Global trajectory tracking control of VTOL-UAVs without linear velocity measurements, Automatica, vol.46, issue.6, pp.1053-1059, 2010. ,
DOI : 10.1016/j.automatica.2010.03.010
Nonlinear stabilization of high angle-of-attack flight dynamics using bifurcation control, American Control Conference, pp.2235-2238, 1990. ,
A History of Aerodynamics: And Its Impact on Flying Machines, 1997. ,
DOI : 10.1017/CBO9780511607158
Fundamentals of Aerodynamics, McGraw Hill Series in Aeronautical and Aerospace Engineering, 2010. ,
Aircraft Loss-of-Control Accident Analysis, AIAA Guidance, Navigation, and Control Conference, pp.1-41, 2010. ,
DOI : 10.2514/6.2010-8004
Polynomial linear quadratic gaussian and sliding mode observer for a quadrotor unmanned aerial vehicle, Journal of Robotics and Mechatronics, vol.17, issue.4, pp.483-495, 2005. ,
Output trajectory tracking for a switched nonlinear non-minimum phase system: The vstol aircraft, IEEE Intl. Conf. on Control Applications, pp.262-269, 2007. ,
Aerodynamics for engineers, 2008. ,
PERFORMANCE IMPROVEMENT OF AN ADAPTIVE CONTROLLER USING MODEL PREDICTIVE CONTROL : APPLICATION TO AN UAV MODEL, 4th IFAC Symposium on Mechatronic Systems, 2006. ,
DOI : 10.3182/20060912-3-DE-2911.00133
A control approach for gas injection in tokamak machines, Fusion Technology 27th (SOFT), 2012. ,
A control approach for gas injection in tokamak machines, Tokamak Machines Fusion Engineering and Design, 2012. ,
MARTe at FTU: The new feedback control, Fusion Engineering and Design, vol.87, issue.12, pp.1917-1920, 2012. ,
DOI : 10.1016/j.fusengdes.2012.08.006
First Steps in the FTU Migration Towards a Modular and Distributed Real-Time Control Architecture Based on MARTe, IEEE Transactions on Nuclear Science, vol.58, issue.4, pp.1778-1783, 2011. ,
DOI : 10.1109/TNS.2011.2158851
PID vs LQ control techniques applied to an indoor micro quadrotor, 2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) (IEEE Cat. No.04CH37566), pp.2451-2456, 2004. ,
DOI : 10.1109/IROS.2004.1389776
URL : http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.149.6169
Backstepping and Sliding-mode Techniques Applied to an Indoor Micro Quadrotor, Proceedings of the 2005 IEEE International Conference on Robotics and Automation, 2005. ,
DOI : 10.1109/ROBOT.2005.1570447
Dimensional analysis, Encyclopedia Britannica, vol.7, pp.439-449, 1969. ,
The role of propeller aerodynamics in the model of a quadrotor uav, European Control Conference, pp.683-688, 2009. ,
URL : https://hal.archives-ouvertes.fr/hal-00473223
The role of propeller aerodynamics in the model of a quadrotor UAV, European Control Conference, pp.683-688, 2009. ,
URL : https://hal.archives-ouvertes.fr/hal-00473223
On Physically Similar Systems; Illustrations of the Use of Dimensional Equations, Physical Review, vol.4, issue.4, pp.345-376, 1914. ,
DOI : 10.1103/PhysRev.4.345
Vertical Takeoff and Landing Aircraft, 1962. ,
DOI : 10.1038/scientificamerican0860-41
Bifurcation Analysis of Nonlinear Aircraft Dynamics, Journal of Guidance, Control, and Dynamics, vol.5, issue.5, pp.529-536, 1982. ,
DOI : 10.2514/3.56198
Hybrid Control Strategy for the Autonomous Transition Flight of a Fixed-Wing Aircraft, IEEE Transactions on Control Systems Technology, vol.21, issue.6, pp.1-18, 2012. ,
DOI : 10.1109/TCST.2012.2221091
Stabilization of a mini rotorcraft with four rotors, IEEE Control Systems Magazine, vol.25, issue.6, pp.45-55, 2005. ,
DOI : 10.1109/MCS.2005.1550152
BIFURCATION CONTROL: THEORIES, METHODS, AND APPLICATIONS, International Journal of Bifurcation and Chaos, vol.10, issue.03, pp.511-548, 2000. ,
DOI : 10.1142/S0218127400000360
Methods of Bifurcation Theory, 1996. ,
DOI : 10.1007/978-1-4613-8159-4
Design and flight testing of a gain-scheduled H/sub ???/ loop shaping controller for wide-envelope flight of a robotic helicopter, Proceedings of the 2003 American Control Conference, 2003., pp.4195-4200, 2003. ,
DOI : 10.1109/ACC.2003.1240494
