| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | 一种基于计算机飞行计划CFP数据的飞机偏航判定方法、装置及存储介质 | CN202011211108.7 | 2020-11-03 | CN112396872A | 2021-02-23 | 赵昂; 马慧; 刘斌; 邱少鹏; 张运好; 刘鹏 |
| 本发明公开了一种基于计算机飞行计划CFP数据的飞机偏航判定方法、装置及存储介质，所述方法包括如下步骤：接收飞机的实时数据；从航班运行控制FOC系统中获取所述飞机所属航班的计算机飞行计划CFP；判断首个确定已经过的航路点；判断所处的航段；根据偏航距离判定是否偏航；以及数据缺失情况下的处理。在飞机发生偏航的时候，可根据基于CFP数据的飞机偏航判定方法得出告警，确保飞机安全飞行。 | ||||||
| 142 | 用于基于飞行计划特定的分布式账本的航空数据链路安全的系统和方法 | CN202280053621.9 | 2022-06-01 | CN117769812A | 2024-03-26 | T·L·凯西; M·R·加涅; B·W·布朗; C·D·科尔曼; A·汤姆森 |
| 本文提出了用于操作在航空通信网络上实现的基于飞行计划的分布式账本系统的系统和方法。根据一方面，与航空通信网络的通信元件之间发生的通信传输相关联的数据可以被记录在该分布式账本系统上。该分布式账本系统中涉及的通信元件可以使用所接收的飞行计划来被确定。飞行计划信息可以用于在该分布式账本系统中涉及的每个通信元件处初始化账本信息。如果飞行偏离原始飞行计划，则该分布式账本系统可以被更新以添加或删除通信元件。在该飞行计划被执行之后，该分布式账本系统可以将账本解激活以及将账本信息存储在集中式存储库中。 | ||||||
| 143 | 描绘测地参考基准面不符合区域、机场和飞行计划要素的系统和方法 | CN201711012643.8 | 2017-10-26 | CN108152834A | 2018-06-12 | P.K.麻尔维亚; P.亨查; V.索马舍卡; S.G.克; N.克; A.斯; S.潘钱加姆 |
| 描绘测地参考基准面不符合区域、机场和飞行计划要素的系统和方法。提供了用于在覆盖图上显示对于飞行器中的全球导航卫星系统（GNSS）导航系统而言不符合的路线的部分的系统和方法。路线符合模块基于GNSS导航系统来限定测地参考基准面标准。导航系统数据库具有对应于多个机场中的每一个的符合信息。飞行管理系统确定飞行器的路线，并且视觉显示器显示路线和覆盖图。路线符合模块基于符合信息来标识与测地参考基准面标准不符合的覆盖图的不符合区域，并且调整视觉显示器以区分在覆盖图的不符合区域内延伸的路线的不符合部分。 | ||||||
| 144 | FLIGHT PLANNING METHODS AND SYSTEMS | PCT/GB2011/050822 | 2011-04-26 | WO2011132002A2 | 2011-10-27 | PENDRY, Steven; HOOD, Timothy |
An electronic flight planning system is provided, arranged to implement a preferred method for identifying conflicts between flight plans for aircraft. In the preferred method, the system receives, as data input from one or more users, a plurality of flight plans each defining a flight by an aircraft; the system determines, for each aircraft and its respective received flight plan, a three- dimensional region of potential conflict, representative both of the uncertainty in the position of the aircraft and of a region of air exclusion appropriate for the aircraft or for the respective received flight plan; and the system determines, on the basis of the determined regions of potential conflict, whether one of the received flight plans is in conflict with any of the other received flight plans. |
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| 145 | DISPLAY OF NON-FLIGHT PLAN WAYPOINTS | PCT/US2001/030638 | 2001-10-01 | WO02031795A2 | 2002-04-18 | |
| The present invention provides systems and methods (100) for an integrated graphical user interface (114) which facilitates the display and editing of non-flight plan information (304). In accordance with various aspects of the present invention, a user located within an aircraft provides input to a processor through a cursor control device (104) and receives visual feedback via a dispaly produced by a monitor (114). The display (114) includes various graphical elements associated with the lateral position, vertical position, flight-plan (302) and/or other indicia of the aircraft's operational state as determined from avionics data and/or various sources. Through use of the cursor control device (104), the user may modify the flight-plan and/or other such indicia graphically in accordance with feedback provided by the display (114). The display (114) includes non-flight-plan data (304). In accordance with another aspect of the present invention, the non-flight plan data (304) comprises data such as Top Of Climb (TOC) (304a') Top Of Descent (TOD) (304b) and the like. | ||||||
| 146 | METHOD FOR DISPLAYING A FLIGHT PLAN | PCT/US2013/046493 | 2013-06-19 | WO2014018191A1 | 2014-01-30 | KOLBE, Dashiell, Matthews; SUGIMOTO, Philip, Dewing; CONRARDY, Peter, Jacob |
A method for displaying a flight plan having at least one waypoint on a flight display of a flight deck of an aircraft having known flight constraints, including receiving a user input for a user-inputted waypoint and generating an alternative waypoint when the user-inputted waypoint is not suitable and displaying same. |
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| 147 | DISPLAY OF NON-FLIGHT PLAN WAYPOINTS | PCT/US0130638 | 2001-10-01 | WO0231795A3 | 2002-06-20 | SNYDER MARK I |
