| 摘要 |
The utility model relates to the systems of stabilization of anti-tank guided missiles. An anti-tank guided missile with laser guiding has a block of receiver of laser radiation, a block of command separation, a block of correction filters, a block of gyroscopic command transformer, an amplifier block, a compensation block, a stabilization block, a block of the drive of aerodynamic steer, a block of the planer of the missile. To decrease the errors of control at aiming in the process of guiding to the missile the block of error analysis is includes, with two outputs, and the block of additional filters of correction. The output of the block of the error analysis is connected to the output of the block of control command separation, the first output of the block of analysis of the error is connected to the input of the correction filters, the second output of the block of error analysis is connected to the inlet of the block of additional filters of correction, the output of the block of additional filters of correction is connected to the input of the block of gyroscopic transformer.
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