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1. 发明授权

US08731744B2 Method and device for aiding the control of guiding modes transitions of an aircraft 有权
标题翻译：用于帮助控制飞机的引导模式转换的方法和装置
公开(公告)号：US08731744B2
公开(公告)日：2014-05-20
申请号：US13182479
申请日：2011-07-14
申请人： Pascale Louise , Alain Dupre , Anthony Atencia , Emmanuel Cortet , Xavier Dal Santo
发明人： Pascale Louise , Alain Dupre , Anthony Atencia , Emmanuel Cortet , Xavier Dal Santo
IPC分类号： G05D1/00
CPC分类号： G05D1/085
摘要： The guiding mode transition aiding device includes a target heading determining device and a mode transition triggering system. The target heading determining device is configured to determine a target heading which represents the heading value reached by the aircraft at the end of a procedure of folding the wings of the aircraft flat from a current operating state. The mode transition triggering system receives the target heading and compares the target heading to a desired heading to be reached by the airplane to assist with triggering a transition between a rolling angle holding mode, in which the aircraft flies with a constant rolling angle, to a heading holding mode, in which the aircraft flies with a constant heading. This device and associated methods may be used during in flight refueling operations.
摘要翻译：引导模式转移辅助装置包括目标航向确定装置和模式转换触发系统。目标航向确定设备被配置为确定在从当前操作状态折叠飞行器的机翼的过程结束时，确定代表飞机达到的航向值的目标航向。模式转换触发系统接收目标航向，并将目标航向与飞机要达到的期望航向进行比较，以协助触发飞机以恒定的滚动角度飞行的滚动角度保持模式之间的过渡到航向保持模式，飞机以恒定航向飞行。在飞行加油操作期间可以使用该装置和相关联的方法。

2. 发明授权

US08695921B2 Automatic method and device for aiding the piloting of an airplane 有权
标题翻译：用于辅助飞机驾驶的自动方法和装置
公开(公告)号：US08695921B2
公开(公告)日：2014-04-15
申请号：US13113632
申请日：2011-05-23
申请人： Thierry Bourret , Pascale Louise , Jean Muller , Xavier Dal Santo
发明人： Thierry Bourret , Pascale Louise , Jean Muller , Xavier Dal Santo
IPC分类号： B64C13/18 , G05D1/04
CPC分类号： G05D1/0077
摘要： A method of aiding the piloting of an airplane ensures the availability of an automatic pilot and a thrust regulation system on board the airplane. To this end, the method includes determining first information by measuring the actual airspeed of the airplane, and this first information is used to control the automatic pilot and the thrust regulation system in a primary mode during normal operations of the airplane. When the first information is lost by becoming unavailable or unreliable, the automatic pilot and the thrust regulation system are each controlled in a secondary mode by control parameters determined using additional flight data independent from the actual airspeed of the airplane and the first information. Consequently, an alternative or redundant control is supplied for ensuring the continued operation of an automatic pilot without necessary intervention from crew members on board the airplane.
摘要翻译：协助飞机驾驶的方法确保飞机上的自动飞行员和推力调节系统的可用性。为此，该方法包括通过测量飞机的实际空速来确定第一信息，并且该第一信息用于在飞机的正常操作期间以主模式控制自动驾驶员和推力调节系统。当第一信息由于变得不可用或不可靠而丢失时，通过与独立于飞机的实际空速和第一信息的附加飞行数据确定的控制参数，自动驾驶和推力调节系统各自被控制在次级模式。因此，提供替代或冗余控制以确保自动飞行员的持续操作，而不需要飞机上的乘务员进行必要的干预。

3. 发明授权

US08477048B2 Method and device for preventing an anti-collision system on board an airplane from emitting alarms, during an altitude capture maneuver 有权
标题翻译：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：US08477048B2
公开(公告)日：2013-07-02
申请号：US13016154
申请日：2011-01-28
申请人： Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
发明人： Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
IPC分类号： G08G5/04 , G01C21/00 , G06F17/10 , G05D1/00 , G01S13/00 , G01S3/02
CPC分类号： G08G5/045 , G01S13/9303 , G08G5/04
摘要： 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.
摘要翻译：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。

4. 发明申请

US20120296498A1 METHOD FOR CONTROLLING THE DECELERATION ON THE GROUND OF A VEHICLE 有权
标题翻译：用于控制车辆地面下降的方法
公开(公告)号：US20120296498A1
公开(公告)日：2012-11-22
申请号：US13448719
申请日：2012-04-17
申请人： Malika ESSADOUNI , Xavier Dal Santo
发明人： Malika ESSADOUNI , Xavier Dal Santo
IPC分类号： B60T8/17
CPC分类号： B64C25/426 , B60T8/1703
摘要： The invention relates to a method for controlling the deceleration on the ground of a vehicle. The method obtains, from the crew of the vehicle or from an outside operator, parameters relating to its current position and its current speed. Then it determines a reference position and speed of the vehicle, the reference position being a theoretical position to be reached by the vehicle. Finally it determines, from indicated parameters and from reference parameters, a deceleration command with a view to ending up at a target position at a preselected speed.
摘要翻译：本发明涉及一种用于控制车辆地面上的减速度的方法。该方法从车辆人员或外部操作员获得与其当前位置及其当前速度有关的参数。然后，它确定车辆的参考位置和速度，参考位置是车辆要达到的理论位置。最后，从指定的参数和参考参数确定减速命令，以预定速度在目标位置结束。

5. 发明授权

US08295996B2 Method and device for preventing useless alarms generated by an anti-collision system on board an airplane 有权
标题翻译：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
申请人： Paule Botargues , Xavier Dal Santo , Pierre Fabre , Xavier Guery
发明人： Paule Botargues , Xavier Dal Santo , Pierre Fabre , Xavier Guery
IPC分类号： G05D1/00
CPC分类号： G08G5/045
摘要： 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).
摘要翻译：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）。