Some open problems and research directions in the mathematical study of fluid dynamics, Mathematics Unlimited-2001 and Beyond, pp.353-360, 2001. ,
Aerodynamic characteristics of naca 0012 airfoil section at angles of attack from 0 to 180, 1955. ,
Continuation methods for qualitative analysis of aircraft dynamics, 2004. ,
A nonlinear controller for parabolic flight, IEEE Conf. on Decision and Control, pp.1513-1518, 1993. ,
Microgravity conditions under nonlinear inversion techniques, Microgravity Quarterly, vol.4, pp.137-145, 1995. ,
Material related to the aerodynamics of airfoils and lifting surfaces, 2004. ,
Hybrid aerial and scansorial robotics, IEEE Conf. on Robotics and Automation, pp.1-6, 2010. ,
DOI : 10.1109/robot.2010.5509397
Modeling and nonlinear control for a coaxial helicopter, IEEE International Conference on Systems, Man and Cybernetics, 2002. ,
DOI : 10.1109/ICSMC.2002.1175550
Autonomous flight and navigation of VTOL UAVs: from autonomy demonstrations to out-of-sight flights, Aerospace Science and Technology, vol.11, issue.2-3, pp.183-193, 2007. ,
DOI : 10.1016/j.ast.2006.05.005
Existence and smoothness of the Navier-Stokes equation. The ClayMathematics Institute, 2000. ,
Guidance and control of ocean vehicles, 1994. ,
Hover, Transition, and Level Flight Control Design for a Single-Propeller Indoor Airplane, AIAA Guidance, Navigation and Control Conference and Exhibit, pp.6318-6336, 2007. ,
DOI : 10.2514/6.2007-6318
URL : http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.93.6304
Trajectory tracking control design for autonomous helicopters using a backstepping algorithm, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334), pp.4102-4107, 2000. ,
DOI : 10.1109/ACC.2000.876993
Application of bifurcation methods to nonlinear flight dynamics problems, Progress in Aerospace Sciences, pp.539-586, 1997. ,
DOI : 10.1016/S0376-0421(97)00001-8
Bounded attitude control of rigid bodies: Real-time experimentation to a quadrotor mini-helicopter, Control Engineering Practice, vol.19, issue.8, pp.790-797, 2011. ,
DOI : 10.1016/j.conengprac.2011.04.004
URL : https://hal.archives-ouvertes.fr/hal-00568075
A discussion of the roll-coupling problem, Progress in Aerospace Sciences, pp.151-180, 1974. ,
DOI : 10.1016/0376-0421(74)90005-0
Dynamic modelling and configuration stabilisation for an x4-flyer, IFAC World Congress, pp.200-212, 2002. ,
DOI : 10.3182/20020721-6-es-1901.00848
DYNAMIC MODELLING AND CONFIGURATION STABILIZATION FOR AN X4-FLYER., IFAC World Congress, pp.200-212, 2002. ,
DOI : 10.3182/20020721-6-ES-1901.00848
The Wind and Beyond. A Documentary Journey into the History of Aerodynamics in America, NASA Hystory office, vol.1, 2003. ,
Nonlinear control design for slightly nonminimum phase systems: Application to V/STOL, Automatica, vol.28, pp.651-670, 1992. ,
A control approach for thrustpropelled underactuated vehicles and its application to vtol drones, IEEE Transactions on Automatic Control, vol.54, pp.1837-1853, 2009. ,
URL : https://hal.archives-ouvertes.fr/hal-00415854
Contributions to the Automatic Control of Aerial Vehicles, 2009. ,
URL : https://hal.archives-ouvertes.fr/tel-00460801
Control of thrust propelled underactuated vehicles, 2008. ,
URL : https://hal.archives-ouvertes.fr/inria-00258092
A control approach for thrust-propelled underactuated vehicles and its application to VTOL drones, IEEE Trans. on Automatic Control, issue.8, pp.541837-1853, 2009. ,
URL : https://hal.archives-ouvertes.fr/hal-00415854
Introduction to feedback control of underactuated vtol vehicles, IEEE Control Systems Magazine, vol.33, pp.61-75, 2013. ,
Aerodynamics and control of autonomous quadrotor helicopters in aggressive maneuvering, 2009 IEEE International Conference on Robotics and Automation, pp.3277-3282, 2009. ,
DOI : 10.1109/ROBOT.2009.5152561
The application of scheduled H/sub infinity / controllers to a VSTOL aircraft, IEEE Transactions on Automatic Control, vol.38, issue.7, pp.1021-1039, 1993. ,
