The invention provides an automatic braking control system and method for civil aircraft landing, and the system comprises a runway state selection module, a runway database, a runway information module, a flight management system, an ADIRU module, a position calculation module, an automatic driving system, an automatic braking system, and a braking control system. The braking control system can perform PID dynamic control on braking of the airplane through the distance between the airplane and the runway separation opening obtained from the position calculation module in real time and the airplane real-time parameters obtained from the ADIRU module in combination with the braking deceleration provided by the automatic braking system, and braking deceleration of the airplane is performed. According to the control system and the control method thereof, the airplane can be continuously and smoothly decelerated instead of being suddenly decelerated, so that the riding comfort and the landing safety of passengers are improved.

    本发明提供一种民机着陆自动刹车控制系统及其控制方法,该系统包括跑道状态选择模块、跑道数据库、跑道信息模块、飞行管理系统、ADIRU模块、位置计算模块、自动驾驶系统、自动刹车系统、刹车控制系统,本发明的刹车控制系统可通过实时从位置计算模块获取的飞机与跑道脱离口之间的距离和从ADIRU模块获取的飞机实时参数,结合自动刹车系统提供的刹车的减加速度进行PID动态控制飞机的刹车,进行飞机刹车减速。本发明的控制系统及其控制方法可以让飞机持续的平滑减速,而非突然减速,提高了旅客的乘坐舒适度和着陆安全。


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    Title :

    Automatic brake control system for landing of civil aircraft and control method thereof


    Additional title:

    一种民机着陆自动刹车控制系统及其控制方法


    Contributors:
    MENG XIAOFENG (author) / ZHANG ZEDONG (author) / HUANG WEILIN (author) / YE CHEN (author) / YU HAO (author) / CUI XINCHAO (author)

    Publication date :

    2023-04-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT