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71. 发明授权

EP3094561B1 SHORT LANDING WARNING 有权
标题翻译：短暂着陆警告
公开(公告)号：EP3094561B1
公开(公告)日：2018-02-21
申请号：EP15709577.9
申请日：2015-02-23
申请人： The Boeing Company
发明人： HENDERSON, Mark H.
IPC分类号： B64D45/04 , G05D1/06 , B64D45/08 , G08G5/00 , G08G5/04
CPC分类号： B64D45/04 , B64D45/08 , G05D1/0607 , G05D1/0653 , G05D1/0676 , G08G5/0047 , G08G5/04 , G08G5/045
摘要： A method can include determining that an aircraft is on approach to a runway. The method can include determining a flight path vector (FPV) location of the aircraft based at least in part on a projected landing location with respect to the runway and determining a current airspeed of the aircraft. The method can also include performing at least one of the following: issuing a landing short alert to a pilot of the aircraft if the FPV location is at or before the runway threshold, issuing an airspeed caution alert if the FPV location is between the runway threshold and the target runway location and if the current airspeed is below a landing short envelope, and determining not to issue an alert if the FPV location is between the runway threshold and the target runway location and if the current airspeed is at or above the landing short envelope.

72. 发明公开

EP3136371A1 AIR VEHICLE NAVIGATION METHOD VIA A COMMON RUNTIME AIRCRAFT INTENT DATA STRUCTURE 审中-公开
标题翻译： LUFTFAHRZEUGNAVIGATIONSVERFAHRENÜBEREINE GEMEINSAME LAUFZEITABSICHTSDATENSTRUKTUR EINES FLUGZEUGS
公开(公告)号：EP3136371A1
公开(公告)日：2017-03-01
申请号：EP15382435.4
申请日：2015-08-31
申请人： The Boeing Company
发明人： NAVARRO FELIX, Francisco A. , QUEREJETA MASAVEU, Carlos , CUADRADO SANCHEZ, Jesús , VIVIANI, Gary
IPC分类号： G08G5/00
CPC分类号： G08G5/003 , G05B15/02 , G05D1/0088 , G05D1/101 , G08G5/0034 , G08G5/0039 , G08G5/0047
摘要： Air vehicle navigation method comprising the following steps: a) establishing initial conditions; b) establishing constraints; c) editing an aircraft trajectory, and; d) flying the air vehicle; wherein editing an aircraft trajectory comprises: i) determining a number of degrees of freedom; ii) establishing as many trajectory threads as degrees of freedom, wherein each thread comprises a series of instruction nodes comprising instructions; iii) determining, for each thread, the instructions satisfying the flight constraints; iv) determining the validity of each instruction in each thread; v) establishing a trigger node associated to each instruction node in each thread, wherein each trigger determines the end of validity of the instruction to which it is associated and the start of validity of the next instruction within the thread; vi) putting in order the instructions and triggers, so that when flying the air vehicle, the latter satisfies all flight constraints at every stage throughout the flight.
摘要翻译：航空器导航方法包括以下步骤：a）建立初始条件; b）建立约束; c）编辑飞机轨迹， d）飞行车辆; 其中编辑飞行器轨迹包括：i）确定自由度的数量; ii）建立与自由度一样多的轨迹线程，其中每个线程包括包括指令的一系列指令节点; iii）为每个线程确定满足飞行约束的指令; iv）确定每个线程中每条指令的有效性; v）建立与每个线程中的每个指令节点相关联的触发节点，其中每个触发器确定与其相关联的指令的有效结束以及该线程内下一条指令的有效性的开始; vi）按照指示和触发方式进行操作，以便在飞行时，后者满足整个飞行中每个阶段的所有飞行限制。