6. 发明申请

US20110187561A1 Method And Device For Preventing An Anti-Collision System On Board An Airplane From Emitting Alarms, During An Altitude Capture Maneuver 有权
标题翻译：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
申请人： Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
发明人： Paule Botargues , Xavier Dal Santo , Olivier Sapin , Vincent Bompart
IPC分类号： G08G5/04
CPC分类号： G08G5/045 , G01S13/9303 , G08G5/04
摘要： 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.
摘要翻译：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。

7. 发明申请

US20100174425A1 METHOD AND DEVICE TO ASSIST IN THE DRIVING OF A VEHICLE, IN PARTICULAR OF AN AIRCRAFT, FOR THE AVOIDANCE OF OBSTACLES 失效
标题翻译：帮助驾驶特别是飞机的车辆避免障碍物的方法和装置
公开(公告)号：US20100174425A1
公开(公告)日：2010-07-08
申请号：US12493950
申请日：2009-06-29
申请人： Xavier DAL SANTO
发明人： Xavier DAL SANTO
IPC分类号： G08G5/04 , G05D1/00 , G08G5/06
CPC分类号： G08G5/045
摘要： A method and a device to assist in the driving of a vehicle, in particular of an aircraft, for the avoidance of obstacles.The device (1) comprises onboard means (2, 3, 5, 8, 11) for determining and using an avoidance trajectory enabling the vehicle to avoid at least one obstacle while reaching a planned destination.
摘要翻译：一种辅助驾驶车辆，特别是飞机的方法和装置，以避免障碍物。装置（1）包括用于确定和使用避免轨迹的车载装置（2,3,5,8,11），使得车辆能够在到达计划的目的地时避免至少一个障碍物。

8. 发明申请

US20090050746A1 METHOD AND DEVICE FOR AUTOMATICALLY PROTECTING AN AIRCRAFT AGAINST A HARD LANDING 有权
标题翻译：用于自动保护飞机抵抗硬盘的方法和装置
公开(公告)号：US20090050746A1
公开(公告)日：2009-02-26
申请号：US12193467
申请日：2008-08-18
申请人： Xavier Dal Santo , Armand Jacob
发明人： Xavier Dal Santo , Armand Jacob
IPC分类号： G05D1/04
CPC分类号： G05D1/0676
摘要： Method and device for automatically protecting an aircraft against a hard landing.The device (1) comprises means (3) for calculating commands for protecting against a hard landing and means (5A, 5B, 5N) for applying these commands to control surfaces (6A, 6B, 6N) which act on the vertical speed of the aircraft.
摘要翻译：自动保护飞机抵御硬着陆的方法和装置。装置（1）包括用于计算用于防止硬着陆的命令的装置（3）和用于将这些命令施加到控制表面（6A，6B，6N）的装置（5A，5B，5N）飞机。

9. 发明授权

US08240615B2 Method and device for automatically protecting an aircraft against a hard landing 有权
标题翻译：自动保护飞机抵御硬着陆的方法和装置
公开(公告)号：US08240615B2
公开(公告)日：2012-08-14
申请号：US12193467
申请日：2008-08-18
申请人： Xavier Dal Santo , Armand Jacob
发明人： Xavier Dal Santo , Armand Jacob
IPC分类号： G05D1/00
CPC分类号： G05D1/0676
摘要： Disclosed is a method and device for automatically protecting an aircraft against a hard landing. A measuring unit measures current vertical speed and current relative height of the aircraft. A first command generating unit generates first commands to act on the vertical speed of the aircraft by determining an intermediate command from the measured vertical speed and height and converting the intermediate command into turn angles. A speed calculation unit applies the first commands to control surfaces. The first commands are generated from the measured current vertical speed and height, taking into account a predetermined reference vertical speed, such that the aircraft touches down on the ground at a vertical speed not greater than the predetermined reference vertical speed.
摘要翻译：公开了一种用于自动保护飞机抵抗硬着陆的方法和装置。测量单元测量飞机的当前垂直速度和当前的相对高度。第一命令生成单元通过从所测量的垂直速度和高度确定中间命令并将中间命令转换成转角来产生作用于飞行器的垂直速度的第一命令。速度计算单元将第一个命令应用于控制面。考虑到预定的参考垂直速度，使得飞机以不大于预定参考垂直速度的垂直速度在地面上接地，从测量的当前垂直速度和高度产生第一命令。

10. 发明申请

US20120016540A1 Method And Device For Aiding The Control Of Guiding Modes Transitions Of An Aircraft 有权
标题翻译：辅助控制飞行器导向模式的方法和装置
公开(公告)号：US20120016540A1
公开(公告)日：2012-01-19
申请号：US13182479
申请日：2011-07-14
申请人： Pascale Louise , Alain Dupre , Anthony Atencia , Emmanuel Cortet , Xavier Dal Santo
发明人： Pascale Louise , Alain Dupre , Anthony Atencia , Emmanuel Cortet , Xavier Dal Santo
IPC分类号： G05D1/00
CPC分类号： G05D1/085
摘要： The device includes means (15A, 15B) for determining and using a heading target which represents the heading value reached by the aircraft (AC) at the end of a procedure of folding the wings of the aircraft (AC) flat, initiated at the current instant, from a rolling angle holding mode.
摘要翻译：该装置包括用于确定和使用标题目标的装置（15A，15B），该标题目标表示在当前开始的飞行器（AC）平面的折叠过程结束时飞行器（AC）所达到的航向值瞬间，从滚动角度保持模式。

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