Design, Manufacturing and Analysis of Unmanned Aerial Vehicle (UAV) |
Author(s): |
| Ansari Aadil Iqbal , Theem College of Engineering; Qureshi Abdullah, Theem College of Engineering; Sufyan Shaikh, Theem College of Engineering; Pawankumar Yadav, Theem College of Engineering |
Keywords: |
| UAV, Unmanned Aerial Vehicle, WING |
Abstract |
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To design the efficient aircraft capable of accurately lifting and dropping a humanitarian aid package from a certain height. Accurately predicting the lifting capacity of the aircraft is the essential part of the project. The wing, tail, fuselage and control systems have been designed by us. We have designed a mono plane aircraft of approximately 2kg in weight which can lift an object of 1 to 2kg. Thus the total weight of aircraft and object will be approximately 4kg. It is controlled by a remote device of frequency 2.4 GHz. |
Other Details |
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Paper ID: IJSRDV3I2056 Published in: Volume : 3, Issue : 2 Publication Date: 01/05/2015 Page(s): 95-97 |
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