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2 122 962

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C1

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IPC

(21) (22)

Application

98110928/28, 1998-06-17

(22)

Actual filing date

1998-06-17

(45)

Published

1998-12-10

(72)

Inventor

Troel'Nikov Ju.V.Feofanov V.V.Abramov V.A.

(73)

Holder

Aktsionernoe Obshchestvo Otkrytogo Tipa Sukhogo"

METHOD OF CONTROL OF CARRIER AEROPLANE AFTER LAUNCHING TV-and COMMAND GUIDED AIR-TO-SURFACE MISSILE Russian patent published in 1998 - IPC

Abstract RU 2122962 C1

FIELD: military aviation. SUBSTANCE: after launching guided missile, aeroplane starts climbing and turning away from target. After the line of communication of carrier aeroplane with guided missile is shifted from front antenna to rear antenna, control is effected in roll only at stabilization of altitude changing the magnitude of roll depending on change of angle of bearing on weapon of rear antenna. EFFECT: absence of limitations for maneuvering of carrier aeroplane.

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RU 2 122 962 C1

Authors

Troel'Nikov Ju.V.

Feofanov V.V.

Abramov V.A.

Dates

1998-12-10—Published

1998-06-17—Filed

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