FIELD: armaments and ammunition.
SUBSTANCE: inertial-satellite guidance system represents the air bomb self-guidance system. At the trajectory final path, self-guidance is made by thermal imager self-guidance head incorporating a correlation algorithm of data processing. The reference target image is input prior to dropping the bomb. The air bomb aerodynamic structure realises a minor static stability which allows low-power steering mechanisms with a small-area aerodynamic rudder to deviate the bomb by major angles of attack thus providing its high maneuverability. The bomb guidance system generates curved hitting trajectories to provided high accuracy and efficiency. The differential error antenna allows a final accuracy of 3 to 5 m.
EFFECT: precise guidance of air bomb at curbed trajectories at invariable grouping of satellites.
2 dwg
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