公开(公告)号：US08768556B2

公开(公告)日：2014-07-01

申请号：US12945449

申请日：2010-11-12

申请人： Gershon Ben-Arie ,  Ilana Segall ,  Asi Dotan

发明人： Gershon Ben-Arie ,  Ilana Segall ,  Asi Dotan

IPC分类号： G01C22/00

CPC分类号： G01C23/00 ,  G01C5/00 ,  G05D1/0646 ,  G05D1/0858

摘要： An apparatus defines a protection envelope in an aircraft, including a processor and at least one sensor, each sensor being coupled with the processor, the processor executing at least one neural network based algorithm. The at least one sensor monitors flight parameters of the aircraft thereby generating monitored flight parameters. The processor divides the performance envelope of the aircraft into predefined flight regimes, wherein for each predefined flight regime, the processor defines and stores a suitable protection envelope. The processor determines an estimated flight regime of the aircraft using the neural network based algorithm based on the monitored flight parameters. The processor selects a respective suitable protection envelope for the aircraft based on the estimated flight regime.

摘要翻译： 一种装置在飞行器中定义保护包络，包括处理器和至少一个传感器，每个传感器与处理器耦合，处理器执行至少一个基于神经网络的算法。 至少一个传感器监测飞行器的飞行参数，从而产生监视的飞行参数。 处理器将飞行器的性能包络分为预定义的飞行状态，其中对于每个预定义的飞行状态，处理器定义并存储合适的保护信封。 处理器基于所监视的飞行参数，使用基于神经网络的算法确定飞行器的估计飞行状态。 处理器基于估计的飞行状况来选择飞机的相应合适的保护信封。

公开(公告)号：US08249761B2

公开(公告)日：2012-08-21

申请号：US12499350

申请日：2009-07-08

申请人： Hasse Persson ,  Jonas Lovgren

发明人： Hasse Persson ,  Jonas Lovgren

IPC分类号： G05D1/00 ,  B64C13/18

CPC分类号： G05D1/101 ,  G05D1/0646

摘要： The invention relates to a method for calculating a flight path avoiding a collision with the ground when an aircraft dives towards the ground. The method includes receiving signals including information of a dive angle of the aircraft in relation to the imaginary ground plane, and a present roll angle of the aircraft, and calculating a flight path that avoids collision with the ground on the basis of the information. The calculation includes calculating a need for rolling the aircraft based on the present roll angle, and calculating a need for changing the direction of the velocity vector of the aircraft so that the change has a component in an upward direction in relation to the reference frame of the aircraft. The calculation of the need for rolling the aircraft is also based on the dive angle so that the calculated flight path turns sideways when the dive angle surpasses a specified dive angle and when the present roll angle is larger than zero degrees, and so that the flight path continues in a forward direction when the dive angle is below the specified dive angle. The invention also relates to a ground collision calculating unit, a computer program, and a computer readable medium.

摘要翻译： 本发明涉及一种用于在飞机潜入地面时计算避免与地面碰撞的飞行路径的方法。 该方法包括接收信号，包括飞行器相对于虚拟地平面的潜水角度的信息，以及飞行器的当前滚动角度，以及基于该信息计算避免与地面碰撞的飞行路径。 该计算包括计算基于当前滚动角度来滚动飞行器的需要，以及计算改变飞行器的速度矢量的方向的需要，使得该变化相对于参考系的参考系具有向上方向的分量 飞机。 对飞机的滚动需求的计算也基于潜水角度，使得当潜水角超过指定的潜水角度时，当当前的倾斜角度大于零度时，所计算的飞行路线将横向转动，并且使得飞行 当潜水角度低于指定的潜水角度时，路径向前延伸。 本发明还涉及地面碰撞计算单元，计算机程序和计算机可读介质。

公开(公告)号：US20120158220A1

公开(公告)日：2012-06-21

申请号：US13324047

申请日：2011-12-13

申请人： Domenico ACCARDO ,  Antonio Moccia ,  Michele Grassi ,  Urbano Tancredi ,  Lucio Caminiti ,  Luigi Fiorillo ,  Alberto Leardi ,  Giuseppe Maresca

