CN114694419A - A method and system for error analysis of air traffic control command - Google Patents

A method and system for error analysis of air traffic control command Download PDF

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CN114694419A
CN114694419A CN202011604038.1A CN202011604038A CN114694419A CN 114694419 A CN114694419 A CN 114694419A CN 202011604038 A CN202011604038 A CN 202011604038A CN 114694419 A CN114694419 A CN 114694419A
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aircraft
track information
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李珂
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Hangzhou Jianguoke Technology Development Co ltd
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    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft
    • G08G5/30Flight plan management

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Abstract

The invention provides an empty management command error analysis method and system. The method comprises the steps of introducing control intention command track information into air traffic management, providing an interactive interface for a controller to input intention command track information into each aircraft before the controller actually commands, and analyzing whether the aircraft conflicts with other aircrafts/restricted operation areas in an area or not according to various traffic operation environment information by the system. Therefore, effective and accurate air traffic conflict advanced analysis and judgment are realized.

Description

一种空管指挥错误分析方法及系统A method and system for error analysis of air traffic control command

技术领域technical field

本发明属于空中交通运行领域,具体涉及一种空中交通活动分析及提示方法及系统。The invention belongs to the field of air traffic operation, and in particular relates to a method and system for analyzing and prompting air traffic activities.

背景技术Background technique

在空中交通指挥中,通过空中交通管制人员人工分析判断实时空域动态,以及空域内各个航空器的运行动态,由此发布相关的指挥调配指令,以引导航空器按特定飞行路径飞向目的地。并在飞行过程中避免与其他航空器发生飞行冲突、避免航空器与其他航空器相撞等内容。In air traffic command, air traffic controllers manually analyze and judge real-time airspace dynamics, as well as the operational dynamics of various aircraft in the airspace, and then issue relevant command and deployment instructions to guide aircraft to fly to their destination according to a specific flight path. And avoid flying conflict with other aircraft during flight, avoid aircraft colliding with other aircraft, etc.

该方法存在以下一些问题:There are some problems with this method:

在人工分析判断时存在缺乏分析处理工作量大,可靠性低、缺乏足够有效的提前预判方式方法的问题。In manual analysis and judgment, there are problems such as lack of analysis and processing workload, low reliability, and lack of sufficient and effective advance prediction methods.

人工限于能力、精力等因素、有其不可避免的局限性,因能力所限,可同时指挥处置的量较少,且单长时间工作,受精力、关注力等因素的限制,失误率将有较大的偏差。且因为缺乏足够有效的分析处理方法,在人工分析判断过程中,无法有效地提前分析判断,使得工作分析量进一步地聚集在实时交通分析管理之中,进一步引起处理工作量大、可靠性低问题。Labor is limited by factors such as ability and energy, and has its unavoidable limitations. Due to the limitation of ability, the amount that can be commanded and disposed of at the same time is relatively small, and a single long-term work is limited by factors such as energy and attention, and the error rate will be higher. larger deviation. And because of the lack of sufficient and effective analysis and processing methods, in the process of manual analysis and judgment, it is impossible to effectively analyze and judge in advance, so that the workload of work analysis is further gathered in the real-time traffic analysis and management, which further causes the problem of large processing workload and low reliability. .

现有的自动化系统通过多种方式以希望辅助人员指挥,但是也存在一些不足Existing automated systems hope to assist human command in various ways, but there are also some shortcomings

未有合适系统采集获悉管制员所拟定的航航空器指挥预案,无法足够有效地根据管制员所拟定的航空器管制方案以充分辅助其进行冲突分析,错误识别。There is no appropriate system to collect and learn the aircraft command plan drawn up by the controller, and it cannot be effectively based on the aircraft control plan drawn up by the controller to fully assist him in conflict analysis and misidentification.

