Relevant bibliographies by topics / Drone propulsion

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Drone propulsion'

Author: Grafiati
Published: 18 April 2022
Last updated: 30 July 2025

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Journal articles on the topic "Drone propulsion"

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Corcau, Jenica-Ileana, Liviu Dinca, Andra-Adelina Cucu, and Dmitrii Condrea. "Drone Electric Propulsion System with Hybrid Power Source." Drones 9, no. 4 (2025): 301. https://doi.org/10.3390/drones9040301.

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Unmanned aerial vehicles, known today as drones, in the beginning, were small-dimension research models powered by small electric motors fed from electrical batteries. The propulsion system for these drones had to be adapted to the specific applications along their development. Electric and hybrid-electric propulsion drones represent a rapidly developing field in the aerospace industry. Electric drones are those with purely electric propulsion fed from batteries, while hybrid-electric ones have a hybrid propulsion system combining a thermal engine and an electric motor. Another class of hybrid
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Jarrah, Khaled, Yazen Alali, Alyssa Lalko, and Osamah Rawashdeh. "Flight Time Optimization and Modeling of a Hybrid Gasoline–Electric Multirotor Drone: An Experimental Study." Aerospace 9, no. 12 (2022): 799. http://dx.doi.org/10.3390/aerospace9120799.

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Drones have evolved rapidly over the decades, but the limited flight time inhibits multirotor drones from performing long-duration tasks. Batteries that power drones are considered an inadequate power source due to their low energy density. As gasoline is an energy-dense source, combining an electric propulsion system with gasoline engines should be considered. This paper proposes a novel hybrid multirotor drone design using two gasoline engines to provide the majority of the lift force and four electric motors to stabilize the drone. These propulsion systems have been characterized and optimi
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Aboelezz, Ahmed, David Wetz, Jane Lehr, Pedram Roghanchi, and Mostafa Hassanalian. "Intrinsically Safe Drone Propulsion System for Underground Coal Mining Applications: Computational and Experimental Studies." Drones 7, no. 1 (2023): 44. http://dx.doi.org/10.3390/drones7010044.

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The mining industry has recently shown increased interest in drones for routine activities in underground and surface mines. Designing a drone for coal mines is extremely complicated since the Mine Safety and Health Administration (MSHA) has tight guidelines for any equipment that can be used in underground coal mines. Due to these criteria, designing a drone for underground coal mining is exceedingly difficult. This paper explores the challenges of creating an intrinsically safe drone propulsion system. To address the challenges of designing an intrinsically safe drone’s propulsion system for
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Fu, Yuxuan, Zihao Chen, Enming Liu, and YuFan Cao. "BLDC Motors: Optimal Propulsion for Multirotor Drones." Applied and Computational Engineering 168, no. 1 (2025): None. https://doi.org/10.54254/2755-2721/2025.24799.

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Nowadays, drone technology is advancing, particularly in fields like agriculture and power inspection, and this has made efficient propulsion systems increasingly necessary. In the creation of multirotor drones, brushless current (BLDC) motors have become a crucial technology due to their numerous advantages over other types of motors, including stepping motors, permanent magnet-type synchronous motors, induction motors, and brush direct current motors. This paper analyzes BLDC motors' suitability for multirotor drones, describing their design and advantages. Because of its contactless design
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Krishna, Jithin, NV Chidvilas, G Dinesh Kumar, and K Arulmozhi. "Investigating Propellers for Drone Applications: Analyzing Varied Designs and Characteristics." Acceleron Aerospace Journal 3, no. 1 (2024): 405–11. http://dx.doi.org/10.61359/11.2106-2434.

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The importance of drones has evidently increased in various aspects of daily life, such as defense, agriculture, disaster management, and more. Drone propellers are crucial for generating the lift and propulsion necessary for steady flight. Efficient propeller design is critical for maximizing flight time and maneuverability in drones. We are currently investigating the impact of different propeller designs on drone performance. Our research focuses on optimizing propeller characteristics to ensure optimal propulsion and overall functionality. By testing three airfoil designs and systematicall
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Xia, Zewei, Yulong Ying, Heli Li, et al. "Optimization of Plasma-Propelled Drone Performance Parameters." Aerospace 11, no. 8 (2024): 667. http://dx.doi.org/10.3390/aerospace11080667.

