FIELD: rocket equipment.
SUBSTANCE: rotating self-guided missile relates to defense equipment and can be used in missiles with single-channel control, launched from the shoulder, as well as from various carriers, providing, including, salvo firing on air targets. Rotating self-guided missile comprises an engine, a wing unit and an instrument compartment. Instrument compartment includes a rocket body position sensor and an electric drive of the missile control elements, an optical homing head. Optical head includes corrected gyroscope with correction winding, bearing winding, gyro rotor position sensor winding, reference signal former, exit sensor and autopilot. Autopilot has a missile turning circuit at the initial section.
EFFECT: easier sighting and carrier control during start-up, reduced time for preparation and launching.
1 cl, 2 dwg
| Title | Year | Author | Number |
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