专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

81. 发明公开

EP2199747A2 Methods for displaying aircraft procedure information 审中-公开
标题翻译： Verfahren zur Anzeige von Flugzeugprozedurinformationen
公开(公告)号：EP2199747A2
公开(公告)日：2010-06-23
申请号：EP09177956.1
申请日：2009-12-03
申请人： Honeywell International Inc.
发明人： Wilson, Blake W. , Engels, Jary , Wyatt, Ivan Sandy , Burgin, Roger W.
IPC分类号： G01C23/00
CPC分类号： G08G5/0047 , G01C23/005 , G08G5/0021 , G08G5/025
摘要： Methods are provided for presenting procedure information for an airport (306) on a display device (102) onboard an aircraft (114). A method comprises displaying a map (300) on a display device (102) and displaying a briefing panel (312) overlying a portion the map (300). The briefing panel (312) includes a plurality of segments (314, 316, 318, 320, 322), wherein each segment (314, 316, 318, 320, 322) is associated with a type of procedure information for the airport (306).
摘要翻译：提供了用于在飞机（114）上的显示设备（102）上呈现机场（306）的过程信息的方法。一种方法包括在显示设备（102）上显示地图（300）并显示覆盖地图（300）的一部分的简报面板（312）。简报面板（312）包括多个段（314,316,318,320,322），其中每个段（314,316,318,320,322）与机场的类型的程序信息（306 ）。

82. 发明公开

EP3404642A1 MINIMUM MANEUVERABLE ALTITUDE DETERMINATION AND DISPLAY SYSTEM AND METHOD 审中-公开
公开(公告)号：EP3404642A1
公开(公告)日：2018-11-21
申请号：EP18171721.6
申请日：2018-05-10
申请人： Honeywell International Inc.
发明人： SINGH, Jaibir , K, Sreenivasan Govindillam , SHAMASUNDAR, Raghu , SINGLA, Abneesh
IPC分类号： G08G5/00 , G05D1/06
CPC分类号： G01C23/005 , G05D1/0661 , G05D1/0676 , G08G5/0013 , G08G5/0047 , G08G5/0065 , G08G5/0086 , G08G5/0091
摘要： A system and method for determining and displaying a minimum maneuverable altitude for an aircraft to turn back includes automatically processing aircraft characteristic data, aircraft flight trajectory data, and environmental/airport services data, in a processing system, to determine a rate of change of aircraft maneuverable altitude with respect to change in aircraft heading. At least the determined rate of change of aircraft altitude with respect to change in aircraft heading is processed, in the processing system, to determine the minimum maneuverable altitude at least engine out conditions. Terrain data is processed, in the processing system, to determine a terrain clearance height above which the minimum maneuverable altitude may be implemented. The minimum maneuverable altitude is rendered, on a display device, on the altitude tape, and a pseudo gate is rendered on the display device that represents a height above the terrain that corresponds to the minimum maneuverable altitude.

83. 发明授权

EP3104125B1 AIRCRAFT NAVIGATION SYSTEM AND METHOD FOR AIRCRAFT NAVIGATION 有权
公开(公告)号：EP3104125B1
公开(公告)日：2018-10-31
申请号：EP15171787.3
申请日：2015-06-12
申请人： Airbus Defence and Space GmbH
发明人： Heinzinger, Olaf , Oberhauser, Matthias , Mamessier, Sébastien , Fernandes de Oliveira, Rafael , Dreyer, Daniel
IPC分类号： G01C23/00
CPC分类号： G01C23/005 , B64D43/00 , G08G5/0047
摘要： An aircraft navigation system and a method for aircraft navigation is presented. The aircraft navigation system comprising: a navigation-map data source (101), navigation-map data provided by the navigation-map data source (101) including information about a multitude of objects O on earth surface which are of high potential visibility and high potential identifiability from elevated positions, each information for an object O ˆˆ O including a position and a type of the respective object O; a first system (102) for measuring an actual aircraft position P(t); a waypoint data source (103) providing waypoints WP i defining an aircraft intended flight track; a second system (104) for selecting per waypoint WP i one object O i (WP i ) with O i (WP i ) ˆˆ O depending on given selection criteria; and a display (105) for displaying an information I(O i (WP i ) referring the selected object O i (WP i ).

84. 发明公开

EP3340208A1 GESTION DES MESSAGES AUX NAVIGANTS AERIENS 审中-公开
公开(公告)号：EP3340208A1
公开(公告)日：2018-06-27
申请号：EP17208682.9
申请日：2017-12-19
申请人： Thales
发明人： BONNET, Antoine-adrien , LERAT, Christophe
IPC分类号： G08G5/00 , G08G5/02
CPC分类号： G08G5/0039 , G06F17/2785 , G08G5/0013 , G08G5/0021 , G08G5/0047 , G08G5/0086 , G08G5/025 , G08G5/065
摘要： Il est décrit un procédé mis en oeuvre par ordinateur de gestion d'un message aux navigants aériens comprenant les étapes consistant à:- recevoir au moins un message aux navigants aériens;- recevoir un ou plusieurs éléments d'une base de données de navigation associée à un plan de vol d'un aéronef; - comparer le contenu du message aux navigants aériens reçu avec les éléments de la base de données de navigation associée à un plan de vol d'un aéronef. Différents développements décrivent notamment la détection d'éléments indisponibles à partir de l'analyse du contenus des messages, des traitements effectués sur la partie des messages exprimée en langage naturel, diverses modalités de notifications à destination du pilote, l'intervention d'opérateurs tiers dans la gestion des messages, l'enrichissement de données et différentes variantes d'implémentations en matière de système (système de gestion de vol FMS et/ou sac de vol électronique EFB).

85. 发明公开

EP3296831A1 METHODS AND SYSTEMS FOR AUTOMATION GUIDANCE 审中-公开
标题翻译：自动化指导的方法和系统
公开(公告)号：EP3296831A1
公开(公告)日：2018-03-21
申请号：EP17190981.5
申请日：2017-09-13
申请人： Honeywell International Inc.
发明人： WHITLOW, Stephen
IPC分类号： G05D1/00 , G08G5/00
CPC分类号： G08G5/0039 , G05D1/0088 , G08G5/0013 , G08G5/0021 , G08G5/0047
摘要： Methods and systems are provided for operating a vehicle that supports an automated action, such as an aircraft supporting autopilot, autothrottle, and various other autonomous operations and operating modes. One exemplary method of operating a vehicle involves obtaining one or more user inputs pertaining to an automated action to be performed by an onboard system, obtaining current vehicle status information, determining an operational objective for the automated action based at least in part on the current status information and the one or more user inputs, and providing guidance information pertaining to the automated action in a manner that is influenced by the operational objective and the current status information. For example, the guidance information may include indication of a remedial action to resolve a discrepancy between the operational objective and a projected aircraft behavior in the context of the operational objective or the current vehicle status.
摘要翻译：提供了用于操作支持自动操作的车辆的方法和系统，例如支持自动驾驶仪，自动油门和各种其他自主操作和操作模式的飞行器。操作车辆的一个示例性方法包括获得与将由车载系统执行的自动动作有关的一个或多个用户输入，获得当前车辆状态信息，至少部分地基于当前状态来确定自动动作的操作目标信息和一个或多个用户输入，并且以受操作目标和当前状态信息影响的方式提供与自动操作有关的指导信息。例如，指导信息可包括补救措施的指示，以解决操作目标与操作目标或当前车辆状态背景下的预测飞行器行为之间的差异。

