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2 365 852

(13)

(51)

IPC

F41G3/22(2006-01-01)

(21) (22)

Application

2008103817/02, 2008-02-06

(24)

Start date

2008-02-06

(22)

Actual filing date

2008-02-06

(45)

Published

2009-08-27

(72)

Inventor

Derjugin Boris BorisovichDiib Bassam AkhmedMan'Ko Valerij LeonidovichStarostin Mikhail MikhajlovichTkachenko Vladimir IvanovichTkachenko Natalija VladimirovnaShul'Ga Sergej Vladimirovich

(73)

Holder

Obshchevojskovaja Akademija Vooruzhennykh Sil Rossijskoj Federatsii Vs Rf)

MISSILE GUIDANCE METHOD Russian patent published in 2009 - IPC F41G3/22

Abstract RU 2365852 C1

FIELD: arms.

SUBSTANCE: proposed method comprises measuring the range to target, determining direction linear speed the aiming line changes at. Distance to target is measured allowing for measurement errors and time passed after range finding. Aiming line is shifted towards lower departure with linear speed directly proportional to linear crosswise speed and inversely proportional to the sum or difference.

EFFECT: reduced, by 25 to 30%, error of aiming line stabilisation and 10 to 15%-higher efficiency of fire in conditions of interferences.

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RU 2 365 852 C1

Authors

Derjugin Boris Borisovich

Diib Bassam Akhmed

Man'Ko Valerij Leonidovich

Starostin Mikhail Mikhajlovich

Tkachenko Vladimir Ivanovich

Tkachenko Natalija Vladimirovna

Shul'Ga Sergej Vladimirovich

Dates

2009-08-27—Published

2008-02-06—Filed