The invention provides an active double-side-rod working mode, which comprises an active synchronous mode, a double-side-rod working mode, a double-side-rod working mode, a double-side-rod working mode, a double-side-rod working mode and a double-side-rod working mode, in the passive synchronous mode, the manipulated variable of a pilot on one side can be sent to the flight control computer, the flight control computer calculates a driving instruction, the driving instruction is sent to the side rod on the other side to drive the side rod on the other side to move, and the manipulated strokes between the two side rods are kept consistent; in the asynchronous mode, the control strokes of the two side rods correspond to the control variables of a main pilot and an auxiliary pilot respectively, and the two side rods are not linked any more, that is, the control strokes of the two side rods are not kept consistent any more; in the clamping stagnation mode, when the side rod on one side has a clamping stagnation fault, the side rod on the side does not generate a control stroke any more, but the control quantity is calculated through pilot control force collected by an internal force sensor; in the cutting mode, the control authority of a pilot on one side is cut; meanwhile, the invention further provides a switching method and a control signal voting method.
本申请提供了一种主动双侧杆工作模式,包括:主动同步模式,能够实现双侧杆之间联动,保持双侧杆之间操纵行程一致;被动同步模式,一侧飞行员的操纵量会发送到飞控计算机,由飞控计算机计算出驱动指令,发送到另一侧侧杆,驱动另一侧侧杆运动,保持双侧杆之间操纵行程一致;异步模式,双侧杆的操纵行程分别对应主/副飞行员的操纵量,双侧杆之间不再联动,即双侧杆间不再保持操纵行程一致;卡滞模式,一侧侧杆出现卡滞故障,该侧侧杆不再产生操纵行程,而是通过内部的力传感器采集到的飞行员操纵力,计算出操纵量;切除模式,切除一侧飞行员的操纵权限;同时,本申请还提供了一种切换方法和一种操纵信号表决方法。
Active double-side-lever working mode, switching method and control signal voting method
主动双侧杆工作模式、切换方法及操纵信号表决方法
2025-02-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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