FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft and aerospace engineering and may be used for control for flight vehicles in atmosphere. The device for the flight vehicle lateral motion control incorporates a unit of generation of programmable roll angle value and roll angle pickup, two adding amplifiers, two signal limiters, roll and yawing angular speed pickups an ailerons drive. The roll angular speed filter with its output connected to the second input of the second adding amplifier is added to the device. The first signal limiter input is connected to the third input of the second adding amplifier with its output connected to the second signal limiter third input.
EFFECT: improved dynamic properties.
3 dwg
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