| 摘要 |
FIELD: FOR TELEORIENTATION OF GUIDED OBJECTIVES, OPTICAL SIGHT OF GUIDED MISSILE GUIDANCE SYSTEM AND PULSE SHAPER. ^ FIELD: remote control of flight vehicles. ^ SUBSTANCE: the invention consists in bringing the searchlight emission in the sighting channel, formation of elision only at the moments when the time intervals between the pulses are equal to the reference values, visualization of the emission that has passed through the sighting channel. Besides, defection of the emission that has passed through the sighting channel. Besides, deflection of the searchlight optical flux in two mutually perpendicular directions is accomplished, which provides for alignment of the sight optical axis and the searchlight information axis. A rotary prism is introduced in the guidance optical sight, and the sighting channel is made on the basis of a TV camera, monitor, sighting mark forming unit, and a sighting mark position control panel. Two AMD circuits and a series-connected decoder and an OR circuit with respective couplings are introduced in the pulse shaper. ^ EFFECT: enhanced accuracy of guidance of the controlled objective. ^ 4 cl, 4 dwg, 1 ex |