DOI : 10.1109/9.231458
Nonlinear Control Systems, 1995. ,
Robust nonlinear motion control of a helicopter, IEEE Transactions on Automatic Control, vol.48, issue.3, pp.413-426, 2003. ,
DOI : 10.1109/TAC.2003.809147
Receding horizon control of the Caltech ducted fan: a control Lyapunov function approach, Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328), pp.51-56, 1999. ,
DOI : 10.1109/CCA.1999.806142
On the roll-coupling instabilities of high-performance aircraft, Philosophical Transactions of the Royal Society of London, vol.356, pp.2223-2239, 1745. ,
Adaptive Trajectory Control for Autonomous Helicopters, Journal of Guidance, Control, and Dynamics, vol.28, issue.3, pp.524-538, 2005. ,
DOI : 10.2514/1.6271
Modeling, control, and flight testing of a small ducted fun aircraft, AIAA Guidance, Navigation, and Control Conference and Exhibit, pp.6281-6633, 2005. ,
Modeling, Control, and Flight Testing of a Small-Ducted Fan Aircraft, Journal of Guidance, Control, and Dynamics, vol.29, issue.4, pp.769-779, 2006. ,
DOI : 10.2514/1.16380
A Fuzzy Gain-Scheduler for the Attitude Control of an Unmanned Helicopter, IEEE Transactions on Fuzzy Systems, vol.12, issue.4, pp.502-515, 2004. ,
DOI : 10.1109/TFUZZ.2004.832539
Aerodynamic characteristics of lenticular and elliptic shaped configurations at a mach number of 6, 1965. ,
Nonlinear Systems, 2003. ,
Nonlinear model predictive tracking control for rotorcraft-based unmanned aerial vehicles, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301), pp.3576-3581, 2002. ,
DOI : 10.1109/ACC.2002.1024483
Ducted Fan UAV Modeling and Simulation in Preliminary Design, AIAA Modeling and Simulation Technologies Conference and Exhibit, pp.2007-6375, 2007. ,
DOI : 10.2514/6.2007-6375
Output tracking control design of a helicopter model based on approximate linearization, Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171), pp.3635-3640, 1998. ,
DOI : 10.1109/CDC.1998.761745
Aircraft Accident Prevention: Loss-of-Control Analysis, AIAA Guidance, Navigation, and Control Conference, 2009. ,
DOI : 10.2514/6.2009-6256
Regulation of relaxed static stability aircraft, IEEE Transactions on Automatic Control, vol.36, issue.11, pp.1315-1323, 1991. ,
DOI : 10.1109/9.100946
Adaptive filtering and image based visual servo control of a ducted fan flying robot, Proceedings of the 45th IEEE Conference on Decision and Control, pp.1751-1757, 2006. ,
DOI : 10.1109/CDC.2006.376767
Robust tracking control of an underactuated quadrotor aerial-robot based on a parametric uncertain model, 2009 IEEE International Conference on Systems, Man and Cybernetics, pp.3187-3192, 2009. ,
DOI : 10.1109/ICSMC.2009.5346158
Feedback linearization vs. adaptive sliding mode control for a quadrotor helicopter, International Journal of Control, Automation and Systems, vol.3, issue.3, pp.419-428, 2009. ,
DOI : 10.1007/s12555-009-0311-8
The micro craft istar micro-air vehicle: Control system design and testing. Annual Frum of the, pp.1-11, 2001. ,
Bifurcation and continuation method Advanced Techniques for Clearance of Flight Control Laws, pp.88-106, 2002. ,
Helicopter H??? control design with robust flying quality, Aerospace Science and Technology, vol.7, issue.2, pp.159-169, 2003. ,
DOI : 10.1016/S1270-9638(02)00012-3
Historico-critical review of dimensional analysis, Journal of the Franklin Institute, vol.292, issue.6, pp.391-402, 1971. ,
DOI : 10.1016/0016-0032(71)90160-8
Hover control via an approximate lyapunov control for a model helicopter, IEEE Conf. on Decision and Control, pp.3490-3495, 1999. ,
DOI : 10.1109/cdc.1999.827874
Loop shaping H ? design applied to the robust stabilization of an helicopter, IEEE Conference on Control Applications, pp.806-811, 1992. ,
Autonomous vertical landing on an oscillating platform: an internal-model based approach, Automatica, vol.38, issue.1, pp.21-32, 2002. ,
DOI : 10.1016/S0005-1098(01)00184-4
Robust full degree-of-freedom tracking control of a helicopter, Automatica, vol.43, issue.11, pp.1909-1920, 2007. ,
