FIELD: weapons and ammunition.
SUBSTANCE: proposed system comprises ballistic computer, unit of manual corrections with its outputs (by number of corrections) are connected to relevant inputs of said ballistic computer, ballistics switch, laser range finder and wind pickup, upward airflow pickup, first and second squaring devices, control board, sight, adder, vertical guidance drive and gun, scaling unit, multiplier and matching device, all connected in series. It differs front know designs in that additionally included are missile guidance system comprising guided missile gravity compensation unit, coordinator, control signal generator, extra adder, control command generator and command transmission line, excess unit, third squaring device, unit of constants, two switches, three extra scaling units, inverter, upward and lengthwise airflow transducers, third squaring device, third extra scaling unit and excess unit with appropriate links.
EFFECT: higher efficiency of fire by guided missile.
1 dwg
Title | Year | Author | Number |
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GUIDANCE SYSTEM OF CONTROLLED MISSILES | 2010 |
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RU2275581C1 |
Authors
Dates
2011-09-20—Published
2009-10-30—Filed