73. 发明公开

EP3045865A1 ROUTE POINT SETTING DEVICE AND ROUTE POINT SETTING PROGRAM 有权
标题翻译：路线点设置装置和路线点设置程序
公开(公告)号：EP3045865A1
公开(公告)日：2016-07-20
申请号：EP16150532.6
申请日：2016-01-08
申请人： Fuji Jukogyo Kabushiki Kaisha
发明人： MIZUTANI, Takuma , YANASE, Yasuhiko
IPC分类号： G01C21/20 , G08G5/00
CPC分类号： G08G5/0034 , G01C21/20 , G08G5/00 , G08G5/0047 , G08G5/0086
摘要： There is provided a route point setting device and route point setting program. A control unit (18) of an aircraft (10) divides map data (155), including at least a departure point (P S ) and an arrival point (P E ), into cells (C) in grid form on a horizontal plane, sets a cell route (Rcell) including consecutive cells between the departure point (P S ) and arrival point (P E ), calculates a bending angle bending angle (θ n ) of the cell route (Rcell) at each cell on the cell route (Rcell), and sets any cell (C) as a waypoint (P W ) in a case where the bending angle (θ n ) at any cell (C) satisfies the expression θ n - 1 ≥ θ n θ n + 1 wherein θ n-1 and θ n+1 respectively represent bending angles at cells C n-1 and C n+1 adjacent to the cell (C) behind and ahead of the cell (C) on the cell route (Rcell).
摘要翻译：提供路线点设定装置和路线点设定程序。飞机（10）的控制单元（18）将包括至少一个出发点（PS）和到达点（PE）的地图数据（155）划分成水平面上网格形式的单元格（C）包括在出发点（PS）和到达点（PE）之间的连续小区的小区路由（Rcell）计算小区路由（Rcell）上的每个小区的小区路由（Rcell）的弯曲角度弯曲角度（θn），并且在任何单元（C）处的弯曲角度（θn）满足其中分别为θn-1和θn+ 1的表达式θn-1≥θn<θn+ 1的情况下将任意单元格（C）设置为路途点表示在小区路由（Rcell）上的小区（C）之前和之后与小区（C）相邻的小区Cn-1和Cn + 1处的弯曲角。

74. 发明公开

EP2525337A3 Upgraded flight management system and method of providing the same 审中-公开
标题翻译：升级飞行管理系统及其方法，用于提供
公开(公告)号：EP2525337A3
公开(公告)日：2016-04-06
申请号：EP12161737.7
申请日：2012-03-28
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram , Knopf, Markus
IPC分类号： G08G5/00
CPC分类号： G08G5/003 , G01S19/13 , G05D1/0077 , G06F16/951 , G08G5/0021 , G08G5/0034 , G08G5/0047
摘要： A preexisting FMS system may be upgraded to increase its functionality while still taking advantage of certain components of the legacy system previously provided on the aircraft and replacing other preexisting components with different components for enhancing the functionality of the FMS system. The preexisting IRU, CADC, DME receiver and DFGC in the upgraded FMS system are in communication with the legacy AFMC but, instead of employing the legacy EFIS which existed in the prrexisting FMS system, the EFIS is replaced by a data concentrator unit as well as the display control panel and integrated flat panel display, and a GPS receiver. The upgraded FMS system is capable of such increased functionality as increased navigation database storage capacity, RNP, VNAV and RNAV capability utilizing a GPS based navigation solution, and RTA capability, while still enabling the legacy AFMC to exploit its aircraft performance capabilities throughout the flight.

