A survey of hybrid Unmanned Aerial Vehicles

Uav roundup 2013, 2013, Aero. Am., 51, 26 Drubin, 2013, Uav market worth $ 8.3 b by 2018, Microw. J., 37 Ping, 2012, Generic unmanned aerial vehicle (uav) for civilian application-a feasibility assessment and market survey on civilian application for aerial imaging, 289 2012 V-22 osprey, [Online, cited 5 December 2017] (August n.d.). URL http://www.boeing.com/defense/v-22-osprey/. Dugan, 2014, Thrust control of vtol aircraft part deux Handy, 2003, 8 Richmond, 1985, 68 U. S. N. C, 2009 Back to the drawing board: The lockheed xfv-1 salmon, [Online, cited 5 December 2017] (n.d.). URL http://www.military-history.org/articles/back-to-the-drawing-board-the-lockheed-xfv-1-salmon.htm. Ling-temco-vought xc-142a tri service, [Online, cited 5 December 2017] (n.d.). URL http://www.aviastar.org/helicopters_eng/ling_xc-142.php. Canadair cl-84 dynavert, [Online, cited 5 December 2017] (n.d.). URL http://www.aviastar.org/helicopters_eng/canadair_dynavert.php. Firefly6, [Online, cited 5 December 2017] (n.d.). URL http://www.birdseyeview.aero/products/firefly6. Introducing the xplusone, [Online, cited 5 December 2017] (n.d.). URL http://xcraft.io/. V-bat, MartinUAV[cited 5 December 2017]. URL http://martinuav.com/products-v-bat/. 2017 Vertol vz-2 (model 76), [Online, cited 5 December 2017] (n.d.). URL https://airandspace.si.edu/collection-objects/vertol-vz-2-model-76. 2017 2017 2017 2015 2017 2016 Streetly, 2013 Bell eagle eye tiltrotor uav, united states of america, [Online, cited 5 December 2017] (n.d.). URL http://www.naval-technology.com/projects/belleagleeyeuav. Yanguo, 2009, Design of flight control system for a small unmanned tilt rotor aircraft, Chin. J. Aeronaut., 22, 250, 10.1016/S1000-9361(08)60095-3 Hirschberg, 2013, Project zero: the exclusive story of agustawestlands all electric technology incubator, Verti-flite, 59, 10 Unmanned aerial vehicles (uavs), [Online, cited 5 December 2017] (n.d.). URL http://www.4frontrobotics.com/products. Papachristos, 2011, Design and experimental attitude control of an unmanned tilt-rotor aerial vehicle, 465 The eagle eye uav, [Online, cited 5 December 2017] (n.d.). URL http://www.odec.ca/projects/2004/flor4a0/public_html/v44.htm. Ozdemir, 2014, Design of a commercial hybrid vtol uav system, J. Intell. Rob. Syst., 74, 371, 10.1007/s10846-013-9900-0 Aktas, 2014, A low cost prototyping approach for design analysis and flight testing of the turac vtol uav, 1029 Vuruskan, 2014, Dynamic modeling of a fixed-wing vtol uav, 483 Carlson, 2014 2014 Quantum tron, [Online, cited 5 December 2017] (n.d.). URL http://www.quantum-systems.com/products/quantum-tron/. Dickeson, 2007, Robust lpv h gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of cg variations, 2773 Holsten, 2011, Design and wind tunnel tests of a tiltwing uav, CEAS Aero. J., 2, 69, 10.1007/s13272-011-0026-4 Ostermann, 2012, 1 Holsten, 2012, 1 W. J. Fredericks, M. D. Moore, R. C. Busan, Benefits of hybrid-electric propulsion to achieve 4x increase in cruise efficiency for a vtol aircraft. Bonn, 2016 2016 Koji Muraoka, 2009, Quad tilt wing vtol uav: aerodynamic characteristics and prototype flight 2014 Çetinsoy, 2011, Design and development of a tilt-wing uav, Turk. J. Electr. Eng. Comput. Sci., 19, 733 K. T. Öner, E. Çetinsoy, M. Ünel, M. F. Akşit, I. Kandemir, K. Gülez, Dynamic model and control of a new quadrotor unmanned aerial vehicle with tilt-wing mechanism. 