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Gotowe bibliografie tematyczne / Automatic landing

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Gotowa bibliografia na temat „Automatic landing”

Autor: Grafiati

Data publikacji: 10 sierpnia 2024

Data aktualizacji: 31 lipca 2025

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Artykuły w czasopismach na temat "Automatic landing"

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Ali, Afrah A., Nizar H. Abbas, and Ahmed Hameed Kaleel. "Automatic Aircraft Landing System: A Review." Journal of Engineering 30, no. 9 (2024): 165–89. http://dx.doi.org/10.31026/j.eng.2024.09.09.

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The aircraft landing phase, marking the finishing of a flight plane, is a critical yet dangerous aerial maneuver. Even though it might seem simple, predicting the complexities of performance during landing presents a big challenge due to the dynamic characteristics of the phase, interaction with piloting methods, as well as inherent uncertainties in aerodynamics. Landing is executed in close proximity to the ground at reduced airspeed, the landing phase entails an escalated safety risk. Notably, incidents and accidents, particularly overruns where aircraft fail to slow sufficiently on the runw

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Liu, Mao Han, Chun Tao Li, and Yi Wang. "UAV Automatic Landing Control Law." Advanced Materials Research 383-390 (November 2011): 1452–57. http://dx.doi.org/10.4028/www.scientific.net/amr.383-390.1452.

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Landing is the most important stage of the Flight of UAV, the study of automatic landing of UAVs has important engineering significance. In this paper, the UAV landing trajectory is divided into approach phase, steep glide phase and flare phase; a cascade control structure controller of height tracking was applied and the landing control law was designed. The digital simulation was done in the MATLAB / simulink environment. The results of simulation indicated that UAV can track the designed landing trajectory very well under the control law of automatic landing and safe landing can be achieved

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Ghous, Hamid, Mubasher H. Malik, Dania Majeed, Fathima Nuzha Mohamed, and Ayesha Nasir. "Evaluation of Safe Landing Site Detection Methods for Unmanned Aerial Vehicles." VAWKUM Transactions on Computer Sciences 11, no. 1 (2023): 281–94. http://dx.doi.org/10.21015/vtcs.v11i1.1474.

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Nowadays, aerial vehicles (drones) are becoming more popular. Over the past few years, Unmanned Aerial Vehicles (UAVs) have been used in various remote sensing applications. Every aerial vehicle is now either partially or completely automated. The tiniest type of aerial vehicle is the UAV. The widespread use of aerial drones requires numerous safe landing site detection techniques. The paper aims to review literature on techniques for automatic safe landing of aerial drone vehicles by detecting suitable landing sites, considering factors such as ground surfaces and using image processing metho

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Rashmi Koushik et al.,, Rashmi Koushik et al ,. "Automatic Landing Control System." International Journal of Mechanical and Production Engineering Research and Development 10, no. 3 (2020): 7639–50. http://dx.doi.org/10.24247/ijmperdjun2020726.

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Caro Fuentes, Vincenzo, Ariel Torres, Danny Luarte, et al. "Digital Classification of Chilean Pelagic Species in Fishing Landing Lines." Sensors 23, no. 19 (2023): 8163. http://dx.doi.org/10.3390/s23198163.

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Fishing landings in Chile are inspected to control fisheries that are subject to catch quotas. The control process is not easy since the volumes extracted are large and the numbers of landings and artisan shipowners are high. Moreover, the number of inspectors is limited, and a non-automated method is utilized that normally requires months of training. In this work, we propose, design, and implement an automated fish landing control system. The system consists of a custom gate with a camera array and controlled illumination that performs automatic video acquisition once the fish landing starts

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Bykov, V. A., S. M. Velikovskiy, A. E. Parnenkov, and S. M. Shulgin. "Approach to forming of assessment of probability of making a landing of the unmanned aerial vehicle of helicopter type on the runway platform of the ship taking into account different operational modes." Radio industry (Russia) 31, no. 2 (2021): 7–14. http://dx.doi.org/10.21778/2413-9599-2021-31-2-7-14.

