AIRCRAFT SIGHT Russian patent published in 2010 - IPC F41G3/22 B64D7/00 

FIELD: arms and ammunition.

SUBSTANCE: invention relates to sighting systems and can be used interceptor aircraft in close-in dogfight conditions. Proposed system comprises onboard radar incorporating mirror aerial with control unit. The latter comprises mirror title, tilt and azimuth turn angle and angular speed transducers, signal processor with its input connected with receiver output, as well as indicator and unit of communication with missiles. Proposed sight incorporates coverage area shift switch and aiming control processor. First input of the latter is connected with attach mode switch, its second input being connected with coverage area shift switch, its third switch being connected with aerial mirror turn angle and angular speed transducers, its fourth input being connected with data output of the unit of communication with missiles, and fifth input being connected with aircraft altitude and roll pickups. Aiming control processor first output is connected to indicator input, its second output is connected to input of the unit of communication with missiles, third output is connected to aerial control unit input and fourth out is connected to synchroniser control input. Note here that processors are interconnected via communication lines.

EFFECT: reduced aiming interval.

2 dwg