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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. Measuring thrust interaction  Top : Total thrust and thrust off interaction
Figure 7. Inputs and outputs of the analytical model
Figure  14  shows  a  synthetic  way,  efforts  created  during  tilting  rotors.  These  results  show  that  the  tilting  of  the  rotors  can  be  used  to  generate  pure  forces  or  moments  pure
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