| CPC G01D 5/12 (2013.01) [H01F 21/06 (2013.01); H01F 27/02 (2013.01)] | 8 Claims |

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1. A rotary variable differential transducer comprising:
a housing;
an armature shaft included within the housing;
an input shaft configured to mate with an airplane shaft, wherein the input shaft is independent from the armature shaft;
a segmented anti-backlash gear attached to the armature shaft;
a pinion gear shaft assembly configured to drive the segmented anti-backlash gear thereby creating a single stage gear reducer assembly; and
a plurality of stop pins included on each side of the segmented anti-backlash gear, wherein the plurality of stop pins configured to prevent the segmented anti-backlash gear from disengaging with the pinion gear shaft.
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