초록 ▼

Firing control system for a direct firing weapon mounted on a rotary-wing aircraft, which is designed to be actuated by the pilot himself and comprises an electronic computer, the said weapon being mounted for rotating about two transverse axes Y-Y′and Z-Z′, due to driving means controlled by the sa

Firing control system for a direct firing weapon mounted on a rotary-wing aircraft, which is designed to be actuated by the pilot himself and comprises an electronic computer, the said weapon being mounted for rotating about two transverse axes Y-Y′and Z-Z′, due to driving means controlled by the said computer. According to the invention, said firing control system is characterized in that it comprises a sighting system on which a target and an adjusting mark can appear simultaneously, which adjusting mark can be moved on the said sighting system by a control of the pilot, as well as means to determine the coordinates of the position of the said adjusting mark with respect to a system of axes tied to the aircraft and to transmit them to said electronic computer at least when the said adjusting mark is brought to a position on the said sight finder where it is superposed on the said target.

대표청구항 ▼

Firing control system for a weapon mounted on an aircraft and firing a projectile which travels in essentially a straight line, said system comprising: an electronic computer; mounting means for mounting said weapon on said aircraft for rotation about two transverse axes; driving means controlled by

Firing control system for a weapon mounted on an aircraft and firing a projectile which travels in essentially a straight line, said system comprising: an electronic computer; mounting means for mounting said weapon on said aircraft for rotation about two transverse axes; driving means controlled by said computer for rotating said weapon about said axes; optical sighting means providing a field of view which is fixed relative to said axes and which permits a direct line-of-sight to a target by a pilot of said aircraft; an electro-optical device generating a luminous mark on a screen which is fixed relative to said axes, the position of said mark on said screen being manually adjustable by said pilot; means for measuring the coordinates of the position of said mark relative to said axes; means for projecting an image of said mark onto said field of view in said optical sighting system; and means for transmitting said coordinates to said computer at least when said image is positioned to lie in said line of sight to a target.