海军航空工程学院学报2017，Vol.32Issue(5)：447-451,468,6.DOI:10.7682/j.issn.1673-1522.2017.05.006
小型固定翼无人机零长发射参数安全边界研究
Reasearch on Zero-Length Launch Parameters'Secure Border Investigation of Small Fixed Wing UAV
陶于金1
作者信息
- 1. 西北工业大学无人机研究所,西安710065
- 折叠
摘要
Abstract
According to the requirement of zero-length launch simulation for small propeller unmanned aerial vehicle,a more refined dynamic model was proposed.The installation angle of rocket used for launching on the unmanned aerial ve?hicle could directly affect the launching safety,which is also the most important parameter to adjust in thrust line design. Based on an unmanned aerial vehicle,the launch process of booster rocket deviated from the center of gravity in longitudi?nal and lateral direction was simulated.The secure border of installation angle was conformed,which could be used as the benchmark in thrust line design.关键词
小型无人机/仿真/零长发射/安全边界Key words
small UAV/simulation/zero-length launch/security border分类
航空航天引用本文复制引用
陶于金..小型固定翼无人机零长发射参数安全边界研究[J].海军航空工程学院学报,2017,32(5):447-451,468,6.