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Problem statement. Now taking-off and landings of human powered helicopters to runway site of the ship, provides the Palubnik-1 complex interacting with other systems of the ship. At the same time creation of system of take off and landing of unmanned aerial vehicles of helicopter type should be made about use of regular aerotechnical means of the ship. In article proposed options of use of the automatic and automated landing system as for piloted, and unmanned aerial vehicles of helicopter type in different operational modes.Objective. To offer approach to forming of technique of assessment o

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Plinge, Walter R. "Automatic Approach and Landing Systems." Measurement and Control 36, no. 6 (2003): 176–80. http://dx.doi.org/10.1177/002029400303600603.

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Nowak, Dariusz, Grzegorz Kopecki, Damian Kordos, and Tomasz Rogalski. "The PAPI Lights-Based Vision System for Aircraft Automatic Control during Approach and Landing." Aerospace 9, no. 6 (2022): 285. http://dx.doi.org/10.3390/aerospace9060285.

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The paper presents the concept of a component of an aircraft’s automatic flight control system, controlling the airplane when in longitudinal motion (i.e., pitch angle, sink rate, airspeed channels) during automatic landing, from a final approach until a touchdown. It is composed of two key parts: a vision system and an automatic landing system. The first part exploits dedicated image-processing algorithms to identify the number of red and white PAPI lights appearing on an onboard video camera. Its output data—information about an aircraft’s position on a vertical profile of a landing trajecto

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Parkinson, B. W., and K. T. Fitzgibbon. "Aircraft Automatic Landing Systems Using GPS." Journal of Navigation 42, no. 1 (1989): 47–59. http://dx.doi.org/10.1017/s0373463300015083.

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abstractThis paper is based on a presentation made at the IAIN International Navigation Congress held in Sydney, Australia, in February 1988.The global positioning system (GPS) offers a new opportunity for the automation of aircraft landing systems. The position and velocity measurements provided by a state-of-the-art GPS receiver using the C/A code and working in a normal or differential mode (D-GPS) and aided by one or two ground-based PseudoLites (PLS), may be able to satisfy the landing accuracy requirements of the FA A.This paper describes the design and simulation of an aircraft automati

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Liu, Hengxi, Yongzhi Wang, Shibo Wen, et al. "A New Blind Selection Approach for Lunar Landing Zones Based on Engineering Constraints Using Sliding Window." Remote Sensing 15, no. 12 (2023): 3184. http://dx.doi.org/10.3390/rs15123184.

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Deep space exploration has risen in interest among scientists in recent years, with soft landings being one of the most straightforward ways to acquire knowledge about the Moon. In general, landing mission success depends on the selection of landing zones, and there are currently few effective quantitative models that can be used to select suitable landing zones. When automatic landing zones are selected, the grid method used for data partitioning tends to miss potentially suitable landing sites between grids. Therefore, this study proposes a new engineering-constrained approach for landing zo

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Rozprawy doktorskie na temat "Automatic landing"

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Bole, Michael. "Design of an automatic landing system for twin rotor vertical take-off and landing unmanned air vehicle." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape3/PQDD_0015/MQ47834.pdf.

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Gising, Andreas. "MALLS - Mobile Automatic Launch and Landing Station for VTOL UAVs." Thesis, Linköping University, Department of Electrical Engineering, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-15980.

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<p>The market for vertical takeoff and landing unmanned aerial vehicles, VTOL UAVs, is growing rapidly. To reciprocate the demand of VTOL UAVs in offshore applications, CybAero has developed a novel concept for landing on moving objects called MALLS, Mobile Automatic Launch and Landing Station. MALLS can tilt its helipad and is supposed to align to either the horizontal plane with an operator adjusted offset or to the helicopter skids. Doing so, eliminates the gyroscopic forces otherwise induced in the rotordisc as the helicopter is forced to change attitude when the skids align to the ground

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Caldeira, Fabrício Reis. "Design of an automatic landing system using linear quadratic tracker." Instituto Tecnológico de Aeronáutica, 2008. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=725.

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This work presents the application of the Linear Quadratic Tracker (LQT) for the automatic landing system of passenger transport airplanes. The design method to achieve an autoland flare law with improved performance and disturbance rejection is described. With this method the design is direct and more formal thus avoiding the somewhat time consuming and more ad-hoc design iterations currently practice in industry. Although the design technique has been used for a autoland system, the approach is general enough to be used in other control applications. The structure of a traditional flare cont

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Lai, Khai Ping. "A deep learning model for automatic image texture classification: Application to vision-based automatic aircraft landing." Thesis, Queensland University of Technology, 2016. https://eprints.qut.edu.au/97992/4/Khai_Ping_Lai_Thesis.pdf.

