FIELD: tool-making industry, possible use in automatic flight control systems for controlling sideward movement of light and ultra light planes, small remotely controlled aircrafts.
SUBSTANCE: in accordance to invention, introduced into aileron control channel is block for generation of nonlinear control rule in format
where k - constant coefficient, ωx - angular speed relatively to longitudinal axis OX, ωy - angular speed relatively to normal axis OY, first input of which is connected to output of angular speed indicator, relatively to normal axis OY, second input of which is connected to output of angular speed indicator relatively to longitudinal axis OX, while output is connected to input of adding amplifier of aileron channel.
EFFECT: expanded functional capabilities.
2 cl, 3 dwg
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