Relevant bibliographies by topics / Fixed-wing unmanned aerial vehicle

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

Academic literature on the topic 'Fixed-wing unmanned aerial vehicle'

Author: Grafiati
Published: 10 August 2024

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Journal articles on the topic "Fixed-wing unmanned aerial vehicle"

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Zou, Jie-Tong, and Pan Zheng-Yan. "THE DEVELOPMENT OF TILT-ROTOR UNMANNED AERIAL VEHICLE." Transactions of the Canadian Society for Mechanical Engineering 40, no. 5 (2016): 909–21. http://dx.doi.org/10.1139/tcsme-2016-0075.

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In this research, we had developed quad-rotor unmanned aerial vehicles with the tilt-rotor mechanism. People are eager to fly therefore the development of aerial vehicles, such as fixed-wing aerial vehicles and multi-rotor aerial vehicles, has grown rapidly in recent years. The multi-rotor vertical take-off and landing (VTOL) unmanned aerial vehicle which can fly stably and hover in a fix position developed the fastest. Comparing the general fixed-wing aircrafts and rotorcrafts, fixed-wing aircrafts can fly with a higher speed than rotorcrafts, but they do not have the VTOL and hovering abilit
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Oktay, Tugrul, Harun Celik, and Ilke Turkmen. "Maximizing autonomous performance of fixed-wing unmanned aerial vehicle to reduce motion blur in taken images." Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 232, no. 7 (2018): 857–68. http://dx.doi.org/10.1177/0959651818765027.

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In this study, reducing motion blur in images taken by our unmanned aerial vehicle is investigated. Since shakes of unmanned aerial vehicle cause motion blur in taken images, autonomous performance of our unmanned aerial vehicle is maximized to prevent it from shakes. In order to maximize autonomous performance of unmanned aerial vehicle (i.e. to reduce motion blur), initially, camera mounted unmanned aerial vehicle dynamics are obtained. Then, optimum location of unmanned aerial vehicle camera is estimated by considering unmanned aerial vehicle dynamics and autopilot parameters. After improvi
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Zhang, Xiangyin, and Haibin Duan. "Altitude consensus based 3D flocking control for fixed-wing unmanned aerial vehicle swarm trajectory tracking." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 230, no. 14 (2016): 2628–38. http://dx.doi.org/10.1177/0954410016629692.

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This paper studies the 3D flocking control problem for unmanned aerial vehicle swarm when tracking a desired trajectory. In order to allow the unmanned aerial vehicle swarm to form the stable flocking geometry on a same horizontal plane, the altitude consensus algorithm is applied to the unmanned aerial vehicle altitude control channel, using the trajectory altitude as the external input signals. The flocking control algorithm is only performed in the horizontal channel to control the horizontal position of unmanned aerial vehicles. The distributed tracking algorithm, which controls the local
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Eftekhari, Shahrooz, and Abdulkareem Sh Mahdi Al-Obaidi. "Investigation of a Cruising Fixed Wing Mini Unmanned Aerial Vehicle Performance Optimization." Indonesian Journal of Science and Technology 4, no. 2 (2019): 280–93. http://dx.doi.org/10.17509/ijost.v4i2.18185.

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The applications of unmanned aerial vehicles have been extended through the recent decades and they are utilized for both civil and military applications. The urge to utilize unmanned aerial vehicles for civil purposes has elevated researchers and industries interest towards the mini unmanned aerial vehicle (MUAV) category due to its suitable configurations and capabilities for multidisciplinary civil purposes. This study is an effort to further enhance the aerodynamic efficiency of MUAVs through a parametric study of the wing and proposing an innovative bioinspired wing design. The research i
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Nasab, Hamed Mortazavi, and Naser Navazani. "Adaptive Control for Trajectory Tracking of an Unmanned Aerial Vehicle." Advanced Engineering Forum 17 (June 2016): 101–10. http://dx.doi.org/10.4028/www.scientific.net/aef.17.101.