现有自动化动化系统往往是针对于单个预计出现飞行冲突发布实时调配策略,并未给与全面实时的提示在实时指挥过程中分析各个目标实时运行情况,并在即将有冲突时给与提示,才给人以提示。而在管制指挥时,如有能在管制员拟定意图信息时,即可判断管制意图是否正确,可带来更多的运行便利。Existing automation systems often issue real-time deployment strategies for a single expected flight conflict, but do not give comprehensive real-time prompts. During the real-time command process, the real-time operation of each target is analyzed, and prompts are given when conflicts are imminent. Just give a hint. When controlling and commanding, if the controller draws up the intention information, it can be judged whether the control intention is correct, which can bring more operational convenience.

基于上述不足,如果有一方法和系统提前采集管制员预计对各航空器指挥航迹信息、可在制定预案时提前获悉各类运行冲突、提前获悉运行错误,以提前查找更正,避免运行冲突情况出现。Based on the above deficiencies, if there is a method and system that collects the information of the controller's expected command track for each aircraft in advance, it is possible to learn about various operational conflicts and operating errors in advance when formulating plans, so as to find and correct them in advance and avoid the occurrence of operational conflicts.

发明内容SUMMARY OF THE INVENTION

发明核心Invention core

本发明提出一种方法及系统。其将管制“意图指挥航迹信息”引入到空中交通管理中,在管制员实际指挥之前,通过提供一交互界面供管制员对各个航空器输入“意图指挥航迹信息”,此后系统根据各类交通运行环境信息(空域实时结构情况、各其他空器运行动态、气象情况,分析航空器按照意图指挥信息是否与区域内其他航空器/限制运行区域/气象等)有冲突。由此实现有效准确的空中交通冲突提前分析及判断。The present invention provides a method and system. It introduces control "intended command track information" into air traffic management. Before the controller actually commands, an interactive interface is provided for the controller to input "intended command track information" for each aircraft. Operational environment information (real-time structure of airspace, operational dynamics of other aircraft, meteorological conditions, analysis of whether the aircraft command information according to intent conflicts with other aircraft in the area/restricted operation area/weather, etc.). Therefore, effective and accurate air traffic conflict analysis and judgment in advance can be realized.

要解决的问题problem to be solved

本发明要解决的问题是:“管制人员在无法有效提前进行分析判断、指挥时分析处理量较多、引起容易出现指挥错误”、“现有自动化系统无法充分贴合管制员意图以提前有效分析交通冲突”The problems to be solved by the present invention are: "the controller cannot effectively analyze and judge in advance, and the analysis and processing volume is large when commanding, which leads to easy command errors", "the existing automation system cannot fully conform to the controller's intention to effectively analyze in advance. traffic conflict"

解决问题的技术手段technical solutions to problems

为解决上述问题,本系统提出一方法和系统。其核心是将管制“意图指挥航迹信息”引入到空中交通管理中,在管制员实际指挥之前,通过提供一交互界面供管制员对各个航空器输入“意图指挥航迹信息”,此后系统根据各类交通运行环境信息(空域实时结构情况、各其他空器运行动态、气象情况,分析航空器按照意图指挥信息是否与区域内其他航空器/限制运行区域/气象等)有冲突。由此实现有效准确的空中交通冲突提前分析及判断。To solve the above problems, the present system proposes a method and system. Its core is to introduce control "intended command track information" into air traffic management. Before the controller actually commands, an interactive interface is provided for the controller to input "intended command track information" for each aircraft. Traffic-like operating environment information (real-time structure of airspace, operational dynamics of other aircraft, meteorological conditions, analysis of whether the aircraft command information according to intent conflicts with other aircraft in the area/restricted operation area/weather, etc.). Therefore, effective and accurate air traffic conflict analysis and judgment in advance can be realized.

带来的有益效果beneficial effect

通过本发明所述方法和系统,可以有效减少管制员在实际指挥时的分析处理工作量,大幅减轻交通指挥复杂度、减少指挥错误时间发生。同时,也可以实现通过计算机设备更好地辅助人工进行指挥,减少人工负荷、大幅提高运行安全。The method and system of the present invention can effectively reduce the analysis and processing workload of the controller during actual command, greatly reduce the complexity of traffic command, and reduce the occurrence of command errors. At the same time, it is also possible to better assist manual command through computer equipment, reduce manual load and greatly improve operational safety.

