HIGH-MANEUVERABILITY AIRCRAFT FLIGHT AUTOMATIC CONTROL METHOD Russian patent published in 2012 - IPC G05D1/00 B64C19/00 

FIELD: transport.

SUBSTANCE: proposed method comprises using floating automatic device of longitudinal control, generating limitation of normal overload preset magnitude as minimum magnitude among magnitudes corresponding to maximum angle of attack and maximum pitch angular speed depending on flight altitude and speed, generating mismatch between limited preset and current normal overload magnitudes depending on flight altitude and speed, dynamic limitation of total control signal of aforesaid floating automatic device of longitudinal control and additional summation with damping signal of pitch angular speed. Proposed allows limiting marginal angles of attack, angular speed and pitch angular acceleration as well as required characteristics of controllability in the entire range of control signal variation.

EFFECT: limiting marginal angles of attack, angular speed and pitch angular acceleration as well as required characteristics of controllability in the entire range of control signal variation.

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