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In this paper, an unmanned aerial vehicle (UAV) with fixed-wing in normal condition flight, and fixed height, is considered and along with this process, kinematics model of UAV, assumed to have parametric uncertainty. In this situation the target of designing of proper controller family, based on switching logic, is to control the speed and roll angle of fixed-wing unmanned aerial vehicle in order to track desired path with minimum error. The desired path will be generated by trajectory maker block. The results of simulation on a fixed-wing UAV are presented to show the efficiency of the metho
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Suroso, Indreswari, and Erwhin Irmawan. "Analysis Of Aerial Photography With Drone Type Fixed Wing In Kotabaru, Lampung." Journal of Applied Geospatial Information 2, no. 1 (2018): 102–7. http://dx.doi.org/10.30871/jagi.v2i1.738.

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In the world of photography is very closely related to the unmanned aerial vehicle called drones. Drones mounted camera so that the plane is pilot controlled from the mainland. Photography results were seen by the pilot after the drone aircraft landed. Drones are unmanned drones that are controlled remotely. Unmanned Aerial Vehicle (UAV), is a flying machine that operates with remote control by the pilot. Methode for this research are preparation assembly of drone, planning altitude flying, testing on ground, camera of calibration, air capture, result of aerial photos and analysis of result ae
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Yang, Mingxiao, Sifan Wang, Kai Hu, and Tongyan Liu. "Wing Optimization Design Based on Composite Global Hawk Unmanned Aerial Vehicle." Journal of Physics: Conference Series 2557, no. 1 (2023): 012087. http://dx.doi.org/10.1088/1742-6596/2557/1/012087.

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Abstract Composite materials have become the approach to solve the high stiffness and light weight of unmanned aerial vehicle structures. The wing had an extremely important influence on the flight of the unmanned aerial vehicle. The optimal composite wing design aroused widespread attention since it enhanced the aerodynamic performance of unmanned aerial vehicles. This article was intended to optimize and design the unmanned aerial vehicle with advantages in aerodynamic performance. According to the parameters of the military-civilian integrated unmanned aerial vehicle, a three-dimensional mo
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Krishnakumar, R., K. Senthil Kumar, and T. Anand. "Design and Development of Vertical Takeoff and Horizontal Transition Mini Unmanned Aerial Vehicle." Advanced Materials Research 1016 (August 2014): 436–40. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.436.

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In recent years Unmanned Aerial Vehicles (UAV) has become a significant segment of the aviation industry. They can be chosen to be designed as fixed wing or Rotary wing type. Fixed-wing aircraft has the performance of fast forward movement, long range and superior endurance due to its gliding capabilities with no power. Unlike the fixed wing models, rotary wing mini-copters are able to fly in all directions, hover in a fixed position with minimal space for takeoff and landing. This makes them the perfect instrument for detailed inspection work or surveying. Implementing a hybrid UAV has the ad
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Challa, Vinay Reddy, and Ashwini Ratnoo. "On Maneuverability of Fixed-Wing Unmanned Aerial Vehicle Formations." Journal of Guidance, Control, and Dynamics 44, no. 7 (2021): 1327–44. http://dx.doi.org/10.2514/1.g005409.

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Zhai, Rui Yong, Wen Dong Zhang, Zhao Ying Zhou, Sheng Bo Sang, and Pei Wei Li. "Trajectory Tracking Control for Micro Unmanned Aerial Vehicles." Advanced Materials Research 798-799 (September 2013): 448–51. http://dx.doi.org/10.4028/www.scientific.net/amr.798-799.448.

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This article considers the problem of trajectory tracking control for a micro fixed-wing unmanned air vehicle (UAV). With Bank-to-Turn (BTT) method to manage lateral deviation control of UAV, this paper discusses the outer loop guidance system, which separates the vehicle guidance problems into lateral control loop and longitudinal control loop. Based on the kinematic model of the coordinated turning of UAV, the aircraft can track a pre-specified flight path with desired error range. Flight test results on a fixed-wing UAV have indicated that the trajectory tracking control law is quite effect
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Dissertations / Theses on the topic "Fixed-wing unmanned aerial vehicle"

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Fuglaas, Simen. "Precision Airdrop from a Fixed-Wing Unmanned Aerial Vehicle." Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for teknisk kybernetikk, 2014. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-25909.

