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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2015
/
Article
/
Tab 2
/
Research Article
Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker
Table 2
Comparison of trim analysis results between wind tunnel test and mathematical modeling [
13
].
ā
(
)
RPM
(deg.)
(deg.)
Wind tunnel test
5
5880
10
5844
15
5752
Mathematical modeling
5
5907
10
5647
15
5602