发明人： Domenico ACCARDO ,  Antonio Moccia ,  Michele Grassi ,  Urbano Tancredi ,  Lucio Caminiti ,  Luigi Fiorillo ,  Alberto Leardi ,  Giuseppe Maresca

IPC分类号： G05D1/00 ,  G08G5/00 ,  G06F19/00

CPC分类号： G08G5/0082 ,  G05D1/0646 ,  G08G5/0052 ,  G08G5/0065

摘要： The invention concerns a method and system for the prediction of aircrafts vertical trajectory, in particular for Air Traffic Management, comprising the following flight calculation modules: Take-off; Climb; Cruise; Descent; and Landing, corresponding to the relevant flight phases, wherein: the calculation of the predicted aircraft trajectory is effected by using a set of TEM equations comprising, as output variables, the vertical rate of climb or descent, the true air speed, the energy share factor, the thrust and the drag, the mass of the aircraft modeled as point-mass, and comprising, as inpu variables, the Mach number depending on true air speed and temperature and altitude, the gravity acceleration, and the fuel flow, and the flight path angle; the calculation of the predicted aircraft trajectory for Cruise phase, wherein only the mass is varying, is performed by using the following analytical solution to said set of TEM equations.

摘要翻译： 本发明涉及用于预测飞机垂直轨迹的方法和系统，特别是用于空中交通管理，其包括以下飞行计算模块：起飞; 爬; 巡航; 下降 和着陆，其对应于相关航班阶段，其中：通过使用一组TEM方程来实现预测飞机轨迹的计算，所述TEM方程式包括作为输出变量的垂直爬升速率或下降速率，真实空速，能量份额 因素，推力和阻力，模拟为点质量的飞机的质量，并且包括作为inpu变量的马赫数，其取决于真实的空气速度，温度和高度，重力加速度和燃料流量，以及 飞行路径角; 通过使用对所述一组TEM方程的以下分析解来执行其中仅质量变化的巡航相的预测飞机轨迹的计算。

公开(公告)号：US08140264B2

公开(公告)日：2012-03-20

申请号：US10583359

申请日：2004-12-08

申请人： Philippe Salmon ,  Hugues Meunier

发明人： Philippe Salmon ,  Hugues Meunier

IPC分类号： G08G1/16

CPC分类号： G05D1/0646

摘要： The field of the invention is that of onboard terrain anticollision systems for aircraft. Collisions with the terrain while the aircraft is fully controlled have been and still remain one of the main causes of air disasters. Several generations of devices for warning of risk of collision with the terrain have been developed for some thirty years now. The most advanced of these systems comprise means of alarm differing according to the maneuver to be performed by the pilot. It is of course vital that the recommended maneuver best guarantee the safety of the aircraft. The device according to the invention proposes a device comprising the calculation of several different safety surfaces or profiles. Their comparisons with the topographic data of the surrounding terrain make it possible to deduce therefrom the best alarm and the best maneuver to be performed to avoid the collision between the aircraft and the ground.

摘要翻译： 本发明的领域是用于飞机的机载地形防撞系统。 飞机完全控制时与地形的碰撞已经仍然是空中灾难的主要原因之一。 近几十年来，已经开发了几代用于警告与地形相撞风险的装置。 这些系统中最先进的装置包括根据驾驶员执行的操纵而不同的报警装置。 当然，推荐的机动动作最好能保证飞机的安全。 根据本发明的装置提出了一种包括计算几个不同安全表面或轮廓的装置。 他们与周围地形的地形数据进行比较，可以从中推导出最佳的报警和最佳的机动，以避免飞机和地面之间的碰撞。

公开(公告)号：US07899613B2

公开(公告)日：2011-03-01

申请号：US11121058

申请日：2005-05-04

申请人： Franck Artini

发明人： Franck Artini

IPC分类号： G06F19/00 ,  G06G7/70 ,  G06G7/76 ,  G05D1/00 ,  G05D3/00 ,  G06F7/00 ,  G06F17/00 ,  G05D1/08 ,  G05D1/06 ,  G01C5/00 ,  G01C23/00 ,  G01C21/00 ,  G08B23/00

CPC分类号： G05D1/0646

摘要： Method and device for ensuring the safety of a low-altitude flight of an aircraft.The device (1) comprises a recording means (8) corresponding to an operation critical instrument for recording, during a low-altitude flight, one part at least of the lateral trajectory of the flight trajectory situated ahead of the current position of the aircraft, a monitoring means (11) for monitoring, during a low-altitude flight, the availability at least of said lateral trajectory, and a guidance system (3) for taking the aircraft up to a safe altitude, taking into account said part of the trajectory recorded by said recording means (8), when said monitoring means (11) has detected a loss of said lateral trajectory.

