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Статті в журналах з теми "Modelling electric aircraft"
Booker, Julian, Caius Patel, and Phillip Mellor. "Modelling Green VTOL Concept Designs for Reliability and Efficiency." Designs 5, no. 4 (October 28, 2021): 68. http://dx.doi.org/10.3390/designs5040068.
Повний текст джерелаFrosina, Emma, Carmine Caputo, Gianluca Marinaro, Adolfo Senatore, Ciro Pascarella, and Giuseppe Di Lorenzo. "Modelling of a Hybrid-Electric Light Aircraft." Energy Procedia 126 (September 2017): 1155–62. http://dx.doi.org/10.1016/j.egypro.2017.08.315.
Повний текст джерелаThirukumaran, Sanmugasundaram, Paul Ratnamahilan Polycarp Hoole, Harikrishnan Ramiah, Jeevan Kanesan, Kandasamy Pirapaharan, and Samuel Ratnajeevan Herbert Hoole. "A new electric dipole model for lightning-aircraft electrodynamics." COMPEL: The International Journal for Computation and Mathematics in Electrical and Electronic Engineering 33, no. 1/2 (December 20, 2013): 540–55. http://dx.doi.org/10.1108/compel-12-2012-0385.
Повний текст джерелаVankan, Jos, and Wim Lammen. "Parallel hybrid electric propulsion architecture for single aisle aircraft - powertrain investigation." MATEC Web of Conferences 304 (2019): 03008. http://dx.doi.org/10.1051/matecconf/201930403008.
Повний текст джерелаKhairuddin, Ismail Mohd, Anwar P. P. A. Majeed, Ann Lim, Jessnor Arif M. Jizat, and Abdul Aziz Jaafar. "Modelling and PID Control of a Quadrotor Aerial Robot." Advanced Materials Research 903 (February 2014): 327–31. http://dx.doi.org/10.4028/www.scientific.net/amr.903.327.
Повний текст джерелаHu, Josin, and Julian Booker. "Preliminary Sizing of Electric-Propulsion Powertrains for Concept Aircraft Designs." Designs 6, no. 5 (October 13, 2022): 94. http://dx.doi.org/10.3390/designs6050094.
Повний текст джерелаLoong, Ling Jin, Chockalingam Aravind Vaithilingam, Gowthamraj Rajendran, and Venkatkumar Muneeswaran. "Modelling and analysis of vienna rectifier for more electric aircraft applications using wide band-gap materials." Journal of Physics: Conference Series 2120, no. 1 (December 1, 2021): 012027. http://dx.doi.org/10.1088/1742-6596/2120/1/012027.
Повний текст джерелаDoctor, Faiyaz, Thomas Budd, Paul D. Williams, Matt Prescott, and Rahat Iqbal. "Modelling the effect of electric aircraft on airport operations and infrastructure." Technological Forecasting and Social Change 177 (April 2022): 121553. http://dx.doi.org/10.1016/j.techfore.2022.121553.
Повний текст джерелаMemmolo, V., F. Orefice, F. Nicolosi, and F. Ricci. "Design of near-zero emission aircraft based on refined aerodynamic model and structural analysis." IOP Conference Series: Materials Science and Engineering 1226, no. 1 (February 1, 2022): 012067. http://dx.doi.org/10.1088/1757-899x/1226/1/012067.
Повний текст джерелаKhan, YM, A. Rolando, F. Salucci, CED Riboldi, and L. Trainelli. "Hybrid-electric and hydrogen powertrain modelling for airplane performance analysis and sizing." IOP Conference Series: Materials Science and Engineering 1226, no. 1 (February 1, 2022): 012071. http://dx.doi.org/10.1088/1757-899x/1226/1/012071.
Повний текст джерелаДисертації з теми "Modelling electric aircraft"
Groch, Matthew. "HV Transmission line and tower inspection safe-fly zone modelling and metrology." Thesis, Stellenbosch : Stellenbosch University, 2013. http://hdl.handle.net/10019.1/85795.
