Design, manufacturing and flight-testing of a fixed-wing, small-scale UAV for the transportation of blood bags to remote locations

被引:1
|
作者
Karageorgiou, A. [1 ]
Kantouris, P. [1 ]
Metallidou, N. [2 ]
Charizani, A. [1 ]
Panagiotou, P. [3 ]
机构
[1] Aristotle Univ Thessaloniki, Dept Mech Engn, Aristotle Space & Aeronaut Team, Thessaloniki 54124, Greece
[2] Aristotle Univ Thessaloniki, Dept Elect & Comp Engn, Aristotle Space & Aeronaut Team, Thessaloniki 54124, Greece
[3] Aristotle Univ Thessaloniki, Dept Mech Engn, Lab Fluid Mech & Turbomachinery, Thessaloniki 54124, Greece
关键词
D O I
10.1088/1742-6596/2526/1/012087
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The current work presents the design, manufacturing, and flight-testing of a fixed-wing, small-scale Unmanned Aerial Vehicle (UAV). The research activities presented in this paper have all been conducted by the Aristotle Space & Aeronautics Team (ASAT), a Greek aerospace student team, for their participation in the international student competition Air Cargo Challenge 2022. Its mission is to carry bags of blood to a remote location. The design requirements refer to a short take-off distance of 60m of rough terrain, climb time of 60s and a cruise/loiter time of 120s. Size restrictions also apply, as the aircraft must fit inside a 1.5m x 1.5m x 0.5m volume, in its deployed form. A step-by-step presentation of the design procedure is conducted, emphasizing on the critical design decisions, such as the airfoil, cargo bay location and wing planform design. The corresponding trade studies are shown, along with the main advantages of the resulting configuration. The in-house manufacturing process is consequently described, focusing on the molds tooling, as well as on the carbon fiber and fiberglass manufacturing techniques. Finally, the results of the flight testing are shown, including the initial challenges that lead to the fine-tuning of the UAV. The test results are validated against the design data and the overall performance of the aerial vehicle is discussed.
引用
收藏
页数:8
相关论文
共 25 条
  • [1] Design of Robust Controller of Fixed-Wing UAV for Transition Flight
    Kohno, Satoshi
    Uchiyama, Kenji
    2014 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS), 2014, : 1111 - 1116
  • [2] Rapid Prototyping of a Fixed-Wing VTOL UAV for Design Testing
    Aktas, Yucel Orkut
    Ozdemir, Ugur
    Dereli, Yasin
    Tarhan, Ahmed Farabi
    Cetin, Aykut
    Vuruskan, Aslihan
    Yuksek, Burak
    Cengiz, Hande
    Basdemir, Serkan
    Ucar, Mesut
    Genctav, Murat
    Yukselen, Adil
    Ozkol, Ibrahim
    Kaya, Metin Orhan
    Inalhan, Gokhan
    JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2016, 84 (1-4) : 639 - 664
  • [3] Rapid Prototyping of a Fixed-Wing VTOL UAV for Design Testing
    Yucel Orkut Aktas
    Ugur Ozdemir
    Yasin Dereli
    Ahmed Farabi Tarhan
    Aykut Cetin
    Aslihan Vuruskan
    Burak Yuksek
    Hande Cengiz
    Serkan Basdemir
    Mesut Ucar
    Murat Genctav
    Adil Yukselen
    Ibrahim Ozkol
    Metin Orhan Kaya
    Gokhan Inalhan
    Journal of Intelligent & Robotic Systems, 2016, 84 : 639 - 664
  • [4] FRACTIONAL ORDER FLIGHT CONTROL OF A SMALL FIXED-WING UAV: CONTROLLER DESIGN AND SIMULATION STUDY
    Chao, Haiyang
    Luo, Ying
    Di, Long
    Chen, YangQuan
    PROCEEDINGS OF THE ASME INTERNATIONAL DESIGN ENGINEERING TECHNICAL CONFERENCES AND COMPUTERS AND INFORMATION IN ENGINEERING CONFERENCE, VOL 3, 2010, : 621 - 628
  • [5] Design, Construction, and Flight Performance of an Electrically Operated Fixed-Wing UAV
    Panagiotopoulos, Ilias
    Sakellariou, Lefteris
    Hatziefremidis, Antonios
    DRONES, 2024, 8 (06)
  • [6] Adaptive Flight Control Design for Fixed-wing UAV based on Neural Network
    Liu, Jinhua
    Wang, Xiaoli
    Zhao, Peiqi
    2022 41ST CHINESE CONTROL CONFERENCE (CCC), 2022, : 2363 - 2368
  • [7] Design, Manufacturing, and Flight Testing of an Experimental Flying Wing UAV
    Chung, Pei-Hsiang
    Ma, Der-Ming
    Shiau, Jaw-Kuen
    APPLIED SCIENCES-BASEL, 2019, 9 (15):
  • [8] Estimation and flight verification of fuel consumption rate of small fixed-wing UAV for a long flight duration
    Hyokawa, Satoshi
    Miura, Masaya
    Yasukawa, Kei
    Hamajima, Koki
    Shibata, Takuma
    Ueba, Masazumi
    IEICE COMMUNICATIONS EXPRESS, 2023, 12 (06): : 322 - 327
  • [9] Guidance and Control Algorithm Design for Terrain-Following Flight of a Fixed-Wing UAV
    Kim, Myungkang
    Ra, Chunggil
    Kim, Seungkeun
    Suk, Jinyoung
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2023, 51 (05) : 299 - 306
  • [10] NMPC-based Control Design for Transition Flight of Fixed-Wing VTOL UAV
    Lee, Jiwon
    Kim, Youdan
    AIAA SCITECH 2024 FORUM, 2024,