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1. 发明授权

US08355831B2 Method and device for assisting in the piloting of an aircraft during a landing 有权
标题翻译：在着陆期间协助飞机驾驶的方法和装置
公开(公告)号：US08355831B2
公开(公告)日：2013-01-15
申请号：US12693277
申请日：2010-01-25
申请人： Fabrice Villaume , Jérôme Journade , Robert Lignee
发明人： Fabrice Villaume , Jérôme Journade , Robert Lignee
IPC分类号： G06F19/00 , B64C25/42
CPC分类号： G05D1/0083
摘要： Method and device for assisting in the piloting of an aircraft during a landing.The device (1) contains means (10, 11) for calculating turnaround times depending on the use of thrust reversers upon landing, as well as means (11) to display these turnaround times.
摘要翻译：在着陆期间协助飞机驾驶的方法和装置。装置（1）包含用于根据着陆时的推力反向器的使用计算周转时间的装置（10,11）以及显示这些周转时间的装置（11）。

2. 发明授权

US08209072B2 Method and device to assist in the piloting of an aircraft in a landing phase 有权
标题翻译：协助在着陆阶段驾驶飞机的方法和装置
公开(公告)号：US08209072B2
公开(公告)日：2012-06-26
申请号：US12051803
申请日：2008-03-19
申请人： Fabrice Villaume , Armand Jacob , Robert Lignee
发明人： Fabrice Villaume , Armand Jacob , Robert Lignee
IPC分类号： G06G7/70
CPC分类号： G08G5/025 , G05D1/0083 , G08G5/0021
摘要： A method and device to assist in the piloting of an aircraft in a landing phase may apply a maximum braking of the aircraft if there is a risk of longitudinal departure from a runway.
摘要翻译：在着陆阶段辅助飞机驾驶的方法和装置，如果存在从跑道纵向离开的风险，可以对飞机进行最大制动。

3. 发明申请

US20100191394A1 METHOD AND DEVICE FOR ASSISTING IN THE PILOTING OF AN AIRCRAFT DURING A LANDING 有权
标题翻译：用于在登陆期间对飞机进行辅助的方法和装置
公开(公告)号：US20100191394A1
公开(公告)日：2010-07-29
申请号：US12693277
申请日：2010-01-25
申请人： Fabrice Villaume , Jerome Journade , Robert Lignee
发明人： Fabrice Villaume , Jerome Journade , Robert Lignee
IPC分类号： G06F19/00 , G05D1/00
CPC分类号： G05D1/0083
摘要： Method and device for assisting in the piloting of an aircraft during a landing.The device (1) contains means (10, 11) for calculating turnaround times depending on the use of thrust reversers upon landing, as well as means (11) to display these turnaround times.
摘要翻译：在着陆期间协助飞机驾驶的方法和装置。装置（1）包含用于根据着陆时的推力反向器的使用计算周转时间的装置（10,11）以及显示这些周转时间的装置（11）。

4. 发明授权

US08214090B2 Method and device for generating a yaw speed order for an aircraft during a taxiing 有权
标题翻译：用于在滑行期间产生飞行器的偏航速度顺序的方法和装置
公开(公告)号：US08214090B2
公开(公告)日：2012-07-03
申请号：US12330372
申请日：2008-12-08
申请人： Fabrice Villaume , Pierre Scacchi
发明人： Fabrice Villaume , Pierre Scacchi
IPC分类号： G05D1/00
CPC分类号： G08G5/065 , G05D1/0083
摘要： Disclosed is a method and device for generating a yaw rate command for an aircraft along a ground trajectory. The yaw rate command is generated by determining a current curvature, lateral deviation and angular deviation of the ground trajectory. A yaw rate calculator then calculates a yaw rate and generates the yaw rate command based on the determined current curvature, lateral deviation and angular deviation.
摘要翻译：公开了一种用于沿着地面轨迹产生飞行器的偏航率指令的方法和装置。通过确定地面轨迹的当前曲率，横向偏差和角度偏差来产生偏航率指令。横摆率计算器然后计算偏航率，并基于所确定的当前曲率，横向偏差和角度偏差来生成横摆率指令。