Повний текст джерелаENGLISH ABSTRACT: The deployment of Unmanned Aerial Vehicles (UAV) for power line inspection requires the definition of safe-fly zones. Transient Over-Voltages (TOVs) on the Overhead Transmission Lines (OHTLs) put the UAV at risk if it encroaches on these zones. In order to determine the safe-fly zones of a UAV in the vicinity of OHTLs, realistic full-scale experimental tests are done. Non-linearity in breakdown effects renders small-scale testing and computational work inaccurate. Experimental work is used to describe the close-up approach distances for worst-case scenarios. Testing cannot provide a full solution due to the limitation of the equipment available. Further tests must therefore be done at a specialised facility. Experiments are run in two phases, namely non-linear and linear tests in the High Voltage (HV) laboratory. The non-linear tests are done to derive Minimum Approach Distances (MAD). The linear experiments are used to calibrate FEKO, the simulation tool, to the measurement environment. Once correlation between the linear test data and the simulated data is found, confidence is derived in both the simulation model and the test setup. The simulations can then be used to determine a geometric factor as an input into F. Rizk’s prediction equations. The Rizk equations are used to describe the safe-fly zones alongside OHTLs as an addition to the non-linear experimental work. Along with the standard’s suggestions, the Rizk predictions are formulated in such a way that line-specific solutions can be determined. The suggested clearance values are provided in terms of per unit values, which can be selected in accordance with historical line data. Power line sparking is investigated to better understand the line radiation phenomenon. This understanding could assist in the line inspection process, as well as in the layout of power lines near radio quiet areas. Knowledge of OHTL radiation patterns can aid in the location of corona and sparking sources in the inspection process. Aerial sparking measurements are taken using a UAV carrying a spectrum analyser. Measured sparking levels are used to verify a Computational Electromagnetic (CEM) model. The CEM model can then be used to further investigate OHTL radiation characteristics.
AFRIKAANSE OPSOMMING: Die aanwending van Onbemande Vliegtuie (UAVs) vir kraglyn inspeksies, vereis die definiëring van veilige vlieg sones. Oorspannings (TOVs) op oorhoofse kraglyne (OHTLs) kan hierdie vliegtuie in gevaar stel as hulle die grense van hierdie sones oorskry. Om die veilige vlieg sones van 'n UAV in die omgewing van OHTLs te bepaal, is realistiese volskaalse toetse gedoen. Die nie-lineariteit in afbreek effekte lewer onakkurate kleinskaal toetse en rekenaar werk. Eksperimentele werk word gebruik om die benaderde afstande vir die ergste geval te beskryf. Hierdie werk kan nie 'n volledige oplossing gee nie as gevolg van ‘n beperking op huidige toerusting. Dit beteken dat verdere toetse, by ‘n meer gespesialiseerde fasiliteit, gedoen moet word. Eksperimente is uitgevoer in twee fases: nie-lineêre en lineêre toetse in die Hoogspannings (HV) laboratorium. Die nie-lineêre toetse word gedoen om die kleinste-benaderde-afstand (MAD) af te lei en die lineêre eksperimente word gebruik om FEKO (‘n numeriese elektromagnetika simulasie program) met die metings omgewing te kalibreer. Sodra daar ‘n korrelasie tussen die lineêre data en die gesimuleerde data is, kan daar aangeneem word dat die simulasie model en die toets-opstelling betroubaar is. Die simulasies kan dan gebruik word om 'n meetkundige faktor te bepaal as 'n bydrae tot F. Rizk se voorspellings vergelykings. Die Rizk vergelykings word gebruik om die veilige vlieg sones langs die OHTLs te beskryf. Dit kan dus gebruik word as ‘n toevoeging tot die nie-lineêre eksperimentele werk. Saam met die normale meet standaard voorstellings, is die Rizk voorspellings geformuleer sodat dit die lyn spesifieke oplossings kan bepaal. Die voorgestelde verklarings waardes word in per eenheid waardes beskryf, wat dan gekies kan word met ooreenstemmende historiese lyn data. Kraglyn-vonke word ondersoek om die lyn-bestraling verskynsel beter te verstaan. Hierdie begrip kan in die lyn inspeksie proses en in die uitleg van kraglyne naby radiostilte-areas help. Kennis van OHTL bestralings patrone kan help met die identifisering van corona en vonk-bronne tydens die inspeksie proses. 'n UAV met 'n aangehegte spektrum analiseerder is gebruik om die lug-vonkende metings te neem. Vonk vlakke wat gemeet is word dan gebruik om 'n Numeriese Elektromagnetiese (CEM) model te bevestig. Die CEM model kan dan gebruik word om OHTL bestralings eienskappe verder te ondersoek.
