Adaptive proportional navigation under side window detection

摘要：

　　This paper investigates the guidance and control problem for missile with the seeker mounted in the side window.To effectively coordinate the flight trajectory and attitude of missile,expand the detection range of target and enhance guidance accuracy,a novel guidance law based on the adaptive technique is proposed.And the navigation ratio changes adaptively as the missile lead angle varies.Numerical simulation results show that the applicability of adaptive proportional navigation is wider than that of parallel navigation and conventional proportional navigation,thus,the guidance law proposed in this paper has a better combination property.

关键词： Guidance System Side Window Detection Adaptive Algorithms Proportional Navigation Parallel Navigation

作者: Ying Yu Mingshan Hou Chunwu Yin

作者单位: School of Automation Northwestern Polytechnical University Xian City, Shanxi Province,China, 710129

会议类型: 国际会议

会议名称: 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference(IAEAC 2015)(2015 IEEE先进信息技术,电子与自动化控制国际会议)

会议地点: 重庆

会议语种:英文

页码: 631-635

在线出版日期: 2015-12-19（万方平台首次上网日期，不代表论文的发表时间）