AIRCRAFT SIDE MOVEMENT AT LANDING APPROACH AUTOMATIC CONTROL SYSTEM Russian patent published in 2018 - IPC G05D1/00 B64D45/00 B64C13/00 

FIELD: transportation; control systems.

SUBSTANCE: aircraft lateral movement during landing approach automatic control system includes sensor of the aircraft angular deviation from the of runway axis, aircraft current heading sensor, runway relative bearing sensor, six scale units, four integrators, nine adders, aircraft preset angle execution comprehensive control system (CCS), aircraft to the ground localizer beacon (LOC) distance sensor, flight speed sensor, roll angle sensor, logic unit, aircraft from the heading line linear deviation identification unit, two units of the aircraft from the runway heading line linear deviation speed identification, four filters, three signal multiplying units, three signals switches, two signals level limiting units, input signal sign determining unit, aircraft to the runway heading line preset approach speed sensor, two trigonometric units connected in a certain manner.

EFFECT: enabling increase in the processes speed during the landing approach, stability of the dynamic characteristics, aircraft stabilization on the runway heading line irrespective of the distance to the runway.

4 cl, 5 dwg