Sliding Mode-Based Missile Guidance Law Design

摘要：

An sliding mode controller design for missiles guidance law is designed under the presence of target maneuvering. To reduce the chattering in sliding mode control, constitute a continuous function instead of signal function which guarantees the practicability of the control scheme. Simulation shows the well tracking performance of the controller. Chattering is erased and the robustness is intensified.

关键词： Guidance Law Sliding Mode Control Maneuvering Target

作者: Yingyuan Li Shuangquan Li

作者单位: School of Automation, Harbin University of Science and Technology Harbin, China

会议类型: 国际会议

会议名称: The 4th International Symposium on Computational Intelligence and Industrial Application(第四届国际计算智能和工业应用研讨会)

会议地点: 哈尔滨

会议语种:英文

页码: 256-260

在线出版日期: 2010-08-01（万方平台首次上网日期，不代表论文的发表时间）