FIELD: automatic flight control.
SUBSTANCE: device has ailerons channels and rudder channels. Input of adding amplifier of ailerons channel is connected through filter to output of block for forming angular speed of maneuver. Block for forming angular speed of maneuver has right multiplication block, adder, root calculation block, third multiplication block. Input of third multiplication block is connected to output of sign calculation block, input of which, connected to inputs of second multiplication block, is input of block for forming angular speed of maneuver, which is connected to multiplication block inputs.
EFFECT: no need to use gyro indicators of position signals, hence decreased mass, dimensions and cost.
2 cl, 8 dwg
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