5. 发明授权

US07908043B2 Method and device for active control of the roll of an aircraft 有权
标题翻译：用于主动控制飞机卷的方法和装置
公开(公告)号：US07908043B2
公开(公告)日：2011-03-15
申请号：US11949233
申请日：2007-12-03
申请人： Fabrice Villaume , David Chabe , Stephane Delannoy
发明人： Fabrice Villaume , David Chabe , Stephane Delannoy
IPC分类号： G05D1/08
CPC分类号： G05D1/0083
摘要： A control device a determination device for determining a roll objective, and a calculation device for calculating, on the basis of the roll objective, a deflection order which is applied exclusively to ailerons of the aircraft.
摘要翻译：一种控制装置，用于确定滚动目标的确定装置，以及用于根据滚动目标计算专门用于飞行器副翼的偏转顺序的计算装置。

6. 发明申请

US20050006524A1 System for aiding control of the deceleration of an aircraft moving over the ground 有权
标题翻译：协助控制飞机在地面上减速的系统
公开(公告)号：US20050006524A1
公开(公告)日：2005-01-13
申请号：US10884988
申请日：2004-07-07
申请人： Fabrice Villaume , Mikael Maas
发明人： Fabrice Villaume , Mikael Maas
IPC分类号： G05D1/00 , B64C25/42
CPC分类号： G05D1/0083 , B60T8/1703 , G08G5/0021 , G08G5/0091 , G08G5/065
摘要： System for aiding control of the deceleration of an aircraft moving over the ground. The system (1) includes braking means (2) for braking the aircraft, a braking unit (3) controlling the braking means (2) on the basis of deceleration orders, a computing unit (5) for computing deceleration orders, which determines a plurality of distance/speed pairs relating to the movement of the aircraft over a landing runway, each of said pairs indicating the speed of movement at the associated distance defined relative to the runway threshold of the landing runway, and an interface element (7) that includes means (14) displaying on a screen (15) a representation (16) of the landing runway, showing the exits, and indications illustrating the distance/speed pairs, aiding an operator in choosing one of the exits, and means (17) enabling an operator to select the chosen exit.
摘要翻译：协助控制飞机在地面上减速的系统。系统（1）包括用于制动飞行器的制动装置（2），基于减速次数控制制动装置（2）的制动单元（3），用于计算减速次数的计算单元（5），其确定与飞机在着陆跑道上的运动相关的多个距离/速度对，每个所述对指示相对于着陆跑道的跑道阈值限定的相关距离的移动速度，以及界面元素（7），其包括在屏幕（15）上显示着陆跑道的表示（16）的装置（14），示出出口，以及示出距离/速度对的指示，帮助操作者选择出口之一，以及装置（17）使操作员能够选择所选出口。

7. 发明授权

US08275501B2 Method and device for aiding the piloting of an aircraft during a landing 有权
标题翻译：在着陆期间协助飞机驾驶的方法和装置
公开(公告)号：US08275501B2
公开(公告)日：2012-09-25
申请号：US12560260
申请日：2009-09-15
申请人： Fabrice Villaume
发明人： Fabrice Villaume
IPC分类号： G06F19/00
CPC分类号： B64D45/04 , G08G5/0021 , G08G5/0091 , G08G5/025
摘要： Disclosed is a method and device for aiding the piloting on an aircraft during a landing phase. One of the landing runways of an airport onto which the aircraft is to land is determined by a runway determination device. A position determining unit is used to determine a current position of the aircraft in a reference frame. A minimum breaking distance is estimated by an estimation unit, upon the aircraft passing above tje determined landing runway. The minimum braking distance is compared by a distance comparison unit with a length of the determined landing runway, and an alert is emitted by an alert unit, when said minimum braking distance is greater than the length of said determined landing runway.
摘要翻译：公开了一种在着陆阶段帮助飞机上的驾驶的方法和装置。飞机要着陆的机场的着陆跑道之一由跑道确定装置确定。位置确定单元用于确定飞行器在参考系中的当前位置。在飞机经过确定的着陆跑道之后，由估计单元估计最小断裂距离。最小制动距离通过距离比较单元与确定的着陆跑道的长度进行比较，并且当所述最小制动距离大于所述确定的着陆跑道的长度时，警报单元发出警报。

