| 无人机绳钩回收仿真研究 |
| |
| 引用本文： | 孙林峰,马晓平,吴佳凯.无人机绳钩回收仿真研究[J].科学技术与工程,2012,12(7):1572-1575. |
| |
| 作者姓名： | 孙林峰 马晓平 吴佳凯 |
| |
| 作者单位： | 西北工业大学无人机特种技术国家级重点实验室,西安,710072 |
| |
| 摘 要： | 比较了几种典型的固定翼无人机回收方式，针对舰载无人机，分析了绳钩回收方式的优点，给出了绳钩回收方案。通过分析绳钩回收情况下无人机的受力状态，建立起无人机绳钩回收仿真模型，并以某型舰载无人机为对象，在Maltab/Simulink中进行仿真验证。仿真结果可以得出无人机过载和回收制动力都在合理范围内，表明本文无人机绳钩回收方式是可行的。
|
| 关 键 词： | 无人机 绳钩回收 回收制动力 |
| 收稿时间： | 12/7/2011 5:01:23 PM |
| 修稿时间： | 2011/12/19 0:00:00 |
Simulation research of Rope-Hook Recovery for Unmanned Aerial Vehicle |
| |
| sun lin feng,ma xiao ping and wu jia kai.Simulation research of Rope-Hook Recovery for Unmanned Aerial Vehicle[J].Science Technology and Engineering,2012,12(7):1572-1575. |
| |
| Authors: | sun lin feng ma xiao ping and wu jia kai |
| |
| Institution: | (National Key Laboratory of Science and Technology on UAV at Northwest Polytechnic University,Xi’an 710072,P.R.China) |
| |
| Abstract: | Some typical recovery methods for fixed wing UAV discisussed.In view of the shipborne UAV’s usage characteristics, the process and advantages of the Rope-Hook Recovery are introduced.Then the stress state of UAV under Rope-Hook Recovery is analyzed.At last the Rope-Hook Recovery model for UAV is built and simulatated in Maltab/Simulink.The simulation results show that,the gload and recovery brake force of UAV is in the go range.The UAV’s Rope-Hook Recovery method is feasible. |
| |
| Keywords: | UAV(Unmanned Aerial Vehicle) rope-hook recovery system recovery brake force |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《科学技术与工程》浏览原始摘要信息 |
| 点击此处可从《科学技术与工程》下载免费的PDF全文 |