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Accurate mapping of the polar regions requires reliable placement ofwireless transmitting sensors, also known as beacons, on icebergs anddrift ice. This thesis considers the use of a specific fixed-wing unmannedaerial vehicle, known as the Penguin B, to accurately deploysaid beacons from the air. An analysis of the possible precision airdropmethods was conducted and the decision was made to release thebeacon in free fall from the aircraft. The estimated trajectory was calculatedand used to decide the optimal release position and direction.Combined this is known as the release configuration. Mo
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Hough, Willem J. "Autonomous aerobatic flight of a fixed wing unmanned aerial vehicle." Thesis, Link to online version, 2007. http://hdl.handle.net/10019/428.

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Alberts, Frederik Nicolaas. "Accurate autonomous landing of a fixed-wing unmanned aerial vehicle." Thesis, Stellenbosch : Stellenbosch University, 2012. http://hdl.handle.net/10019.1/71672.

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Thesis (MScEng)-- Stellenbosch University, 2012.<br>ENGLISH ABSTRACT: This thesis presents the analysis, design, simulation and practical implementation of a control system to achieve an accurate autonomous landing of a fixed-wing unmanned aerial vehicle in the presence of wind gust atmospheric disturbances. Controllers which incorporate the concept of direct-lift control were designed based on a study of the longitudinal dynamics of the UAV constructed as a testbed. Direct-lift control offers the prospect of an improvement in the precision with which aircraft height and vertical velocit
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Oland, Espen. "Nonlinear Control of Fixed-Wing Unmanned Aerial Vehicles." Doctoral thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for teknisk kybernetikk, 2014. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-27263.

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Gaum, Dunross Rudi. "Agressive flight control techniques for a fixed wing unmanned aerial vehicle." Stellenbosch : University of Stellenbosch, 2009. http://hdl.handle.net/10019.1/3112.

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Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2009.<br>This thesis investigates aggressive all-attitude flight control systems. These are flight controllers capable of controlling an aircraft at any attitude and will enable the autonomous execution of manoeuvres such as high bank angle turns, steep climbs and aerobatic flight manoeuvres. This class of autopilot could be applied to carry out evasive combat manoeuvres or to create more efficient and realistic target drones. A model for the aircraft’s dynamics is developed in such a way that its high ba
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Mullen, Jon. "FILTERED-DYNAMIC-INVERSION CONTROL FOR FIXED-WING UNMANNED AERIAL SYSTEMS." UKnowledge, 2014. http://uknowledge.uky.edu/me_etds/45.

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Instrumented umanned aerial vehicles represent a new way of measuring turbulence in the atmospheric boundary layer. However, autonomous measurements require control methods with disturbance-rejection and altitude command-following capabilities. Filtered dynamic inversion is a control method with desirable disturbance-rejection and command-following properties, and this controller requires limited model information. We implement filtered dynamic inversion as the pitch controller in an altitude-hold autopilot. We design and numerically simulate the continuous-time and discrete-time filtered-dyna
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Basson, Matthys Michaelse. "Stall prevention control of fixed-wing unmanned aerial vehicles." Thesis, Stellenbosch : University of Stellenbosch, 2010. http://hdl.handle.net/10019.1/4310.

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Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2010.<br>ENGLISH ABSTRACT: This thesis presents the development of a stall prevention flight control subsystem, which can easily be integrated into existing flight control architectures of fixed-wing unmanned aerial vehicles (UAV’s). This research forms an important part of faulttolerant flight control systems and will ensure that the aircraft continues to operate safely within its linear aerodynamic region. The focus of this thesis was the stall detection and prevention problem. After a thorough literat
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Persson, Linnea. "Cooperative Control for Landing a Fixed-Wing Unmanned Aerial Vehicle on a Ground Vehicle." Thesis, KTH, Skolan för elektro- och systemteknik (EES), 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-187667.

