FIELD: military equipment. SUBSTANCE: according to invention two sight lines are formed and matched with target. Deviations of rocket from first and second sight lines are measured and control instructions are formed in correspondence with its deviation from specified sight lines and signal to controls of rocket is generated in accordance with sum of first and second control commands. EFFECT: enhanced accuracy and speed of guidance system, noise immunity and protection in process of shooting. 1 cl, 1 dwg
Title | Year | Author | Number |
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Authors
Dates
2002-11-10—Published
2000-07-04—Filed