8. 发明授权

US08229604B2 Method and system for automatically managing a convoy of aircraft during a taxiing 有权
标题翻译：在滑行期间自动管理飞机车队的方法和系统
公开(公告)号：US08229604B2
公开(公告)日：2012-07-24
申请号：US12475197
申请日：2009-05-29
申请人： Fabrice Villaume , Pierre Scacchi
发明人： Fabrice Villaume , Pierre Scacchi
IPC分类号： G05D1/00
CPC分类号： G08G5/0043 , G08G1/22
摘要： Disclosed is a method and system for managing a convoy of aircraft during taxiing. Taxi management is carried out by exchanging, by a first data transmission unit, information between the aircraft of the convoy concerning aircraft flight parameters of the aircraft within the convoy, and exchanging, between the aircraft of the convoy and at least one control station that manages the convoy collectively, information relating to the collective convoy. The exchange can be carried out by a second data transmission unit, with the ground control station receiving from each aircraft in the convoy information relating to convoy status, centralizing the received information, scheduling the convoy, and transmitting to each aircraft a convoy status table that indicates overall status of the convoy.
摘要翻译：公开了一种在滑行期间管理飞机车队的方法和系统。出租车管理是通过第一数据传输单元交换车队飞机之间关于车队内的飞机的飞行器飞行参数之间的信息，以及在车队的飞机与至少一个管理的控制站之间进行交换的信息车队集体，与集体车队有关的信息。交换可以由第二数据传输单元进行，地面控制站从车队接收到车队中与车队状态有关的信息，集中接收的信息，调度车队，并向每个飞机发送一个车队状态表，表示车队总体状况。

9. 发明授权

US07853369B2 Active pitch control method and device for an aircraft 有权
标题翻译：主动桨距控制方法和飞机装置
公开(公告)号：US07853369B2
公开(公告)日：2010-12-14
申请号：US11937935
申请日：2007-11-09
申请人： Fabrice Villaume
发明人： Fabrice Villaume
IPC分类号： G05D1/08
CPC分类号： G05D1/0623
摘要： A device has a pitch acceleration instruction calculator that calculates a pitch acceleration instruction depending on a pitch objective and a deflection instruction calculator that calculates, from the pitch acceleration instruction, a deflection instruction for elevators of an aircraft.
摘要翻译：一种装置具有俯仰加速指令计算器，其根据俯仰目标计算俯仰加速度指令，以及偏航指令计算器，其从俯仰加速指令计算飞行器电梯的偏转指令。

10. 发明授权

US08280562B2 Method and device concerning the taxiing of an aircraft, which is automatic at least in part 有权
标题翻译：关于飞机滑行的方法和装置，至少部分是自动的
公开(公告)号：US08280562B2
公开(公告)日：2012-10-02
申请号：US12330361
申请日：2008-12-08
申请人： Fabrice Villaume , Pierre Scacchi
发明人： Fabrice Villaume , Pierre Scacchi
IPC分类号： G01C23/00
CPC分类号： G08G5/065 , G05D1/0083
摘要： A method and device automatically controls the driving of an aircraft along a ground path of an airport domain. A guidance system is configured to determine, with the aid of at least one current value of the aircraft and a ground rolling trajectory, a yaw rate setpoint enabling the aircraft to follow the ground rolling trajectory by application of a yaw rate command. The guidance system, with the aid of measured current values of parameters of the aircraft, the determined ground rolling trajectory and a speed profile that incorporates a variation of the longitudinal speed along the ground trajectory, a longitudinal speed setpoint that represents a longitudinal speed command to drive the aircraft along the ground trajectory, while complying with the speed profile. A piloting aid system calculates setpoints from the yaw rate command and applies the setpoints to control yaw motion of the aircraft.
摘要翻译：一种方法和装置自动地控制沿着机场域的地面路径的飞行器的驾驶。引导系统被配置为借助于飞机的至少一个当前值和地面滚动轨迹来确定使飞机能够通过应用偏航率命令跟随地面滚动轨迹的横摆角速度设定点。引导系统借助于飞行器参数的测量电流值，确定的地面滚动轨迹和包含沿着地面轨迹的纵向速度变化的速度曲线，纵向速度设定点，其表示纵向速度命令沿着地面轨迹驱动飞机，同时遵守速度曲线。驾驶辅助系统从偏航速度指令计算设定值，并施加设定值以控制飞行器的偏航运动。

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