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A Vectoring Thrust Coaxial Rotor for Micro Air Vehicle: Modeling, Design and Analysis

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Figure

Figure 1. Control mechanism  based on pivoting rotors
Figure 4. Comparison between the theoretical model and  experimental data, for the Mz component  (Iso-Fz versus Rpm U  & Rpm L  Thick lines : Measurments  Thin lines : Theoretical model Black line : Rpm U  = Rpm L)

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