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High Altitude Long Endurance (HALE) platforms are a type of Unmanned Aerial Vehicle (UAV). With their relatively easy deployment and independence of a fixed orbit, HALE UAVs have the potential to replace satellites for certain tasks in the future. A challenge with this technology is that the current platforms are too heavy to fly for a long period of time. A suggested method for reducing the weight is to remove the landing gear to instead use alternative methods for take-off and landing. One such alternative method is to land the UAV on top of a cooperating ground vehicle. In this thesis, the coo
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Smit, Samuel Jacobus Adriaan. "Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS." Thesis, Stellenbosch : Stellenbosch University, 2013. http://hdl.handle.net/10019.1/80122.

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Thesis (MScEng)--Stellenbosch University, 2013.<br>ENGLISH ABSTRACT: This dissertation presents the design and practical demonstration of a flight control system (FCS) that is capable of autonomously landing a fixed-wing, unmanned aerial vehicle (UAV) on a stationary platform aided by a high-precision differential global positioning system. This project forms part of on-going research with the end goal of landing a fixed-wing UAV on a moving platform (for example a ship’s deck) in windy conditions. The main aim of this project is to be able to land the UAV autonomously, safely and accurately
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Alatorre, Sevilla Armando. "Landing of a fixed-wing unmanned aerial vehicle in a limited area." Electronic Thesis or Diss., Compiègne, 2024. http://www.theses.fr/2024COMP2801.

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Le projet de thèse consiste à développer une solution pour l'atterrissage d'un drone à voilure fixe de configuration classique dans une zone limitée. Le principal défi consiste à réduire la vitesse de l'avion à une phase minimale pendant le vol, à l'aide d'algorithmes de contrôle automatique. La réduction de la vitesse d'un drone à voilure fixe s'effectue en augmentant son angle d'attaque, ce qui implique un freinage par la force de traînée. Cependant, cette manœuvre est critique pour un avion conventionnel, parce que si son angle d'attaque augmente au-delà de l'angle de décrochage, le véhicul
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Books on the topic "Fixed-wing unmanned aerial vehicle"

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Greer, Daniel S. Avionics System development for a Rotary Wing Unmanned Aerial Vehicle. Naval Postgraduate School, 1998.

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Tran, Fleischer Van, and Hugh L. Dryden Flight Research Center, eds. Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles: Formulation of Ko displacement theory. National Aeronautics and Space Administration, Dryden Flight Research Center, 2010.

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Office, General Accounting. Unmanned aerial vehicles: No more Hunter systems should be bought until problems are fixed : report to the Secretary of Defense. The Office, 1995.

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Avionics System Development for a Rotary Wing Unmanned Aerial Vehicle. Storming Media, 1998.

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Wich, Serge A., and Lian Pin Koh. Typology and anatomy of drones. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198787617.003.0002.

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In this chapter we discuss the typology of drones that are currently being used for different kinds of environmental and conservation applications. Drones are also commonly known variously as Remotely Piloted Aircraft Systems (RPAS), Unmanned Aerial Vehicles (UAV), and Unmanned Aircraft Systems (UAS). We focus on the most popular aircraft types including multirotor (of various configurations), fixed wing, and hybrid ‘vertical-take-off-and-landing’ (VTOL) craft, and briefly discuss the relative pros and cons of each type. We also broadly discuss the essential components common to all remotely p
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Book chapters on the topic "Fixed-wing unmanned aerial vehicle"

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Özbek, Emre, Selcuk Ekici, and T. Hikmet Karakoc. "An Evaluation on Landing Gear Configurations of Fixed-Wing, Rotary-Wing, and Hybrid UAVs." In Unmanned Aerial Vehicle Design and Technology. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-45321-2_9.

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Dobrokhodov, Vladimir. "Kinematics and Dynamics of Fixed-Wing UAVs." In Handbook of Unmanned Aerial Vehicles. Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-90-481-9707-1_53.

