METHOD OF AIRCRAFT CONTROL IN "LANDING" AUTOMATIC CONTROL SYSTEM MODE Russian patent published in 2024 - IPC G05D1/00 G08G5/00 

FIELD: aviation; aircraft control methods.

SUBSTANCE: invention relates to aircraft control in "Landing" automatic control system mode. Method consists in the fact that, using signals of glide path beacon, localizer beacon and signals of inertial navigation system, which form values of magnetic track angle and yaw angle, on the aircraft stabilization section on the landing course, the course angle averaging procedure is performed at a certain altitude using the automatic control system, averaging is completed, performing the preset heading redefinition and generating the rudder signal based on minimizing the difference between the current course angle and the redefined heading value, control of ailerons is switched from control by localizer beacon signals to control aimed at minimization of bank angle, and rudder control is switched from minimizing slip angle to holding aircraft on runway axis on signals of runway course deviation and yaw angle.

EFFECT: higher quality of landing.

1 cl, 3 dwg