| The present invention provides systems and methods (100) for an integrated graphical user interface (114) which facilitates the display and editing of non-flight plan information (304). In accordance with various aspects of the present invention, a user located within an aircraft provides input to a processor through a cursor control device (104) and receives visual feedback via a dispaly produced by a monitor (114). The display (114) includes various graphical elements associated with the lateral position, vertical position, flight-plan (302) and/or other indicia of the aircraft's operational state as determined from avionics data and/or various sources. Through use of the cursor control device (104), the user may modify the flight-plan and/or other such indicia graphically in accordance with feedback provided by the display (114). The display (114) includes non-flight-plan data (304). In accordance with another aspect of the present invention, the non-flight plan data (304) comprises data such as Top Of Climb (TOC) (304a') Top Of Descent (TOD) (304b) and the like. | ||||||
| 148 | DETERMINING A PREFERRED FLIGHT PLAN | PCT/AU2015/050771 | 2015-12-04 | WO2016086278A1 | 2016-06-09 | XU, Zhe; FITCH, Robert; MASON, Bertrand; SUKKARIEH, Salah; CARTER, Michael; POON, Leon; GAN, Seng Keat; LAWRANCE, Nicholas; VLASKINE, Vsevolod |
A method and system for determining a preferred flight path is disclosed. In one aspect, a processing system constructs a probabilistic roadmap search graph 360 including PRM nodes (362) and PRM edges (370). Each PRM node 362 includes a latitude/longitude pair (364) and an altitude (366). Each PRM edge (370) extends between two PRM nodes (362). Departure and destination nodes (380, 390) for take-off and landing weights (384, 394) are connected to the search graph (360) thereby generating costed climb and descent edges (386, 396) to reachable PRM nodes (362). The search graph (360) is searched by the processing system (100) to determine one or more of a cost minimised potential flight path between the locations (382, 392). A cost of traversed PRM edges (370) are calculated during the search. A potential flight path is selected using an objective function for outputting a preferred flight plan. |
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| 149 | 비행계획서를 통한 가상 비행궤적 모의 방법 | KR1020100091453 | 2010-09-17 | KR1020120029578A | 2012-03-27 | 은연주; 전대근; 염찬홍 |
| PURPOSE: A virtual flight trajectory simulation method is provided to closely simulate the movement of a flight by using a flight plane of an ICAO standard. CONSTITUTION: A flight plan is received through a flight plan of an ICAO(International Civil Aviation Organization) standard(S1). A location and high degree of a principal point are calculated through the flight plan(S2). A flight mode is classified according to the location and high degree of the principal point(S3). A trace plan is generated according to the flight mode(S4). The flight mode is classified into uniform velocity level flight, uniform acceleration level flight, and balance circling flight. | ||||||
| 150 | 정지궤도 인공위성 관제를 위한 비행역학 분석계획 장치 | KR1020080122337 | 2008-12-04 | KR101059043B1 | 2011-08-24 | 이병선; 황유라; 김해연; 김재훈 |
| 본 명세서는, 비행역학 분석계획 장치가 개시된다. 비행역학 분석계획 장치는 인공위성의 궤도 정보를 기반으로 상기 인공위성의 궤도를 결정 및 예측하는 궤도 처리부, 상기 궤도 정보를 기반으로 상기 인공위성에 관한 이벤트를 예측하는 이벤트 예측부 및 상기 인공위성의 위치를 유지 및 이동하는 위치 처리부를 포함한다. 궤도 결정, 궤도 예측, 이벤트 예측, 추력기 | ||||||
| 151 | 비행계획 상태 추적 장치 및 그 방법 | KR1020130140887 | 2013-11-19 | KR1020150057479A | 2015-05-28 | 최병철; 이성현; 이덕규; 김용균; 한종욱; 박효달 |
| 본발명은비행계획상태추적장치및 그방법에관한것으로, 입력되는비행계획정보를근거로비행계획상태천이구조를생성하는비행계획구조생성부; 항공고정통신망을통해전달되는비행전문을근거로비행계획상태를설정하는비행계획설정부; 및설정된비행계획상태를토대로하여상기비행계획상태천이구조에포함된비행계획상태를추적하는비행계획추적부;를포함한다. | ||||||
| 152 | SYSTEM AND METHOD FOR TEXTUALLY DISPLAYING AN ORIGINAL FLIGHT PLAN AND A MODIFIED FLIGHT PLAN SIMULTANEOUSLY | PCT/US2001/042458 | 2001-10-02 | WO02029363A2 | 2002-04-11 | |
| A navigational system includes a display device and logic that simultaneously presents a textual display of an original flight plan and a modified flight plan on the display device. The textual display includes a textlist of waypoints that are on the original flight plan and the modified flight plan and performance data for common waypoints that are on both the original flight plan and the modified flight plan, as well as for new waypoints that are added to the modified flight plan. The performance data for each common waypoint includes performance data for the waypoint on the original flight plan and for the waypoint on the modified flight plan. The system may further include an interface device that allows an operator to change the modified flight plan. The logic updates the textlist of waypoints on the textual display when the modified flight plan is changed and updates the performance data on the textual display for common waypoints when the modified flight plan is changed. The logic may also designate on the textual display waypoints to be removed, which correspond to waypoints that are on the original flight plan but not on the modified flight plan, and, when the modified flight plan is activated to become a new flight plan, the logic removes from the textual display the waypoints that are designated to be removed. | ||||||
