Dynamic Analysis and Optimization of Pneumatic Wedge-Shaped Launcher for UAV

• 作 者: Huang Min He Cheng Pei Jinhua
• 机 构: CollegeofAerospaceEngineering,KeyLaboratoryofUAV’sAdvancedTechnology（NanjingUniversityofAeronauticsa
• 出 处: 南京航空航天大学学报：英文版
• 发表日期: 2018年5期
• 关键词: unmanned AERIAL vehicle PNEUMATIC LAUNCHING dynamic simulation system optimizati
• 基金项目: This work was supported by the National Natural Science Foundation of China(No.11602105),and the Natural Science Foundation of Jiangsu Province(No.BK20160782).

The constitution,structure,working principle and launching process of the wedge-shaped pneumatic launcher of an unmanned aerial vehicle(UAV)are described.By simplifying its physical model,two dynamic models of the UAV launch system are established based o