AA MISSILE GUIDANCE SYSTEM Russian patent published in 2010 - IPC F41G7/22 F42B15/01 

Abstract RU 2400690 C1

FIELD: weapons and ammunition.

SUBSTANCE: proposed system compares signals from optical and IR digital photo cameras and radar signal to differentiate between true and false targets. System generates anticipation trajectory via feedback between rudders with movable homing head, that is, the latter turns in direction opposite the rudder deviation unless the rudders stay in neutral position. System can perform leading anticipation towards airframe via shifting rudders position transducer neutral toward the side coinciding with homing head deviation, or its additional deviation toward the same side.

EFFECT: high probability of heating maneuvering target.

4 cl, 3 dwg

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RU 2 400 690 C1

Authors

Staroverov Nikolaj Evgen'Evich

Dates

2010-09-27Published

2009-03-19Filed