| 153 | FLIGHT MANAGEMENT SYSTEM HAVING INTERACTIVE FLIGHT PLAN SELECTION ARRANGEMENT | PCT/US2008069880 | 2008-07-11 | WO2009035757A3 | 2009-05-14 | BLOCK GERALD J |
| A flight management system for aircraft includes a navigation database that stores data representative of flight plans and a user interface for receiving user inputs. The system also includes a processor adapted to receive and convert, in response to the user inputs received from the user interface, the data from the navigation database into a format representative of images of the flight plans. A display device is operatively coupled to the processor to render the images of the flight plans. The user interface includes a rotationally or linearly displaceable positioning element for causing the flight plan images to be displayed on the display device in a prescribed sequence that does not omit any intervening flight plans arising in the sequence. | ||||||
| 154 | LOGIC METHOD AND APPARATUS FOR TEXTUALLY DISPLAYING AN ORIGINAL FLIGHT PLAN AND A MODIFIED FLIGHT PLAN SIMULTANEOUSLY | PCT/US2001/030700 | 2001-10-02 | WO02031796A2 | 2002-04-18 | |
| A method of simultaneously presenting a textual display of an original flight plan and a modified flight plan includes displaying a texlist of waypoints, copying waypoints from the original flight plan into the modified flight plan, comparing each waypoint on the modified flight plan with waypoints on the original flight plan, determining, in a first determining step, for each modified flight plan waypoint, whether the modified flight plan waypoing originated from a waypoint in the original flight plan, and adding, in a first adding step, the modified flight plan waypoint to the textlist, when it is determined in the determining step that the modified flight plan waypoint did not originate from a waypoint in the original flight plan. The method may also include determining, in a second determining step, a position of the originating waypoint in the original flight plan relative to the position of the modified flight plan waypoint in the modified flight plan, when it is determine in the first determining step that the modified flight plan waypoint originated from a waypoint in the original flight plan; and adding, in a second adding step, the modified flight plan waypoing to the textlist, when it is determined in the second determining step that the position of the originating waypoint in the original flight plan corresponds to the position of the modified flight plan waypoint in the modified flight plan. | ||||||
| 155 | Method for in-flight adjusting of flight plan | JP2013029561 | 2013-02-19 | JP2013177120A | 2013-09-09 | BOLLAPRAGADA SRINIVAS; KLOOSTER JOEL KENNETH |
| PROBLEM TO BE SOLVED: To provide a method for in-flight adjusting of a flight plan of an aircraft to provide a low cost flight.SOLUTION: Based on at least present state data of an aircraft along a flight plan, performance data for the aircraft, and the flight plan data, a method 100 is based on a step 102 for predicting trajectory for completing the flight and a step 104 for computing cost of completing the flight plan, chooses the minimum cost trajectory from a set of the acceptable predicted trajectories, and operates the aircraft. | ||||||
| 156 | FLIGHT MANAGEMENT SYSTEM HAVING INTERACTIVE FLIGHT PLAN SELECTION ARRANGEMENT | PCT/US2008/069880 | 2008-07-11 | WO2009035757A2 | 2009-03-19 | BLOCK, Gerald, J. |