摘要翻译： 确保飞机低空飞行安全的方法和装置。 装置（1）包括对应于操作临界工具的记录装置（8），用于在低空飞行期间记录位于飞行器当前位置之前的飞行轨迹的至少横向轨迹的至少一部分， 用于在低空飞行期间至少监视所述横向轨迹的可用性的监视装置（11），以及用于将飞行器乘以安全高度的引导系统（3），其考虑到所述轨迹的所述部分 当所述监视装置（11）检测到所述横向轨迹的损失时，由所述记录装置（8）记录。

公开(公告)号：US07826971B2

公开(公告)日：2010-11-02

申请号：US12047633

申请日：2008-03-13

申请人： Sylvain Fontaine ,  Nicolas Marty ,  Pierre Gamet

发明人： Sylvain Fontaine ,  Nicolas Marty ,  Pierre Gamet

IPC分类号： G08G1/16

CPC分类号： G05D1/0646

摘要： A method for filtering anti-collision alarms for aircraft, the said aircraft comprising means for calculating its speed and extrapolated positions on its trajectory, the said extrapolated positions being calculated over a fixed maximum time period, called extrapolation time, and a topographical database of the terrain, the said database comprising, within a given perimeter, data on the density of obstacles, comprises a calculation of a weighting coefficient for the extrapolation time of the calculated extrapolated trajectories of the aircraft as a function of the density of obstacles within a surface area included within the perimeter.

摘要翻译： 一种用于过滤飞行器的防碰撞报警的方法，所述飞行器包括用于计算其速度和在其轨迹上的外推位置的装置，所述外推位置是在固定的最大时间段（称为外推时间）上计算的，以及地形数据库 所述数据库在给定的周长内包括关于障碍物密度的数据，包括作为所述飞行器计算的外推轨迹的外推时间的加权系数的计算，作为表面区域内的障碍物的密度的函数 包括在周边。

公开(公告)号：US20100100261A1

公开(公告)日：2010-04-22

申请号：US12582240

申请日：2009-10-20

申请人： Paule Botargues ,  Nicolas Caule ,  Christelle Ledauphin ,  Jerome Bailly ,  Isabelle Lacaze ,  Sylvain Thezelais ,  Jerome Goyet

发明人： Paule Botargues ,  Nicolas Caule ,  Christelle Ledauphin ,  Jerome Bailly ,  Isabelle Lacaze ,  Sylvain Thezelais ,  Jerome Goyet

IPC分类号： G06F7/00 ,  G08B23/00

CPC分类号： G08G5/04 ,  G01C5/005 ,  G05D1/0646

摘要： According to the invention, an altitude profile (PA) representative of the terrain overflown by the aircraft (AC) is established, and then an altitude limit curve (C) which comprises an intersection with said profile (PA) upon the engagement of a terrain avoidance maneuver is determined. As soon as there is no longer any intersection of the limit curve (C) with the altitude profile (PA), said terrain avoidance maneuver is interrupted.

摘要翻译： 根据本发明，建立了代表由飞行器（AC）溢出的地形的高度分布（PA），然后在地形接合时包括与所述轮廓（PA）的交点的高度极限曲线（C） 确定回避机动。 一旦极限曲线（C）与高度剖面（PA）不再有任何交点，则所述的地形回避机动被中断。

