English  |  正體中文  |  简体中文  |  全文笔数/总笔数 : 56437/90265 (63%)
造访人次 : 11705426      在线人数 : 37
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/987654321/83703

    题名: Unscented Kalman Filtering for Attitude Determination Using MEMS Sensors
    作者: Shiau, Jaw-Kuen;Wang, I-Chiang
    贡献者: 淡江大學航空太空工程學系
    关键词: Flight Information Measurement;Nonlinear Kalman Filter;Quaternion;Complementary Filter
    日期: 2013-06
    上传时间: 2013-03-20 16:55:35 (UTC+8)
    出版者: 新北市:淡江大學
    摘要: This paper presents the results of a quaternion-based unscented Kalman filtering for attitude estimation using low cost MEMS sensors. The unscented Kalman filter uses the pitch and roll angles computed from gravity force decomposition as the measurement for the filter. The immeasurable gravity accelerations are deduced from the outputs of the three axes accelerometers, the relative accelerations, and the accelerations due to body rotation. The constraint of the four elements of the quaternion method is treated as a perfect measurement and is integrated into the system to form a constrained unscented Kalman filter. The heading angle is obtained from a complimentary filter which uses the heading signal derived from the magnetic force information from an electronic magnetic sensor and the GPS-derived heading as the inputs. An experiment using an in-house designed motion platform is conducted to evaluate the proposed algorithm. The noise characteristics of the sensor signals are examined using the laboratory data. Approximations of the time-varying noise variances of the measured signals are obtained through Taylor series expansions. The algorithm is intuitive and easy to implement. Moreover, the proposed algorithm and the filter design are successfully demonstrated through a complete set of flight test data.
    關聯: Journal of Applied Science and Engineering 16(2), pp.165-176
    DOI: 10.6180/jase.2013.16.2.08
    显示于类别:[航空太空工程學系暨研究所] 期刊論文


    档案 描述 大小格式浏览次数



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