FIELD: optical guidance systems of self-propelled projectiles, applicable in guided weapon systems with teleorientation in a laser beam. SUBSTANCE: the optical sight of the missile guidance system includes a target sighting channel, range-finding channel and a guidance channel containing a radiator, modulator, device for excess introduction and a pancratic optical system, introduced is a logical device, whose outputs are connected to the radiator, modulator, device for excess introduction, pancratic optical system, range-finding channel and the control bus-bar is the range-finding channel, and the member of optical communication with the launcher, sight optical axis guidance drive and the sight optical axis position transducer. The element of optical communication with the launcher may be made in the form of a radiator or in the form of a radiation receiver. EFFECT: enhanced accuracy and reliability of the armament complex due to fitness of the device to automated alignment of the launcher with the sight optical axis. 3 cl, 2 dwg
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Authors
Dates
2003-09-20—Published
2001-12-06—Filed