具体技术方案specific technical solutions

具体来说,本发明所述方法为包含以下几个步骤组成的方法Specifically, the method described in the present invention is a method comprising the following steps

S1采集用户输入的意图航迹信息S1 collects the intended track information input by the user

提供界面窗口供采集用户输入的意图航迹信息,所述用户航迹信息,所述航迹信息为水平上的2维飞行路径信息、或者包括2维水平飞行路径信息以及3维在空间上的信息。An interface window is provided for collecting the intended track information input by the user, the user track information, and the track information is the 2-dimensional flight path information on the level, or includes the 2-dimensional horizontal flight path information and the 3-dimensional flight path information on the space. information.

S2采集交通运行环境中各航班运行信息、空中交通运行各类环境信息S2 collects various flight operation information and various environmental information of air traffic operation in the traffic operation environment

采集交通运行环境中的各个航班运行信息,所述航班运行信息可包括,航空器计划/预计/受指令/实际飞行路线信息、航空器目标飞行位置点、航空器性能等信息。Collect flight operation information in the traffic operation environment, and the flight operation information may include information such as aircraft planned/predicted/commanded/actual flight route information, aircraft target flight position, and aircraft performance.

采集空中交通运行各类环境信息,其可包括动态变化的运行环境中因地形/空域设置等限制所确定的可飞行空间、动态的根据恶劣天气所确定的可飞行空间、动态的因军事互动限制所确定的可飞行空间、空中各空间风向风速等内容Collect various environmental information of air traffic operation, which can include the flightable space determined by the terrain/airspace settings and other restrictions in the dynamically changing operating environment, the dynamic flightable space determined by severe weather, and the dynamic limit due to military interaction. The determined flyable space, wind direction and speed of each space in the air, etc.

S3分析处理用户输入的意图航迹信息,生成航空器在时空上的参考航迹信息或运行范围信息S3 analyzes and processes the intended track information input by the user, and generates the reference track information or operating range information of the aircraft in space and time

根据用户输入的意图航迹信息,通过计算机系统生成该航空器按照该意图航迹信息飞行时,在时空上形成的位置点信息。其亦可以理解为各个时间点在空间上的位置。According to the intended track information input by the user, the computer system generates position point information formed in space and time when the aircraft flies according to the intended track information. It can also be understood as the position of each time point in space.

所述空间上的范围可理解为所述意图航迹信息在划设时,未完全确定某些要素、比如高度、速度等内容,故得出的预测飞行航迹在某时间点时在一个范围内的任意一点。The spatial range can be understood as the fact that certain elements, such as altitude, speed, etc., are not completely determined when the intended track information is set, so the predicted flight track obtained is within a range at a certain time point. any point within.

S4分析航空器根据用户输入意图航迹信息执行时,是否会出现运行错误S4 analyzes whether there will be operating errors when the aircraft executes according to the user's input intent track information

分析判断航空器根据用户输入意图航迹进行执行时,该航空器在各个时间点上的位置是否与其他航空器所对应位置有“间隔可能小于特定值得情况"、以及各个时间点上,航空器是否可能会进入因空域地形、可用情况、军事活动等因素造成的不可进入空域。上述分析是否会有错误的具体分析方法见于具体实施方式部分Analyze and determine whether the position of the aircraft at each time point has a "separation that may be smaller than a certain value" from the position of the aircraft at each time point when the aircraft executes the trajectory according to the user's input intention, and whether the aircraft may enter the Inaccessible airspace due to airspace topography, availability, military activity, etc. The specific analysis method of whether there will be errors in the above analysis can be found in the specific implementation section

进一步地,在所述步骤S1,用户输入的航迹信息可为一个大致的飞行航迹信息,比如对于飞行具体的水平路径,用户仅需划设一个大致的几何航迹如直线、曲线、在特定点转弯的示意路径,此后由系统根据航空器需求划设出一个与航空器实际飞行能力相贴合的水平路径。Further, in the step S1, the track information input by the user can be a rough flight track information, for example, for a specific horizontal path of the flight, the user only needs to draw a rough geometric track such as a straight line, a curve, a The indicated path for turning at a specific point, after which the system draws a horizontal path that fits the actual flight capability of the aircraft according to the needs of the aircraft.

