旋翼无人机集群快速收发装置设计与动力学仿真分析  

Design and Dynamics Simulation Analysis of Launch and Recovery Device for UAV Cluster

作　　者：鹿迎 朱效洲 桂健钧 姚雯 邓宝松 LU Ying;ZHU Xiaozhou;GUI Jianjun;YAO Wen;DENG Baosong(National Innovation Institute of Defense Technology,Academy of Military Sciences,Beijing 100071,China)

机构地区：[1]军事科学院国防科技创新研究院,北京100071

出　　处：《机械设计与研究》2022年第2期61-65,共5页Machine Design And Research

基　　金：国家自然科学基金资助项目(61902423)。

摘　　要：介绍了无人机集群技术的基本概念,重点阐述了无人机集群发射与回收技术的发展现状,针对旋翼无人机集群发射与回收问题,开展了旋翼无人机和收发装置结构设计。设计了可以堆叠存放的无人机机身结构,解决了无人机密集存储的问题。设计的收发装置包括筒形外壳和剪刀式升降平台,用于实现无人机的自主起飞发射和降落回收。针对设计的原型系统,基于多体动力学仿真软件Recurdyn建立虚拟样机,进行机构运动学和动力学仿真分析,验证了设计的可行性。The fundamentals of the unmanned aerial vehicle swarm(UAVS)are presented in this paper,and the development on UAV launch and recovery technology is elaborated.Aiming at the problem of launch and recovery of UAVs,the structural design of UAVs and“hive”is carried out.A stackable UAV shell is designed and the UAVS are placed compactly.The"hive"is composed of a cylinder and a lifting platform.The dynamic simulation analysis is carried out to verify the feasibility of the design based on software named Recurdyn.

关 键 词：无人机发射回收 回收装置设计 动力学分析 结构设计 

分 类 号：TH13[机械工程—机械制造及自动化] TP2[自动化与计算机技术—检测技术与自动化装置]