Folding Mechanism Design and Analysis of High-Altitude Gliding UUV Wings

摘要：

　　High-altitude gliding unmanned underwater vehicles(HAGUUVs)are released in high attitude and works in water after a short glide in the air.According to the High-altitude Gliding UUV airborne emission requirements,the folding mechanism of wings of the HAGUUV is desighed.On the basis of mechanics analysis of the organization,the dynamics modeling of organizations unfolding process is given by using Lagrange equation,and the wings unfolding movement characteristics are discussed through numerical simulation.Analysis results show that the designed folding mechanism can achieve the requirement of High-altitude gliding system performance,and provides theoretical guidance for further drop experiment.

关键词： high-altitude gliding folding wing dynamics modeling numerical simulation

作者: Yilin Li Baowei Song

作者单位: School of Marine Science and Technology Northwestern Polytechnical University Xian,China

会议类型: 国际会议

会议名称: 2017 IEEE 2nd Advanced Information Technology,Electronic and Automation Control Conference(IAEAC 2017)(2017 IEEE 第2届先进信息技术、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: 1948-1951

在线出版日期: 2017-03-25（万方平台首次上网日期，不代表论文的发表时间）