The embodiment of the invention relates to the technical field of aircraft brake control, and discloses an aircraft brake configuration recognition method, which comprises the following steps: acquiring a power-on initialization completion result; if the power-on initialization is completed and a preset configuration recognition condition is met, performing configuration recognition on the target aircraft, and if the configurations recognized within a first preset duration are consistent, determining that the configuration recognition is successful; and if the preset configuration identification condition is not met, or the configurations identified within the first preset duration are inconsistent, performing configuration identification waiting, and when the configuration identification waiting time exceeds a second preset duration, determining that the configuration identification fails, and uploading a configuration identification failure alarm. According to the method, logic judgment is carried out through the power-on initialization completion mark, the brake software bus data packet refreshing mark, the brake software bus data packet hardware monitoring mark and the time sequence, aircraft brake configuration recognition is safely and reliably achieved, the configuration recognition false alarm rate is reduced, and safety is remarkably improved.
本申请的实施例涉及飞机刹车控制技术领域,公开了一种飞机刹车构型识别方法,该方法包括:获取上电初始化完成结果;若上电初始化完成且满足预设构型识别条件,对目标飞机进行构型识别,若在第一预设时长内识别出的构型均一致,则确定构型识别成功;若不满足预设构型识别条件,或在第一预设时长内识别出的构型存在不一致,则进行构型识别等待,当构型识别等待时间超过第二预设时长后,确定构型识别失败,上传构型识别失败告警。本申请通过上电初始化完成标志、刹车软件总线数据包刷新标志、刹车软件总线数据包硬件监控标志以及时序进行逻辑判断,安全可靠的实现了飞机刹车构型识别,降低了构型识别虚警率,安全性显著提高。
Aircraft brake configuration identification method
一种飞机刹车构型识别方法
2024-09-13
Patent
Electronic Resource
Chinese
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