进一步地,所述步骤S1中,用户输入的航迹信息可为一个包含部分航迹要素的意图航迹信息,比如相较于完整的包含水平、垂直高度的完整航迹信息,用户可划设一个水平信息,以及一部分航段上的垂直路径信息,此后系统根据计算机分析计算其在空间上的运行范围Further, in the step S1, the track information input by the user may be an intended track information including some track elements. A horizontal information, and vertical path information on a part of the flight segment, after which the system calculates its operating range in space based on computer analysis

进一步地,在用户输入部分非完整意图航迹时,S3可变为:S3分析处理用户处理的意图航迹信息,生成航空器在时空上的运行范围信息。Further, when the user inputs part of the incomplete intended track, S3 can be changed to: S3 analyzes and processes the intended track information processed by the user, and generates the operating range information of the aircraft in space and time.

根据用户输入的意图航迹信息,通过计算机系统生成该航空器按照该意图航迹信息飞行时,在时空上形成的位置范围信息。其亦可以理解为各个时间点在空间上的位置范围。所述空间上的范围可理解为所述意图航迹信息在划设时,未完全确定某些要素、比如高度、速度等内容,故得出的预测飞行航迹在某时间点时在一个范围内的任意一点。According to the intended track information input by the user, the computer system generates the position range information formed in time and space when the aircraft flies according to the intended track information. It can also be understood as the location range of each time point in space. The spatial range can be understood as the fact that certain elements, such as altitude, speed, etc., are not completely determined when the intended track information is set, so the predicted flight track obtained is within a range at a certain time point. any point within.

具体来说,本发明的系统内容如下Specifically, the system content of the present invention is as follows

所述系统有以下几个部分组成The system consists of the following parts

意图航迹采集单元Intent track acquisition unit

该单元提供用户界面,或者输入窗口等内容,供用户输入意图航迹。This unit provides a user interface, or an input window, etc., for the user to enter the intended track.

交通运行环境各类信息采集单元Various information collection units for traffic operation environment

该单元包含各类采集设备或采集接口,采集交通运行环境中各类信息。This unit includes various collection devices or collection interfaces to collect various information in the traffic operation environment.

分析处理单元。Analysis processing unit.

该单元包含处理分析装置。按照本发明所述方法中的分析处理用户处理的意图航迹信息、以及“分析航空器根据用户输入意图航迹信息执行时,是否会出现运行错误”,并得出相关结果The unit contains processing analysis means. According to the analysis and processing of the intended track information processed by the user in the method of the present invention, and "analyze whether an operation error occurs when the aircraft is executed according to the intended track information input by the user", and obtain relevant results

所述系统通过以下步骤实现所述功能The system implements the function through the following steps

Sx1意图航迹采集单元用户采集用户输入的意图航迹信息Sx1 Intended Track Collection Unit The user collects the intended track information input by the user

Sx2交通运行环境各类信息采集单元采集交通运行环境各类信息Various information collection units of Sx2 traffic operation environment collect various information of traffic operation environment

Sx3分析处理单元分析处理用户输入的意图航迹信息The Sx3 analysis processing unit analyzes and processes the intended track information input by the user

Sx4分析处理单元分析分析“航空器根据用户输入意图航迹信息执行时,是否会出现运行错误” 。The Sx4 analysis and processing unit analyzes and analyzes "whether an operation error will occur when the aircraft executes according to the user's input intent track information".

