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The Overview of Vertical Take-Off and Landing Technology
- 1 Shandong Experimental High School, Jinan, China
* Author to whom correspondence should be addressed.
Abstract
Vertical takeoff and landing (VTOL) technology is garnering significant attention in the aviation industry due to its distinct benefits and wide range of potential applications. A long runway is not necessary when using VTOL technology, which allows aircraft to take off and land vertically straight from the ground. Air mobility in cities, military activities, and emergency response are just a few of the areas where this technology is beneficial. This essay will provide an overview of the development, application, and future of vertical takeoff and landing technology. The technology’s operating principles, advantages and limitations will also be explored. Overall, VTOL technology offers a tremendous leap in aircraft technology, with numerous possible uses. Even though there are still difficulties, more research and development will probably result in improvements and broader use.
Keywords
Vertical take-off and landing technology, aviation industry, applications
[1]. WANG G L & Wu Z. (2006). Vertical take-off and Landing technology and its application on UAVS. Airborne Missiles (06), 20-25. doi: 10. 16338 / j . issn .1009 - 1319. 2006. 06. 008.
[2]. Gao Hongbo, Zhang Zhaohai, Su Zhou, Liang Zhen. (2019). How to choose electric fixed-wing drone. Technology (31),21.doi:10.19392/j.cnki.1671-7341.201931020.
[3]. Tammy, Liu Yingjie. SPRINT project promotes the development of high-speed vertical take-off and landing aircraft [J]. Aerodynamics,2024, No. 36(01): 47-49.
[4]. Deng Tao, Tan Xi, Xiong Zhihao, ZHENG Yuwei. Design and Simulation of Hybrid electric Propulsion System for Fixed wing UAVs in Vertical Take-off and Landing [J]. Journal of Chongqing Jiaotong University (Natural Science Edition),2023(10): 156-162.
[5]. ZHU Rui, Wen Weiqi, HE Xingyu, Zhao Chenhong, Zhang Huanbin, Liu Zhirong. Design and Experiment of VTOL UAV with Variable rotor [J]. Experimental Technology and Management,2023(03):145-151. (in Chinese) DOI: 10.16791 / J.CNki.SJG.2023.03.024.
[6]. Yang Daliang. Implementation of wind resistance characteristics and wind disturbance control of fixed-rotor UAV during vertical take-off and landing [J]. Science and Technology Information,2022(17):55-57+93.DOI:10.16661/ j.cnki.1672-3791.2201-5042-7135.
[7]. Sun Bin, Fu Shuangjia, MOU Haolei, Qiao Ge, Xu Junhu. Research and Suggestions on Airworthiness Certification Rules for new Vertical Take-off and Landing (VTOL) aircraft [J]. Civil Aviation Administration, 2022, No.376(02):61-64.
[8]. Jiang Yankun, Liu Weiwei. EASA small vertical take-off and landing aircraft special conditions and compliance method research [J]. Journal of aircraft maintenance and engineering, 2021 (03) : 101-104. The DOI: 10.19302 / j.carol carroll nki. 1672-0989.2021.03.029.
[9]. Peng Weicheng, Zhang Bing. Vertical take-off and landing carrier unmanned aerial vehicle (uav) the design and optimization of [J]. Journal of horizon of science and technology, 2019 (7): 27-28, DOI: 10.19694 / j.carol carroll nki issn2095-2457.2019.07.011.
[10]. Ma Zhao, Zhao Chuqing, Xu Jie, Jin Donglei, ZHAO Jiahui. Vertical take-off and landing fixed-wing unmanned aerial vehicle (uav) application in highway custody [J]. Mechanical and electrical integration, 2018 (6) : 41-44 + 56. DOI: 10.16413 / j.carol carroll nki. Issn 1007-080 - x. 2018.06.007.
[11]. Kuang Yinhu, Liu Mingyuan, Shi Kanglin. Four rotor vertical take-off and landing a fixed wing aircraft design [J]. Journal of horizon of science and technology, 2016 (24) : 36-38. DOI: 10.19694 / j.carol carroll nki issn2095-2457.2016.24.026.
[12]. Globol. Russia develops 5-seat flying taxi that can take off and land vertically in parking space [J]. Dual-use Technologies and Products,2017 (21):23. doi: 10.19385 / j.cnki.1009-8119.2017.21.025.
[13]. Xu Qingjiu, Qu Dongcai, Wu Xiaonan. Development and Revelations of the ship-borne vertical take-off and landing unmanned helicopter [J]. Journal of maneuverable missile, 2010 (10): 71-75. The DOI: 10.16338 / j.i SSN. 1009-1319.2010.10.003.
Cite this article
Yuan,D. (2024). The Overview of Vertical Take-Off and Landing Technology. Applied and Computational Engineering,93,40-44.
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