公开(公告)号：US20080243316A1

公开(公告)日：2008-10-02

申请号：US12066499

申请日：2006-10-24

申请人： Jerome Sacle ,  Francois Coulmeau

发明人： Jerome Sacle ,  Francois Coulmeau

IPC分类号： G06F17/00

CPC分类号： G01C5/06 ,  G01C25/00

摘要： The invention relates to a method for aiding the setting of the barometric altitude of an aircraft equipped with a means (11, 12) for determining the altitude not using the barometric pressure, determining with the aid of the means (11, 12) for determining the altitude an altitude (Zv, Zi, Zr, Zh) and its relative precision (Pzv, Pzr), comparing the determined altitude (Zv, Zi, Zr, Zh) with a barometric altitude measured aboard the aircraft, generating an alert when the discrepancy between the determined altitude (Zv, Zi, Zr, Zh) and the measured barometric altitude exceeds a predefined value and proposing a barometric altitude setting value.

摘要翻译： 本发明涉及一种用于帮助设置具有用于确定不使用大气压力的高度的装置（11,12）的飞行器的气压高度的设置的方法，借助于用于确定的装置（11,12）来确定 将高度（Zv，Zi，Zr，Zh）及其相对精度（Pzv，Pzr）与确定的高度（Zv，Zi，Zr，Zh）进行比较，与飞机上测量的气压高度进行比较，产生警报 确定的高度（Zv，Zi，Zr，Zh）和测量的气压高度之间的差异超过预定值，并提出气压高度设定值。

公开(公告)号：US20080195264A1

公开(公告)日：2008-08-14

申请号：US11923283

申请日：2007-10-24

申请人： Guy Deker ,  Jerome Sacle ,  Francois Coulmeau

发明人： Guy Deker ,  Jerome Sacle ,  Francois Coulmeau

IPC分类号： G05D1/00

CPC分类号： G05D1/0204

摘要： The invention relates to a method of automatically managing the flight of an aircraft in turbulent air comprising notably the determination of the current speed (Vc), of an optimal turbulence speed (Vt), of a current thrust value (P). The data relating to a turbulence is acquired. An optimal turbulence speed is determined. Measuring a deviation (Δ) between the current speed (Vc) and the turbulence speed (Vt). Comparing the deviation (Δ) and a maximum deviation value (Δmax). Iterating k times of the previous three steps, to determine whether the deviation (Δ) is greater than the maximum deviation (Δmax) for the kth consecutive time, and the readjustment of the current thrust (P) so as to reduce the deviation (Δ) to a value less than that of the maximum deviation (Δmax) and to make the current speed (Vc) converge to the turbulence speed (Vt).

摘要翻译： 本发明涉及一种在湍流空中自动管理飞行器的飞行的方法，其特别包括当前速度（V SUB）的最佳湍流速度（V < SUB>），当前推力值（P）。 获取与湍流有关的数据。 确定最佳湍流速度。 测量当前速度（V SUB）与湍流速度（V SUB）之间的偏差（Delta）。 比较偏差（Delta）和最大偏差值（Delta max max）。 迭代前三个步骤的k次，以确定对于第k个连续时间，偏差（Delta）是否大于最大偏差（ΔL> max ），并且 重新调整当前推力（P），以将偏差（Delta）减小到小于最大偏差（Delta max max）的值，并使当前速度（V SUB） ）收敛到湍流速度（V SUB）。

公开(公告)号：US20080177431A1

公开(公告)日：2008-07-24

申请号：US11951197

申请日：2007-12-05

申请人： Francois Coulmeau ,  Francois Hoofd

发明人： Francois Coulmeau ,  Francois Hoofd

IPC分类号： G01C21/20 ,  G06F19/00

CPC分类号： G05D1/101

摘要： The present invention relates to a method for replacing legs in an air navigation procedure described as a series of legs, the legs forming part of an initial family of legs. The method includes: a step of determining a restricted family of legs included in the initial family of legs, so that each leg not belonging to the restricted family corresponds to a combination of legs belonging to the restricted family: The method also includes: a step of replacing in the navigation procedure the legs not belonging to the restricted family with combinations of legs belonging to the restricted family.

摘要翻译： 本发明涉及一种用于替换被描述为一系列腿部的空中航行程序中的腿部的方法，所述腿部形成初始腿部系列的一部分。 所述方法包括：确定包含在所述初始家庭系列中的受限家庭的一个步骤，使得不属于所述限制家庭的每个腿对应于属于受限家庭的腿的组合：所述方法还包括：步骤 在导航程序中使用属于受限制家庭的双腿的组合来替代不属于受限制家庭的腿。

公开(公告)号：US20080065312A1

公开(公告)日：2008-03-13

申请号：US11845724

申请日：2007-08-27

申请人： Francois COULMEAU ,  Guy Deker

发明人： Francois COULMEAU ,  Guy Deker

IPC分类号： G06F19/00

CPC分类号： G08G5/006 ,  G01C23/00 ,  G08G5/0013 ,  G08G5/045

摘要： The present invention relates to a guidance method for temporarily deviating a vehicle initially following a predefined path. The method is characterized in that the modalities according to which the vehicle leaves the predefined path, accompanied by conditions based on which it rejoins it, are sent to the guided vehicle in the form of an alphanumeric message via a digital data link.

