公开(公告)号：US20080161982A1

公开(公告)日：2008-07-03

申请号：US11963724

申请日：2007-12-21

申请人： Francois COULMEAU ,  Guy Deker

发明人： Francois COULMEAU ,  Guy Deker

IPC分类号： G01C21/00

CPC分类号： G08G5/0082 ,  G01C23/00 ,  G08G5/0039 ,  G08G5/045

摘要： The subject of the present invention is a method for improving route and 4D prediction calculations by FMS in the framework of ATC tactical flight instructions, which method enables the FMS of an aircraft to carry out its usual predictions as precisely as possible when it has left or anticipates leaving its initial flight plan following an instruction from the air traffic controller, and has no instructions telling it where and when to return to the initial flight plan, and the invention is characterized in that it consists in transmitting to the aircraft, from an air traffic control centre, information enabling the FMS system to be aware of traffic crossing points (X1) and control sector changes, and to use this information to predict the coordinates of a point (X2) at which it is supposed to rejoin its initial flight plan at the earliest opportunity after the crossing point that required an alteration of trajectory and at the latest opportunity on the last point of the current sector.

摘要翻译： 本发明的主题是用于在ATC战术飞行指令的框架内改进FMS的路线和4D预测计算的方法，该方法使得飞行器的FMS能够在其离开时精确地执行其通常的预测， 预计将按照空中交通管制员的指示离开其初始飞行计划，并且没有指示说明何时以及何时返回到初始飞行计划，并且本发明的特征在于其包括从空中传输到飞机 交通控制中心，使FMS系统能够了解交通点（X 1）和控制部门变化的信息，并使用该信息来预测其应该重新加入其中的点（X 2）的坐标 过渡点之后的飞行计划最早需要改变轨迹，并在目前最后一点的最新机会 ctor。

公开(公告)号：US20070225876A1

公开(公告)日：2007-09-27

申请号：US11571484

申请日：2005-06-28

申请人： Christophe Caillaud ,  Guy Deker

发明人： Christophe Caillaud ,  Guy Deker

IPC分类号： G05D1/06

CPC分类号： G08G5/02 ,  G08G5/0013 ,  G08G5/0039 ,  G08G5/025

摘要： The invention relates to a method of changing the approach procedure of an aircraft comprising steps of selecting a new landing runway of the destination airport and of selecting a landing aid system or non-precision approach procedure associated with this runway. The selection steps comprise an automatic selection of a pair associating the new landing runway with the landing aid system or with the non-precision approach procedure, the pair originating from a database containing the pairs related to the destination airport.

摘要翻译： 本发明涉及一种改变飞机接近程序的方法，包括以下步骤：选择目的地机场的新的着陆跑道，以及选择与该跑道相关联的着陆援助系统或非精密进场程序。 选择步骤包括自动选择将新的着陆跑道与着陆援助系统或非精确进场过程相关联的对，该对来自包含与目的地机场相关的对的数据库。

公开(公告)号：US20070150170A1

公开(公告)日：2007-06-28

申请号：US10583143

申请日：2004-12-13

申请人： Guy Deker

发明人： Guy Deker

IPC分类号： G06G7/76

CPC分类号： G05D1/0646

摘要： The invention relates to a method for assisting low-altitude navigation of an aircraft equipped with a system suited to determining a flight-plan ground trajectory based on intermediate points P at an altitude alt(P), and the aircraft's performance. It comprises the following steps: for each point P, calculating a safe altitude, alt safe, to obtain a point Psafe, calculating a safe profile formed from segments joining the points Psafe, extracting summits S from among the points Psafe, determining the aircraft's weight at these points S as a function of the distance between the aircraft and S and of its consumption over this distance, where the consumption is one aspect of its performance, for each point S, determining the maximum climb slope MaxClimbFPA and the maximum descent slope MaxDescFPA as a function of the performance and the weight, defining two performance segments which have slopes MaxClimbFPA and MaxDescFPA on either side of the point S and calculating a performance profile formed from performance segments and which makes it possible to associate at each point P of the safe profile a performance altitude, alt perf (P).

