The invention belongs to the technical field of aircraft double-side-lever control design, and particularly relates to an aircraft double-side-lever control system and a method thereof.According to the aircraft double-side-lever control system, a main side lever and an auxiliary side lever are arranged at the main pilot position and the co-pilot position of an aircraft correspondingly; the main side rod and the auxiliary side rod are respectively provided with a longitudinal instruction sensor, a transverse instruction sensor and an authority switching and automatic driving disconnection button; based on whether the automatic driving of the airplane is switched on or not and whether the longitudinal instruction sensor and the transverse instruction sensor of the main side rod and the auxiliary side rod are in a normal state or not, the main side rod and the auxiliary side rod are switched off; through authority switching of a main side rod and an auxiliary side rod and an automatic driving disconnection button, the control modes of the double side rods of the airplane are switched among a double-side control mode, a main side locking control mode, a main side temporary control mode, an auxiliary side locking control mode and an auxiliary side temporary control mode, and automatic driving of the airplane can be controlled to be disconnected. And the aircraft can be greatly conveniently controlled by a main driver and an auxiliary driver.
本申请属于飞机双侧杆操纵设计技术领域,具体涉及一种飞机双侧杆操纵系统及其方法,其中,飞机双侧杆操纵系统,其在飞机主、副驾驶位置分别设置主侧杆、副侧杆,并为主侧杆、副侧杆分别配置纵向指令传感器、横向指令传感器、权限切换及其自动驾驶断开按钮,基于飞机自动驾驶是否接通以及主侧杆、副侧杆的纵向指令传感器、横向指令传感器是否处于正常状态,通过主侧杆、副侧杆的权限切换及其自动驾驶断开按钮,对飞机双侧杆操纵模态在双侧操纵模态、主侧锁定操纵模态、主侧临时操纵模态、副侧锁定操纵模态、副侧临时操纵模态间进行切换,且可操纵将飞机自动驾驶断开,能够极大方便主、副驾驶员对飞机的操纵。
Airplane double-side-lever control system and method thereof
一种飞机双侧杆操纵系统及其方法
2023-04-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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