English  |  正體中文  |  简体中文  |  全文笔数/总笔数 : 49983/85139 (59%)
造访人次 : 7802291      在线人数 : 112
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
搜寻范围 查询小技巧:
  • 您可在西文检索词汇前后加上"双引号",以获取较精准的检索结果
  • 若欲以作者姓名搜寻,建议至进阶搜寻限定作者字段,可获得较完整数据
  • 进阶搜寻


    jsp.display-item.identifier=請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/106078


    题名: Development Scenario of Micro Ornithopters
    作者: Lung-Jieh Yang;Suseendar Marimuthu;Kuan-Cheng Hung;Hao-Hsiang Ke;Yow-Ting Lin;Chien-Wei Chen
    关键词: Ornithopter;Flapping Micro Air Vehicle (FMAV);Short Take-Off and Landing (STOL);Photo-Voltaic (PV);Microcontroller
    日期: 2015/12/01
    上传时间: 2016-04-22 13:19:04 (UTC+8)
    出版者: 中華民國航太學會
    摘要: Regarding the 15 gram-weight flapping micro-air-vehicles (FMAVs) or micro ornithopters, how to prolong the operation time and improve the flight control is very critical to their scenario of development. Using the available transducer devices, this work presents four new features for ornithopters and the corresponding feasibility discussion respectively. The 1st feature is repeatable short take-off and landing (re-STOL) so that the ornithopter can automatically land on the ground at times of wind gusts beyond operational bracket, while resetting to an orientation suited for re-take-off. The 2nd feature is to recharge the onboard lithium battery by flexible thin film photo-voltaic (PV) on the tail. The 3rd feature is toward the autonomous flight control of ornithopters. It is realized by integrating gram-weighted micro-controller integrated with MEMS inertial measurement units (IMUs). Orientation control and light-triggered take-off are proposed herein firstly. The 4th feature is to develop new flapping mechanisms with large flap angle with no phase lag between two flapping wings. The above four newly developed features of ornithopters can preliminarily solve their current four shortcomings, i.e., vulnerability to gust wind, short flight endurance, difficulty in autonomous control and small payload.
    關聯: Journal of Aeronautics, Astronautics and Aviation 47(4), pp.397-406
    DOI: 10.6125/15-1203-868
    显示于类别:[機械與機電工程學系暨研究所] 期刊論文

    文件中的档案:

    档案 描述 大小格式浏览次数
    index.html0KbHTML103检视/开启

    在機構典藏中所有的数据项都受到原著作权保护.

    TAIR相关文章

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