| 摘要 |
radio control, applicable in semi-active and passive homing systems of flight vehicles for homing on an air target. SUBSTANCE: the method consists in formation of control signals in the horizontal and vertical planes acting on the flight vehicle control surfaces and determined by relations , where js- is the current value of linear acceleration of the flight vehicle; is the angular rate of rotation of the sighting line; k is the gain, Va is the flight speed of the flight vehicle; deltas is the correction; p is the attenuation coefficient. The device for formation of flight vehicle control signals has an antenna, direction finder, hydrostabilizer, autopilot, vertical and horizontal control surfaces, formation channels of control signals in the horizontal and vertical planes, as well as a flight vehicle flight speed meter and formation channels of control signal corrections in the horizontal and vertical planes. EFFECT: reduced time of flight to the lead point of impact with the target. 2 cl, 4 dwg
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