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2 146 353

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C1

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IPC

(21) (22)

Application

98120585/02, 1998-11-13

(24)

Start date

1998-11-13

(22)

Actual filing date

1998-11-13

(45)

Published

2000-03-10

(72)

Inventor

Arkhangel'Skij I.I.Bolotov E.G.Mizrokhi V.Ja.Svetlov V.G.

(73)

Holder

Mashinostroitel'Noe Konstruktorskoe Bjuro Im.Akad.P.D.Grushina

DEVICE CONTROLLING HIGH-MANEUVERABILITY ROCKET Russian patent published in 2000 - IPC

Abstract RU 2146353 C1

FIELD: rocket engineering. SUBSTANCE: invention is specifically related to guided rockets launched on to targets which homing heads needed intensive maneuvering for interception over high-precision direction finding section directly before point of impact. Given invention involves measurement of angular velocity of sighting line over section of direction finding of target by homing head to specify correcting force, action with correcting force in direction perpendicular to longitudinal axis of missile approaching target. Phase misalignment between vector of miss and vector of correcting force is measured in process of action and additional correcting force is formed to diminish orthogonal component of miss. In particular case technical result is achieved by continuous turn of vector of correcting force in process of its action for alignment with vector of miss relative to longitudinal axis of rocket. EFFECT: increased guidance precision. 2 cl, 9 dwg

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RU 2 146 353 C1

Authors

Arkhangel'Skij I.I.

Bolotov E.G.

Mizrokhi V.Ja.

Svetlov V.G.

Dates

2000-03-10—Published

1998-11-13—Filed

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