Khanna, Yash. "Conceptual design and development of thermal management system for hybrid electric aircraft engine. : A study to develop a physical model and investigate the use of Mobil Jet Oil II as coolant for aircraft electrical propulsion under different scenarios and time horizons." Thesis, Mälardalens högskola, Framtidens energi, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-46612.
Повний текст джерелаGlassock, Richard R. "Design, modelling and measurement of hybrid powerplant for unmanned aerial vehicles (UAVs)." Thesis, Queensland University of Technology, 2012. https://eprints.qut.edu.au/61052/1/Richard_Glassock_Thesis.pdf.
Повний текст джерелаWu, Tao. "Integrative system modelling of aircraft electrical power systems." Thesis, University of Nottingham, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.537690.
Повний текст джерелаZoccatelli, Michele, and Edoardo Nascimbeni. "Transformation of the Aviation industry : Exploring alternative renewal fuel pathways." Thesis, KTH, Skolan för industriell teknik och management (ITM), 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-301640.
Повний текст джерелаDetta examensarbete kommer att ingå i ett större projekt som heter Sustainable Energy Transition in Aviation (SETA), vilket kommer att göras i samarbete med avdelningen för hållbarhet, industriell dynamik och entreprenörskap (SIDE) vid INDEK. Den övergripande avhandlingen syftar till att bidra till att påskynda energiövergången inom flygsektorn, med fokus på tre tekniker: biobaserade jetbränslen, vätgasbränslen och elektriska flygplan. Detta forskningsprojekt pågår eftersom luftfarten skapar stora mängder koldioxidutsläpp i Sverige. Det står för 5% av de totala svenska utsläppen (Klimatpolitiska Rådet, 2020). På grund av dess komplexitet som ett sociotekniskt system och dess snäva samband mellan komponenter, kämpar luftfarten för att förändras. Därför ökar ett transformerande tryck för att nå 2030 och 2045 mål. Syftet med forskningen är att belysa hur införandet av alternativa bränslen och tekniker kan hjälpa luftfarten att nå koldioxidneutralitet. Dessutom kan flygindustrin klassificeras som ett socio-tekniskt system, varigenom en konceptuell ram användes för att bättre analysera dess övergång. Multi-Level Perspective Framework (MLP) tillämpades således med avsikten att beskriva hur den hållbara energiomvandlingen kommer att ske på de olika nivåerna. Genom intervjuer var det möjligt att ta fram de olika utmaningarna inom flygsystemet, samtidigt som man framhävde framtida scenarier inom lufttransportsektorn. Genom att utveckla en modelleringsanalys genom LEAPprogramvaran var det dessutom möjligt att hypotisera flera scenarier där biodrivmedel, väte och elektriska flygplanstillväxt varierar under specifika antaganden. Slutligen visade analysen att införandet av dessa alternativa tekniker kommer att vara avgörande för att stödja luftfarten i dess gröna omvandling. Mellan 2015 och 2045 minskade de totala utsläppen från den analyserade transportsektorn med 90%. Därför kommer luftfarten i huvudsak att behöva dessa nya tekniker för att förändras och bli grönare.
Yang, Tao. "Development of dynamic phasors for the modelling of aircraft electrical power systems." Thesis, University of Nottingham, 2013. http://eprints.nottingham.ac.uk/13548/.
Повний текст джерелаHandy, Peter James. "The characterisation, modelling and detection of series arc faults in aircraft electrical power distribution systems featuring solid state power controllers (SSPCs)." Thesis, University of Warwick, 2016. http://wrap.warwick.ac.uk/80134/.