具体实施方式Detailed ways

以下举几个本发明所述方案的一些示例实施范例对本发明实施例中的技术方案进一步清楚、完整地描述,显然,所描述的实施例是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention are further described clearly and completely by taking some exemplary embodiments of the solutions described in the present invention below. Obviously, the described embodiments are part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

实施例1Example 1

本实施例提出了本发明方法的一种实施示例。其包含以下几个步骤This embodiment presents an implementation example of the method of the present invention. It includes the following steps

S1采集用户输入的意图航迹信息S1 collects the intended track information input by the user

S2采集交通运行环境中各航班运行信息、空中交通运行各类环境信息S2 collects various flight operation information and various environmental information of air traffic operation in the traffic operation environment

S3分析处理用户输入的意图航迹信息,生成航空器在时空上的参考航迹信息或运行范围信息S3 analyzes and processes the intended track information input by the user, and generates the reference track information or operating range information of the aircraft in space and time

S4分析航空器根据用户输入意图航迹信息执行时,是否会出现运行错误S4 analyzes whether there will be operating errors when the aircraft executes according to the user's input intent track information

在S1中,用户在通过一个设计好的计算机图形输入界面,在界面上显示空域中各个航空器界面,用户在某个航空器在实际进入指挥空域之前,对提前根据自身初步对空中交通环境的判断,对该航空器划设出一个后续意图让其飞行的飞行路线的水平面上的几何路径,并在该界面中输入在垂直飞行剖面上航空器在各个位置所需飞行的高度层路径。In S1, the user displays each aircraft interface in the airspace through a designed computer graphic input interface. Before an aircraft actually enters the command airspace, the user makes a preliminary judgment on the air traffic environment in advance according to his own. Delineate a geometric path on the horizontal plane of the subsequent flight route intended for the aircraft to fly, and input the altitude path that the aircraft needs to fly at each position on the vertical flight profile in this interface.

在S2中,系统根据各采集装置、采集接口、采集交通运行环境中各航班运行信息、空中交通运行各类环境信息。可以具体采集的内容参见于发明内容部分对应的S2步骤。In S2, the system collects various flight operation information and air traffic operation environmental information in the traffic operation environment according to each acquisition device and acquisition interface. For details that can be collected, see step S2 corresponding to the content of the invention.

在S3中,计算机系统根据采集到的用户航迹信息,生成航空器在时空上的参考航迹信息。在本实施例中,其可以以以下步骤进行。In S3, the computer system generates the reference track information of the aircraft in space and time according to the collected user track information. In this embodiment, it can be performed in the following steps.

a.生成水平上的水平面二维航迹信息,根据航空器划设的水平航迹信息,得出该航空器后续飞行路径在水平面上的几何路径。a. Generate the two-dimensional track information on the horizontal plane, and obtain the geometric path of the subsequent flight path of the aircraft on the horizontal plane according to the horizontal track information drawn by the aircraft.

b.根据用户划设的在垂直飞行剖面上航空器预计所需飞行的高度层路径,结合步骤a中划设出的水平航迹路径,两者相结合,得出用户意图该航空器在空间上的飞行路径信息。b. According to the level path that the aircraft is expected to fly on the vertical flight profile drawn by the user, combined with the horizontal track path drawn in step a, the two are combined to obtain the user's intention for the aircraft in space. flight path information.

c.结合航空器性能、空域中各空间的风向风速气压信息,推算得出航空器沿着路径点在各个时间点的飞行空间的位置信息信息。c. Combined with the performance of the aircraft and the wind direction, wind speed and pressure information of each space in the airspace, calculate the position information of the flight space of the aircraft at each time point along the waypoint.

在S4中,分为两个方面进行分析判断,第一方面:分析判断该航空器沿着用户输入的意图航迹,是否与其他航空器有冲突。第二方面:分析判断该航空器沿着飞行是否会进入非可用空域情况。具体来说,可以按照以下方式进行判断In S4, the analysis and judgment are divided into two aspects. The first aspect is to analyze and determine whether the aircraft is in conflict with other aircraft along the intended track input by the user. The second aspect: analyze and determine whether the aircraft will enter the unusable airspace along the flight. Specifically, it can be judged as follows