DOI : 10.1016/j.automatica.2007.03.028
Aggressive control of helicopters in presence of parametric and dynamical uncertainties, Mechatronics, vol.18, issue.7, pp.381-389, 2008. ,
DOI : 10.1016/j.mechatronics.2007.10.004
Straight Up: A History of Vertical Flight, 1962. ,
A different look at output tracking: control of a vtol aircraft, Automatica, vol.32, issue.1, pp.101-107, 1996. ,
DOI : 10.1016/0005-1098(95)00099-2
Low-speed single-element airfoil synthesis, NASA/SSA Third International Symposium on the Science and Technology of Low- Speed and Motorless Right, 1979. ,
Prototypin, Modeling and control of a Class of VTOL Aerial Robots, 2008. ,
Prototyping, Modeling and Control of a Class of VTOL Aerial Robots, 2008. ,
Optimal transition maneuvers for a class of V/STOL aircraft, Automatica, vol.47, issue.5, pp.47870-879, 2011. ,
DOI : 10.1016/j.automatica.2011.01.027
Switched nonlinear control of a VSTOL aircraft, Proceedings of the 38th IEEE Conference on Decision and Control (Cat. No.99CH36304), pp.2685-2690, 1999. ,
DOI : 10.1109/CDC.1999.831335
Nonlinear Control of Underactuated Mechanical Systems with Application to Robotics and Aerospace vehicles, 2001. ,
Global configuration stabilization for the VTOL aircraft with strong input coupling, IEEE Transactions on Automatic Control, vol.47, issue.11, pp.1949-1952, 2002. ,
DOI : 10.1109/TAC.2002.804457
Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art, 45th AIAA Aerospace Sciences Meeting and Exhibit, pp.85-100, 1998. ,
DOI : 10.2514/6.2007-1051
Practical near hover flight control of a ducted fan (SLADe), Control Engineering Practice, vol.17, issue.1, pp.48-58, 2009. ,
DOI : 10.1016/j.conengprac.2008.05.004
Commande d'un minidrone a helice carenee: de la stabilisation dans le vent a la navigation autonome, 2006. ,
Commande d'un minidrone à hélice carénée: de la stabilisation dans le vent à la navigation autonome, 2006. ,
Modeling and attitude control analysis of a ducted-fan micro aerial vehicle, Control Engineering Practice, vol.18, issue.3, pp.209-218, 2010. ,
DOI : 10.1016/j.conengprac.2009.09.009
A hierarchical control strategy for the autonomous navigation of a ducted fan flying robot, Proceedings 2006 IEEE International Conference on Robotics and Automation, 2006. ICRA 2006., pp.2491-2496, 2006. ,
DOI : 10.1109/ROBOT.2006.1642076
Hovering flight stabilization in wind gusts for ducted fan UAV, 2004 43rd IEEE Conference on Decision and Control (CDC) (IEEE Cat. No.04CH37601), pp.3491-3496, 2004. ,
DOI : 10.1109/CDC.2004.1429251
Effect of steady rolling on longitudinal and directional stability, 1948. ,
Nonlinear control of underactuated vehicles with uncertain position measurements and application to visual servoing, 2012 American Control Conference (ACC), pp.3253-3259, 2012. ,
DOI : 10.1109/ACC.2012.6315115
Attitude control of rigid body dynamics from biased IMU measurements, 2007 46th IEEE Conference on Decision and Control, pp.4620-4625, 2007. ,
DOI : 10.1109/CDC.2007.4434173
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
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
Static <mml:math altimg="si10.gif" display="inline" overflow="scroll" xmlns:xocs="http://www.elsevier.com/xml/xocs/dtd" xmlns:xs="http://www.w3.org/2001/XMLSchema" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns="http://www.elsevier.com/xml/ja/dtd" xmlns:ja="http://www.elsevier.com/xml/ja/dtd" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:tb="http://www.elsevier.com/xml/common/table/dtd" xmlns:sb="http://www.elsevier.com/xml/common/struct-bib/dtd" xmlns:ce="http://www.elsevier.com/xml/common/dtd" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:cals="http://www.elsevier.com/xml/common/cals/dtd"><mml:msub><mml:mrow><mml:mi mathvariant="script">H</mml:mi></mml:mrow><mml:mrow><mml:mo>???</mml:mo></mml:mrow></mml:msub></mml:math> loop shaping control of a fly-by-wire helicopter, Automatica, vol.41, issue.9, pp.1517-1528, 2005. ,
