GUIDED MISSILE FIRING METHOD Russian patent published in 2014 - IPC F41G7/30 

Abstract RU 2534206 C1

FIELD: weapons and ammunition.

SUBSTANCE: invention can be used at the guided missile (GM) firing. Location survey of a target finder and a launching installation (LI) with regard to terrain is performed; the target coordinates are detected and measured; the target coordinates are transferred to a firing position control panel; firing settings are calculated and transferred in an online mode to an automation unit of LI and the missile; time of waiting for the missile readiness for launching is set; readiness of the missile for launching is controlled; a permit for the missile launching is formed out of a set of readiness parameters of onboard navigation satellite equipment (number of the observed satellites is not less than the number of satellites set by an operator, a channel of a homing head, an altimeter, flight mission parameters, and a GM communication channel), and the missile is launched.

EFFECT: improving reliability and safety of GM launching and probability of GM hitting the specified target.

3 cl

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RU 2 534 206 C1

Authors

Obrazumov Vladimir Ivanovich

Podchufarov Jurij Borisovich

Ovsenev Sergej Sergeevich

Larin Dmitrij Viktorovich

Kushnikov Dmitrij Vjacheslavovich

Larin Andrej Viktorovich

Kanishcheva Anna Borisovna

Dates

2014-11-27Published

2013-05-29Filed