对于判断航空器是否有冲突的情况,根据采集到的其他航空器各类飞行路径信息、根据各个飞行路径信息的准确程度、优先级,对其进行整合形成一条包含一定容差范围的其他航空器在各个时间点在空间上的位置范围信息。此后根据S3中获得的航空器在时空上的参考航迹信息。分析各个时刻该航空器的位置与其他航空器对应运行范围是否存在可能接近的情况,由此分析得出航空器是否有与其他航空器冲突的可能性。In the case of judging whether the aircraft has a conflict, according to the collected flight path information of other aircraft, according to the accuracy and priority of each flight path information, it is integrated to form a certain tolerance range for other aircraft at each time. The location range information of the point in space. After that, according to the reference track information of the aircraft in space and time obtained in S3. Analyze whether the position of the aircraft may be close to the corresponding operating range of other aircraft at each moment, so as to obtain the possibility of conflict between the aircraft and other aircraft.

对于航空器是否进入非可用空域的情况,根据S3中推测的航空器在各个时间点上的位置信息,结合For the situation of whether the aircraft enters the unusable airspace, according to the position information of the aircraft at various time points estimated in S3, combined with

对于在S3中分析出的航空器在其飞行各个时间在空间上的位置、结合S2采集到的动态变化的因各因素所确定的可用飞行空间,判断航空器在各个时间点上是否有与或者进入非可用空间的可能。For the spatial position of the aircraft at each time of its flight analyzed in S3, and the available flight space determined by various factors combined with the dynamic changes collected in S2, it is determined whether the aircraft has and or entered a non-stop at each time point. free space possible.

实施例2Example 2

本实施例提出一个在实施例基础上一个实施示例,其特征为在所述步骤S1,用户输入的意图航迹信息可为一个大致的飞行航迹信息,比如对于飞行具体的水平路径,用户仅需划设一个大致的几何航迹如直线、曲线、在特定点转弯的示意路径,此后在系统分析处理中,系统根据航空器需求划设出一个与航空器实际飞行能力相贴合的水平路径。This embodiment proposes an implementation example based on the embodiment, which is characterized in that in the step S1, the intended track information input by the user may be a general flight track information. For example, for a specific horizontal flight path, the user only It is necessary to draw a rough geometric track, such as a straight line, a curve, and a schematic path of turning at a specific point. After that, in the system analysis and processing, the system draws a horizontal path that fits the actual flight capability of the aircraft according to the needs of the aircraft.

具体来说,其可为以下一些方式:Specifically, it can be in the following ways:

对于S1中初步划设的几何航迹,在后续系统分析中,系统结合该航空器转弯、上升、下降等的性能特性,在一个容差范围内调整用户输入的意图航迹信息,使得所得出的意图航迹信息在贴合航空器飞行需求的同时,也管制员输入的航迹内容.For the geometric track initially set in S1, in the subsequent system analysis, the system adjusts the intended track information input by the user within a tolerance range based on the performance characteristics of the aircraft's turning, ascent, descent, etc., so that the obtained The intended track information not only fits the flight requirements of the aircraft, but also the track content input by the controller.

实施例3:Example 3:

本实施示例提出一个基于实施例1的一个实施例,其特征为,包含实施例1的特征,且用户输入的航迹信息可以为部分航迹信息,比如相较于“完整的即包含水平航迹路径、亦包含垂直航迹路径的航迹信息”,用户可以输入一个“仅包含水平航迹路径的意图航迹”,“且设定后续航空器高度将低于某制定高度(如3600)”的意图航迹信息。此后系统可根据规则,设定生成航空器在时空上的运行范围信息,该运行范围即为,在各个时间点,航空器以推测水平位置点作为该航空器水平上位置点,高度在0-3600米范围的一个运行范围。并在此后的分析计算中,以该范围来测算航空器是否存在与其他航空器有冲突或与是否进入非可进入空域。This embodiment provides an embodiment based on Embodiment 1, which is characterized in that it includes the features of Embodiment 1, and the track information input by the user may be partial track information, The user can enter an "intended track that contains only the horizontal track path", "and set the subsequent aircraft altitude to be lower than a certain altitude (such as 3600)" the intended track information. After that, the system can set and generate the operating range information of the aircraft in space and time according to the rules. The operating range is that at each time point, the aircraft takes the estimated horizontal position point as the horizontal position point of the aircraft, and the altitude is in the range of 0-3600 meters. an operating range. And in the subsequent analysis and calculation, use this range to measure whether the aircraft has conflicts with other aircraft or whether it enters the non-accessible airspace.