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Recently, the world’s first plasma-propelled drone was successfully flown, demonstrating that plasma propulsion technology is suitable for drone flight. The research on plasma propulsion drones has sparked a surge of interest. This study utilized a proxy model and the NSGA-II multi-objective genetic algorithm to optimize the geometric parameters based on staggered thrusters that affect the performance of electroaerodynamics (EAD) thrusters used for solid-state plasma aircraft. This can help address key issues, such as the thrust density and the thrust-to-power ratio of solid-state plasma aircr
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Akhdan Fadhil, Muhammad, Romie Oktovianus Bura, Gita Amperiawan, and Sovian Aritonang. "TECHNOLOGY OF PROPULSION SYSTEM FOR UNMANNED COMBAT AERIAL VEHICLE (UCAV) – A REVIEW." International Journal of Education and Social Science Research 05, no. 03 (2022): 88–107. http://dx.doi.org/10.37500/ijessr.2022.5306.

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Unmanned Combat Aerial Vehicle (UCAV) is an unmanned aerial vehicle (UAV) that is used for intelligence, surveillance, target acquisition, and reconnaissance and carries aircraft ordnance such as missiles, ATGMs, and/or bombs in hardpoints for drone strikes. These drones are usually under realtime human control, with varying levels of autonomy. Unlike unmanned surveillance and reconnaissance aerial vehicles, UCAVs are used for both drone strikes and battlefield intelligence. Unmanned Combat Aerial Vehicle (UCAV) propulsion technology is significantly related to the flight performance of UCAVs,
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Rushikesh, Patil. "Design of power supply and EHD system for ion-propulsion drone." BOHR International Journal of Engineering 1, no. 1 (2022): 33–36. http://dx.doi.org/10.54646/bije.2022.07.

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An initial preparation stage for the design of an ion-propulsion drone with no moving parts is presented in this study. Ion-propulsion drone technology is still not significantly mature; however, the technology has the potential to bring about evolution in the drone and aerospace industries. An essential part of the system is to generatea high-voltage (HV) DC power supply in order to propel the drone. This study presents the design of a power supply circuit to generate a HV DC supply system along with the design of electrohydrodynamics is presented in this study.
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Rushikesh, Patil, Pulkit Jain, and Harjot Singh Gill. "Design and optimization of ion propulsion drone." BOHR International Journal of Material Sciences and Engineering 1, no. 1 (2023): 25–31. http://dx.doi.org/10.54646/bjmse.2023.05.

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Electric propulsion technology is widely used in many kinds of vehicles in recent years, and aircrafts are noexception. Technically, UAVs are electrically propelled but tend to produce a significant amount of noise andvibrations. Ion propulsion technology for drones is a potential solution to this problem. Ion propulsion technologyis proven to be feasible in the earth’s atmosphere. The study presented in this article shows the design of EHDthrusters and power supply for ion propulsion drones along with performance optimization of high-voltage powersupply for endurance in earth’s atmosphere.
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Rushikesh, Patil, Pulkit Jain, and Harjot Sing Gill. "Design and optimization of ion propulsion drone." BOHR International Journal of Material Sciences and Engineering 1, no. 1 (2023): 25–31. http://dx.doi.org/10.54646/bijmse.2023.05.

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Electric propulsion technology is widely used in many kinds of vehicles in recent years, and aircrafts are no exception. Technically, UAVs are electrically propelled but tend to produce a significant amount of noise and vibrations. Ion propulsion technology for drones is a potential solution to this problem. Ion propulsion technology is proven to be feasible in the earth’s atmosphere. The study presented in this article shows the design of EHD thrusters and power supply for ion propulsion drones along with performance optimization of high-voltage power supply for endurance in earth’s atmospher
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Dissertations / Theses on the topic "Drone propulsion"

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Joe, Hyunsik. "Sensor Craft Control Using Drone Craft with Coulomb Propulsion System." Thesis, Virginia Tech, 2005. http://hdl.handle.net/10919/42781.

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The Coulomb propulsion system has no exhaust plume impingement problem with neighboring spacecraft and does not contaminate their sensors because it requires essentially no propellant. It is suitable to close formation control on the order of dozens of meters. The Coulomb forces are internal forces of the formation and they influence all charged spacecraft at the same time. Highly nonlinear and strongly coupled equations of motion of Coulomb formation makes creating a Coulomb control method a challenging task. Instead of positioning all spacecraft, this study investigates having a sensor craft
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Bronz, Murat. "Conception mini-drone longue endurance." Phd thesis, Toulouse, ISAE, 2012. http://tel.archives-ouvertes.fr/tel-00993465.

