The NederDrone: A hybrid lift, hybrid energy hydrogen UAV

A lot of UAV applications require vertical take-off and landing (VTOL) combined with very long-range or endurance. Transitioning UAVs have been proposed to combine the VTOL capabilities of helicopters with the efficient long-range flight properties of fixed-wing aircraft. But energy is still a bottleneck for many electric long endurance applications. While solar power technology and battery technology have improved a lot, in rougher conditions they still respectively lack the power or total amount of energy required for many real-world situations. In this paper, we introduce the NederDrone, a hybrid lift, hybrid energy hydrogen-powered UAV which can perform vertical take-off and landings using 12 propellers while flying efficiently in forward flight thanks to its fixed wings. The energy is supplied from a mix of hydrogen-driven fuel-cells to store large amounts of energy and battery power for high power situations. The hydrogen is stored in a pressurized cylinder around which the UAV is optimized. This paper analyses the selection of the concept, the implemented safety elements, the electronics and flight control and shows flight data including a 3h38 flight at sea, starting and landing on a small moving ship.

[1]  Marco Klaus Furrutter,et al.  Small fuel cell powering an unmanned aerial vehicle , 2009, AFRICON 2009.

[2]  Dieter Moormann,et al.  Control of Departure and Approach Maneuvers of Tiltwing VTOL Aircraft , 2017 .

[3]  Mohamed Gadalla,et al.  Analysis of a hydrogen fuel cell-PV power system for small UAV , 2016 .

[4]  Gonzalo Pajares,et al.  Overview and Current Status of Remote Sensing Applications Based on Unmanned Aerial Vehicles (UAVs) , 2015 .

[5]  A Long Range Fuel Cell/Soaring UAV System for Crossing the Atlantic Ocean , 2019 .

[6]  E. Troncoso,et al.  Off-grid test results of a solar-powered hydrogen refuelling station for fuel cell powered Unmanned Aerial Vehicles , 2014 .

[7]  L. Vermeer,et al.  A review of wind turbine wake research at TU Delft , 2001 .

[8]  Dries Verstraete,et al.  Fuel cell propulsion in small fixed-wing unmanned aerial vehicles: Current status and research needs , 2017 .

[9]  T. Hikmet Karakoc,et al.  Evaluation of design methodology, limitations, and iterations of a hydrogen fuelled hybrid fuel cell mini UAV , 2020 .

[10]  Joris De Schutter,et al.  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 , 2015 .

[11]  Vladimir Molkov,et al.  BLAST WAVE FROM A HIGH-PRESSURE GAS TANK RUPTURE IN A FIRE: STAND-ALONE AND UNDER-VEHICLE HYDROGEN TANKS , 2015 .

[12]  Guido C. H. E. de Croon,et al.  Adaptive Incremental Nonlinear Dynamic Inversion for Attitude Control of Micro Air Vehicles , 2016 .

[13]  Suk Woo Nam,et al.  Humidification of polymer electrolyte membrane fuel cell using short circuit control for unmanned aerial vehicle applications , 2014 .

[14]  N. Lapeña-Rey,et al.  A fuel cell powered unmanned aerial vehicle for low altitude surveillance missions , 2017 .

[15]  M. Molnarne,et al.  Hazardous properties of hydrogen and hydrogen containing fuel gases , 2019, Process Safety and Environmental Protection.

[16]  Sejin Kwon,et al.  Fuel cell system with sodium borohydride as hydrogen source for unmanned aerial vehicles , 2011 .

[17]  Seth B. Anderson,et al.  Historical Overview of V/STOL Aircraft Technology , 1997 .

[18]  R. Metkemeijer,et al.  PEMFC application for aviation: Experimental and numerical study of sensitivity to altitude , 2012 .

[19]  Wai Yee Yeong,et al.  Additive manufacturing in unmanned aerial vehicles (UAVs): Challenges and potential , 2017 .

[20]  Ib Chorkendorff,et al.  Toward sustainable fuel cells , 2016, Science.

[21]  Ahmad Bani Younes,et al.  A survey of hybrid Unmanned Aerial Vehicles , 2018 .

[22]  Ben M. Chen,et al.  Autonomous reconfigurable hybrid tail-sitter UAV U-Lion , 2017, Science China Information Sciences.

[23]  Erdal Kayacan,et al.  Unsteady aerodynamic modeling and control of pusher and tilt-rotor quadplane configurations , 2019, Aerospace Science and Technology.

[24]  Antoine Drouin,et al.  The Paparazzi Solution , 2006 .

[25]  J. A. Sparks,et al.  Low cost technologies for aerospace applications , 1997, Microprocess. Microsystems.

[26]  Maxime Bertin,et al.  One year OSIRHYS IV project synthesis: mechanical behaviour of 700 bar type iv high pressure vessel code qualification. , 2012 .

[27]  Maj Mirmirani,et al.  Development of a Small Long Endurance Hybrid PEM Fuel Cell Powered UAV , 2007 .

[28]  Sejin Kwon,et al.  Design and development of a fuel cell-powered small unmanned aircraft , 2012 .

[29]  A. Preumont Vibration Control of Active Structures , 1997 .

[30]  Rogelio Lozano,et al.  Quad-Tilting Rotor Convertible MAV: Modeling and Real-Time Hover Flight Control , 2012, J. Intell. Robotic Syst..

[31]  Balazs Gati,et al.  Open source autopilot for academic research - The Paparazzi system , 2013, 2013 American Control Conference.

[32]  Taegyu Kim,et al.  NaBH4 (sodium borohydride) hydrogen generator with a volume-exchange fuel tank for small unmanned aerial vehicles powered by a PEM (proton exchange membrane) fuel cell , 2014 .

[33]  Stuart H. Zweben,et al.  Evaluation of design methodologies , 1982, SOEN.

[34]  Kevin van Hecke,et al.  Design, control, and visual navigation of the DelftaCopter VTOL tail‐sitter UAV , 2017, J. Field Robotics.

[35]  Michael Rottmayer,et al.  Fuel Cell Hybrid Power System Development for Extended Endurance SUAS Applications , 2011 .

[36]  Dimitri N. Mavris,et al.  Flight Test Results for a Fuel Cell Unmanned Aerial Vehicle , 2007 .

[37]  Andreas Züttel,et al.  Hydrogen storage methods , 2004, Naturwissenschaften.

[38]  Louis V. Schmidt,et al.  Introduction to Aircraft Flight Dynamics , 1998 .

[39]  Yancheng You,et al.  Current technologies and challenges of applying fuel cell hybrid propulsion systems in unmanned aerial vehicles , 2020 .

[40]  Mohamed El-Sharkawy,et al.  Integration of UAVs with Real Time Operating Systems using UAVCAN , 2019, 2019 IEEE 10th Annual Ubiquitous Computing, Electronics & Mobile Communication Conference (UEMCON).

[41]  Zhefei Pan,et al.  Recent advances in fuel cells based propulsion systems for unmanned aerial vehicles , 2019, Applied Energy.

[42]  Mohamed Benbouzid,et al.  A critical review on unmanned aerial vehicles power supply and energy management: Solutions, strategies, and prospects , 2019 .

[43]  B. D. W. Remes,et al.  Design and Testing of a Vertical Take-Off and Landing UAV Optimized for Carrying a Hydrogen Fuel Cell with a Pressure Tank , 2020, Unmanned Syst..

[44]  B. Kang,et al.  Weight optimization of hydrogen storage vessels for quadcopter UAV using genetic algorithm , 2020 .

[45]  Qiping Chu,et al.  Cascaded incremental nonlinear dynamic inversion for MAV disturbance rejection , 2018 .