A balancing control system for an aircraft steering column comprises a balancing controller, a manual balancing switch, an automatic driving controller, a flap control computer, a balancing actuator and the steering column, and the balancing controller comprises a manual balancing control module, an automatic driving balancing module, a flap balancing module and a balancing priority level judgment module. The manual trimming module generates a manual trimming signal according to the state of a manual trimming switch and sends the manual trimming signal to the trimming priority level judgment module, and the automatic driving trimming module generates an automatic driving trimming signal according to the automatic driving actuator torque sent by the automatic driving controller and sends the automatic driving trimming signal to the trimming priority level judgment module. The flap balancing module generates a flap balancing signal according to the change rate of the flap angle sent by the flap control computer and sends the flap balancing signal to the balancing priority level judgment module, balancing priority level judgment logic is built in the balancing priority level judgment module, and the flap balancing module judges the flap angle according to the balancing priority level judgment logic. And outputting a balancing rate corresponding to the priority balancing signal to a balancing actuator.
一种飞机驾驶杆配平控制系统,含有配平控制器、人工配平开关、自动驾驶控制器、襟翼控制计算机、配平作动器、驾驶杆,所述的配平控制器含有人工配平控制模块、自动驾驶配平模块、襟翼配平模块、配平优先级别判断模块,人工配平模块根据人工配平开关的状态产生人工配平信号,发送给配平优先级别判断模块,自动驾驶配平模块根据自动驾驶控制器发送的自动驾驶作动器力矩产生自动驾驶配平信号,发送给配平优先级别判断模块,襟翼配平模块根据襟翼控制计算机发送的襟翼角度的变化速率产生襟翼配平信号,发送给配平优先级别判断模块,配平优先级别判断模块内置有配平优先级别判断逻辑,根据配平优先级别判断逻辑,向配平作动器输出优先配平信号对应的配平速率。
Aircraft steering column trim control system
一种飞机驾驶杆配平控制系统
2024-03-08
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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