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L'objet de cette thèse est de démonter la faisabilité de conception d'un mini-drone longue endurance sans recourir à des véhicules de grande envergure qui nécessite des infrastructures supplémentaires, des systèmes de lancement complexes et un personnel d'exploitation important. Pour ce faire, une approche d'optimisation globale du problème a été utilisée, en s'appuyant sur les spécificités de chacun des aspects de la conception de mini-drones. Ce concept de mini-drone longue endurance doit repousser les limites dans plusieurs disciplines telles que l'aérodynamique, la propulsion, les structur
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Thipyopas, Chinnapat. "Optimisation aérodynamique de configurations de microdrones à voilure fixe : effet biplan, voilure souple et interaction aéropropulsive." Toulouse, ENSAE, 2007. http://www.theses.fr/2007ESAE0007.

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Les micro-drones ont été développés depuis 1997 pour des missions militaires de renseignement. Ils peuvent également être utilisés pour des applications civiles de reconnaissance en milieu contaminé ou difficile d'accès. Les micro-drones ont une dimension maximale typique de 15 à 20 cm, un rayon d'action de 500 m, une endurance de 30 min, ils sont compacts, autonomes et portables par un seul opérateur. En raison de leur charge alaire relativement élevée (due aux divers composants électroniques et d'une contrainte de taille sévère, il est d'usage de recourir à des ailes d'allongement faible (all
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Chaalane, Amar. "Microsystème de propulsion a propergol solide sur silicium : application au controle d'assiette de micro-drone." Phd thesis, Université Paul Sabatier - Toulouse III, 2008. http://tel.archives-ouvertes.fr/tel-00433508.

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Les travaux de cette thèse ont porté sur la conception, la réalisation et la caractérisation de matrices de micro-propulseurs à propergol solide intégrés sur silicium. Ces structures sont dédiées la stabilisation de drone miniature et pouvant aussi être utilisées pour la propulsion des Micro/Nano-Satellites. Les travaux se sont effectués dans le cadre d'un projet financé par la Direction Générale pour l'Armement (DGA) en collaboration entre le LAAS-CNRS et la société PROTAC du groupe THALES. Le principe de fonctionnement d'un micropropulseur repose sur l'initiation thermique d'un matériau pyro
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Chaalane, Amar. "Microsystème de propulsion à propergol solide sur silicium : application au contrôle d'assiete de micro-drone." Toulouse 3, 2008. http://thesesups.ups-tlse.fr/724/.

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Les travaux de cette thèse ont porté sur la conception, la réalisation et la caractérisation de matrices de micro-propulseurs à propergol solide intégrés sur silicium. Ces structures sont dédiées la stabilisation de drone miniature et pouvant aussi être utilisées pour la propulsion des Micro/Nano-Satellites. Les travaux se sont effectués dans le cadre d'un projet financé par la Direction Générale pour l'Armement (DGA) en collaboration entre le LAAS-CNRS et la société PROTAC du groupe THALES. Le principe de fonctionnement d'un micropropulseur repose sur l'initiation thermique d'un matériau pyro
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Hanefors, Victor, and Shaya Rahmanian. "Sharkbait - A self-stabilising underwater drone : Evalution of response time, propulsion and steering in a underwater environment." Thesis, KTH, Skolan för industriell teknik och management (ITM), 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264442.

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This projects purpose was to build an underwater remote operated vehicle with software controlled self-stabilisation for evaluation of the response time, propulsion and steering to see what could be achieved. A prototype was constructed and tested in dry conditions at first. The prototype features an Arduino and a Raspberry Pi as control units, controlling six thrusters. With the help of a controller the user can manoeuvre the vehicle and when exposed to unexpected forces sensors detect this allowing the software to counteract it. Due to risk of massive electrical failure as a result of failed
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McClure, Erin Kathleen. "An evolving-requirements technology assessment process for advanced propulsion concepts." Diss., Available online, Georgia Institute of Technology, 2006, 2006. http://etd.gatech.edu/theses/available/etd-07062006-101749/.