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This project aims to investigate a robust Deep Learning architecture to classify different type of textural imagery. The findings will eventually be part of a central processing algorithm used for Automatic Image Classification for Automatic Aircraft Landing.

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Hill, Steven James. "DGPS/ILS integration for an automatic landing system using Kalman Filtering." Ohio University / OhioLINK, 1996. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1178311128.

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Aribal, Seckin. "Development Of An Autopilot For Automatic Landing Of An Unmanned Aerial Vehicle." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613391/index.pdf.

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This thesis presents the design of an autopilot and guidance system for an unmanned aerial vehicle. Classical (PID) and modern control (LQT, Sliding Mode) methods for autonomous navigation and landing in adverse weather conditions are implemented. Two different guidance systems are designed in order to navigate through waypoints during normal and/or emergency flight. The nonlinear Pioneer UAV model is used in controller development and simulations. Aircraft is linearized at different trim points and total airspeed, altitude, roll and yaw autopilots are designed using Matlab/Simulink environmen

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Magnus, Vestergren. "Automatic Takeoff and Landing of Unmanned Fixed Wing Aircrafts : A Systems Engineering Approach." Thesis, Linköpings universitet, Datorteknik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-133078.

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The purpose of this thesis is to extend an existing autopilot with automatic takeoff and landing algorithms for small fixed wing unmanned aircrafts. The work has been done from a systems engineering perspective and as for solution candidates this thesis has a bias towards solutions utilizing fuzzy logic. The coveted promises of fuzzy logic was primarily the idea to have a design that was easily tunable with very little knowledge beyond flight experience for a particular aircraft. The systems engineering perspective provided a way to structure and reason about the project where the problem has

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Trittler, Martin [Verfasser]. "Automatic Landing for Fixed-Wing Unmanned Aerial Vehicles with Optical Sensors / Martin Trittler." Aachen : Shaker, 2018. http://d-nb.info/1162794321/34.

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Hermansson, Joel. "Vision and GPS based autonomous landing of an unmanned aerial vehicle." Thesis, Linköping University, Automatic Control, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-57735.

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<p>A control system for autonomous landing of an unmanned aerial vehicle (UAV)with high precision has been developed. The UAV is a medium sized model he-licopter. Measurements from a GPS, a camera and a compass are fused with anextended Kalman filter for state estimation of the helicopter. Four PID-controllers,one for each control signal of the helicopter, are used for the helicopter control.During the final test flights fifteen landings were performed with an average land-ing accuracy of 35 cm. A bias in the GPS measurements makes it impossible to land the helicopter withhigh precision usi

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Lugo, Cárdenas Israel. "Autonomous take-off and landing for a fixed wing UAV." Thesis, Compiègne, 2017. http://www.theses.fr/2017COMP2364/document.

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Ce travail étudie certains des problèmes les plus pertinents dans le sens de la navigation et contrôle présentés dans une classe particulière de mini-véhicules aériens. L'un des principaux objectifs c'est à réaliser un véhicule léger et facile à déployer dans un court laps de temps, un véhicule sans pilote drone capable de suivre une mission complète, du décollage aux points de cheminement suivants et de terminer la mission avec un atterrissage autonome à l'intérieur d'une zone délimitée en utilisant une interface graphique dans un ordinateur ou une tablette. La génération de trajectoire II es

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Książki na temat "Automatic landing"

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Hueschen, Richard M. Implementation and flight tests for the digital integrated automatic landing system (DIALS). National Aeronautics and Space Administration ,Langley Research Center, 1986.

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Zhu, Shangxiang. Automatic landing through the turbulent planetary boundary layer. Institute for Aerospace Studies, 1985.

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Center, Langley Research, ed. Implementation and flight tests for the Digital Integrated Automatic Landing System (DIALS). National Aeronautics and Space Administration, Langley Research Center, 1986.

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David, McNally B., and Ames Research Center, eds. Flight test evaluation of the Stanford University/United Airlines differential GPS category III automatic landing system. National Aeronautics Administration, Ames Research Center, 1995.

