FIELD: weapons.
SUBSTANCE: invention relates to military equipment, in particular to ballistic missiles. Ballistic missile comprises head part, body, propulsion unit, control system on active section. According to the invention, the missile additionally comprises a control unit on the trajectory final section, which is installed during the missile preparation for launching. This unit comprises a bearing housing and satellite navigation equipment. This equipment is intended for determination of current coordinates of missile flight. It has receive antenna on the external surface of control unit, strap-free inertial navigation system. This system is designed to generate commands for stabilization of roll of missile, damping of longitudinal and transverse oscillations and guidance in accordance with position in space determined by satellite navigation equipment. There is also an on-board calculator for starting execution of the cyclogram, steering actuators, aerodynamic rudders, a power supply. On-board equipment for remote reception of flight task from ground flight preparation and transmission equipment is provided by receiving coordinates of target and the cyclogram of the missile in flight. To provide electric connection of head part with control system, transit electric cable is provided.
EFFECT: technical result is higher accuracy of firing.
6 cl, 7 dwg
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Authors
Dates
2019-04-22—Published
2017-11-07—Filed