2015 Öner, 2012, Mathematical modeling and vertical flight control of a tilt-wing uav, Turk. J. Electr. Eng. Comput. Sci., 20, 149 Heredia, 2012, Modeling and simulation of the hada reconfigurable uav, J. Intell. Rob. Syst., 65, 115, 10.1007/s10846-011-9561-9 Quadcruiser, an innovative hybrid aircraft concept, Airbus Group. Arcturus uav - complete unmanned aircraft systems, [Online, cited 5 December 2017] (n.d.). URL http://arcturus-uav.com/. Latitude, [Online, cited 5 December 2017] (n.d.). URL https://latitudeengineering.com/products/hq. 2014 2012 Yeo, 2009, Optimum design of a compound helicopter, J. Aircraft, 46, 1210, 10.2514/1.40101 Hada-helicopter adaptive aircraft, [Online, cited 5 December 2017] (n.d.). URL https://www.embention.com/en/projects/hada-helicopter-adaptive-aircraft/. 2013 D. R. Jenkins, T. Landis, J. Miller, American x-vehicles: An inventory x-1 to x-50 centennial of flight edition. Tayman, 2011 Pandya, 2001, Computation of external aerodynamics for a canard rotor/wing aircraft, AIAA, 997 Low, 2017, Design and dynamic analysis of a transformable hovering rotorcraft (thor), 6389 2017 2006 Flexrotor, [Online] (n.d.). URL http://aerovelco.com/flexrotor/#. Jung, 2012, Development and application of controller for transition flight of tail-sitter uav, J. Intell. Rob. Syst., 65, 137, 10.1007/s10846-011-9585-1 Aerovel flexrotor vtol uav transition flight tests, Aerovel[cited 5 December 2017]. URL https://www.youtube.com/watch?v=NP3P1Dgos-s. 2009 Kubo, 2008, Tail-sitter vertical takeoff and landing unmanned aerial vehicle: transitional flight analysis, J. Aircraft, 45, 292, 10.2514/1.30122 Maqsood, 2009, Study on aerodynamic assisted transition control technique for versatile uav, vol. 60, 2009 Jung, 2010, 305 R. G. N. Ananthkrishnan, H.C. Shim, Controlled near-hover to cruise transition using a dynamic inversion law, IDeA Research & Development, American Institute of Aeronautics and Astronautics. Omar, 2008, The development of a new vtol uav configuration for law enforcement R. Stone, G. Clarke, The t-wing: a vtol uav for defense and civilian applications, University of Sydney. Stone, 1996, Preliminary design of a tandem-wing tail-sitter uav using multi-disciplinary design optimization, 163 Stone, 2008, Flight testing of the t-wing tail-sitter unmanned air vehicle, J. Aircraft, 45, 673, 10.2514/1.32750 Fisher, 2016 Shkarayev, 2008, Aerodynamic design of micro air vehicles for vertical flight, J. Aircraft, 45, 1715, 10.2514/1.35573 Aksugur, 2010, Design methodology of a hybrid propulsion driven electric powered miniature tailsitter unmanned aerial vehicle, J. Intell. Rob. Syst., 57, 505, 10.1007/s10846-009-9368-0 D. D. Sander Hulsman, Jurjen de Groot, Atmos uav, Leonardo Times. Hochstenbach, 2015, Design and control of an unmanned aerial vehicle for autonomous parcel delivery with transition from vertical take-off to forward flight–vertikul, a quadcopter tailsitter, Int. J. Micro Air Veh., 7, 395, 10.1260/1756-8293.7.4.395 2014 2015 2013 Tara, 2012 Coxworth, 2011 Theys, 2016, A control approach for transitioning vtol uavs with continuously varying transition angle and controlled by differential thrust, 118 B. Theys, J. De Schutter, Parameter selection method and performance assessment for the preliminary design of electrically powered transitioning vtol uavs, in: Proceedings of IMAV 2016, vol. 2016, pp. 221–228. Fang, 2012, Control Strategy Design for the Transitional Mode of Tiltrotor uav, 248 Kendoul, 2005, Modeling and control of a small autonomous aircraft having two tilting rotors, 8144 Ta, 2012, Modeling and control of a tilt tri-rotor airplane, 131 Papachristos, 2012, Modeling and control simulation of an unmanned tilt tri-rotor aerial vehicle, 840 Flores, 2013, Transition flight control of the quad-tilting rotor convertible mav, 789 Abdollahi, 2010 Abras, 2010, Analysis of cfd modeling techniques over the mv-22 tiltrotor, 11 Kleinhesselink, 2007 Tekinalp, 2009, Simulation and flight control of a tilt duct uav, 10 Bhanja Chowdhury, 2012, A generalized control method for a tilt-rotor uav stabilization, 309 Flores, 2014, A nonlinear control law for hover