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首页 / 专利库 / 飞行计划 / 专利数据
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 CN112396872B 2022-04-08 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 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。
143 一种雷达数据、飞行计划数据与ADS-B数据融合系统 CN201220099146.2 2012-03-16 CN202549080U 2012-11-21 杨晓嘉
本实用新型公开了一种雷达数据、飞行计划数据与ADS-B数据融合系统,其中,基础数据管理子系统分别与综合数据处理子系统、监视数据处理子系统、飞行数据处理子系统和数据显示终端子系统连接,所述监视数据处理子系统、飞行数据处理子系统和数据显示终端子系统分别与综合数据处理子系统连接,所述监视数据处理子系统还与数据显示终端子系统连接。本实用新型的有益效果是:能够将ADS-B数据与多部雷达数据融合处理;解决了ATC监视要求中航迹精度与航迹平滑连续的统一;实现融合定位优选惯性融合修正技术,提高多类型传感器相关融合精度;实现卫星系统、飞机以及地基系统协同监视。
144 Emergency flight plan US11785674 2007-04-19 US20080167763A1 2008-07-10 Simone Duranti; Erik Petrini
An emergency flight plan useable for an aircraft provided with a navigation system wherein the flight plan includes a pointer matrix including a number of cells. Each cell of the matrix has a unique identification and each cell corresponds to a geographical area, and wherein each cell of the matrix includes an identification of a cell corresponding to a next waypoint in an emergency route.
145 Emergency flight plan US11785674 2007-04-19 US07729817B2 2010-06-01 Simone Duranti; Erik Petrini
An emergency flight plan useable for an aircraft provided with a navigation system wherein the flight plan includes a pointer matrix including a number of cells. Each cell of the matrix has a unique identification and each cell corresponds to a geographical area, and wherein each cell of the matrix includes an identification of a cell corresponding to a next waypoint in an emergency route.
146 飛行計劃意圖警告系統及方法 TW088117871 2000-02-25 TW477962B 2002-03-01 胡伯特L.奈摩; 派翠克G.克隆; 派翠克K.柯拉茲
飛行計劃資訊以具有屬性之一系列導航點形式提供,該屬性較佳地包含其中之緯度、經度、高度限制以及導航點識別符。以此資訊定義之飛行路徑被模式化,且該飛行計劃模式和地形資訊核對以定位任何情況,其中存在潛在不安全飛行高度。在飛行中,飛行路徑模式被使用飛機位置更新,以致於由飛機位置至次一個導航點的飛行路徑在該模式中反應。假使潛在不安全飛行高度被偵測到時,可以發出警告給飛行人員。該飛行人員就可以修正飛行計劃或是採取其他合適的動作。
147 METHOD FOR INSERTING A SEGMENT OF FLIGHT PLAN IN A FLIGHT PLAN US14795199 2015-07-09 US20160012733A1 2016-01-14 Vincent GIRARDEAU; Marie ROMMEL; Manuel GUTIERREZ-CASTANEDA
The invention relates to a method for inserting a segment (Tins) of flight plan into an initial flight plan (Pini) of an aircraft, performed by a flight management system (FMS) of the said aircraft, the initial flight plan (Pini) comprising an ordered series of initial legs (Sini), the said fixed initial legs being indexed with an index i that varies from 1 to n, the method comprising the steps involving: identifying (110), using a first iterative calculation on the index i, in the segment to be inserted (Tins), the fixed legs to be inserted that have a position identical to the position of the leg of index i Sini(i)), the said legs thus determined being referred to as occurrences of the leg of index i, the said occurrences (O1, O2) being ordered by rank k varying from 1 to m, as a function of their position in the segment that is to be inserted (Tins), and searching, among the identified occurrences, for the occurrence of lowest index i and lowest rank k (Oi0(k0)) that has a type and attribute values identical to the segment of index i, referred to as equivalent point, when the said equivalent point exists, inserting the segment that is to be inserted (Tins) from the said equivalent point, otherwise, inserting the segment that is to be inserted (Tins) from the identified occurrence of lowest index i and lowest rank k (Oi1(k1)) referred to as a pseudo equivalent point, when the said pseudo equivalent point exists.
148 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.
149 Methods for in-flight adjusting of a flight plan EP13156562.4 2013-02-25 EP2631890A2 2013-08-28 Bollapragada, Srinivas; Klooster, Joel Kenneth

A method (100) of in-flight adjusting a flight plan of an aircraft to provide a low cost flight based on predicting a trajectory (102) for the completion of the flight based on at least the current state data of the aircraft along the flight plan, performance data for the aircraft, and the flight plan data, and computing the cost of completing the flight plan (104).

150 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.
151 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.

152 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.

153 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.

154 Methods for in-flight adjusting of a flight plan EP13156562.4 2013-02-25 EP2631890A3 2013-12-25 Bollapragada, Srinivas; Klooster, Joel Kenneth

A method (100) of in-flight adjusting a flight plan of an aircraft to provide a low cost flight based on predicting a trajectory (102) for the completion of the flight based on at least the current state data of the aircraft along the flight plan, performance data for the aircraft, and the flight plan data, and computing the cost of completing the flight plan (104).

155 METHOD OF ASSISTING IN THE NAVIGATION OF AN AIRCRAFT WITH AN UPDATING OF THE FLIGHT PLAN US11686339 2007-03-14 US20070219679A1 2007-09-20 Francois COULMEAU
The invention relates to a method of assisting in the navigation of an aircraft comprising a step for updating a flight plan according to a new clearance originating from an air traffic control authority and received on board by a ground/onboard communication system. The clearance comprises an action conditional on the flight plan linked to a floating point of the path defined by a time constraint of the aircraft; on receipt of the new clearance, the update is performed directly by means of the FMS linked to the communication system. This is a predictive method.
156 System and method for textually displaying an original flight plan and a modified flight plan simultaneously US09680280 2000-10-06 US06922631B1 2005-07-26 David B. Dwyer; Jan G. Hart
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.
157 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.
158 Flight Management System with Optimization of the Lateral Flight Plan US12634128 2009-12-09 US20100198433A1 2010-08-05 Stéphanie Fortier; Jérôme Sacle
Flight management system for aircraft comprising computation means capable of determining a gain or a loss in terms of flight time remaining to a point of arrival, and in terms of fuel consumption, following the input by an operator of a modification of an initial flight plan using the Direct To function. The computation means are capable of suggesting to the operator a modification of the lateral flight plan that procures an optimum gain. The flight management system also comprises a display interface capable of presenting to the operator the information concerning the gain or the loss in time and/or consumption, and of prompting the operator to accept or refuse the modification.
159 METHOD OF ASSISTING IN THE NAVIGATION OF AN AIRCRAFT WITH AN UPDATING OF THE FLIGHT PLAN US11686337 2007-03-14 US20070219678A1 2007-09-20 Francois Coulmeau
The invention relates to a method of assisting in the navigation of an aircraft comprising a step for updating a flight plan according to a new clearance received on board by a ground/onboard communication system. The clearance comprises an action conditional on the flight plan linked to a floating point of the path defined by an altitude constraint of the aircraft; on receipt of the new clearance, the update is performed directly by means of the FMS linked to the communication system. This is a predictive method.
160 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.