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11.发明授权Method and device for preventing useless alarms generated by an anti-collision system on board an airplane 有权用于防止飞机上的防碰撞系统产生的无用报警的方法和装置公开(公告)号：US08295996B2
公开(公告)日：2012-10-23
申请号：US12563661
申请日：2009-09-21
Applicant: Paule Botargues , Xavier Dal Santo , Pierre Fabre , Xavier Guery
Inventor： Paule Botargues , Xavier Dal Santo , Pierre Fabre , Xavier Guery
IPC: G05D1/00
CPC classification number: G08G5/045
Abstract: The invention describes a method and device for preventing useless alarms generated by an anticollision system on board an airplane and according to which the duration (dcap) of a phase of capture of a setpoint altitude (Zc) by the airplane is between a predetermined minimum execution deadline (dmin) and a predetermined maximum execution deadline (dmax).
Abstract translation: 本发明描述了一种用于防止由飞机上的防冲突系统产生的无用警报的方法和装置，根据该方法和装置，由飞机捕获设定点高度（Zc）的相位的持续时间（dcap）在预定的最小执行 截止日期（dmin）和预定的最大执行期限（dmax）。
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12.发明申请Method And Device For Updating A Target Altitude For An Emergency Descent Of An Aircraft 有权用于更新飞机紧急下降目标海拔的方法和装置公开(公告)号：US20120022725A1
公开(公告)日：2012-01-26
申请号：US13184174
申请日：2011-07-15
Applicant: Paule Botargues , Erwin Grandperret , Lucas Burel , Thierry Bourret
Inventor： Paule Botargues , Erwin Grandperret , Lucas Burel , Thierry Bourret
CPC classification number: G05D1/0055 , G01C5/005 , G05D1/0607
Abstract: Method and device for updating a target altitude for an emergency descent of an aircraft.The device (1) comprises means (2, 3, 4, 7) for determining an updated target altitude which takes into account variations of barometric pressure and which is able to replace a target altitude that must be reached at the end of the emergency descent.
Abstract translation: 用于更新飞机紧急下降的目标高度的方法和装置。 装置（1）包括用于确定更新的目标高度的装置（2,3,4,7），其考虑到气压的变化并且能够替代在紧急下降结束时必须达到的目标高度 。
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13.发明申请公开(公告)号：US20120022723A1
公开(公告)日：2012-01-26
申请号：US13184040
申请日：2011-07-15
Applicant: Paule Botargues , Erwin Grandperret , Lucas Burel
Inventor： Paule Botargues , Erwin Grandperret , Lucas Burel
IPC: G05D1/04
CPC classification number: G05D1/0055 , G05D1/0607
Abstract: Method and device for determining and updating a target altitude for an emergency descent of an aircraftThe device (1) includes means (3, 4, 8, 10) for determining a target altitude from a security altitude defined along the current trajectory of the aircraft on a particular distance ahead of the aircraft.
Abstract translation: 用于确定和更新飞行器紧急下降的目标高度的方法和装置装置（1）包括用于从沿着飞行器的当前轨迹定义的安全高度确定目标高度的装置（3,4,8,10） 在飞机前面的特定距离处。
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14.发明申请Method And Device For Preventing An Anti-Collision System On Board An Airplane From Emitting Alarms, During An Altitude Capture Maneuver 有权方法和装置，用于防止发生警报的飞机上的防碰撞系统，在高度捕获机动公开(公告)号：US20110187561A1
公开(公告)日：2011-08-04
申请号：US13016154
申请日：2011-01-28
Applicant: Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
Inventor： Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
IPC: G08G5/04
CPC classification number: G08G5/045 , G01S13/9303 , G08G5/04
Abstract: According to the invention, the device (1) comprises means (3) for detecting, during an altitude capture maneuver, the emission of a first type alarm by the anti-collision system (2) and means (4) for controlling the vertical speed of said airplane (AC), after the emission of such an alarm, until the triggering of the capture phase.
