| 摘要 |
Optron indicator of angular displacement of rudder surface of aircraft has emitter, clip for its fixation and holder that is arc of circle that is described with rudder surface, with radius equal to length of rudder surface. For improvement of output signals of indicator as emitter IR diode is used, and on holder photo-diodes are fixed, those react on infrared radiation. Photo-diodes are connected to inputs of electronic circuit for signal processing, this includes n comparison circuits, 8n elements AND. |
