指挥控制与仿真2016，Vol.38Issue(6)：109-112,4.DOI:10.3969/j.issn.1673-3819.2016.06.023
无人机伞降回收系统设计与实现
Design and Implementation of P arachute Recovery System for Unmanned Aerial Vehicle
刘靖1
作者信息
- 1. 解放军92419部队，辽宁 兴城 125106
- 折叠
摘要
Abstract
Based on studying the composition and working principle of the parachute recovery system for a certain unmanned aerial vehicle, the recovery system is detailed designed according to the general requirements of the UAV. Considering the dynamic load of opening the parachute, landing speed and recovery damping requirements, the system uses a guiding decel⁃erating parachute, the main parachute convergent technology and the damping airbag buffer. Through the simulation analysis and actual flight test validation, the system is designed to be reasonable and meet the recovery requirements.关键词
无人机/伞降回收/飞行试验Key words
unmanned aerial vehicle/parachute recovery/flight test分类
军事科技引用本文复制引用
刘靖..无人机伞降回收系统设计与实现[J].指挥控制与仿真,2016,38(6):109-112,4.