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Yu, Ziquan, Youmin Zhang, Bin Jiang, and Chun-Yi Su. "Fixed-Wing UAV Model." In Fault-Tolerant Cooperative Control of Unmanned Aerial Vehicles. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-7661-4_2.

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Owen, Mark, Randal W. Beard, and Timothy W. McLain. "Implementing Dubins Airplane Paths on Fixed-Wing UAVs*." In Handbook of Unmanned Aerial Vehicles. Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-90-481-9707-1_120.

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Mills, Steven J., Jason J. Ford, and Luis Mejías. "Vision Based Control for Fixed Wing UAVs Inspecting Locally Linear Infrastructure Using Skid-to-Turn Maneuvers." In Unmanned Aerial Vehicles. Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-94-007-1110-5_4.

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Ryaciotaki-Boussalis, Helen, and Darrell Guillaume. "Computational and Experimental Design of a Fixed-Wing UAV." In Handbook of Unmanned Aerial Vehicles. Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-90-481-9707-1_121.

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Kownacki, Cezary, and Daniel Ołdziej. "Flocking Algorithm for Fixed-Wing Unmanned Aerial Vehicles." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_24.

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Agarwal, Varun, and Rajiv Ranjan Tewari. "Delivering Newspapers Using Fixed Wing Unmanned Aerial Vehicles." In Advances in Intelligent Systems and Computing. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-6981-8_49.

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Zhong, Gang, Yi Mao, Liandong Zhang, Shangwen Yang, and Hao Liu. "Fast Path Planning for Fixed-Wing Unmanned Aerial Vehicle with Multiple Constraints." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-5615-7_6.

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Bakirci, Murat, and Muhammed Mirac Ozer. "Adapting Swarm Intelligence to a Fixed Wing Unmanned Combat Aerial Vehicle Platform." In Studies in Big Data. Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-38325-0_18.

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Conference papers on the topic "Fixed-wing unmanned aerial vehicle"

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Tahar, Khairul Nizam, Anuar Ahmad, Wan Abdul Aziz Wan Mohd Akib, and Wan Mohd Naim Wan Mohd. "Aerial mapping using autonomous fixed-wing unmanned aerial vehicle." In 2012 IEEE 8th International Colloquium on Signal Processing & its Applications (CSPA). IEEE, 2012. http://dx.doi.org/10.1109/cspa.2012.6194711.

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El Tin, Fares, Inna Sharf, and Meyer Nahon. "Fire Monitoring with a Fixed-wing Unmanned Aerial Vehicle." In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2022. http://dx.doi.org/10.1109/icuas54217.2022.9836074.

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Petrík, Nikolas Michael, and Pavol Pecho. "Design and construction of a UAV device with a fixed wing for the conditions of rescue services." In Práce a štúdie. University of Zilina, 2021. http://dx.doi.org/10.26552/pas.z.2021.2.32.

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The paper is focused on comprehensive design of an unmanned aerial vehicle with fixed wing, which would add efficiency to specific activities performed by rescue services. The current rapid development of unmanned aerial vehicles is slowly becoming part of many industries around the world. The aim of this paper is to design an unmanned aerial vehicle that could provide safe, reliable, and efficient operation. The overall design, construction, and installation of the proposed unmanned aerial vehicle should integrate several modern technologies. To make an ideal design of unmanned aerial vehicle
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Raghuwaiya, Krishna, and Roneel Chand. "3D Motion Planning of a Fixed-Wing Unmanned Aerial Vehicle." In 2018 5th Asia-Pacific World Congress on Computer Science and Engineering (APWC on CSE). IEEE, 2018. http://dx.doi.org/10.1109/apwconcse.2018.00046.

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Akbar, Mahesa, Ahmad Riyad Firdaus, Sapto Wibowo, and Nanda Wirawan. "Piezoelectric Energy Harvesting from A Fixed-wing Unmanned Aerial Vehicle." In 2019 2nd International Conference on Applied Engineering (ICAE). IEEE, 2019. http://dx.doi.org/10.1109/icae47758.2019.9221651.

