Helicopter UAV readied for flight test

被引：0
|
作者：
Wall, R
机构：
来源：
AVIATION WEEK & SPACE TECHNOLOGY | 2000年 / 153卷 / 08期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：31 / 31
页数：1
相关论文
共 50 条
  • [21] Flight-test evaluation of a helicopter airborne lidar
    Matayoshi, Naoki
    Asaka, Kirnio
    Okuno, Yoshinori
    JOURNAL OF AIRCRAFT, 2007, 44 (05): : 1712 - 1720
  • [22] Hummingbird UAV begins flight test program
    Wall, R
    AVIATION WEEK & SPACE TECHNOLOGY, 2002, 156 (05): : 37 - 37
  • [23] Flight safety control and ground test on UAV
    Deng Dawei
    Li Baoan
    2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2014, : 388 - 392
  • [24] UAV flight safety ground test and evaluation
    Deng, Dawei
    Yuan, Haiwen
    2015 IEEE AUTOTESTCON, 2015, : 422 - 427
  • [25] UAV Flight Test Characterization Using Minimal Test Equipment
    Michalowski, Brent
    Varano, Nathaniel
    2017 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS'17), 2017, : 1737 - 1741
  • [26] Design and implementation of a nonlinear flight control law for the yaw channel of a UAV helicopter
    Cai, Guowei
    Chen, Ben M.
    Peng, Kemao
    Dong, Miaobo
    Lee, Tong H.
    PROCEEDINGS OF THE 46TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-14, 2007, : 1257 - 1262
  • [27] A Robust Flight Control System Design for a Small-Scale UAV Helicopter
    Liu, Peng
    Meng, Zhijun
    Wu, Zhe
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2013, 56 (02) : 96 - 103
  • [28] Flight Test of Flight Control Performance for Airplane Mode of Smart UAV
    Kang, Young-shin
    Park, Bum-jin
    Cho, Am
    Yoo, Chang-sun
    Koo, Sam-Ok
    2012 12TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS), 2012, : 1738 - 1741
  • [29] Station commercialization set as assembly flight readied
    Covault, C
    AVIATION WEEK & SPACE TECHNOLOGY, 1998, 149 (22): : 26 - +
  • [30] Flight-weight scramjet readied for tests
    Kandebo, SW
    AVIATION WEEK & SPACE TECHNOLOGY, 2002, 156 (25): : 95 - 96
12345