FIELD: airpower.
SUBSTANCE: three-coordinate manual control station contains a steering wheel, walking beams, rods, brackets. Wherein the station has an additional degree of freedom in the control of the roll, relative to the longitudinal axis of the aircraft (AC), which is provided by installing a thin-walled tube fixed in the hinges. Inside the tube, as far as the walking axis passes, the steering rods of the elevator and the rudder pass, which almost excludes the influence of roll channel on elevator and rudder.
EFFECT: independent simultaneous pitch, roll and yaw control, simple design.
4 dwg
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