A Study of Chattering Suppression in Sliding Mode-Based Missile Guidance Law
A sliding mode controller with chattering suppression 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. In the numerical simulation, it is obviously that the proposed guidance law reduces the chattering phenomenon and
guidnace law sliding mode control maneuvering target Missile
Yuan Liying Wu Junfeng Yu Lianyong Cui Jiashan Sun Lili
School of Automation,Harbin University of Science and Technology Harbin,China Yantai Wellsys Electronic Co. Ltd ,Yantai,China
国际会议
The 6th International Forum on Strategic Technology(IFOST 2011)(第六届国际战略技术论坛)
哈尔滨
英文
924-926
2011-08-22(万方平台首次上网日期,不代表论文的发表时间)