公开(公告)号：US20160147224A1

公开(公告)日：2016-05-26

申请号：US14951420

申请日：2015-11-24

Applicant: THALES

Inventor： Michel ROGER ,  Alexandre DARBOIS

IPC: G05D1/00 ,  G08G5/00

CPC classification number: G05D1/0077 ,  G08G5/003 ,  G08G5/0047

Abstract: A method of error detection of a flight management system coupled with a guidance of an aircraft according to a flight plan, comprises the steps of: generating a first reference guidance order, monitoring the integrity of the first reference position, when the first reference position is not monitored as being dependable: invalidating the first FMS assembly and the associated guidance system, when the first reference position and the first reference trajectory are monitored as being dependable: generating a first monitoring guidance order, generating a first reference flight control, generating a first monitoring flight control, in monitoring the integrity of the first reference guidance order when the first reference guidance order is not monitored as being dependable: invalidating the first FMS assembly and the associated guidance.

Abstract translation: 根据飞行计划与飞行器的引导相结合的飞行管理系统的错误检测方法包括以下步骤：产生第一参考指导指令，监视第一参考位置的完整性，当第一参考位置是 不被监视为可靠的：当第一参考位置和第一参考轨迹被监视为可靠时，使第一FMS组件和相关联的引导系统无效：产生第一监视引导顺序，产生第一参考飞行控制，产生第一参考飞行控制 监控飞行控制，在第一个参考指导指令不被监视为可靠时监视第一参考指南顺序的完整性：使第一个FMS组件和相关指导无效。

公开(公告)号：US20150323933A1

公开(公告)日：2015-11-12

申请号：US14707946

申请日：2015-05-08

Applicant: THALES

Inventor： Alexandre DARBOIS ,  Mathieu LE MERRER ,  Johan BOYER

IPC: G05D1/02

CPC classification number: G05D1/0005

Abstract: A method implemented by computer for optimizing the cruising trajectory of an aircraft comprises the steps consisting in receiving the parameters of a reference trajectory, the trajectory comprising one or more plateaus and the transitions between these plateaus, the transitions being ascending or descending; and determining, in response to a request received in the course of the flight, at least one candidate alternative trajectory; and determining one or more indicators associated with the candidate alternative trajectory such as determined. Developments comprise the optional display of at least one indicator, indicators associated with the fuel consumption, with a difference in flight time or with the operational cost of the flight of the aircraft, the use of ratios of indicators, the inhibition of descending transitions, particular plateau length transitions as well as economical modes of transition. System aspects are described, comprising avionic or non-avionic means.

Abstract translation: 用于优化飞行器巡航轨迹的计算机实现的方法包括以下步骤：接收参考轨迹的参数，所述轨迹包括一个或多个平台，以及这些平台之间的转换，所述转换是上升或下降; 以及响应于在飞行过程中接收的请求确定至少一个候选替代轨迹; 以及确定与候选替代轨迹相关联的一个或多个指示符，例如确定的。 发展包括可选地显示至少一个指标，与燃料消耗相关联的指标，飞行时间的差异或飞行器的飞行的运行成本，指示器的使用比例，下降转换的抑制，特别是 平台长度转换以及经济的转型模式。 描述了系统方面，包括航空电子或非航空手段。

公开(公告)号：US20170301244A1

公开(公告)日：2017-10-19

申请号：US15476486

申请日：2017-03-31

Applicant: THALES

Inventor： Marc RIEDINGER ,  Emmanuel DEWAS ,  Alexandre DARBOIS

IPC: G08G5/00

Abstract: A method for manipulating aircraft flight plan segments is provided. A result of an avionics calculation, such as a flight plan sequencing, is selected from among a plurality of results determined by a plurality of systems executed in parallel and placed in competition, each system communicating to at least part of the other systems conditions to be satisfied by the result of a calculation, the method comprises the steps of a given system from among the plurality of systems shares its own calculation result with at least one other system only if its own calculation result satisfies the conditions received from at least one other system. Developments describe various modalities of negotiation and/or selection of the results, the switch to independent and/or the deactivation of a system, voting and/or weighting mechanisms. Software and system aspects are described.