary-Wing Aerodynamics, 1979.

A. Appendix, . Simulated, and . Model, 15 m, ? wing(s) area ? = 0.21 m 2 , ? wing density ? 2 = 30 kg/m 3 (EEP Foam 1.9), ? mass of the wing(s), the actuated servo(s), and linkage(s ) to rotate the wing(s) m 2 = ? 2 ?(18%c) + 0.1 = 0.27 kg, ? mass of the UAV except the wing(s)