FIELD: systems for automatic flying control.
SUBSTANCE: apparatus includes pickups for measuring errors of pitch angle and of angular velocity connected with inlets of summing amplifier; linear sped and linear acceleration pickups connected with inlets of unit for generating non-linear control signal whose outlet is connected with inlet of summing amplifier. Signal of summing amplifier is fed to steering system directly acting upon elevator. Invention allows to suppress wind disturbances due to adding to control law signal proportional to flying speed error.
EFFECT: enhanced accuracy of control process.
2 cl, 3 dwg
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