METHOD OF GUIDED MISSILE DIRECTING Russian patent published in 2008 - IPC F41G3/22 

FIELD: weapons.

SUBSTANCE: in directing the guided missile, additional features are introduced, i.e. a line of aim, an initial range of the said missile from the target and an availability of control signal of the circumference aligned with the line of aim and the said circumference size and colour. The guided missile flight along the line of aim is simulated by varying the introduced circumference size in proportion to the current range from the target. Adjusting the line of aim is made more accurate by using the line of aim as an additional laying mark, its position is made symmetric about the aim point, its brightness is varied periodically, while the colour is changed when the control signal appears/disappears.

EFFECT: 20-25% higher noise immunity and target destruction probability in the conditions of light interferences.

2 cl, 1 ex