FIELD: tool-making industry, possible use in automatic flight control systems for controlling sideward movement of light and ultra light planes, small remotely controlled aircraft and the like.
SUBSTANCE: in accordance to method, angular speed is performed relatively to normal axis OY and longitudinal axis OX of an aircraft. Control signal of aileron channel is generated, proportional to angular speed relatively to longitudinal axis OX of an aircraft. Control signal of rudder channel is generated by adding signal, proportional to angular speed relatively to normal axis OY of aircraft and signal, proportional to angular speed relatively to normal axis OY.
EFFECT: expanded functional capabilities.
3 dwg
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