86. 发明公开

EP3232157A1 AIRCRAFT NAVIGATION USING EXPONENTIAL MAP 审中-公开
标题翻译：使用指示图的飞机导航
公开(公告)号：EP3232157A1
公开(公告)日：2017-10-18
申请号：EP17166184.6
申请日：2017-04-12
申请人： GE Aviation Systems LLC
发明人： CABELLO, Juan Jose
IPC分类号： G01C21/20 , B25J9/02 , B25J9/16
CPC分类号： G08G5/0047 , G01C21/20 , G01S19/43 , G01S19/47 , G01S19/51 , G08G5/003
摘要： Systems and methods 200 for determining navigation information for an aircraft are provided. In one embodiment, a method 200 can include accessing 202 a satellite-based positioning signal received at a receiver on an aircraft. The satellite-based positioning signal can be indicative of a distance between a satellite and the receiver. The method can include identifying 204 from the satellite-based positioning signal a first vector associated with a distance between the satellite and the receiver and identifying 206 a second vector from the satellite-based positioning signal associated with a distance between a reference point and the satellite. The method can include generating 208 a kinematic model for determining a geometric position of the aircraft based at least in part on a robotic arm using the first vector and the second vector and determining 210 navigation information for the aircraft based at least in part on the kinematic model.
摘要翻译：提供了用于确定飞行器的导航信息的系统和方法200。在一个实施例中，方法200可以包括访问202在飞机上的接收器处接收的基于卫星的定位信号。基于卫星的定位信号可以指示卫星和接收器之间的距离。该方法可以包括从基于卫星的定位信号中识别204与卫星和接收器之间的距离相关联的第一矢量，并且从基于卫星的定位信号识别206第二矢量与参考点和卫星之间的距离。该方法可以包括：至少部分地基于使用第一矢量和第二矢量的机器人臂来生成（208）用于确定飞行器的几何位置的运动学模型;以及至少部分地基于运动学来确定用于飞机的210导航信息模型。

87. 发明公开

EP3133413A3 NAVIGATION SYSTEM FOR A SELF-GUIDED AERIAL VEHICLE UTILIZING MULTIPLE OPTICAL SENSORS 审中-公开
标题翻译：使用多个光学传感器的自导式空中飞行器导航系统
公开(公告)号：EP3133413A3
公开(公告)日：2017-07-12
申请号：EP16182339.8
申请日：2016-08-02
申请人： The Boeing Company
发明人： Wright, Steven A.
IPC分类号： G01S5/16 , G05D1/00 , F41G7/34 , F41G7/20 , G01S19/48 , G01S19/15 , G01S19/18
CPC分类号： G08G5/0047 , B64D47/08 , F41G7/20 , F41G7/343 , F41G7/346 , F41G7/36 , G01S5/16 , G01S19/15 , G01S19/18 , G01S19/39 , G01S19/48 , G05D1/00 , G05D1/107 , G06T7/70 , G06T7/74 , G06T2207/10032 , G06T2207/30184 , G06T2207/30244 , H04N5/247 , H04N5/33 , H04N7/183
摘要： Disclosed is a Global Positioning System ("GPS") independent navigation system ("GINS") (100) for a self-guided aerial vehicle ("SAV") (200, 500, 600, 700, 800). The SAV has a housing (202), where the housing has an outer surface (204), a length (206), a front end (208), and a longitudinal axis (210) along the length of the housing. The GINS includes a first optical sensor (102), a second optical sensor (104), a storage unit (106), and a comparator (110).
摘要翻译：公开了用于自动飞行器（“SAV”）（200,500,600,700,800）的全球定位系统（“GPS”）独立导航系统（“GINS”）（100）。 SAV具有壳体（202），其中壳体沿着壳体的长度具有外表面（204），长度（206），前端（208）和纵向轴线（210）。 GINS包括第一光学传感器（102），第二光学传感器（104），存储单元（106）和比较器（110）。

