FIELD: aviation.SUBSTANCE: group of inventions relates to a control system for controlling actuators of an aircraft, an aircraft comprising such a system, control method of executive elements of aircraft steering surface. System comprises at least one preliminary control unit and a differential force controller. Aircraft comprises at least one steering surface and two actuating elements connected to the steering surface. To implement the method, actuators are adjusted/controlled to impart overall simulated characteristics and alignment of control deviations using a differential force controller.EFFECT: providing optimum separation of power of actuators of one steering surface to each other.11 cl, 4 dwg
УПРАВЛЯЮЩАЯ СИСТЕМА ДЛЯ УПРАВЛЕНИЯ ИСПОЛНИТЕЛЬНЫМИ ОРГАНАМИ ЛЕТАТЕЛЬНОГО АППАРАТА
2019-06-17
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |
СИСТЕМА И СПОСОБ УПРАВЛЕНИЯ ПЕРЕМЕЩЕНИЕМ ЗАКРЫЛКОВ ЛЕТАТЕЛЬНОГО АППАРАТА
European Patent Office | 2018