公开(公告)号：US20130154936A1

公开(公告)日：2013-06-20

申请号：US13720845

申请日：2012-12-19

Applicant: Thales

Inventor： Enrique-Roberto LASO-LEON ,  Amandine AUDOUY ,  Mathieu LE MERRER

IPC: G06F3/0354

CPC classification number: G06F3/033 ,  G06F3/016 ,  G06F3/03549 ,  G06F3/04812 ,  G06F3/04842 ,  G06F2203/014

Abstract: A computer equipment comprises a trackball used to point to objects on a screen of the equipment. A method for driving the computer equipment is also provided. The trackball comprises a moving part and a body inside which the moving part can be displaced, the computer being configured to display at least one object and a pointer on the screen. The trackball comprises means making it possible to exert a tangential force on the moving part, means driven by the computer. The computer is configured to modulate the force according to the shape of the object displayed and the position of the pointer relative to the object.

Abstract translation: 计算机设备包括用于指向设备的屏幕上的物体的轨迹球。 还提供了一种用于驱动计算机设备的方法。 轨迹球包括移动部分和主体，移动部分可移动到该主体内，计算机被配置为在屏幕上显示至少一个对象和指针。 轨迹球包括能够在移动部件上施加切向力的装置，由计算机驱动的装置。 计算机被配置为根据显示的对象的形状和指针相对于对象的位置来调制力。

公开(公告)号：US20160163201A1

公开(公告)日：2016-06-09

申请号：US14958068

申请日：2015-12-03

Applicant: THALES

Inventor： Mathieu LE MERRER ,  Benoit DACRE-WRIGHT ,  François COULMEAU

IPC: G08G5/00

CPC classification number: G08G5/003 ,  G05D1/0005 ,  G06Q10/047 ,  G08G5/0034

Abstract: The present invention relates to a method for computing a setpoint trajectory of an aircraft comprising at least two subsets. It is characterized in that it comprises the formulation and the solving of an optimization problem for the trajectory, and that the formulation of the said problem comprises at least the formulation of a constraint related to a transition of legs on at least one first subset of the trajectory, and the formulation of a constraint related to a transition of vertical flight phases on at least one second subset of the trajectory. The invention also relates to a system and a computer program for the computation of a trajectory.

Abstract translation: 本发明涉及一种用于计算包括至少两个子集的飞机的设定轨迹的方法。 其特征在于，其包括对轨迹的优化问题的公式和求解，并且所述问题的公式至少包括与腿的至少一个第一子集上的腿的转变有关的约束的公式 轨迹，以及与轨迹的至少一个第二子集上的垂直飞行相位的转变有关的约束的公式。 本发明还涉及用于计算轨迹的系统和计算机程序。

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。