• B.John Wesley
• B.Sandeep
• N.Praveena
• K.Sanjay Preetham
• K.Sankar Mahadev

This paper goal is to design a (UAV) Un Manned Aerial Vehicle (Quad copter) capable of self-sustained flight via wireless communications while utilizing a microcontroller. Quad copter is an aerial vehicle operated to fly independently and is one of the representations of a UAV.Drones are of different types and have different configurations for example, bi-copters, tri-copters, quad-copters, hexa-copters, etc. They have different uses and accordingly respective configurations are used. Control of motion of vehicle is achieved by altering the rotating rate of one or more discs, there by changing its torque and thrust/lift characteristics. Quad-copters have different structures and designs according to the work needed to be done by it. Components like motors, batteries electronic speed controllers (ESC’s) also vary according to the power needed and work done by the quad-copter. Also enhancements like GPS trackers or cameras or infrared cameras are used also that they could add value to missions like disaster relief, search and rescue, agriculture and 3D mapping of the geography of an area.

Quad Copter, Wireless Communication, Bernoulli's Principle, Newton's Third Law,, GPS, Micro Controller

"DESIGN & FABRICATION OF UNMANNED AERIAL VEHICLE (UAV)", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 5, page no.231_240, May-2019, Available :http://www.jetir.org/papers/JETIRBT06033.pdf

"DESIGN & FABRICATION OF UNMANNED AERIAL VEHICLE (UAV)", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 5, page no. pp231_240, May-2019, Available at : http://www.jetir.org/papers/JETIRBT06033.pdf