| 摘要 |
Device for measurement of angular deflection of rudder surface of aircraft includes IR diode as emitter, clip for its fixation, photoreceivers that react on infrared radiation, those are fixed on holder that is arc of circle described by rudder surface with radius equal to length of rudder surface, at that arc of circle is placed in plane normal to rudder surface of aircraft, photo-diodes are connected to inputs of electronic circuit of signal processing. To the device element of construction is included, as metal arc that has 8n openings for installation of photoreceivers fixed to fixed surface of the aircraft. |
