NDLI: Unmanned Aerial Vehicles (UAV): Design Trends

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Unmanned Aerial Vehicles (UAV): Design Trends

Content Provider	The American Society of Mechanical Engineers (ASME) Digital Collection
Author	Shetty, Devdas Manzione, Louis
Copyright Year	2011
Abstract	This paper looks at the trends in design procedures in Unmanned Aerial Vehicles (UAVs). Rapid advances in technology are enabling more and more capability to be placed on smaller airframes which is spurring a large increase in the number of UAVs being deployed in the army. The military role of UAV is growing at unprecedented rates. The UAV is an acronym for Unmanned Aerial Vehicle, which is an aircraft with no pilot on board. UAVs can be remote controlled aircraft (e.g. flown by a pilot at a ground control station) or can fly autonomously based on pre-programmed flight plans or more complex dynamic automation systems. A variety of design configurations are in use. The primary driving parameters in all UAVs is the need for maximizing available wing area and wing effectiveness, while minimizing the required storage volume. The major factors in determining the relative merit of the different concepts are the evaluation of structural viability, mechanical complexity and overall system survivability by G forces. This paper examines some of the design methodologies and hardware-in-the loop simulation environment to support and validate the UAV hardware and software development.
Starting Page	345
Ending Page	352
Page Count	8
File Format	PDF
ISBN	9780791854877
DOI	10.1115/IMECE2011-64518
Volume Number	Volume 1: Advances in Aerospace Technology; Energy Water Nexus; Globalization of Engineering; Posters
Conference Proceedings	ASME 2011 International Mechanical Engineering Congress and Exposition
Language	English
Publisher Date	2011-11-11
Publisher Place	Denver, Colorado, USA
Access Restriction	Subscribed
Subject Keyword	G-test Aerodynamic design Unmanned aerial vehicles Uav Projectile Hardware in the loop Design Hardware
Content Type	Text
Resource Type	Article

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