THE RESEARCH OF 3 DOF HELICOPTER TRACKING CONTROLLER

摘要：

In this paper, an uncertain state-space model is implemented for a 3 DOF helicopter, the Linear Quadratic Regulator (LQR) tracking control law is given and the robust tracking control law which is satisfied the request of R,Q and H∞ is designed by means of Linear Matrix Inequality (LMI).The results show the validity of this approach.

关键词： 3 DOF helicopter LQR Robust tracking control

作者: PEI-RAN LI TAO SHEN

作者单位: School of Control Science & Engineering, University of Jinan

会议类型: 国际会议

会议名称: 2007 International Conference on Machine Learning and Cybernetics(IEEE第六届机器学习与控制论国际会议)

会议地点: 香港

会议语种:英文

页码: 578-582

在线出版日期: 2007-08-19（万方平台首次上网日期，不代表论文的发表时间）