Повний текст джерелаGiraud, Xavier. "Méthodes et outils pour la conception optimale des réseaux de distribution d'électricité dans les aéronefs." Phd thesis, Institut National Polytechnique de Toulouse - INPT, 2014. http://tel.archives-ouvertes.fr/tel-00955887.
Повний текст джерелаЧастини книг з теми "Modelling electric aircraft"
Yazar, Isil, Ranjan Vepa, and Fikret Caliskan. "Current State of the Art of Modelling and Simulation of Propulsion Systems for Hybrid-Electric Aircraft." In Progress in Sustainable Aviation, 37–64. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-12296-5_3.
Повний текст джерелаТези доповідей конференцій з теми "Modelling electric aircraft"
Kascak, Peter, Timothy Dever, and Ralph Jansen. "Electric Aircraft Propulsion Power System Impedance Modelling Methodology." In AIAA Propulsion and Energy 2021 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3307.
Повний текст джерелаDever, Timothy P., Peter E. Kascak, and Ralph H. Jansen. "Megawatt Electric Aircraft Propulsion Power System Impedance Modelling." In 2022 IEEE/AIAA Transportation Electrification Conference and Electric Aircraft Technologies Symposium (ITEC+EATS). IEEE, 2022. http://dx.doi.org/10.1109/itec53557.2022.9814046.
Повний текст джерелаMarshall, J. "Reliability enhancement methodology and modelling for electronic equipment - the REMM project." In IEE Colloquium. Electrical Machines and Systems for the More Electric Aircraft. IEE, 1999. http://dx.doi.org/10.1049/ic:19990841.
Повний текст джерелаLukic, Milos, Paolo Giangrande, Christian Klumpner, and Michael Galea. "Modelling and Analysis of an Aircraft On-board Electric Taxiing System." In 2019 22nd International Conference on Electrical Machines and Systems (ICEMS). IEEE, 2019. http://dx.doi.org/10.1109/icems.2019.8921709.
Повний текст джерелаCross, A. M., A. J. Forsyth, and G. Mason. "Modelling and Simulation Strategies for the Electric Systems of Large Passenger Aircraft." In Power Systems Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2002. http://dx.doi.org/10.4271/2002-01-3255.
Повний текст джерелаPorru, Mario, Alessandro Serpi, Andrea Floris, and Alfonso Damiano. "Modelling and real-time simulations of electric propulsion systems." In 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC). IEEE, 2016. http://dx.doi.org/10.1109/esars-itec.2016.7841438.
Повний текст джерелаHammadi, Moncef, Jean-Yves Choley, Olivia Penas, and Alain Riviere. "Multidisciplinary approach for modelling and optimization of Road Electric Vehicles in conceptual design level." In 2012 Electrical Systems for Aircraft, Railway and Ship Propulsion (ESARS). IEEE, 2012. http://dx.doi.org/10.1109/esars.2012.6387488.
Повний текст джерелаGomez, Pere Izquierdo, Alberto Barragan Moreno, Jun Lin, and Tomislav Dragicevic. "Data-Driven Thermal Modelling for Anomaly Detection in Electric Vehicle Charging Stations." In 2022 IEEE/AIAA Transportation Electrification Conference and Electric Aircraft Technologies Symposium (ITEC+EATS). IEEE, 2022. http://dx.doi.org/10.1109/itec53557.2022.9813767.
Повний текст джерелаYang, T., S. V. Bozhko, and G. M. Asher. "Fast functional modelling for 18-pulse autotransformer rectifier units in more- electric aircraft." In 6th IET International Conference on Power Electronics, Machines and Drives (PEMD 2012). IET, 2012. http://dx.doi.org/10.1049/cp.2012.0205.
Повний текст джерелаJones, Catherine E., Kieran Millar, Kenny Fong, Rafael Pena Alzola, Patrick Norman, and Graeme Burt. "A Modelling Design Framework for Integrated Electrical Power and Non-Electrical Systems Design on Electrical Propulsion Aircraft." In 2022 IEEE/AIAA Transportation Electrification Conference and Electric Aircraft Technologies Symposium (ITEC+EATS). IEEE, 2022. http://dx.doi.org/10.1109/itec53557.2022.9813810.
Повний текст джерела