FIELD: aviation industry.
SUBSTANCE: proposed autopilot contains pitch and yaw channels adders whose inputs are connected to control command forming unit, angular rate sensors and linear acceleration transducers of corresponding channels, integrators whose inputs in pitch and yaw channels are connected to outputs of corresponding adders. Inputs of integrator in roll channel is connected with output of roll rate pickup. Servos are provided whose inputs are connected with outputs of integrators and angular rate sensors of corresponding channels. Unit for compensation of integrator kinematic drift is provided. Inputs of said unit are connected with outputs of adders and roll rate pickup, and outputs with inputs of integrators.
EFFECT: improved quality of stabilization.
2 dwg
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