75. 发明公开

EP2991057A3 SYSTEM AND METHOD FOR DISPLAYING TRAFFIC AND ASSOCIATED ALERTS ON A THREE-DIMENSIONAL AIRPORT MOVING MAP DISPLAY 审中-公开
标题翻译：系统和方法用于显示，交通相关的警告与机场移动的卡的三维显示
公开(公告)号：EP2991057A3
公开(公告)日：2016-03-16
申请号：EP15181644.4
申请日：2015-08-19
申请人： Honeywell International Inc.
发明人： KATHIRVEL, Kannan , SONGA, Anil Kumar , MOHIDEEN, Mohammed Ibrahim , NELSON, Bill
IPC分类号： G08G5/00 , G08G5/06
CPC分类号： G08G5/0043 , G08G5/0008 , G08G5/0021 , G08G5/0047 , G08G5/0078 , G08G5/065
摘要： A flight deck display system and method comprises a first source of host aircraft feature data and a second source of traffic data. A processor is coupled to the first and second sources and is configured to (a) receive host aircraft data; (2) receive traffic data; (3) filter traffic based on a predetermined set of separation criteria to identify vital traffic; (4) generate symbology graphically representative of vital traffic; (5) generate symbology graphically representative of the host aircraft; and (6)display the host aircraft and the vital traffic on an AMM display.

76. 发明公开

EP2993545A1 Follow-me system for unmanned aircraft vehicles 审中-公开
标题翻译： Nachfolgesystemfürein unbemanntes Flugzeug
公开(公告)号：EP2993545A1
公开(公告)日：2016-03-09
申请号：EP14290265.9
申请日：2014-09-05
申请人： Airbus Defence and Space GmbH
发明人： Bousquet, Joy , Vitte, Thomas
IPC分类号： G05D1/10 , G08G5/00
CPC分类号： G08G5/0047 , G05D1/104 , G08G5/0008 , G08G5/0052 , G08G5/0056
摘要： The present invention relates to a system for navigating an aircraft. The system comprises a first aircraft (10) with a first communication unit (12) and a second aircraft (20) with a second communication unit (22). The first aircraft (10) is adapted for determining coordinates of a position of a waypoint (40). The first communication unit (12) is adapted to transmit the coordinates of the position of the waypoint (40) to the second communication unit (22). The second aircraft (20) is adapted to navigate to the position of the waypoint (40). Several waypoints (40) can be provided in this manner such that a flight trajectory (41) is established along which the second aircraft (20) may follow the first aircraft (10). The invention also relates to a system for navigating an aircraft, wherein the second aircraft (20) adapted to follow the first aircraft (10) based on a received identification signal. With this system it is possible that the second aircraft (20) can follow the first aircraft (10) in case of a failure of systems of the second aircraft (20). The present invention also relates to a method for navigating an aircraft.
摘要翻译：本发明涉及一种用于航空飞行器的系统。该系统包括具有第一通信单元（12）的第一飞行器（10）和具有第二通信单元（22）的第二飞行器（20）。第一飞行器（10）适于确定航点（40）的位置的坐标。第一通信单元（12）适于将航点（40）的位置的坐标传送到第二通信单元（22）。第二飞机（20）适于导航到航点（40）的位置。可以以这种方式提供几个航路点（40），使得建立飞行轨迹（41），第二航空器（20）沿着飞行轨迹（41）跟随第一航空器（10）。本发明还涉及一种用于导航飞行器的系统，其中第二飞行器（20）适于基于接收的识别信号跟随第一飞行器（10）。利用该系统，在第二飞行器（20）的系统故障的情况下，第二飞行器（20）可能跟随第一飞行器（10）是可能的。本发明还涉及一种用于导航飞行器的方法。

77. 发明公开

EP2944921A1 Method of calculating an analytical flight path 有权
标题翻译：一种用于计算飞行路径的分析方法
公开(公告)号：EP2944921A1
公开(公告)日：2015-11-18
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
摘要： A method of calculating a smooth analytical flight trajectory from a series of position measurements on a real flight path comprises the steps of applying Kalman smoothing to the measurements to provide track vectors (18, 20), and fitting a special continuous polygon (22) first to the track vectors and in further iterative steps to the position measurements. The special continuous polygon allows the generation of a continuous and differentiable analytically-defined flight path. The invention allows a smoothed flight path to be calculated, the path having a lower noise level than that achievable using Kalman smoothing alone. The invention provides an improved flight path for certain safety-relevant calculations and other tasks which require a high level of reliability.