Abstract translation: 根据本发明，装置（1）包括用于在高空拍摄操作期间检测由防撞系统（2）发射第一类型警报的装置（3）和用于控制垂直速度的装置（4） 的所述飞机（AC），在发出这样的报警之后，直到触发捕获阶段。
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公开(公告)号：US20080021647A1
公开(公告)日：2008-01-24
申请号：US11576658
申请日：2005-10-06
Applicant: Fabien Daveze , Vincent Foucart , Paule Botargues , Didier Averseng
Inventor： Fabien Daveze , Vincent Foucart , Paule Botargues , Didier Averseng
IPC: G01C23/00
CPC classification number: G08G5/045 , G08G5/0021
Abstract: The invention relates to an avoidance method and system for an aircraft, said avoidance system (1) comprising an anti-collision system (3), calculation means (4) for automatic determination of avoidance instructions, on an alarm, from avoidance information received from the anti-collision system (3) and an avoidance aid system (6, 21), connected to the calculation means (4) which aid the piloting of the aircraft (A), by means of the instructions received from said calculation means (4).
Abstract translation: 本发明涉及一种用于飞机的回避方法和系统，所述回避系统（1）包括防冲突系统（3），用于在报警器上自动确定回避指令的计算装置（4），从避免信息接收到的回避信息 所述防撞系统（3）以及与所述计算装置（4）相连接的辅助系统（6,21），所述避免辅助系统借助于从所述计算装置（4）接收到的指令来辅助飞机（A）的驾驶 ）。
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Patent Agency Ranking
公开(公告)号：US08725401B2
公开(公告)日：2014-05-13
申请号：US11576658
申请日：2005-10-06
Applicant: Fabien Daveze , Vincent Foucart , Paule Botargues , Didier Averseng
Inventor： Fabien Daveze , Vincent Foucart , Paule Botargues , Didier Averseng
CPC classification number: G08G5/045 , G08G5/0021
Abstract: Disclosed is a method and system for avoiding collision between an aircraft A and an intruder aircraft. The method and system involve determining avoidance presets to avoid a collision between the aircraft A and the intruder aircraft, in which the avoidance presets comprise a vertical speed preset. The presets are determined from avoidance information received from an anticollision system, and the determined avoidance presets are transmitted to at least one guidance device that guides the aircraft A based on the avoidance presets.
Abstract translation: 公开了一种用于避免飞机A和入侵者飞机之间的碰撞的方法和系统。 该方法和系统包括确定避免预设以避免飞机A与入侵者飞机之间的碰撞，其中回避预设包括垂直速度预设。 从防冲突系统接收的回避信息来确定预设，并且将确定的回避预设传送到至少一个引导装置，其基于回避预设来引导飞行器A.
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17.发明授权公开(公告)号：US08467917B2
公开(公告)日：2013-06-18
申请号：US13184123
申请日：2011-07-15
Applicant: Paule Botargues , Erwin Grandperret , Lucas Burel , Jacques Rosay , Didier Ronceray
Inventor： Paule Botargues , Erwin Grandperret , Lucas Burel , Jacques Rosay , Didier Ronceray
IPC: G05D1/00
CPC classification number: G05D1/0055 , G05D1/101
Abstract: A method for automatically managing a lateral trajectory upon triggering an emergency descent includes determining a value of lateral offset and generating an offset setpoint by using the value of lateral offset. The generating an offset setpoint includes calculating a sum of the value of lateral offset and any initial value of lateral offset defined between a central axis of a protected sector that the aircraft travels along and an initial lateral trajectory. The offset setpoint is selected to be the smaller of the sum or a lateral offset maximum, which maintains the aircraft within the protected sector at all times. The aircraft is then operated to move the aircraft to the offset setpoint during the emergency descent, which helps avoid further air traffic that may be located at different altitude levels within the same protected sector, especially along the central axis.
