English  |  正體中文  |  简体中文  |  Items with full text/Total items : 49287/83828 (59%)
Visitors : 7153799      Online Users : 86
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/79548


    Title: Autopilots for Ultra Lightweight Robotic Birds: Automatic Altitude Control and System Integration of a Sub-10 g Weight Flapping-Wing Micro Air Vehicle
    Authors: 蕭富元;Hsiao, Fu-Yuen;Yang, Lung-Jieh;楊龍杰;Lin, Sen-Huang;Chen, Cheng-Lin;Shen, Jeng-Fu
    Contributors: 淡江大學機械與機電工程學系暨研究所
    淡江大學航空太空工程學系
    Keywords: Bioengineering;Communication, Networking & Broadcasting;Components, Circuits, Devices & Systems;Computing & Processing (Hardware/Software);Engineered Materials, Dielectrics & Plasmas;Fields, Waves & Electromagnetics;Geoscience;Photonics & Electro-Optics;Signal Processing & Analysis
    Date: 2012-10
    Issue Date: 2012-12-11 13:46:36 (UTC+8)
    Publisher: IEEE
    Abstract: This article described a control law for stabilizing the vertical motion of a flapping-wing MAV and developed a system architecture that is potentially beneficial in realizing the autonomous flight of flapping-wing MAVs fewer than 10 g. The article began with a brief introduction to the Golden Snitch, including its development history and the development of the overall system. The vertical dynamics were given for altitude control. The use of wind tunnel tests to obtain aerodynamical parameters was described. Due to the limited payload-carrying capability, the control architecture was modified so that automatic control of flight altitude of a flapping-wing MAV fewer than 10 g is possible using current technology. Taking the hardware constraint into account, it was shown that the modified P-control can stabilize the vertical motion and track altitude commands. Numerical simulations and flight tests were presented that demonstrate the function of the developed control law and the system architecture. We believe this flapping-wing MAV to be the first under 10 g able to automatically maintain its flight altitude.
    Relation: IEEE Control Systems Magazine 32(5), pp.35-48
    DOI: 10.1109/MCS.2012.2205475
    Appears in Collections:[機械與機電工程學系暨研究所] 期刊論文
    [航空太空工程學系暨研究所] 期刊論文

    Files in This Item:

    File Description SizeFormat
    45_CSM_06302313.pdffull paper3267KbAdobe PDF432View/Open

    All items in 機構典藏 are protected by copyright, with all rights reserved.


    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback