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1.发明授权Method and device for monitoring the ability to navigate of an aircraft during a phase of flight close to the ground 有权用于监视在靠近地面的飞行阶段飞机导航能力的方法和装置公开(公告)号：US08275495B2
公开(公告)日：2012-09-25
申请号：US12575304
申请日：2009-10-07
申请人： Fabien Joyeux , Adrien Ott , Melanie Morel , Romain Merat , Stephane Dattler , Francois Barre , Armelle Seillier
发明人： Fabien Joyeux , Adrien Ott , Melanie Morel , Romain Merat , Stephane Dattler , Francois Barre , Armelle Seillier
IPC分类号： G01C5/00
CPC分类号： G05D1/0646 , G05D1/0676 , G08G5/0021 , G08G5/0086
摘要： Disclosed is a method and device, which provide an enhanced ability to monitor the navigation of an aircraft during a phase of flight in which the aircraft is close to the ground in which the aircraft uses positional information supplied by a satellite positioning system for the navigation. A display screen is used to display a first characteristic sign representing a selected setpoint value for a height parameter of the aircraft. The display screen also displays a second characteristic sign representing a current auxiliary value expressed in the form of an achievable height parameter. An alert is emitted when the second characteristic sign is determined to be within a predetermined height value of the first characteristic sign, and the alert is shown in visual format on the display screen. An alarm is also emitted following a predetermined time after the alert is emitted, if the setpoint value is not replaced by a new setpoint value.
摘要翻译： 公开了一种方法和装置，其提供了在飞行器靠近地面的飞行阶段期间监视飞行器的导航的增强的能力，其中飞行器使用由卫星定位系统提供的用于导航的位置信息。 显示屏用于显示表示飞机高度参数的选定设定值的第一特征符号。 显示屏幕还显示表示以可实现的高度参数的形式表示的当前辅助值的第二特征符号。 当第二特征符号被确定在第一特征符号的预定高度值内时，发出警报，并且在显示屏幕上以视觉格式示出警报。 在发出警报之后的预定时间后，如果设定点值未被新的设定值更换，则也发出报警。
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公开(公告)号：US20070279254A1
公开(公告)日：2007-12-06
申请号：US11651624
申请日：2007-01-10
申请人： Vincent Markiton , Francois Barre
发明人： Vincent Markiton , Francois Barre
IPC分类号： G08B7/00
CPC分类号： G05D1/0607 , G05D1/105 , G08G5/0052 , G08G5/0086
摘要： The device (1) comprises means (3) for determining a descent axis making it possible to fly from a safe altitude to a decision height, said descent axis being secured relative to the ground being flown over, and a guidance system (5) to assist in the guiding of the aircraft along said descent axis in a descent phase.
摘要翻译： 装置（1）包括用于确定下降轴的装置（3），使得可以从安全高度飞行到决定高度，所述下降轴相对于被飞过的地面固定，以及引导系统（5）至 在下降阶段帮助沿着所述下降轴的飞机引导。
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3.发明申请Method to automatically monitor a person using a cellular telephone, server and cellular telephone implementing this method 审中-公开使用实现此方法的蜂窝电话，服务器和蜂窝电话自动监视人的方法公开(公告)号：US20050037729A1
公开(公告)日：2005-02-17
申请号：US10641409
申请日：2003-08-14
CPC分类号： H04W4/029
摘要： The invention relates to a method for monitoring a person carrying a cellular telephone through a communication network wherein: An expected path for the monitored person is determined by identifying a sequence of successive places or checkpoints, and A real path followed by the monitored person is detected and compared with the expected path, both in space and in sequence, so that An alert is sent to at least one individual, called alertee, through the communication network when the real path differs from the expected path in place, sequence or in both place and sequence. The invention also relates to a cellular telephone and a server implementing such method.
摘要翻译： 本发明涉及一种通过通信网络监视携带蜂窝电话的人的方法，其中：通过识别连续的地点或检查点的序列来确定被监视人的预期路径，并且检测被监视人的跟踪真实路径 并且与空间和序列中的预期路径进行比较，使得当实际路径与预期路径不同时，通过通信网络将警报发送到至少一个被称为alertee的个人，或者在两者中 和序列。 本发明还涉及蜂窝电话和实现这种方法的服务器。
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4.发明申请Method and Device For Assisting the Flying of an Aircraft During an Autonomous Approach 有权在自主方法下协助飞机飞行的方法和装置公开(公告)号：US20080269966A1
公开(公告)日：2008-10-30
申请号：US12095229
申请日：2007-01-10
IPC分类号： G05D1/10
CPC分类号： G01C23/00 , G05D1/0676 , G08G5/025
摘要： The invention relates to a method and a device for assisting the flying of an aircraft, said method and device being used to determine an approach path and comprising a guidance system for helping to guide the aircraft along this approach path. The inventive method and device define a main approach path (AI) and a corrected approach path that has an extra vertical margin (ΔH) related to the ground over which the craft is flying as compared with a main approach path representing a category 1 precision approach. Said guiding system guides the aircraft following the corrected approach path.
摘要翻译： 本发明涉及一种用于辅助飞行器飞行的方法和装置，所述方法和装置用于确定进近路径，并且包括用于帮助沿着该进近路径引导飞行器的引导系统。 本发明的方法和装置定义了与代表1类精密方法的主进场路线相比，主飞行路线（AI）和修正的进场路径具有与飞行器所飞行的地面相关的额外的垂直边距（DeltaH） 。 所述引导系统引导飞机遵循校正的进近路径。
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公开(公告)号：US20050273222A1
公开(公告)日：2005-12-08
申请号：US11121053
申请日：2005-05-04
CPC分类号： G01C23/00
摘要： The flight control indicator (1) comprises a central unit (3) able to determine any change of trajectory corresponding to a vertical change which represents a change of vertical segment or a lateral change which represents a change of lateral branch, and means of display (5) which are able to present, on a viewing screen (7), a first means of indication indicating a next vertical change and a second means of indication indicating a next lateral change, and which are formed in such a way as to present at least one of said first and second means of indication, namely the one indicating the change of trajectory which is closest, from the current position of the aircraft.
摘要翻译： 飞行控制指示器（1）包括中央单元（3），其能够确定对应于垂直变化的任何轨迹变化，所述垂直变化表示垂直段的变化或表示横向分支变化的横向变化，以及显示装置 5），其能够在观察屏幕（7）上呈现指示下一个垂直变化的第一指示装置和指示下一个横向变化的第二指示装置，并且以这样的方式形成： 所述第一和第二指示装置中的至少一个，即指示与飞行器的当前位置最接近的轨迹的变化的指示。
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