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Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2007.<br>Danielle Soban, Committee Member ; Dimitri Mavris, Committee Chair ; Alan Porter, Committee Member ; Gary Seng, Committee Member ; Daniel Schrage, Committee Member.
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Lindahl, Peter Allan. "Simulation, design and validation of a solid oxide fuel cell powered propulsion system for an unmanned aerial vehicle." Thesis, Montana State University, 2009. http://etd.lib.montana.edu/etd/2009/lindahl/LindahlP0509.pdf.

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This thesis presents a physically-based model for design and optimization of a fuel cell powered electric propulsion system for an Unmanned Aerial Vehicle (UAV). Components of the system include a Solid Oxide Fuel Cell (SOFC) providing power, motor controller, Brushless DC (BLDC) motor, and a propeller. Steady-state models for these components are integrated into a simulation program and solved numerically. This allows an operator to select constraints and explore design trade-offs between components, including fuel cell, controller, motor and propeller options. We also presents a graphical pr
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Soueid, Houssam. "Optimisation of the kinematics of flapping airfoils for micro air vehicle applications." Toulouse 3, 2008. http://thesesups.ups-tlse.fr/791/.

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L'optimisation du battement d'un profil d'aile est réalisée par simulations numériques. L'objectif principal est d'identifier les paramètres de battement capables d'assurer à un micro-drone de bonnes performances aérodynamiques en termes de forces de poussée, de portance et de rendement propulsif. Les variables de contrôle sont les amplitudes des oscillations verticales et de tangage, leur déphasage, leur fréquence, et l'angle d'incidence moyen. Une fois déterminées, les cinématiques optimales sont confrontées aux valeurs observées dans la nature. La méthodologie est basée sur la résolution de
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Raminhos, Gonçalo. "Development of a F.W.M.A.V. with livestreaming capabilities." Master's thesis, Academia da Força Aérea, 2020. http://hdl.handle.net/10400.26/39745.

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Books on the topic "Drone propulsion"

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Gal-Or, Benjamin. Vectored propulsion, supermaneuverability, and robot aircraft. Springer-Verlag, 1990.

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Krasilʹshchikov, M. N., G. G. Sebri͡akov та K. K. Veremeenko. Sovremennye informat͡sionnye tekhnologii v zadachakh navigat͡sii i navedenii͡a bespilotnykh manevrennykh letatelʹnykh apparatov. Fizmatlit, 2009.

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Kucinski, William. So You Want to Design Engines: UAV Propulsion Systems. SAE International, 2018.

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Kucinski, William. So You Want to Design Engines: UAV Propulsion Systems. SAE International, 2018.

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Book chapters on the topic "Drone propulsion"

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Mahakalkar, Sachin G., Jayant P. Giri, Neeraj Sunheriya, et al. "Propulsion Effectiveness Using Propeller Selection, Ducted Propellers and Tilting Mechanism in a Quadrotor Drone." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-3173-2_26.

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Aslansefat, Koorosh, Francisco Marques, Ricardo Mendonça, and José Barata. "A Markov Process-Based Approach for Reliability Evaluation of the Propulsion System in Multi-rotor Drones." In IFIP Advances in Information and Communication Technology. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-17771-3_8.

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Wąsik Mateusz and Skarka Wojciech. "Simulation of Crash Tests for Electrically Propelled Flying Exploratory Autonomous Robot." In Advances in Transdisciplinary Engineering. IOS Press, 2016. https://doi.org/10.3233/978-1-61499-703-0-937.

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The need for continuous technical development brings fresh innovatory solutions and at the same time indicates new trends. For years, common applied solutions have not been adequate enough to the newly established and evolving needs. Furthermore, the global development brings new challenges and needs for the aviation propulsions. An example of such a problem can be particularly noticeable in recent years, with the growing popularity of remotely controlled, small flying objects, commonly called drones, which designated new opportunities in the field of aviation, as well as become a source of ne
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Baskaran, Rajadurai, Varun Kumar, Manikandan Sekar, and Malarselvam Velayudham. "DESIGN AND DEVELOPMENT OF AN AMPHIBIOUS TRICOPTER DRONE: AEROGI." In Futuristic Trends in Mechanical Engineering Volume 3 Book 7. Iterative International Publisher, Selfypage Developers Pvt Ltd, 2024. http://dx.doi.org/10.58532/v3bfme7p9ch1.