DOI : 10.1016/j.automatica.2005.04.001
Helicopter Performance, Stability, and Control, 2005. ,
Flight dynamics and control in relation to stall, 2012 American Control Conference (ACC), pp.118-124, 2012. ,
DOI : 10.1109/ACC.2012.6315035
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
Modeling for control of symmetric aerial vehicles subjected to aerodynamic forces, p.41, 2012. ,
URL : https://hal.archives-ouvertes.fr/hal-01342414
Modeling for control of symmetric aerial vehicles subjected to aerodynamic forces, 2013. ,
URL : https://hal.archives-ouvertes.fr/hal-01342414
Adaptive Position Tracking of VTOL UAVs, IEEE Transactions on Robotics, vol.27, issue.1, pp.129-142, 2011. ,
DOI : 10.1109/TRO.2010.2092870
A method for predicting the static aerodynamic characteristics of typical missile configurations for angles of attack to 180 degrees, 1971. ,
Simple real-time stabilization of a VTOL aircraft with bounded signals, Journal of Guidance, Control, and Dynamics, issue.4, p.31, 2008. ,
URL : https://hal.archives-ouvertes.fr/hal-00449921
Vision-based autonomous landing of an unmanned aerial vehicle, Proceedings 2002 IEEE International Conference on Robotics and Automation (Cat. No.02CH37292), pp.2799-2804, 2002. ,
DOI : 10.1109/ROBOT.2002.1013656
Overview of the basic parts and control surfaces of a typical aircraft, 2002. ,
Aerodynamics of Low Reynolds Number Flyers, 2008. ,
DOI : 10.1017/CBO9780511551154
Application of bifurcation methods to nonlinear aircraft dynamics, Journal of the Aeronautical Society of India, vol.53, issue.4, pp.253-270, 2001. ,
Dimensional analysis, 2001. ,
Flight dynamics, Aircraft Engineering and Aerospace Technology, vol.77, issue.3, 2004. ,
DOI : 10.1108/aeat.2005.12777cae.002
Aircraft Control and Simulation, Aircraft Engineering and Aerospace Technology, vol.76, issue.5, 2003. ,
DOI : 10.1108/aeat.2004.12776eae.001
Control architecture for a tail-sitter unmanned air vehicle, 5th Asian Control Conference, pp.736-744, 2004. ,
DOI : 10.1007/978-3-540-33453-8_38
Synthesis and evaluation of an H2 control law for a hovering helicopter, Journal of Guidance, Control, and Dynamics, vol.16, issue.3, pp.579-584, 1993. ,
DOI : 10.2514/3.21048
Introduction to the aerodyanmics of flight, 2005. ,
Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem, IEEE Transactions on Automatic Control, vol.53, issue.6, pp.1516-1520, 2008. ,
DOI : 10.1109/TAC.2008.927789
URL : http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.215.6924
Attitude stabilization of a VTOL quadrotor aircraft, IEEE Transactions on Control Systems Technology, vol.14, issue.3, pp.562-571, 2006. ,
DOI : 10.1109/TCST.2006.872519
A switching scheme for full-envelope control of a V/STOL aircraft using LQ bumpless transfer, Proceedings of the International Conference on Control Applications, 2002. ,
DOI : 10.1109/CCA.2002.1040172
Nonlinear modelling and control of helicopters, Automatica, vol.39, issue.9, pp.1583-1596, 2003. ,
DOI : 10.1016/S0005-1098(03)00168-7
Experimental autonomous flight of a small-scaled helicopter using accurate dynamics model and low-cost sensors, IFAC World Congress, pp.14642-14650, 2008. ,
DOI : 10.3182/20080706-5-KR-1001.02480
URL : https://hal.archives-ouvertes.fr/hal-00473214
The Wind and Beyond, Journal of Applied Mechanics, vol.36, issue.1, 1967. ,
DOI : 10.1115/1.3564576
The attitude control problem, IEEE Transactions on Automatic Control, vol.36, issue.10, pp.1148-1162, 1991. ,
DOI : 10.1109/9.90228
Introduction to Applied Nonlinear Dynamical Systems and Chaos, 1990. ,
DOI : 10.1007/978-1-4757-4067-7
Global stabilization of a PVTOL aircraft model with bounded inputs, International Journal of Control, vol.76, issue.18, pp.761833-1844, 2003. ,
DOI : 10.1109/9.536496
Fluid forces on a very low Reynolds number airfoil and their prediction, International Journal of Heat and Fluid Flow, vol.32, issue.1, pp.329-339, 2011. ,
DOI : 10.1016/j.ijheatfluidflow.2010.07.008