| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: principle of optic beam guidance of a missile launching from a mobile carrier includes formation on the carrier of a laser beam with an information control field, guidance on a target of an optic sight, the axis of which is aligned with the information field axis, orientation of the launching system axis in the beam axis direction, launch of the missile with retracted aerodynamic rudders and introduction of the missile to the information field, opening on the missile of an emission receiver and shaping of control commands depending on position of the missile relative to the information field axis, extension of aerodynamic rudders and their deviation. At the moment of the missile ejection an angular position of the launching system axis relative to the coordinate system related to the carrier, as well as angular position of the carrier relative to the earth referenced coordinate system is stored; extension of rudders is performed with time delay relative to the emission receiver opening; at the moment of opening of the emission receiver the beam information field axis is aligned with the launching system position stored at the missile ejection moment, and at the point of time of rudders extension the alignment of laser beam information field axis with the target sighting line is started.EFFECT: improving accuracy and reducing the time required for placing of the missile in the beam axis.2 cl, 5 dwg |
