Research on Adaptive Guidance Technology of UAV Ship Landing System Based on Net Recovery

摘要：

　　According to the characteristics of the target ship in motion in the net recovery process of UAV,this paper put forward the guidance law based on angle of sight by taking missile guidance law of proportional guidance law for reference,and introduced the backstepping guidance law to improve the adaptability of guidance law.Since the angle of sight guidance law is to make the UAV flight path angle and angle of sight be proportional to the rate of change,flight path angle can be tracked by controlling the angle of sight.That taking the guidance law into use can reduce the sensitivity of UAV motion on the ship parameters change,thereby to obtain more stable trajectory.The simulation shows the feasibility of this guidance law,and has strong robustness.

关键词： UAV ship landing net recovery proportional guidance

作者: Wang Kai Sun Chunzhen Jiang Yi

作者单位: Nanjing University of Aeronautics and Astronautics,29 Yudao St.Nanjing 210016,China

会议类型: 国际会议

会议名称: 2014 Asia-Pacific International Symposium on Aerospace Technology(2014亚太航空航天技术学术会议)

会议地点: 上海

会议语种:英文

页码: 1-8

在线出版日期: 2014-09-24（万方平台首次上网日期，不代表论文的发表时间）