首页 | 本学科首页   官方微博 | 高级检索  
     

无人机投放分离特性仿真与优化
引用本文:曾丽芳,黎军,王天琪,邵雪明. 无人机投放分离特性仿真与优化[J]. 气体物理, 2022, 7(4): 19-27. DOI: 10.19527/j.cnki.2096-1642.0923
作者姓名:曾丽芳  黎军  王天琪  邵雪明
作者单位:浙江大学航空航天学院, 浙江 杭州 310027
基金项目:浙江省重点研发计划2020C05001
摘    要:用于远程投放作战的无人机在与母机分离的过程中, 其姿态变化与运动轨迹直接影响母机的安全性和自身稳定性。基于重叠网格技术, 提出了一种流体-刚体运动耦合数值模拟方法, 对无人机动态投放分离过程进行仿真。采用WPFS标模进行计算, 发现仿真与试验结果吻合度高, 数值模拟方法得到有效验证。采用上述数值模拟方法实现无人机投放过程的仿真, 得到无人机在投放分离过程中位置与姿态随时间的变化规律。进一步基于仿真结果, 完成了无人机弹射方案的优化设计。 

关 键 词:投放分离   数值模拟   重叠网格   无人机   稳定性
收稿时间:2021-03-12

Simulation and Optimization of the Separation Process for UAV
Affiliation:School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China
Abstract:In the separation process of long-range-launched UAV, the attitude change and trajectory directly affect the safety and stability of the parent aircraft. In this paper, based on overset grids, a fluid and rigid body motion coupling method was proposed to simulate the dynamic separation process of UAV. WPFS standard model was used for validation. It is found that the simulation results are in good agreement with the experimental data, and the numerical simulation method is effectively verified. The simulation of UAV separation process was realized by using the proposed numerical simulation method, and the change of UAV's position and attitude with time in the process of separation was obtained. Based on the simulation results, an optimal design of UAV launching scheme was proposed. 
Keywords:
点击此处可从《气体物理》浏览原始摘要信息
点击此处可从《气体物理》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号