SMALL-SIZED GUIDED SPINNING MISSILE Russian patent published in 2015 - IPC F42B15/00 

Abstract RU 2561319 C1

FIELD: weapons and ammunition.

SUBSTANCE: invention relates to guided spinning missiles. The small-sized guided spinning missile comprises the electronic control equipment, control units, and an inertial measurement unit. The inertial measurement unit comprises three micromechanical gyroscopes (MMG) and a biaxial linear acceleration sensor (LAS) placed on a common panel mounted perpendicular to the longitudinal axis X of the missile rotation. The electronic control equipment comprises a microcontroller of preliminary treatment and conversion of signals of three MMG and biaxial LAS into signals corresponding to the transverse axes Y and Z, and a non-volatile reprogrammable memory device for storing the calibration coefficients.

EFFECT: improving the accuracy of targeting and increasing the firing range with the guided missile.

2 dwg

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RU 2 561 319 C1

Authors

Aksenov Aleksej Alekseevich

Zharov Jurij Nikolaevich

Gutsal Viktor Gerasimovich

Lutaj Igor' Ivanovich

Voropaev Sergej Nikolaevich

Odintsov Andrej Jur'Evich

Dates

2015-08-27Published

2014-04-25Filed