公开(公告)号：US20100010693A1

公开(公告)日：2010-01-14

申请号：US12499350

申请日：2009-07-08

申请人： Hasse Persson ,  Jonas Lövgren

发明人： Hasse Persson ,  Jonas Lövgren

IPC分类号： G05D1/06

CPC分类号： G05D1/101 ,  G05D1/0646

摘要： The invention relates to a method for calculating a flight path avoiding a collision with the ground when an aircraft dives towards the ground. The method includes receiving signals including information of a dive angle of the aircraft in relation to the imaginary ground plane, and a present roll angle of the aircraft, and calculating a flight path that avoids collision with the ground on the basis of the information. The calculation includes calculating a need for rolling the aircraft based on the present roll angle, and calculating a need for changing the direction of the velocity vector of the aircraft so that the change has a component in an upward direction in relation to the reference frame of the aircraft. The calculation of the need for rolling the aircraft is also based on the dive angle so that the calculated flight path turns sideways when the dive angle surpasses a specified dive angle and when the present roll angle is larger than zero degrees, and so that the flight path continues in a forward direction when the dive angle is below the specified dive angle. The invention also relates to a ground collision calculating unit, a computer program, and a computer readable medium.

摘要翻译： 本发明涉及一种用于在飞机潜入地面时计算避开与地面碰撞的飞行路径的方法。 该方法包括接收信号，包括飞行器相对于虚拟地平面的潜水角度的信息，以及飞行器的当前滚动角度，以及基于该信息计算避免与地面碰撞的飞行路径。 该计算包括计算基于当前滚动角度来滚动飞行器的需要，以及计算改变飞行器的速度矢量的方向的需要，使得该变化相对于参考系的参考系具有向上方向的分量 飞机。 对飞机的滚动需求的计算也基于潜水角度，使得当潜水角超过指定的潜水角度时，当当前的倾斜角度大于零度时，所计算的飞行路线将横向转动，并且使得飞行 当潜水角度低于指定的潜水角度时，路径向前延伸。 本发明还涉及地面碰撞计算单元，计算机程序和计算机可读介质。

公开(公告)号：US07499773B2

公开(公告)日：2009-03-03

申请号：US11438227

申请日：2006-05-23

申请人： Richard Pire ,  Francois-Xavier Filias

发明人： Richard Pire ,  Francois-Xavier Filias

IPC分类号： B64D43/00 ,  G06F19/00

CPC分类号： G08G5/0086 ,  G01S13/94 ,  G05D1/0646 ,  G08G5/045

摘要： In a method of the invention for assisting the piloting of an aircraft, a guard curve (CGS) is determined as a function of the resources of the aircraft, the position of an obstacle (O) or a terrain point situated in front of the aircraft is measured by telemetry, the distance D between the guard curve and the obstacle (O) or the terrain point is calculated, and a pull-down order or a pull-up order is produced as a function of the distance D.

摘要翻译： 在本发明的一种用于辅助飞机驾驶的方法中，根据飞机的资源，位于飞机前方的障碍物（O）或地形点的位置确定保护曲线（CGS） 通过遥测测量，计算防护曲线与障碍物（O）或地形点之间的距离D，并且产生下拉顺序或上拉顺序作为距离D的函数。

公开(公告)号：US07440826B2

公开(公告)日：2008-10-21

申请号：US10528027

申请日：2003-08-29

申请人： Nicolas Franceschini ,  Franck Ruffier ,  Stéphane Viollet ,  Marc Boyron

发明人： Nicolas Franceschini ,  Franck Ruffier ,  Stéphane Viollet ,  Marc Boyron

IPC分类号： G05D1/08 ,  G06F19/00

CPC分类号： G05D1/0646 ,  G05D1/0858

摘要： A steering aid system for altitude and horizontal speed of an aircraft (4) includes: a measuring device (22) for delivering a measured signal based on the aircraft altitude and horizontal speed, a common predetermined reference value (26) for the aircraft altitude and horizontal speed, and elements (20) for slaving the signal to the reference value by pitch loop, the elements being adapted to vary automatically the pitch and/or propulsive performance of the lifting members to lock the measured signal to the reference value.

摘要翻译： 一种用于航空器（4）的高度和水平速度的转向辅助系统包括：用于基于飞行器高度和水平速度传送测量信号的测量装置（22），用于飞行器高度的公共预定参考值（26） 水平速度和用于通过俯仰环将信号逐渐减小到参考值的元件（20），所述元件适于自动改变提升构件的俯仰和/或推进性能以将测量信号锁定到参考值。