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Germany) International Symposium on Precision Approach and Automatic Landing (2000 Munich. International Symposium on Precision Approach and Automatic Landing, ISPA 2000, Munich, Germany, 18-20 July 2000: Symposium proceedings. German Institute of Navigation, 2000.

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Bundick, W. Thomas. Results of aircraft open-loop tests of an experimental magnetic leader cable system for guidance during roll-out and turnoff. Langley Research Center, 1990.

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B, Middleton David, Poole William L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Results of aircraft open-loop tests of an experimental magnetic leader cable system for guidance during roll-out and turnoff. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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B, Middleton David, Poole William L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Results of aircraft open-loop tests of an experimental magnetic leader cable system for guidance during roll-out and turnoff. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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Erkelens, L. J. J. Investigation on MLS approach path interception and transition techniques, Part II: Flight simulator investigation. National Aerospace Laboratory, 1985.

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Center, Langley Research, ed. Automatic braking system modification for the Advanced Transport Operating System (ATOPS) Transportation System Research Vehicle (TSRV). National Aeronautics and Space Administration, Langley Research Center, 1986.

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Części książek na temat "Automatic landing"

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Georghiou, Luke, J. Stanley Metcalfe, Michael Gibbons, Tim Ray, and Janet Evans. "Smiths Industries: Aircraft Automatic Landing Equipment." In Post-Innovation Performance. Palgrave Macmillan UK, 1986. http://dx.doi.org/10.1007/978-1-349-07455-6_35.

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Murray-Smith, D. J. "Case Study II — An Aircraft Automatic Landing System." In Continuous System Simulation. Springer US, 1995. http://dx.doi.org/10.1007/978-1-4615-2504-2_11.

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Anand, Amitesh, Subhabrata Barman, Nemani Sathya Prakash, Naba Kumar Peyada, and Jayashri Deb Sinha. "Vision Based Automatic Landing of Unmanned Aerial Vehicle." In Recent Advances in Intelligent Information Systems and Applied Mathematics. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-34152-7_8.

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Juang, Jih-Gau, and Li-Hsiang Chien. "Adaptive Fuzzy Neural Network Control for Automatic Landing System." In Computational Collective Intelligence. Technologies and Applications. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-16693-8_53.

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Nagothu, Sudheer Kumar, and G. Anitha. "Automatic Landing Site Detection for UAV Using Supervised Classification." In Springer Series in Geomechanics and Geoengineering. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-77276-9_27.

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Cheng, Chi-Bin, and Huan-Jyh Shyur. "Automatic Causal Analysis and Reporting of Hard Landing Events." In Studies in Systems, Decision and Control. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-1235-2_8.

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Huh, Sungsik, and David Hyunchul Shim. "A Vision-Based Automatic Landing Method for Fixed-Wing UAVs." In Selected papers from the 2nd International Symposium on UAVs, Reno, Nevada, U.S.A. June 8–10, 2009. Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-8764-5_11.

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Suzuki, Satoshi. "Automatic Take-Off and Landing Control for Small Unmanned Helicopter." In Advances in Intelligent Systems and Computing. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-37374-9_16.

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Suzuki, Satoshi. "Control Scheme for Automatic Takeoff and Landing of Small Electric Helicopter." In Intelligent Systems, Control and Automation: Science and Engineering. Springer Japan, 2013. http://dx.doi.org/10.1007/978-4-431-54276-6_5.

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Subrahmanyam, M. Bala. "H ∞ Design of the F/A-18A Automatic Carrier Landing System." In Finite Horizon H∞ and Related Control Problems. Birkhäuser Boston, 1995. http://dx.doi.org/10.1007/978-1-4612-4272-7_6.

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Streszczenia konferencji na temat "Automatic landing"

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Zhang, Yirui, Shibin Yang, and Xulong Xi. "Study on Automatic Landing of Civil Aircraft Based on LADRC." In 2024 11th International Forum on Electrical Engineering and Automation (IFEEA). IEEE, 2024. https://doi.org/10.1109/ifeea64237.2024.10878772.

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Chen, Quanrui, Zhiying Chen, Zhuo Zhang, Liangchao Guo, and Xiaoliang Sun. "Vision-guided autonomous landing technology for noncooperative target." In Third International Conference on Machine Vision, Automatic Identification and Detection, edited by Renchao Jin. SPIE, 2024. http://dx.doi.org/10.1117/12.3035597.