Abstract translation: 用于在触发紧急下降时自动管理横向轨迹的方法包括通过使用横向偏移值来确定横向偏移的值并产生偏移设定点。 产生偏移设定点包括计算横向偏移值和在飞行器沿着保护扇区的中心轴线和初始横向轨迹之间限定的横向偏移的任何初始值的和。 偏移设定点被选择为总和或横向偏移最大值中的较小者，它始终将飞机保持在受保护的扇区内。 然后飞行器在紧急下降期间将飞机移动到偏移设定点，这有助于避免可能位于相同受保护扇区内的不同高度水平的进一步空中交通，特别是沿着中心轴线。
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18.发明授权Method and device for preventing an anti-collision system on board an airplane from emitting alarms, during an altitude capture maneuver 有权在高空拍摄操作期间，用于防止飞机上的防碰撞系统发射报警的方法和装置公开(公告)号：US08446295B2
公开(公告)日：2013-05-21
申请号：US13015938
申请日：2011-01-28
Applicant: Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
Inventor： Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
CPC classification number: G08G5/045 , G01S13/9303
Abstract: According to the invention, the device (1) comprises means (4) for adapting the altitude capture maneuver, means (5) for first detecting the emission of a first type alarm, means (6) for determining a first alarm threshold and means (7) for establishing an activation height threshold from said first alarm threshold and airplane vertical speed at the time of the alarm emission, so that, when the height separating said aircraft (AC) from the altitude set level is strictly higher than said height threshold at the time of the alarm emission, said adaptation means (4) are disabled.
Abstract translation: 根据本发明，装置（1）包括用于适应高度捕获机动的装置（4），用于首先检测第一类型报警的发射的装置（5），用于确定第一报警阈值的装置（6） 7），用于在所述报警发射时从所述第一报警阈值和飞机垂直速度建立激活高度阈值，使得当所述飞行器（AC）与所述高度设定水平分离的高度严格高于所述高度阈值时 报警发射的时间，所述适配装置（4）被禁用。
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19.发明授权Method and device for determining and updating a target altitude for an emergency descent of an aircraft 有权用于确定和更新飞机紧急下降的目标高度的方法和装置公开(公告)号：US08224505B2
公开(公告)日：2012-07-17
申请号：US13184040
申请日：2011-07-15
Applicant: Paule Botargues , Erwin Grandperret , Lucas Burel
Inventor： Paule Botargues , Erwin Grandperret , Lucas Burel
IPC: G05D1/00
CPC classification number: G05D1/0055 , G05D1/0607
Abstract: A method and device are provided for determining a target altitude for an emergency descent of an aircraft that is to be reached by the end of the emergency descent. The method includes determining an initial target altitude representative of the initial position of the aircraft and then repeatedly determining a current target altitude along a reference horizontal distance. The current target altitude is compared to the initial target altitude and is used to update the emergency descent if the current target altitude is lower than the initial target altitude. Each target altitude is selected as the larger of a predetermined threshold altitude and a security altitude that ensures any obstructions along a remaining horizontal distance are avoided.
Abstract translation: 提供一种方法和装置，用于确定在紧急下降结束时到达的飞机的紧急下降的目标高度。 该方法包括确定代表飞行器初始位置的初始目标高度，然后沿参考水平距离重复确定当前目标高度。 将当前目标高度与初始目标高度进行比较，如果当前目标高度低于初始目标高度，则用于更新紧急下降。 每个目标高度被选择为预定阈值高度的较大者，并且避免了沿着剩余水平距离的任何障碍物的安全高度。
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公开(公告)号：US08200421B2
公开(公告)日：2012-06-12
申请号：US12582240
申请日：2009-10-20
Applicant: Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jerome Bailly , Isabelle Lacaze , Sylvain Thezelais , Jerome Goyet
Inventor： Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jerome Bailly , Isabelle Lacaze , Sylvain Thezelais , Jerome Goyet
CPC classification number: G08G5/04 , G01C5/005 , G05D1/0646
Abstract: An altitude profile representative of the terrain overflown by an aircraft is established. Thereafter, an altitude limit curve which comprises an intersection with the altitude profile upon the engagement of a terrain avoidance maneuver is determined. As soon as there is no longer any intersection of the limit curve with the altitude profile, the terrain avoidance maneuver is interrupted.
Abstract translation: 建立代表航空器溢出的地形的高度剖面。 此后，确定在地形回避机动的接合时包括与高度分布的交点的高度极限曲线。 一旦极限曲线与高度剖面不再有任何交点，地形回避机动就会中断。
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