GUIDED MISSILE GUIDANCE SYSTEM Russian patent published in 2010 - IPC F41G7/26 

Abstract RU 2382315 C1

FIELD: weapons.

SUBSTANCE: invention relates to guidance systems and can be incorporated with tank and antitank complexes as well as in small-size antiaircraft complexes. Control station additionally incorporates unit to generate two flat orthogonal beams, course- and pitch-scanned perpendicular to their planes, which adds to security of control process due to small instantaneous area and short duration of terrain illumination in target area. Control station also incorporates synchroniser and unit to generate codes and pulse codes transmitting, on scanned beams, the data on spatial position in the form of time-pulse modulation in preset, for given complex, level of security to increase efficiency in simultaneous fire from several complexes and provide security of control thanks to pulsed radiation mode (minor radiation power). Missile incorporates unit to gate received signal, gate pulse unit, onboard pulse code synchroniser and analyser to extract missile coordinates transmitted on their pulse code level.

EFFECT: higher noise immunity and accuracy thanks to generation and transmission of commands of dynamic error compensation.

3 dwg

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RU 2 382 315 C1

Authors

Morozov Vladimir Ivanovich

Nedosekin Igor' Alekseevich

Minakov Vladimir Mikhajlovich

Nazarov Jurij Mikhajlovich

Tarasov Viktor Ivanovich

Dates

2010-02-20Published

2008-07-15Filed