南京航空航天大学学报2012，Vol.44Issue(1)：14-19,6.
无人机伞回收动力学分析
Dynamics Analysis on Parachute Recovery of Unmanned Aerial Vehicle
郭亮 1张红英 2童明波2
作者信息
- 1. 成都飞机设计研究所,成都,610041
- 2. 南京航空航天大学飞行器先进设计技术国防重点学科实验室,南京,210016
- 折叠
摘要
Abstract
Based on six degrees of freedom(DOF) flight dynamics model of UAV and parachute recovery dynamic model , a quantitative prediction of the whole motion process is given after simulation. For validating the method, a comparison is made between the computational results and available flight test data , and achieves favorable agreement. The simulation results include relative movement of UAV and recovery system and predict dangerous situations at recovery stage, which are an important reference for the design of UAV control law and recovery system.关键词
无人机/回收/伞系统/动力学Key words
unmanned aerial vehicle/ recovery/ parachute system/ dynamics分类
数理科学引用本文复制引用
郭亮,张红英,童明波..无人机伞回收动力学分析[J].南京航空航天大学学报,2012,44(1):14-19,6.
