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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2013
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Article
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Fig 3
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Research Article
Attitude Control of a Single Tilt Tri-Rotor UAV System: Dynamic Modeling and Each Channel's Nonlinear Controllers Design
Figure 3
Nonlinear model with LQR control gain in each channel.
(a)
Roll
(b)
Pitch
(c)
Yaw