公开(公告)号：US07797102B2

公开(公告)日：2010-09-14

申请号：US11637836

申请日：2006-12-13

申请人： Stéphanie Fortier

发明人： Stéphanie Fortier

IPC分类号： G01C21/00

CPC分类号： G08G5/0034 ,  G08G5/0052

摘要： A flight management system for an aircraft, for executing a flight plan comprising referenced waypoints comprising a start point, an end point and intermediate waypoints, the said aircraft having a specified fuel quantity at the start of the said flight plan, executes a function of monitoring the fuel consumption with respect to at least one threshold value. The function comprises an operation for estimating if the quantity of fuel remaining on board drops below a threshold at any point in the flight plan included between the start point and the end point, and inserts a corresponding pseudo-waypoint in the flight plan, corresponding to the point where the said threshold is passed. The inserted pseudo-point is displayed on screens for displaying the flight plan.

摘要翻译： 一种用于飞行器的飞行管理系统，用于执行飞行计划，其包括参考航路点，其包括起点，终点和中间飞行点，所述飞行器在所述飞行计划开始时具有指定的燃料量，执行监视功能 相对于至少一个阈值的燃料消耗。 该功能包括用于估计在起点和终点之间包括的飞行计划中的任何点处的船上剩余燃料量是否下降到阈值以下的操作，并且在飞行计划中插入对应的伪航点，对应于 所述阈值通过的点。 插入的伪点显示在显示飞行计划的屏幕上。

公开(公告)号：US20100324812A1

公开(公告)日：2010-12-23

申请号：US12780684

申请日：2010-05-14

申请人： Jérôme Sacle ,  Stéphanie Fortier ,  François Coulmeau

发明人： Jérôme Sacle ,  Stéphanie Fortier ,  François Coulmeau

IPC分类号： G01C21/00

CPC分类号： G01C23/00 ,  G01C21/00 ,  G05D1/0202

摘要： Method of formulating a lateral flight trajectory for the rejoining by an aircraft (200) of a trajectory of a flight plan (910) comprising a plurality of waypoints (911, 912, 913), the aircraft (200) flying outside of the flight plan (910) and according to a divergent track with respect to the trajectory of the flight plan (210), characterized in that the method: determines a waypoint (913) of the flight plan for the rejoining, defined as the first waypoint (913) of the flight plan included in a capture zone defined by the flight plan trajectory situated downstream of the point of intersection between the straight line defined by an angle (α) with the perpendicular to the track of the aircraft and the trajectory of the flight plan, formulates the optimal lateral flight trajectory for a rejoining by the aircraft (200) at the determined waypoint. Advantageously, the flight trajectory formulation method allows the application of speed and/or altitude constraints to the aircraft (200) taking into account speed and/or altitude constraints imposed along the trajectory of the flight plan (910).

摘要翻译： 制定由飞行计划（910）的轨迹的飞行器（200）重新连接的侧向飞行轨迹的方法，该飞行计划包括多个航路点（911,912,913），飞行器（200）飞行在飞行计划之外 （910）并且根据相对于飞行计划（210）的轨迹的发散轨迹，其特征在于，所述方法：确定被定义为所述第一航点（913）的重新连接的飞行计划的航点（913） 包括在由飞行计划轨迹定义的捕获区域中的飞行计划，该飞行计划轨迹位于由角度（α）与垂直于飞行器的轨迹的垂线之间的交点点和飞行计划的轨迹之间的交点处的下游， 制定航空器（200）在确定航路点重新连接的最佳横向飞行轨迹。 有利地，飞行轨迹拟合方法允许考虑到沿着飞行计划的轨迹施加的速度和/或高度约束，对飞行器（200）应用速度和/或高度限制（910）。

公开(公告)号：US08498769B2

公开(公告)日：2013-07-30

申请号：US12780684

申请日：2010-05-14

申请人： Jérôme Sacle ,  Stéphanie Fortier ,  François Coulmeau

发明人： Jérôme Sacle ,  Stéphanie Fortier ,  François Coulmeau

IPC分类号： G01C22/00

CPC分类号： G01C23/00 ,  G01C21/00 ,  G05D1/0202

摘要： Method of formulating a lateral flight trajectory for the rejoining by an aircraft (200) of a trajectory of a flight plan (910) comprising a plurality of waypoints (911, 912, 913), the aircraft (200) flying outside of the flight plan (910) and according to a divergent track with respect to the trajectory of the flight plan (210), characterized in that the method: determines a waypoint (913) of the flight plan for the rejoining, defined as the first waypoint (913) of the flight plan included in a capture zone defined by the flight plan trajectory situated downstream of the point of intersection between the straight line defined by an angle (α) with the perpendicular to the track of the aircraft and the trajectory of the flight plan, formulates the optimal lateral flight trajectory for a rejoining by the aircraft (200) at the determined waypoint. Advantageously, the flight trajectory formulation method allows the application of speed and/or altitude constraints to the aircraft (200) taking into account speed and/or altitude constraints imposed along the trajectory of the flight plan (910).

摘要翻译： 制定由飞行计划（910）的轨迹的飞行器（200）重新连接的侧向飞行轨迹的方法，该飞行计划包括多个航路点（911,912,913），飞行器（200）飞行在飞行计划之外 （910）并且根据相对于飞行计划（210）的轨迹的发散轨迹，其特征在于，所述方法：确定被定义为所述第一航点（913）的重新连接的飞行计划的航点（913） 飞行计划中包含的飞行计划包括在由飞行计划轨迹定义的捕获区域中，该飞行计划轨迹位于由角度（α）与垂直于飞行器的轨迹的垂线之间的交点点和飞行计划的轨迹之间的交点处的下游， 制定航空器（200）在确定航路点重新连接的最佳横向飞行轨迹。 有利地，飞行轨迹拟合方法允许考虑到沿着飞行计划的轨迹施加的速度和/或高度约束，对飞行器（200）应用速度和/或高度限制（910）。

公开(公告)号：US20100198433A1

公开(公告)日：2010-08-05

申请号：US12634128

申请日：2009-12-09

申请人： Stéphanie Fortier ,  Jérôme Sacle

发明人： Stéphanie Fortier ,  Jérôme Sacle

IPC分类号： G06F19/00 ,  G06F17/16

CPC分类号： G01C23/00 ,  G05D1/0005 ,  G08G5/0021 ,  G08G5/0039

摘要： Flight management system for aircraft comprising computation means capable of determining a gain or a loss in terms of flight time remaining to a point of arrival, and in terms of fuel consumption, following the input by an operator of a modification of an initial flight plan using the Direct To function. The computation means are capable of suggesting to the operator a modification of the lateral flight plan that procures an optimum gain. The flight management system also comprises a display interface capable of presenting to the operator the information concerning the gain or the loss in time and/or consumption, and of prompting the operator to accept or refuse the modification.

摘要翻译： 用于飞行器的飞行管理系统包括计算装置，该计算装置能够根据运营人输入的初始飞行计划的修改，确定在剩余到达点的飞行时间的增益或损失以及燃料消耗。 直接到功能。 计算装置能够向操作者建议获得最佳增益的侧向飞行计划的修改。 飞行管理系统还包括显示界面，能够向操作者呈现关于增益或时间和/或消耗的损失的信息，并且提示操作者接受或拒绝修改。