H∞ State Feedback Control for the Stabilization of the Three Euler Angles of Helicopter Based on LMI

摘要：

The H∞ state feedback control for the stabilization of the three Euler angles of helicopter is studied. The little perturbation model of helicopter is introduced. The proper generalized control variables are chosen and the generalized control object is established. The H∞ state feedback algorithm is developed based on the Iterative Linear Matrix Inequality (LMI) approach and the digital simulation is finished. The simulation results demonstrate the effectiveness of the H∞ state feedback controller.

作者: Rong Xie Xinmin Wang Yan Li

作者单位: School of Automation, Northwestern Polytechnical University, Xian 710072, China

会议类型: 国际会议

会议名称: International Conference on Intelligent Computation Technology and Automation(2008 智能计算技术与自动化国际会议 ICICTA 2008)

会议地点: 长沙

会议语种:英文

页码: 375-379

在线出版日期: 2008-10-20（万方平台首次上网日期，不代表论文的发表时间）