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2 231 735

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IPC

(21) (22)

Application

2003127770/02, 2003-09-16

(24)

Start date

2003-09-16

(22)

Actual filing date

2003-09-16

(45)

Published

2004-06-27

(72)

Inventor

Vishnevskij V.S.Vishnevskij A.V.Kukushkin V.N.Balabanov Ju.V.Supalov V.A.Merzljakov G.V.Toporov M.I.Vanetsian R.A.Osipov A.A.Barynin V.A.Dolaberidze Ju.I.Galjutin Ju.A.

(73)

Holder

Zakrytoe Aktsionernoe Obshchestvo Nauchno-Tekhnicheskij Kompleks I Mekhanizatsija Tekhnologij"

METHOD AND SYSTEM OF GUIDANCE OF SPIN-STABILIZED MISSILE BY FREQUENCY LASER RADIATION REFLECTED FROM TARGET Russian patent published in 2004 - IPC

Abstract RU 2231735 C1

FIELD: armament, in particular, artillery guided missiles with laser guidance.

SUBSTANCE: target lighting is switched on at the final section of the trajectory, then analog signals are formed with the aid of the optoelectronic correction head. These signals are numbered and introduced in a microprocessor for computation of the missile angular velocity spin, as well as of the value and phase of the miss. According to the number of the impulse vernier engine selected by the program, the signal of its starting is formed at the time instant computer with due account made for the tubular dependence of the corrective pulse length on the engine powder charge. The guidance system has functional units and circuits required for realization of the method.

EFFECT: enhanced accuracy and simplified guidance system.

2 cl, 3 dwg

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RU 2 231 735 C1

Authors

Vishnevskij V.S.

Vishnevskij A.V.

Kukushkin V.N.

Balabanov Ju.V.

Supalov V.A.

Merzljakov G.V.

Toporov M.I.

Vanetsian R.A.

Osipov A.A.

Barynin V.A.

Dolaberidze Ju.I.

Galjutin Ju.A.

Dates

2004-06-27—Published

2003-09-16—Filed