FIELD: automatic control systems. SUBSTANCE: control system includes two control channels with strong feedback, having rolling angular velocity pickup 1 and yawning angular velocity pickup 7, adders 2, 8, amplifiers 3,9, the aileron drive mechanism 4, the rudder drive mechanism 10, the aileron position sensor 5 and the rudder position sensor 11 respectively. Due to using of the calculator 12 for calculating rolling angle values, the accelerometer 13, the flying speed meter 14, the flying height meter 15 and the setter 16, the system for controlling side motion of the pilot-free small-size flying object is provided with small dimensions and mass because of determining current values of rolling angles by calculation. Such system ensures lateral stability of the flying object. EFFECT: enhanced stability of flying object in its rolling control system equipment. 2 cl, 2 dwg
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Authors
Dates
1995-08-20—Published
1993-02-02—Filed