| 摘要 |
FIELD: aviation. ^ SUBSTANCE: invention belongs to the field of missile guidance and can be used in tank systems and anti-tank armaments and also in lightweight anti-aircraft systems. The essence of the invention is that it is a means for guiding remote operated missiles fired from a launch device with initial parallax equipment for guidance, carrying out orientation of launch device with the missile facing the direction of the field being controlled. During the missile's flight guidance signals are generated with the proportional coordinates of the deviation of the missile from the axis of the guiding field from the axis on the vertical and horizontal planes and this produces the deviation of the missile's control according to the generated signals for its guidance. During which, programme commands are generated, proportionate to the value of the initial parallax, which is deducted from the control signals of the missile. ^ EFFECT: increased accuracy of fire in the nearest zone of attacks taking into account the reduction of deviation of the central mass of the missile from line of the target at the initial site. ^ 2 dwg |
