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四旋翼无人机可视化半实物仿真平台研究
  • ISSN号:0254-3087
  • 期刊名称:仪器仪表学报
  • 时间:0
  • 页码:2572-2578
  • 分类:TP[自动化与计算机技术]
  • 作者机构:[1]Institute of Robotics and Autonomous System, Tianjin Key Laboratory of Process Measurement and Control, and School of Electrical Engineering and Automation, Tianjin University
  • 相关基金:supported by the National Natural Science Foundation of China (Nos. 90916004, 60804004); the Program for New Century Excellent Talents in University (No. NCET-09-0590)
  • 相关项目:吸气式乘波体高超声速飞行器动态分析与非线性鲁棒自适应跟踪控制研究
中文摘要:

This paper proposes a new asymptotic attitude tracking controller for an underactuated 3-degree-of-freedom (DOF) laboratory helicopter system by using a nonlinear robust feedback and a neural network (NN) feedforward term. The nonlinear robust control law is developed through a modified inner-outer loop approach. The application of the NN-based feedforward is to compensate for the system uncertainties. The proposed control design strategy requires very limited knowledge of the system dynamic model, and achieves good robustness with respect to system parametric uncertainties. A Lyapunov-based stability analysis shows that the proposed algorithms can ensure asymptotic tracking of the helicopter's elevation and travel motion, while keeping the stability of the closed-loop system. Real-time experiment results demonstrate that the controller has achieved good tracking performance.

英文摘要:

This paper proposes a new asymptotic attitude tracking controller for an underactuated 3-degree-of-freedom (DOF) laboratory helicopter system by using a nonlinear robust feedback and a neural network (NN) feedforward term. The nonlinear robust control law is developed through a modified inner-outer loop approach. The application of the NN-based feedforward is to compensate for the system uncertainties. The proposed control design strategy requires very limited knowledge of the system dynamic model, and achieves good robustness with respect to system parametric uncertainties. A Lyapunov-based stability analysis shows that the proposed algorithms can ensure asymptotic tracking of the helicopter's elevation and travel motion, while keeping the stability of the closed-loop system. Real-time experiment results demonstrate that the controller has achieved good tracking performance.

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期刊信息
  • 《仪器仪表学报》
  • 中国科技核心期刊
  • 主管单位:中国科学技术协会
  • 主办单位:中国仪器仪表学会
  • 主编:张钟华
  • 地址:北京东城区北河沿大街79号
  • 邮编:100009
  • 邮箱:yqyb@vip.163.com
  • 电话:010-84050563
  • 国际标准刊号:ISSN:0254-3087
  • 国内统一刊号:ISSN:11-2179/TH
  • 邮发代号:2-369
  • 获奖情况:
  • 1983年评为机械部科技进步三等奖,1997年评为中国科协优秀科技期刊三等奖
  • 国内外数据库收录:
  • 美国化学文摘(网络版),荷兰文摘与引文数据库,美国工程索引,日本日本科学技术振兴机构数据库,中国中国科技核心期刊,中国北大核心期刊(2004版),中国北大核心期刊(2008版),中国北大核心期刊(2011版),中国北大核心期刊(2014版),英国英国皇家化学学会文摘,中国北大核心期刊(2000版)
  • 被引量:42481