to level flight for the quad tilt-rotor uav, vol. 19, 11055 Park, 2013, Fault tolerant flight control system for the tilt-rotor uav, J. Franklin Inst., 350, 2535, 10.1016/j.jfranklin.2013.01.014 Bhanja Chowdhury, 2012, Back-stepping control strategy for stabilization of a tilt-rotor uav, 3475 K. T. Öner, E. Çetinsoy, E. Sırımoğlu, C. Hancer, T. Ayken, M. Ünel, Lqr and smc stabilization of a new unmanned aerial vehicle. Çetinsoy, 2012, Design and construction of a novel quad tilt-wing uav, Mechatronics, 22, 723, 10.1016/j.mechatronics.2012.03.003 Ostermann, 2012, Control concept of a tiltwing uav during low speed manoeuvring Vargas-Clara, 2012, Dynamics and control of a stop rotor unmanned aerial vehicle, Int. J. Electr. Comput. Eng., 2, 597 A. V. Clara, S. Redkar, Dynamics of a vertical takeoff and landing (vtol) unmanned aerial vehicle (uav) , International Journal of Engineering Research & Innovation, 3(1). Argyle, 2013, The vertical bat tail-sitter: dynamic model and control architecture, 806 Frank, 2007 Wong, 2007, Attitude stabilization in hover flight of a mini tail-sitter uav with variable pitch propeller, 2642 VanderMey, 2011 Manouchehri, 2011, Hovering control of a ducted fan vtol unmanned aerial vehicle (uav) based on pid control, 5962 Guerrero, 2009, Robust control design based on sliding mode control for hover flight of a mini tail-sitter unmanned aerial vehicle, 2342 Knoebel, 2008, Adaptive quaternion control of a miniature tailsitter uav, 2340 Kohno, 2014, Design of Robust Controller of Fixed-wing uav for Transition Flight, 1111 S. R. Osborne, Transitions between hover and level flight for a tailsitter uav. Bilodeau, 2010, Modeling and control of a hovering mini tail-sitter, Int. J. Micro Air Veh., 2, 211, 10.1260/1756-8293.2.4.211 Casau, 2011, Autonomous transition flight for a vertical take-off and landing aircraft, 3974 Escareno, 2006, Attitude stabilization of a convertible mini birotor, 2202 Escareno, 2006, Modeling and control of a convertible vtol aircraft, 13 Escareno, 2009, Modeling and global control of the longitudinal dynamics of a coaxial convertible mini-uav in hover mode, 261 Casau, 2013, Hybrid control strategy for the autonomous transition flight of a fixed-wing aircraft, IEEE Trans. Contr. Syst. Technol., 21, 2194, 10.1109/TCST.2012.2221091 Matsumoto, 2010, A hovering control strategy for a tail-sitter vtol uav that increases stability against large disturbance, 54 Forshaw, 2014, Transitional control architecture and methodology for a twin rotor tailsitter, J. Guid. Contr. Dynam., 37, 1289, 10.2514/1.G000314 Stone, 2004, Control architecture for a tail-sitter unmanned air vehicle, vol. 2, 736 Sanchez, 2008, Autonomous hovering of a noncyclic tiltrotor uav: modeling, control and implementation, 803 Oosedo, 2010, Design and simulation of a quad rotor tail-sitter unmanned aerial vehicle, 254 Stevens, 2003 How, 2015, 529 Vepa, 2014, 333 Herisse, 2008, Hovering flight and vertical landing control of a vtol unmanned aerial vehicle using optical flow, 801 Armutcuoglu, 2004, Tilt duct vertical takeoff and landing uninhabited aerial vehicle concept design study, J. Aircraft, 41, 215, 10.2514/1.271 Okan, 2002, Flight control of a tilt-duct vtol uav Koshkouei, 2000, Adaptive backstepping control of nonlinear systems with unmatched uncertainty, vol. 5, 4765 D’Sa, 2016, Suav: Q-an improved design for a transformable solar-powered uav, 1609 Lu, 2017, Design and implementation of a gasoline-electric hybrid propulsion system for a micro triple tilt-rotor vtol uav, 433 Wang, 2017, Vision-aided tracking of a moving ground vehicle with a hybrid uav, 28 Nurimbetov, 2017, Motion planning for hybrid uavs in dense urban environments, 1627 W. Saengphet, C. Thumthae, Conceptual design of fixed wing-vtol uav for aed transport.