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This research article presents the development and evaluation of an Amphibious Tricopter Drone, "Aerogi," designed to operate in air and water environments. The project aimed to bridge the research gap in creating a versatile unmanned aerial vehicle (UAV) capable of seamless transitions between aerial and aquatic modes. The study outlines the methodology, including selecting components such as brushless motors, electronic speed controllers, flight controllers, and tilting mechanisms. Extensive flight testing assessed "Aerogi's" stability, altitude performance, weight-carrying capacity, flight
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Zenowicz, Kamil, and Wojciech Skarka. "Analysis and Optimization of the Propeller Shape for a Stratospheric Drone Research Platform." In Advances in Transdisciplinary Engineering. IOS Press, 2021. http://dx.doi.org/10.3233/atde210126.

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Fix-wings small aircraft or drones, for flight, must be equipped with a source of thrust. In most cases, it will be propulsion systems including engine and propeller that generate the necessary thrust force. Regardless of whether the system includes an electric motor, combustion, or hydrogen engine of torque moment, the most important element of the system is the propeller. It is the element responsible for generating thrust, which is the force necessary for the flight in each of its stages. The article presents all stages of the analysis and optimization of the propeller for the considered hi
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Desroches G., Louis N., Dumas R., Vaslin P., Gorce P., and Chèze L. "Shoulder joint moment contribution to movement during manual wheelchair propulsion." In Assistive Technology Research Series. IOS Press, 2010. https://doi.org/10.3233/978-1-60750-080-3-73.

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The purpose of this study was to establish the contribution (e.g. driving or stabilizing) of net shoulder joint moment to shoulder movement during manual wheelchair (MW) propulsion. Two male able-bodied propelled in a wireless wheelchair ergometer. Kinetics and kinematics of propulsion were recorded simultaneously bilaterally. An inverse dynamic method was used to compute net joint moment and angular velocity at shoulder level. The 3D angle between net shoulder joint moment and angular velocity was computed over the propulsive cycle to determine if net moment mainly drove (angle close to 0 or
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Wąsik Mateusz and Skarka Wojciech. "Design Optimization of Electric Propulsion of Flying Exploratory Autonomous Robot." In Advances in Transdisciplinary Engineering. IOS Press, 2015. https://doi.org/10.3233/978-1-61499-544-9-367.

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The main idea of the paper is to optimise the design parameters of the electric propulsion of exploratory autonomous robot designed for flying in specified extremely unfavourable environment. There are still a lot of unsolved needs in the flying autonomous robots area. A lack of solutions for drones flying in the unpredictable and turbulent conditions has been identified. As examples of such needs the following could be distinguished: exploration of the space-planets with their own atmosphere different from Earths or on Earth drones being used in mountain and marine emergency services which op
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"PROPULSION SYSTEMS AND ELECTRICAL SOURCES FOR DRONES AND UAVS." In Theory, Design, and Applications of Unmanned Aerial Vehicles. CRC Press, 2016. http://dx.doi.org/10.1201/9781315371191-11.

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"Propulsion Systems and Electrical Sources for Drones and UAVs." In Theory, Design, and Applications of Unmanned Aerial Vehicles. CRC Press, 2016. http://dx.doi.org/10.1201/9781315371191-6.

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Conference papers on the topic "Drone propulsion"

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Iliev, Ilian, and Desislava Mihaylova. "Review of underwater drones vibration propulsion." In 2025 7th International Congress on Human-Computer Interaction, Optimization and Robotic Applications (ICHORA). IEEE, 2025. https://doi.org/10.1109/ichora65333.2025.11017145.

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Schmid, Sebastian, Muscan Karadayi, Daniel Tataru, and Jacob Cook. "Modeling, Simulation and System Identification of a Tilt-Wing Aircraft." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-295.

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A simulation framework is essential for the development of a hybrid-electric tilt-wing aircraft such as Dufour Aerospace's Aero2 drone. The tilt-wing design with its complex interaction effects between the propellers and the aerodynamic surfaces presents unique modeling challenges, especially during early stages of development when only limited data is available. Furthermore, a delicate balance between accuracy and performance must be found while keeping complexity low to allow for rapid development. This paper introduces a modular design approach for a simulation framework, details the aero-p
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Al Dabbous, Mohammed, and Mohammad Al-Kadem. "Oil Field Downhole Drone." In SPE/IATMI Asia Pacific Oil & Gas Conference and Exhibition. SPE, 2021. http://dx.doi.org/10.2118/205587-ms.

