海军航空工程学院学报2017，Vol.32Issue(5)：452-456,5.DOI:10.7682/j.issn.1673-1522.2017.05.007
基于Simulink的小型无人机弹射架性能仿真
Performance Simulation of Small UAV Ejection Frame Based on Simulink
摘要
Abstract
The ejection system dynamic model was established for the catapult launch analysis and design simulation plat?form to improve high credibility.The UAV catapult dynamics and kinematics model was established,by which the catapult launching system was researched in this paper.Based on the Matlab/Simulink module,the analyses were conducted on the elastic coefficient,elastic element guide rail length,the plane launch speed parameters.In the process of simulation,by changing different parameters of system,the influence law of these parameters on the ejection system performance was ob?tained.Reasonable matching these parameters,eject a variety of models of UAV could use this system,improve the effi?ciency,save the test resources and funds.At the same time it provided theory for UAV ejection system research and devel?opment.关键词
无人机/Simulink/弹射起飞/仿真模型Key words
UAV/Simulink/catapult launching/simulation model分类
航空航天引用本文复制引用
高永,孟浩,李冰,王玉伟..基于Simulink的小型无人机弹射架性能仿真[J].海军航空工程学院学报,2017,32(5):452-456,5.基金项目
"泰山学者"建设工程专项基金资助项目 （）
