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2 269 452

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C2

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IPC

B64C13/00(2006-01-01)

B64D1/00(2006-01-01)

(21) (22)

Application

2004110774/11, 2004-04-12

(24)

Start date

2004-04-12

(22)

Actual filing date

2004-04-12

(45)

Published

2006-02-10

(72)

Inventor

Demchenko Oleg FedorovichDolzhenkov Nikolaj NikolaevichPopovich Konstantin FedorovichMatveev Andrej IvanovichShkolin Vladimir PetrovichKalugin Vjacheslav GeorgievichShapovalov Viktor NikolaevichKodola Valerij Grigor'EvichGorbachevskij Andrej Alekseevich

(73)

Holder

Oao Im. A.S. Jakovleva"Demchenko Oleg FedorovichDolzhenkov Nikolaj NikolaevichPopovich Konstantin FedorovichMatveev Andrej IvanovichShkolin Vladimir PetrovichKalugin Vjacheslav GeorgievichShapovalov Viktor NikolaevichKodola Valerij Grigor'EvichGorbachevskij Andrej Alekseevich

METHOD OF CONTROL OF FLYING VEHICLE AFTER LAUNCHING MISSILE Russian patent published in 2006 - IPC B64C13/00 B64D1/00 

Abstract RU 2269452 C2

FIELD: military aviation; conducting aerial combat.

SUBSTANCE: after launching the missile, aircraft is turned-away to orthogonal course which is corrected continuously for maintaining its orthogonality. Antenna of aircraft onboard radar station is turned in synchronism with aircraft turning-away, thus ensuring tracking the enemy aircraft and guidance of missile. Simultaneously with aircraft turning-away to orthogonal course, its flying altitude is reduced. Probable obstacles during orthogonal maneuver are revealed by means of onboard laser radar for enveloping them.

EFFECT: enhanced safety of aircraft.

2 cl, 8 dwg

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RU 2 269 452 C2

Authors

Demchenko Oleg Fedorovich

Dolzhenkov Nikolaj Nikolaevich

Popovich Konstantin Fedorovich

Matveev Andrej Ivanovich

Shkolin Vladimir Petrovich

Kalugin Vjacheslav Georgievich

Shapovalov Viktor Nikolaevich

Kodola Valerij Grigor'Evich

Gorbachevskij Andrej Alekseevich

Dates

2006-02-10—Published

2004-04-12—Filed

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