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Abstract The downhole drone is directed toward an autonomous Oil &amp; Gas (O&amp;G) utilization of a drone in subsurface wells. The autonomous submersible O&amp;G drone comprises a circular shaped housing, a propulsion system with one or more spinner blades located at the front and rear sides driven by electromotors that can pivot along the axis of drone for locomotion determination and a control package unit: wireless transponder, power, control and data storage and sensors. Existing technologies for surveying, such as production logging conveyed into the wellbore by coiled tubing limits wel
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Asri, M. H. Mohd, Z. Sahwee, and N. L. Mohd Kamal. "Propulsion System Drag Reduction for Vertical Takeoff and Land (VTOL) Unmanned Aerial Vehicle (UAV)." In 2019 International Conference on Computer and Drone Applications (IConDA). IEEE, 2019. http://dx.doi.org/10.1109/iconda47345.2019.9034687.

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Woo, Jongbin, Younghyeon Kim, and Sangseok Yu. "Development of an Elaborated Fuel Cell Stack Model for Drone Fuel Cell System With Liquid Cooling." In ASME 2023 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/imece2023-113224.

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Abstract Recently, the drone is tried to employ in the logistics industry that is known as cargo drone. Since a cargo drones requires high power density to allow large payload, hydrogen fuel cell is considered as power propulsion system for cargo drone. Typically, the fuel cell system of small drone is equipped with air cooled fuel cell system but the large payload of cargo drone requires liquid cooling fuel cell system. Since the high power density of cargo drone allows more weight for payload, the fuel cell should be operated with higher current density at the take-off. Those conditions resu
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Ruffin, Alessandro, matteo fagherazzi, Nicolas Bellomo, Francesco Barato, Daniele Pavarin, and Mario Pessana. "Development of the Propulsion System for a Moon Drone Vehicle Demonstrator." In AIAA Propulsion and Energy 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3564.

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"Advances in UAV Applications and Propulsion Technologies Drive the Development of UAV Propulsion Standards." In Default for White Papers. SAE International, 2018. http://dx.doi.org/10.4271/wp-0009.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;The number of small unmanned aerial vehicles (UAVs) used for private and commercial applications is growing exponentially, beyond the domain of hobby enthusiasts. However, standards development has not been keeping up with the applications and technologies now available. The advent of inexpensive battery-powered quadcopters as stable aerial photography and remote-viewing platforms has expanded the utility of these systems into commercial and private applications for inspection and surveillance. With drone-delivered packa
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Dinelli, Christopher, Jarod Fisher, Brenden Herkenhoff, and Mostafa Hassanalian. "Design of a Hybrid Detachable Amphibious Drone for Monitoring Marine Environment." In AIAA Propulsion and Energy 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-3965.

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Soloiu, Valentin, Drake T. Grall, Marcel Ilie, Cesar Carapia, Richard C. Smith, and Austin Brant. "Numerical and Experimental Analysis of a Single Stage Drone Jet Engine." In AIAA Propulsion and Energy 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3488.

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Rivilla Casado, Juan, and Amelia D. Greig. "Solid State Atmosphere Breathing Plasma Propulsion for an Autonomous Mars Drone." In ASCEND 2020. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-4021.

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Reports on the topic "Drone propulsion"

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Christensen, Lance. PR-459-133750-WEB Fast, Accurate, Automated System to Find and Quantify Natural Gas Leaks. Pipeline Research Council International, Inc. (PRCI), 2019. http://dx.doi.org/10.55274/r0011608.

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Thursday, August 8, 2019 11:00 am ET PRESENTER: Lance Christensen, PhD, NASA Jet Propulsion Laboratory HOST: Francois Rongere, PG and E MODERATOR: Carrie Greaney, PRCI CLICK BUY/DOWNLOAD TO ACCESS WEBINAR REGISTRATION LINK Join the PRCI Surveillance, Operations and Maintenance Technical Committee as they present research, conducted by NASA Jet Propulsion Laboratory (JPL), related to the Open Path Laser Spectrometer (OPLS). New advances in sensor technology, with high sensitivity towards detecting methane and ethane, present the energy pipeline industry with cost effective ways to improve safet
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