摘要翻译： 本发明涉及一种辅助飞机的低空导航的方法，该飞机配备有适合于基于高度alt（P）的中间点P确定飞行平面地面轨迹的系统以及飞行器的性能。 它包括以下步骤：对于每个点P，计算安全高度，alt安全，以获得点P _{安全，计算由连接点P 安全< 从点P＆lt;安全中提取顶点S，确定飞机在这些点S处的重量，作为飞机和S之间的距离以及在该距离上的消耗的函数，其中消耗 是其性能的一个方面，对于每个点S，确定作为性能和重量的函数的最大爬坡坡度MaxClimbFPA和最大下降坡度MaxDescFPA，定义在点的任一侧上具有斜坡MaxClimbFPA和MaxDescFPA的两个性能段 并且计算由性能段形成的性能轮廓，并且使得可以在安全轮廓的每个点P处关联性能高度alt perf（P）。}

公开(公告)号：US20050283306A1

公开(公告)日：2005-12-22

申请号：US10529787

申请日：2003-09-23

申请人： Guy Deker

发明人： Guy Deker

IPC分类号： G05D1/04 ,  G05D1/06 ,  G01C21/00

CPC分类号： G05D1/0653

摘要： The invention relates to a method of automatic navigation assistance for an aircraft. A capture zone being a zone in which the aircraft can capture a predetermined vertical profile segment by applying a transition between the guidance submode which the aircraft is in and the guidance submode adapted to the following of the vertical profile segment to be captured, it comprises the step consisting in determining the width of the capture zone as a function of the height h of the vertical profile to be captured and of the speed v which the aircraft has when plumb with this height when the aircraft is not on the profile or at this height when the aircraft is on the profile.

摘要翻译： 本发明涉及一种用于飞行器的自动导航辅助的方法。 捕获区域，其中飞行器可以通过在飞行器所在的引导子模式之间进行转换并且适应于要捕获的垂直剖面段的跟踪的引导子模式之间的过渡来捕捉预定垂直剖面段，其包括 确定捕获区域的宽度作为要捕获的垂直剖面图的高度h的函数，以及当飞机不在轮廓上或在该高度时飞机具有该高度的速度v 当飞机在轮廓上时。

公开(公告)号：US06269301B1

公开(公告)日：2001-07-31

申请号：US09147335

申请日：1999-02-24

申请人： Guy Deker

发明人： Guy Deker

IPC分类号： G06F1700

CPC分类号： G05D1/0202 ,  G01C21/00

摘要： Method for piloting a vehicle while making a change of heading. The vehicle follows a first rectilinear portion of a route, so as to meet up with a second rectilinear portion of the route forming a predetermined angle with the first portion. The route passes through the meeting point of the two portions. The vehicle computes and follows a curved change of heading trajectory which passes through the meeting point whose turning center lies on the interior bisector of the angle formed by the two portions of the route.

摘要翻译： 改变航向时驾驶车辆的方法。 车辆遵循路线的第一直线部分，以便与第一部分形成预定角度的路线的第二直线部分相遇。 路线通过两部分的会合点。 车辆计算并跟随通过会合点的航向轨迹的弯曲变化，其转动中心位于由路线的两个部分形成的角度的内部平分线上。

公开(公告)号：US06181987B2

公开(公告)日：2001-01-30

申请号：US08921340

申请日：1997-08-29

申请人： Guy Deker ,  Muriel Bomans

发明人： Guy Deker ,  Muriel Bomans

IPC分类号： G06F1700

CPC分类号： G01C23/00

摘要： The disclosed method is implemented by a system aboard an aerodyne comprising a processor, a terminal and memories in which there are stored all the information necessary for the carrying out of a flight, the system being connected to the other on-board electronic equipment. In order to define a new flight plan to meet a new situation caused by an event, the method comprises: the interpretation of the event to determine the corrective actions to be undertaken given the context in which the aerodyne is located, the analysis of the possibilities of reconfiguring the flight plan that correspond to the corrective actions, according to predetermined and modifiable criteria, the selection of the flight plan solutions that meet the predetermined criteria, and the presenting of these flight plan solutions in association with the significant parameters that have served as the grounds for their selection.

摘要翻译： 所公开的方法由包括处理器，终端和存储器的空气中的系统来实现，其中存储执行飞行所需的所有信息，该系统连接到另一个车载电子设备。 为了确定一个新的飞行计划来满足一个事件引起的新情况，该方法包括：根据航空所在的环境，对事件进行解释以确定要采取的纠正措施，分析可能性 根据预定和可修改的标准重新配置对应于纠正措施的飞行计划，选择满足预定标准的飞行计划解决方案，以及将这些飞行计划解决方案与已经用作 选择的理由。