S3分析处理用户处理的意图航迹信息,生成航空器在时空上的运行范围信息。S3 analyzes and processes the intended track information processed by the user, and generates the operating range information of the aircraft in space and time.

根据用户输入的意图航迹信息,通过计算机系统生成该航空器按照该意图航迹信息飞行时,在时空上形成的位置范围信息。其亦可以理解为各个时间点在空间上的位置范围。所述空间上的范围可理解为所述意图航迹信息在划设时,未完全确定某些要素、比如高度、速度等内容,故得出的预测飞行航迹在某时间点时在一个范围内的任意一点。According to the intended track information input by the user, the computer system generates the position range information formed in time and space when the aircraft flies according to the intended track information. It can also be understood as the location range of each time point in space. The spatial range can be understood as the fact that some elements, such as altitude, speed, etc., are not completely determined when the intended track information is set, so the predicted flight track obtained is within a range at a certain time point. any point within.

对于本发明内容中所叙述的其他技术方案,可根据发明内容的叙述,或者结合上述实施例,可以较明显的推测得出,此处不再一一举例叙述。Other technical solutions described in the content of the present invention can be clearly inferred according to the description of the content of the present invention or in combination with the above-mentioned embodiments, and will not be described one by one here.

Claims (4)

1.一种空管指挥错误分析方法,其包含以下几个步骤S1 采集用户输入的意图航迹信息、S2 采集交通运行环。中各航班运行信息、空中交通运行各类环境信息S3 分析处理用户输入的意图航迹信息,生成航空器在时空上的参考航迹信息或运行范围信息S4 分析航空器根据用户输入意图航迹信息执行时,是否会出现运行错误。1. An air traffic control command error analysis method, which comprises the following steps: S1 collecting the intended track information input by the user, and S2 collecting the traffic operation loop. S3 Analyze and process the intended track information input by the user, and generate the reference track information or operating range information of the aircraft in space and time S4 Analyze when the aircraft executes according to the intended track information input by the user , whether an operation error occurs. 2.一种基于权利要求1的方法,其特征在于,在所述步骤S1,用户输入的航迹信息可为一个大致的飞行航迹信息。2 . A method based on claim 1 , wherein, in the step S1 , the track information input by the user can be a general flight track information. 3 . 3.一种基于权利要求1的方法,其特征在于,所述步骤S1 中,用户输入的航迹信息可为一个包含部分航迹要素的意图航迹信息。3 . A method based on claim 1 , wherein, in the step S1 , the track information input by the user can be an intended track information including some track elements. 4 . 4.一种空管指挥错误分析系统,其包含意图航迹采集单元、交通运行环境各类信息采集单元、分析处理单元。其中,分析处理单元 “分析航空器根据用户输入意图航迹信息执行时,是否会出现运行错误。4. An air traffic control command error analysis system, comprising an intended track acquisition unit, various information acquisition units of traffic operation environment, and an analysis and processing unit. Among them, the analysis and processing unit "analyzes whether there will be operating errors when the aircraft executes according to the user's input intent track information.
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Publication number Priority date Publication date Assignee Title
CN117709696A (en) * 2024-02-06 2024-03-15 中国民用航空飞行学院 Method and system for automatically generating program control plans based on expert system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117709696A (en) * 2024-02-06 2024-03-15 中国民用航空飞行学院 Method and system for automatically generating program control plans based on expert system
CN117709696B (en) * 2024-02-06 2024-07-02 中国民用航空飞行学院 Method and system for automatically generating program control plans based on expert system

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