摘要翻译： 本发明涉及一种用于临时偏离最初沿着预定路径的车辆的引导方法。 该方法的特征在于，车辆离开预定路径的伴随着其重新加入的条件的模式通过数字数据链路以字母数字消息的形式被发送到被引导的车辆。

公开(公告)号：US08849478B2

公开(公告)日：2014-09-30

申请号：US12876952

申请日：2010-09-07

申请人： Francois Coulmeau ,  Jerome Sacle ,  Lionel Verot

发明人： Francois Coulmeau ,  Jerome Sacle ,  Lionel Verot

IPC分类号： G06F19/00 ,  G06G7/76 ,  G08G5/04

CPC分类号： G08G5/045 ,  G08G5/0056 ,  G08G5/065

摘要： An aircraft piloting assistance method and system including determining at least one flyable slope with which the aircraft is assumed to be able to fly, based on a value of at least one flight parameter including the weight of the aircraft. The step for determining said slope or slopes with which the aircraft is able to fly, called flyable slopes is performed by a computer, and presenting the flyable slope to a decision-maker.

摘要翻译： 一种飞机驾驶辅助方法和系统，包括基于包括飞行器的重量的至少一个飞行参数的值来确定假定飞行器能够飞行的至少一个飞行坡度。 用于确定飞机能够飞行的所述斜坡或斜坡的步骤称为可飞行斜坡，由计算机执行，并将可飞行坡度呈现给决策者。

公开(公告)号：US08509966B2

公开(公告)日：2013-08-13

申请号：US12358853

申请日：2009-01-23

申请人： Francois Coulmeau ,  Guilhem Putz ,  Olivier Friedmann

发明人： Francois Coulmeau ,  Guilhem Putz ,  Olivier Friedmann

IPC分类号： G01C23/00 ,  G05D1/00 ,  G05D3/00 ,  G06F7/00 ,  G06F17/00 ,  G01W1/00

CPC分类号： G01W1/00 ,  G01C23/00 ,  G08G5/0091

摘要： The subject of the present invention is a method of estimating, at any point of a path of an aircraft, characteristics of the wind making it possible to take very close account of the winds to construct predictions of the times of passage and of the consumption of the aircraft along its flight plan, and this method is characterized in that it consists in collecting, around the trajectory of the aircraft, a grid of parameter values of winds at a predetermined number of points in space, in comparing these values to those deriving from space-time wind trend models, in selecting, path section by section, the most likely model, and in interpolating, for each section, the local characteristics of the wind of all the points of interest of the trajectory.

摘要翻译： 本发明的主题是在飞行器的路径的任何点处估计风的特征的方法，使得可以非常仔细地考虑风，以构建通过时间和消耗时间的预测 飞机沿其飞行计划，该方法的特征在于，将这些值与从空中飞行计划得到的值进行比较，在飞行器的轨迹周围收集预定数量的空间中的风的参数值的网格 时空风向模型，逐段选择路径，最可能的模型，以及为每个部分插入轨迹的所有兴趣点的风的局部特征。

公开(公告)号：US08275499B2

公开(公告)日：2012-09-25

申请号：US12579272

申请日：2009-10-14

申请人： Francois Coulmeau ,  Manuel Gutierrez-Castaneda ,  Nicolas Marty

发明人： Francois Coulmeau ,  Manuel Gutierrez-Castaneda ,  Nicolas Marty

IPC分类号： G01C23/00 ,  G06G7/78

CPC分类号： G08G5/006

摘要： The invention relates to a device for formulating a flight plan ensuring sufficient safety margins for a duration of a few minutes in relation to the set of flight constraints that could arise and comprising means for: detecting the surrounding moving objects (aircraft or meteorological phenomena), evaluating their type and the danger that they represent, formulating a reconfiguration flight plan ensuring a separation with these phenomena and taking best account of the constraints of the initially followed flight plan, avoiding prohibited or regulated airspaces and avoiding the surrounding relief with ad hoc operational margins.

