Comparative Analysis of the Impact of Operating Parameters on Military and Civil Applications of Mini Unmanned Aerial Vehicle (UAV)

被引：22
作者：
Ramesh, P. S. [1 ]
Jeyan, J. V. Muruga Lal [1 ]
机构：
[1] Lovely Profess Univ, Sch Mech Engn, Dept Aerosp, Jalandhar, India
来源：
3RD INTERNATIONAL CONFERENCE ON FRONTIERS IN AUTOMOBILE AND MECHANICAL ENGINEERING (FAME 2020) | 2020年 / 2311卷
关键词：
D O I：
10.1063/5.0033989
中图分类号：
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号：
0807 ; 0820 ;
摘要：
Mini Unmanned Aerial Vehicle (UAV) provides cost effective solutions to a variety of applications. Hence, the flying platform is being increasingly used for a multitude of applications, both military and civil. However, the requirement of operating parameters varies between the military and civil applications. Parameters like size, range, endurance, operating altitude, maximum take-off weight (MTOW) has implications both for the deployment and employment of UAVs. This paper explores the impact of the operating parameters on military and civil applications of Mini UAV.
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页数：10
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