Design of a Variable Structure Adaptive Midcourse Guidance Law

摘要：

Applying the concept of the generalized interception spot,basing oil the variable structure adaptive theory and choosing the relative velocity deflection angle as the sliding-mode,a variable structure adaptive midcourse guidance law is designed.The simulation results show that the indexes of the missile perfectly fulfill the need,which validates the feasibility and the effectivity of the designed guidance law.

关键词： the generalized interception spot variable structure adaptive the relative velocity deflection angle midcourse guidance law

作者: Hu Yun-an Zhao Yong-tao Liu Jian-cheng Wang ying

会议类型: 国际会议

会议名称: The International Conference Information Computing and Automation(2007国际信息计算与自动化会议)

会议地点: 成都

会议语种:英文

页码: 1088-1091

在线出版日期: 2007-12-19（万方平台首次上网日期，不代表论文的发表时间）