摘要翻译： 本发明涉及一种用于制定飞行计划的装置，其确保相对于可能出现的一组飞行约束，持续几分钟的足够的安全裕度，并且包括用于：检测周围的运动物体（飞机或气象现象）的装置， 评估他们的类型和他们所代表的危险，制定重新配置飞行计划，确保与这些现象分离，并充分考虑到最初跟踪的飞行计划的限制，避免被禁止或受规管的空域，并避免周围的特殊运营利润减轻 。

公开(公告)号：US20090076721A1

公开(公告)日：2009-03-19

申请号：US12208460

申请日：2008-09-11

申请人： Francois COULMEAU ,  Herve Goutelard ,  Jerome Sacle

发明人： Francois COULMEAU ,  Herve Goutelard ,  Jerome Sacle

IPC分类号： G01C21/00

CPC分类号： G01C23/005 ,  G01C21/20 ,  G08G5/0039

摘要： The invention relates to a navigation aid method and device for an aircraft. The aircraft occupies a position PPOS outside its flight plan and seeks to rejoin the flight plan. The flight plan includes a succession of waypoints. A waypoint WPTi is called sequenced once the aircraft has passed by the waypoint WPTi at a lateral distance within the limits of the fixed sequencing conditions. The next unsequenced waypoint is called the active waypoint. The method includes the computation of at least one path to rejoin the flight plan from the current position PPOS, the computation of a potential active waypoint in the flight plan based on a rejoining path, the display of the potential active waypoint, if the pilot confirms the potential active waypoint, the sequencing of the waypoints situated upstream of the potential active waypoint, the said potential active waypoint becoming the new active waypoint.

摘要翻译： 本发明涉及飞机的导航辅助方法和装置。 该飞机在飞行计划之外占据了PPOS的位置，并寻求重新加入飞行计划。 飞行计划包括一系列航点。 一旦航空器在固定排序条件的限度内以横向距离通过航点WPTi，则将航点WPTi称为测序。 下一个未排序的航路点称为主动航路点。 该方法包括至少一条路径的计算，以从当前位置PPOS重新加入飞行计划，基于重新连接路径计算飞行计划中的潜在主动航点，潜在的主动航点的显示，如果飞行员确认 潜在的主动航点，位于潜在主动航点的上游的航点的排序，所述潜在的主动航路点成为新的主动航点。

公开(公告)号：US20080300738A1

公开(公告)日：2008-12-04

申请号：US12130267

申请日：2008-05-30

申请人： Francois Coulmeau ,  Guy Deker ,  Herve Goutelard

发明人： Francois Coulmeau ,  Guy Deker ,  Herve Goutelard

IPC分类号： G06F17/00

CPC分类号： G01C21/20 ,  G05D1/0005

摘要： A method of optimizing a flight plan of an aircraft used in a flight management system of an aircraft is disclosed. This method makes it possible to constrain the real cost index of the mission executed to the optimal cost index CIopt predetermined by the aircraft operator, by acting on objectives ETAopt and EFOBopt of values of ETA and of EFOB to be achieved. Objectives are linked to this optimal cost index, in order to make the system return from a cost index CIm to the optimal cost index CIopt, while taking account of various constraints imposed by the ATC or the CTFM. Both constraints mext influence the cost index and constraints which limit the field of possible solutions.

摘要翻译： 公开了一种优化飞行器飞行管理系统中使用的飞机的飞行计划的方法。 这种方法可以通过执行要达到的ETA和EFOB的目标ETAopt和EFOBopt的目标ETAopt和EFOBopt来限制执行的任务的实际成本指数为飞机运营商预先确定的最佳成本指数CIopt。 目标与这个最优成本指标相关联，以便使系统从成本指数CIm返回到最佳成本指数CIopt，同时考虑到ATC或CTFM施加的各种约束。 这两个约束条件都会影响成本指标和限制可能解决方案领域的限制。

公开(公告)号：US20080262665A1

公开(公告)日：2008-10-23

申请号：US12103122

申请日：2008-04-15

申请人： Francois COULMEAU ,  Guilhem Putz

发明人： Francois COULMEAU ,  Guilhem Putz

IPC分类号： G01C21/00

CPC分类号： G08G5/025 ,  G05D1/0676 ,  G08G5/0039 ,  Y02T50/84

摘要： The general field of the invention relates to a method of calculating a so-called continuous descent approach procedure for aircraft. The method comprises calculation steps making it possible to determine a minimum distance making it possible to attain the runway by using the highest possible descent angles allowed by the performance of the aircraft, a maximum distance making it possible to attain the runway by using the lowest possible descent angles allowed by the performance of the aircraft, a step of comparing the minimum and maximum distances with a reference distance, the continuous descent approach procedure being possible if this reference distance is less than the maximum distance and greater than the minimum distance. The method also envisages replacing certain indeterminate points of the flight plan by points arising from the minimum and maximum distance calculations.

摘要翻译： 本发明的一般领域涉及一种计算飞机所谓的连续下降接近程序的方法。 该方法包括计算步骤，使得可以确定最小距离，使得可以通过使用由飞机执行所允许的最高可能下降角获得跑道，最大距离使得可以通过使用尽可能低的速度达到跑道 航空器性能允许的下降角度，将最小和最大距离与参考距离进行比较的步骤，如果该参考距离小于最大距离并且大于最小距离，连续下降接近程序是可能的。 该方法还设想通过最小和最大距离计算产生的点来替代飞行计划的某些不确定点。