Flight Characterization of Small Scale UAV

Honors College Thesis

公开 Deposited

Citeable URL: https://ir.library.oregonstate.edu/concern/honors_college_theses/df65v9764

Descriptions

Attribute Name	Values
Creator	Scheer, Jacob
Abstract	The purpose of this thesis was to understand the relation between the actual performance and the design performance of the manufacturing plane which was designed for the 2016 Design/Build/Fly competition. The actual performance was determined using an Arduino Uno based system with data from an accelerometer, gyroscope and pitot tube. While the data did not represent a statistically significant sample size it did suggest a few things: o The cruise speed and takeoff speed while similar were slightly lower than the analytical results. o The turning radius was slightly higher than expected, but at a lower airspeed. o The aircraft is statically stable, but improvements in trim can be used to change the steady state settling angle. Key Words: UAV, Airplane, Arduino, Flight Characterization
License	All rights reserved
Resource Type	Honors College Thesis
Date Available	2016-06-07T16:26:23+00:00
Date Issued	2016-05-27
Degree Level	Bachelor's
Degree Name	Honors Bachelor of Science (H.B.S.)
Degree Field	Mechanical Engineering
Degree Grantor	Oregon State University
Commencement Year	2016
Advisor	Squires, Nancy
Non-Academic Affiliation	Oregon State University. Honors College
权利声明	In Copyright
Funding Statement (additional comments about funding)	Nancy Squires
Publisher	Oregon State University
Peer Reviewed	No
Language	English [eng]
Replaces	http://hdl.handle.net/1957/59077

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