88. 发明授权

EP2944921B1 Method of calculating an analytical flight path 有权
标题翻译：弗雷泽伦
公开(公告)号：EP2944921B1
公开(公告)日：2017-05-10
申请号：EP14001710.4
申请日：2014-05-15
申请人： Airbus Defence and Space GmbH
发明人： Konle, Wolfgang
IPC分类号： G01C21/00 , G05D1/00 , G08G5/00
CPC分类号： G01C21/005 , G08G5/0047

89. 发明公开

EP3082121A1 AIRCRAFT SYSTEMS AND METHODS TO DISPLAY MOVING LANDING PLATFORMS 审中-公开
标题翻译： FLUGZEUGSYSTEME UND VERFAHREN ZUR ANZEIGE BEWEGTER LANDUNGSPLATTFORMEN
公开(公告)号：EP3082121A1
公开(公告)日：2016-10-19
申请号：EP16164133.7
申请日：2016-04-06
申请人： Honeywell International Inc.
发明人： SONGA, Anil Kumar , VENKATASWAMY, Sadguni , B M, Sudheer , ALIMI, Sandeep
IPC分类号： G08G5/00 , G08G5/02
CPC分类号： G08G5/025 , G08G5/0013 , G08G5/0021 , G08G5/0047
摘要： A display system for an aircraft includes a processing unit and a display device. The processing unit is configured to receive data representative of a landing platform on a movable carrier, and the data includes current energy parameters of the movable carrier. The processing unit is further configured to generate display commands associated with the landing platform and the energy parameters of the movable carrier. The display device is coupled the processing unit for receiving the display commands and operable to render first symbology representing the landing platform and second symbology representing the energy parameters of the movable carrier.
摘要翻译：一种用于飞行器的显示系统，包括处理单元和显示装置。处理单元被配置为在可移动载体上接收表示着陆平台的数据，并且数据包括可移动承载件的当前能量参数。处理单元还被配置为产生与着陆平台相关联的显示命令和可移动托架的能量参数。显示装置连接处理单元，用于接收显示命令并且可操作以呈现表示着陆平台的第一符号系统和表示可移动承载件的能量参数的第二符号系统。

90. 发明公开

EP2975595A3 SCALAR PRODUCT BASED SPACING CALCULATION 有权
标题翻译：基于标量产品的间隔计算
公开(公告)号：EP2975595A3
公开(公告)日：2016-06-29
申请号：EP15175772.1
申请日：2015-07-07
申请人： Honeywell International Inc.
发明人： KLANG, Pavel , CASEK, Petr , BRAZDILOVA, Silvie Luisa
IPC分类号： G08G5/00
CPC分类号： G08G5/0047 , G01C21/20 , G01C23/005 , G08G5/0008 , G08G5/0021 , G08G5/0026 , G08G5/0052 , G08G5/0073 , G08G5/0078 , G08G5/0082
摘要： A method is described that includes receiving, by a spacing system of an ownship aircraft, a current position of the ownship aircraft and a reference position of a target aircraft, wherein the reference position is a position of the target aircraft prior to a current position of the target aircraft. The method may also include, projecting, by the spacing system of the ownship aircraft, the reference position on a trajectory of the ownship aircraft, determining a first distance between the projected reference position and the current position, projecting, by the spacing system of the ownship aircraft, the current position on a trajectory of the reference position, determining a second distance between the projected current position and the reference position, and adjusting, by the spacing system and based on an average between the first distance and the second distance, a velocity of the ownship aircraft.
摘要翻译：描述了一种方法，该方法包括通过本籍飞机的间隔系统接收本籍飞机的当前位置和目标飞机的基准位置，其中基准位置是目标飞机在当前位置之前的位置目标飞机。该方法还可以包括由本籍飞机的间隔系统投影本籍飞机的轨迹上的基准位置，确定投影的基准位置与当前位置之间的第一距离，本机位置在参考位置的轨迹上，确定投影的当前位置和参考位置之间的第二距离，以及通过间隔系统并基于第一距离和第二距离之间的平均值来调整本机的速度。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式