公开(公告)号：US09188461B2

公开(公告)日：2015-11-17

申请号：US13728731

申请日：2012-12-27

Applicant: THALES

Inventor： Camille Rieunier ,  Jerome Sacle ,  Joseph Huysseune ,  Xavier Chazottes

IPC: G01D1/00 ,  G01C23/00 ,  G08G5/00

CPC classification number: G01C23/00 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0052

Abstract: A configured aircraft flight management aid system comprises: means of interpretation receiving data taken from external instructions from an external control center, data relating to aircraft equipment failures, cabin problems and problems related to the environment of the aircraft; means of determination receiving data from the means of interpretation and determining at least one reference constraint associated with at least one parameter representative of a flight path, a reference constraint associated with a reference parameter comprising a new constraint, different from the initial constraint when the item of data effectively necessitates following a new path, different from the initial path, and a reference constraint comprising the initial constraint when the means of determination do not have access to any data relating to an event effectively necessitating following a new path; warning means generating a warning to an operator when the path actually flown does not comply with said reference constraint.

Abstract translation: 配置的飞机飞行管理援助系统包括：从外部控制中心接收外部指令的数据的解释手段，与飞机设备故障有关的数据，客舱问题以及与飞机环境有关的问题; 确定从所述解释装置接收数据并确定与代表飞行路径的至少一个参数相关联的至少一个参考约束的装置，与包括新约束的参考参数相关联的参考约束，所述参考参数与所述初始约束不同，当所述项目 的数据有效地需要遵循与初始路径不同的新路径，以及包括初始约束的参考约束，当确定方法不能访问与事件相关的任何数据时，有效地需要跟随新路径; 当路径实际飞行不符合所述参考约束时，警告意味着向操作者产生警告。