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Liang, Chao, and Chenxiao Cai. "Modeling of a rotor/fixed-wing hybrid unmanned aerial vehicle." In 2017 36th Chinese Control Conference (CCC). IEEE, 2017. http://dx.doi.org/10.23919/chicc.2017.8029181.

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Chakraborty, Anusna, Clark N. Taylor, Rajnikant Sharma, and Kevin M. Brink. "Cooperative localization for fixed wing unmanned aerial vehicles." In 2016 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE, 2016. http://dx.doi.org/10.1109/plans.2016.7479689.

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Gryte, Kristofer, Richard Hann, Mushfiqul Alam, Jan Rohac, Tor Arne Johansen, and Thor I. Fossen. "Aerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehicle." In 2018 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2018. http://dx.doi.org/10.1109/icuas.2018.8453370.

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Phelps, David, Kanishke Gamagedara, Jeremey Waldron, Kalpesh Patil, and Murray Snyder. "Ship Air Wake Detection Using Small Fixed Wing Unmanned Aerial Vehicle." In 2018 AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0784.

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Levin, Joshua, Aditya Paranjape, and Meyer Nahon. "Motion Planning for a Small Aerobatic Fixed-Wing Unmanned Aerial Vehicle." In 2018 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE, 2018. http://dx.doi.org/10.1109/iros.2018.8593670.

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Reports on the topic "Fixed-wing unmanned aerial vehicle"

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Yang, Justin A. Conceptual Aerodynamic Modeling of a Flapping Wing Unmanned Aerial Vehicle. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada592189.

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She, Ruifeng, and Yanfeng Ouyang. Analysis of Drone-based Last-mile Delivery Systems under Aerial Congestion: A Continuum Approximation Approach. Illinois Center for Transportation, 2023. http://dx.doi.org/10.36501/0197-9191/23-014.

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This paper presents a systematic analysis and design framework for a spectrum of last-mile delivery systems that leverage unmanned aerial vehicles (UAVs). Four distinct modes are considered: (1) direct drone deliveries from a fixed depot; (2) drone deliveries from parked trucks that carry bulk parcels to customer neighborhoods; (3) drone deliveries from nonstopping trucks that tour customer neighborhoods; and (4) as a benchmark, traditional truck-based home deliveries. We present a new continuum-approximation approach that is used for analysis of both truck routing and aerial-UAV traffic. We c
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Christensen, Lance. PR-459-133750-R03 Fast Accurate Automated System To Find And Quantify Natural Gas Leaks. Pipeline Research Council International, Inc. (PRCI), 2019. http://dx.doi.org/10.55274/r0011633.

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Miniature natural gas sensors weighing a few hundred grams with 10 ppb s-1 sensitivity towards methane and ppb s-1 sensitivity towards methane and ethane present the energy industry with cost effective ways to improve safety, comply with State and Federal regulations, decrease natural gas emissions, and attribute natural gas indications to thermogenic or biogenic sources. One particularly promising implementation is on small unmanned aerial systems (sUASs) flown by service providers or in-house personnel or even more ambitiously as part of larger network conducting autonomous, continual monito
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Price, Donald. SM-403-148100-R01 Mineral Wells 2012 RAM Gas and Oil Leak Detection Field Study Results. Pipeline Research Council International, Inc. (PRCI), 2015. http://dx.doi.org/10.55274/r0010851.

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In June 2012, the RAM Program conducted a comprehensive field study to evaluate the performance of current off the shelf sensor technologies for detecting gas and oil leaks on pipelines. This study had three key objectives: 1. Evaluate the capabilities of current technologies that are offered commercially for methane leak detection monitoring using standard pipeline patrol aircraft 2. Provide a test location for development of emerging technologies that are not yet commercially available for pipeline leak detection 3. Assess the feasibility of using airborne sensors to detect staged liquid oil
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