78. 发明公开

EP2808856A3 System and method for displaying a runway position indicator 有权
标题翻译：系统和方法，用于跑道位置指示器的显示
公开(公告)号：EP2808856A3
公开(公告)日：2015-01-28
申请号：EP14167602.3
申请日：2014-05-08
申请人： Honeywell International Inc.
发明人： Gannon, Aaron , Wyatt, Ivan Sandy , Nichols, Troy , Suddreth, John G.
IPC分类号： G08G5/00 , G08G5/02
CPC分类号： G08G5/025 , G08G5/0021 , G08G5/0047
摘要： A dynamic runway indicator (930) is displayed overlying a conformal runway (932) for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon (934), that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.

79. 发明公开

EP2775470A3 Ground based system and methods for providing multiple flightplan re-plan scenarios to a pilot during flight 审中-公开
标题翻译：基于地面的系统和方法，用于在飞行期间为导频提供多个路基飞行规划方案
公开(公告)号：EP2775470A3
公开(公告)日：2014-12-24
申请号：EP14157094.5
申请日：2014-02-27
申请人： Honeywell International Inc.
发明人： Harihar, Anand Agarwal , Brabham, David Allen , Redner, Trip , Payasam, SatyaBhaskar
IPC分类号： G08G5/00
CPC分类号： G08G5/0039 , G08G1/16 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/0047 , G08G5/006 , G08G5/0082 , G08G5/0091
摘要： Methods and apparatus are provided for transmitting re-routing options to a plurality of in-flight aircraft in accordance with preconfigured pilot preferences. The apparatus comprises a data store module containing data sets against which the pilot preferences are evaluated during flight, including weather, airspace and flight restrictions, ground delay programs, and air traffic information. The apparatus further includes a flight path module containing route and position information for each aircraft. An incursion alert processing module evaluates the flight path, data store, and pilot preferences and generates incursion alerts which are transmitted to each aircraft during flight. Upon receipt of an incursion alert or, alternatively, independent of an incursion alert, the pilot may request re-routing options. Once received and reviewed, the pilot selects the optimum re-routing option, and an associated micro flight plan is uplinked and loaded into the FMS (Flight Management System).
摘要翻译：提供了用于发射重路由选项，在飞行的飞机在雅舞蹈多个具有预配置的飞行员偏好的方法和设备。该装置包括数据存储模块包含数据集针对的飞行员偏好在飞行过程中评估，包括天气，空域和飞行限制，地面延期规划和空中交通信息。该装置包括：一个飞行路径包含用于每个飞机航线和位置信息进一步模块。侵入警报处理模块评价飞行路径，数据存储和飞行员偏好和基因利率侵入警报哪些是飞行过程中反式mitted每架飞机。一旦接收到侵入警报的，或者可选地，独立的侵入警报的，导频可以请求重新路由选项。一旦收到并审查，导频选择最优重新路由选项，并以相关联的微飞行计划上行和下载到FMS（飞行管理系统）。

80. 发明公开

EP2696171A2 Aircraft systems and methods for displaying weather information along a flight path 有权
标题翻译：飞机系统和沿飞行路线的天气信息显示方法
公开(公告)号：EP2696171A2
公开(公告)日：2014-02-12
申请号：EP13177898.7
申请日：2013-07-24
申请人： Honeywell International Inc.
发明人： Ramaiah, Vinoda , Krishna, Kiran Gopala
IPC分类号： G01C23/00 , G08G5/00 , G01W1/02
CPC分类号： G01W1/02 , G01C23/00 , G08G5/0013 , G08G5/0021 , G08G5/0047 , G08G5/0052 , G08G5/0091
摘要： A display system for an aircraft is provided. The system includes a processing unit configured to receive weather information associated with a flight path of a flight plan and to generate display commands based on the weather information. The flight plan includes a first waypoint associated with a first altitude. The system further includes a display device coupled with the processing unit and configured to receive the display commands and to display symbology representing the weather information. The weather information includes first weather information for the first altitude and second weather information at a second altitude, different from the first altitude.

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