The invention discloses a pressure closed-loop control system for an electro-hydraulic pressure servo valve of an aircraft braking system. The pressure closed-loop control system comprises a braking instruction sensor, an FPGA module, a DSP module, a pressure sensor and the electro-hydraulic pressure servo valve. The FPGA module is connected with the DSP module, the brake instruction sensor, the pressure sensor and the electro-hydraulic pressure servo valve. By adopting the incremental PID algorithm and adding the transparent transmission link, the response speed and the control precision of the system are effectively improved, and meanwhile, the problem of brake failure caused by the fault of the pressure sensor is avoided. According to the method, the command pressure change can be quickly responded, and accurate control of the brake pressure is ensured, so that the brake efficiency is improved, the risk of uneven temperature of a brake disc of an aircraft wheel and aircraft yawing is reduced, and the reliability and the safety of an aircraft brake system are enhanced.
本发明公开了一种飞机刹车系统电液压力伺服阀压力闭环控制系统,包括:刹车指令传感器、FPGA模块、DSP模块、压力传感器和电液压力伺服阀;FPGA模块分别与DSP模块、刹车指令传感器、压力传感器和电液压力伺服阀连接。本发明通过采用增量式PID算法和增加透传环节,有效提高了系统的响应速度和控制精度,同时避免了因压力传感器故障导致的刹车失效问题。本发明能够快速响应指令压力变化,确保刹车压力的精确控制,从而提升刹车效率,减少飞机机轮的刹车盘温度不均和飞机偏航的风险,增强了飞机刹车系统的可靠性和安全性。
Pressure closed-loop control system for electro-hydraulic pressure servo valve of airplane brake system
一种飞机刹车系统电液压力伺服阀压力闭环控制系统
2025-02-28
Patent
Electronic Resource
Chinese
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