| http://www.w3.org/ns/prov#value | - The attitude processor 12 of FIG. 7 receives input voltages proportional to the angular rate of the aircraft in the a, b and c axes of the aircraft where the a axis describes the axis from nose to tail of the aircraft in the aircraft plane AP, c describes the axis extending out the left wing of the aircraft in the aircraft plane AP and b is a vector extending out the top of the aircraft perpendicu
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