A flight management system for aircraft includes a navigation database that stores data representative of flight plans and a user interface for receiving user inputs. The system also includes a processor adapted to receive and convert, in response to the user inputs received from the user interface, the data from the navigation database into a format representative of images of the flight plans. A display device is operatively coupled to the processor to render the images of the flight plans. The user interface includes a rotationally or linearly displaceable positioning element for causing the flight plan images to be displayed on the display device in a prescribed sequence that does not omit any intervening flight plans arising in the sequence. |
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| 157 | 운항정보관리시스템의 주기장 운영 스케줄 관리 장치 및 그 방법 | KR1020100042568 | 2010-05-06 | KR101124829B1 | 2012-03-26 | 김태영; 황인웅; 김갑식; 이정훈; 유서연; 최웅식; 김호겸 |
| 본 발명은 운항정보관리시스템의 주기장 운영 스케줄 관리 장치 및 그 방법에 관한 것으로, 운용자로부터 입력된 각각의 주기장별 운영 정보로부터 각 주기장의 운영 스케줄을 설정하는 주기장 운영 스케줄 설정부, 각 주기장의 운영 스케줄의 설정 정보를 주기장 운영에 따른 스케줄 관리 정보가 저장되는 DB에 저장하고, 설정 정보에 따라 각 주기장의 운영 스케줄을 관리하는 주기장 운영 스케줄 관리부, 운용자로부터 주기장 변경 정보가 입력되면, 주기장의 운영 스케줄을 변경 처리하고, 주기장에 대한 변경 히스토리를 DB에 저장하는 스케줄 변경 처리부, 주기장 운영 스케줄러 구동 시 각 주기장의 운영 스케줄의 설정 정보를 주기장 운영 스케줄러에 연동시키고, 주기장 운영 스케줄러를 통해 각 주기장의 운영 스케줄을 모니터링하는 스케줄러 관� ��부, 및 운용자의 요청에 따라 DB에 저장된 각 주기장의 운영 스케줄의 설정 정보에 근거하여 주기장 운영 스케줄러의 화면을 구성하는 스케줄러 화면 구성부를 포함한다.
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| 158 | PROCÉDÉ DE GESTION D'UN PLAN DE VOL VERTICAL | PCT/EP2012/074107 | 2012-11-30 | WO2013079666A1 | 2013-06-06 | DEKER, Guy; ORZAN, Samuel; CAUDRON DE COQUERAUMONT, Bertrand; CHAIX, Philippe |
La présente invention concerne un procédé de gestion d'un plan de vol vertical comportant • une première étape de décomposition (21) d'un plan de vol initial en une succession de segments contigus (22), chaque segment comportant un changement d'altitude et/ou de vitesse; • une deuxième étape de calcul d'une trajectoire latérale (24) du plan de vol à partir des segments contigus; • une troisième étape de calcul d'un profil vertical et d'un profil de vitesse (28) à partir de la trajectoire latérale calculée; • une quatrième étape de détermination d'un segment actif (201) au cours du vol de l'aéronef, par un séquencement longitudinal en distance (200) des segments contigus. La présente invention est notamment adaptée à l'intégration de segments de vol tactiques dans un plan de vol. |
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| 159 | SYSTEM AND METHOD FOR FLIGHT PLAN DATA CAPTURE | PCT/US2006018817 | 2006-05-12 | WO2006124828A3 | 2007-01-11 | FLYNN LORRAINE; FLYNN MARY; STEINBERG JAMES |
| A system and method for providing to a user a candidate list of flight plans that specify one or more planned routes of flight from one location to another location, such routes satisfying certain criteria. These criteria include ranking the candidate list of flight plans according to the probability that the flight plan may be allowed or cleared by a controlling authority based on historic cleared flight plans; further qualifying this list by considering only candidate flight plans cleared during specified weather conditions; or specified time periods; or requested speed and/or altitude and/or aircraft type of flight parameters. Various embodiments include providing the candidate list of flight plans to the user by means of a communication system that is composed of a combination of a wide-area network, a wireless network or the internet. Additionally, an embodiment includes providing the flight plan data to a global positioning system (GPS) of a user. | ||||||
| 160 | PROCEDE ET DISPOSITIF D'AFFICHAGE POUR UN AERONEF QUI SUIT UN PLAN DE VOL | PCT/FR2006/001379 | 2006-06-19 | WO2006136687A2 | 2006-12-28 | ROUQUETTE, Patrice; LAVEANT, Nolween; HAVE, Didier; LE TELLIER, Arnaud |
Procédé et dispositif d'affichage pour un aéronef qui suit un plan de vol. Le dispositif comporte un moyen pour calculer la position effective de l'aéronef (A), un moyen pour déterminer au moins un écart maximal autorisé (E1) autour d'une position de consigne sur une trajectoire de vol (5) issue du plan de vol, en fonction de performances de précision et d'intégrité de calcul de ladite position effective et d'une contrainte de zone de vol autorisée dans un couloir de vol (6A, 6B), et un système d'affichage (7) pour présenter sur un écran de visualisation (8), au moins une échelle de distance (9), au moins un symbole fixe (10) qui indique ladite position effective, et deux indicateurs mobiles (13, 14) qui indiquent les limites (15A, 15B) dudit écart maximal autorisé (E1). |
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