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Liu, Yu, Yuanyuan Zhang, and Renfu Li. "Fixed-time command-filtered adaptive neural control for automatic carrier landing." In 2024 43rd Chinese Control Conference (CCC). IEEE, 2024. http://dx.doi.org/10.23919/ccc63176.2024.10662356.

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Zhu, Qing. "Automatic landing control system for large passenger aircraft under artificial intelligence." In 9th International Conference on Electromechanical Control Technology and Transportation (ICECTT 2024), edited by Jinsong Wu and Azanizawati Ma'aram. SPIE, 2024. http://dx.doi.org/10.1117/12.3039854.

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König, Eva, Nicolai Voget, Max Hartmann, and Dieter Moormann. "Automatic Identification of Safety Landing Points for VTOL UAVs Using Geodata." In 2025 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2025. https://doi.org/10.1109/icuas65942.2025.11007811.

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Zhimin, Han, and Hong Guanxin. "Landing Error Analysis of the Automatic Carrier Landing System." In AIAA Guidance, Navigation and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-6335.

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Gribanov, A. S. "Automatic Landing of a Helicopter." In 2019 International Multi-Conference on Industrial Engineering and Modern Technologies (FarEastCon). IEEE, 2019. http://dx.doi.org/10.1109/fareastcon.2019.8934014.

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Wang, Rongshun, Liaoni Wu, and Fuqiang Bing. "Automatic Landing Control Design of Gyroplane." In 2019 IEEE 3rd Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC). IEEE, 2019. http://dx.doi.org/10.1109/imcec46724.2019.8984061.

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Meng, Lin, Yang Gao, Jiachao Zhang, and Liangbao Jiao. "Automatic longitudinal landing control of FanWing." In 2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022), edited by Xuexia Ye. SPIE, 2022. http://dx.doi.org/10.1117/12.2635153.

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Nho, Kyungmoon, and Ramesh Agarwal. "Automatic landing system design using fuzzy logic." In Guidance, Navigation, and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-4484.

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Raporty organizacyjne na temat "Automatic landing"

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Sinclair, Samantha, and Sally Shoop. Automated detection of austere entry landing zones : a “GRAIL Tools” validation assessment. Engineer Research and Development Center (U.S.), 2022. http://dx.doi.org/10.21079/11681/45265.

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The Geospatial Remote Assessment for Ingress Locations (GRAIL) Tools software is a geospatial product developed to locate austere entry landing zones (LZs) for military aircraft. Using spatial datasets like land classification and slope, along with predefined LZ geometry specifications, GRAIL Tools generates binary suitability filters that distinguish between suitable and unsuitable terrain. GRAIL Tools combines input suitability filters, searches for LZs at user‐defined orientations, and plots results. To refine GRAIL Tools, we: (a) verified software output; (b) conducted validation assessmen

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McQueen, Bob, ed. Unsettled Issues Concerning Urban Air Mobility Infrastructure. SAE International, 2021. http://dx.doi.org/10.4271/epr2021025.

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Urban air mobility (UAM) refers to urban transportation systems that move people by air. UAM offers the potential for reducing traffic congestion in cities and providing an integrated approach to urban mobility. With the emergence of electric vertical takeoff and landing (eVTOL) aircraft, drone technology, and the possibility of automated aircraft, interest in this topic has grown considerably for private sector solution providers—including aerospace and technology companies—as well as urban planners and transportation professionals. Unsettled Issues Concerning Urban Air Mobility Infrastructur

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Tzonev, Nick, and Eric Pesty. PR-396-113704-R02 Methods for Detection of Gases and VOCs from Floating Roofs of Aboveground Storage Tanks. Pipeline Research Council International, Inc. (PRCI), 2013. http://dx.doi.org/10.55274/r0010794.

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Describes the development of an automated system that can effectively replace the EPA-mandated in-service and out-of-service inspections of the Internal Floating Roofs (IFR) in Aboveground Storage Tanks (ASTs). The ultimate goal is to increase the internal inspection interval to twenty (20) years, which would coincide with the interval used by the American Petroleum Institute's (API) Standard 653 for out-of-service general mechanical inspection of the entire tank. Extending the IFR internal inspection interval will eliminate the negative elements associated with additional AST entry events and

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