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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Fig 19
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Research Article
Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance
Figure 19
Roll rate of the FMW with closed-loop wing warping double: (a) rudder inputs from pilot; (b) roll rates of the FMW mini-UAV.
(a)
(b)