机械制造与自动化2025，Vol.54Issue(2)：258-261,4.DOI:10.19344/j.cnki.issn1671-5276.2025.02.050
某型无人机助推火箭推力线偏差优化设计及安全影响分析
Optimal Design and Safety Impact Analysis of Thrust Line Deviation of Rocket-assisted UAV
袁小磊 1张栋 1马少博 1邵振宇 1朱寓卿1
作者信息
- 1. 航天时代飞鸿技术有限公司,北京 100094
- 折叠
摘要
Abstract
Rocket-assisted launch is a widely used method for UAV take-off,and thrust line deviation is the key to the safe and stable launch of rocket-assisted UAV.This paper formulates a measurement method for thrust line deviation for a certain medium-range high-speed fixed-wing UAV,and analyzes the safety impact of thrust line deviation combined with a dynamic simulation model,obtaining the optimal design range of thrust line deviation.The flight test results show that the design is reasonable and feasible,and can be of quantitative standard for UAV thrust line adjustment ensuring safe and reliable UAV launch.关键词
火箭助推/固定翼无人机/推力线/安全影响Key words
rocket-assisted/fixed-wing UAV/thrust line/safety impact分类
航空航天引用本文复制引用
袁小磊,张栋,马少博,邵振宇,朱寓卿..某型无人机助推火箭推力线偏差优化设计及安全影响分析[J].机械制造与自动化,2025,54(2):258-261,4.
