CN115148053A - Aircraft early warning method and device, terminal device and storage medium - Google Patents
Aircraft early warning method and device, terminal device and storage medium Download PDFInfo
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Abstract
本申请公开了一种飞行器预警方法、装置、终端设备以及存储介质，属于航空领域。所述飞行器预警方法包括：获取飞行器的航行信息；基于所述飞行器的航行信息进行预警判断，得到预警报告；将所述预警报告加载至预先获取的飞行器航线视景中进行预警。基于本申请方案，针对当下飞行员(或无人驾驶)的过程中缺乏有效预警手段的问题，提出了一种能够对飞行器的航行过程进行有效预警的方案，本方案通过对飞行器的各种信息进行预警判断，生成预警报告并在飞行器航线视景中加载显示，实现了飞行器航行中的及时预警，能够辅助飞行员及时处理航行中的各种情况，从而提高了飞行器航行过程的安全性，有效消除了安全隐患。
The present application discloses an aircraft early warning method, device, terminal device and storage medium, which belong to the field of aviation. The aircraft early warning method includes: acquiring navigation information of the aircraft; performing early warning judgment based on the navigation information of the aircraft to obtain an early warning report; and loading the early warning report into a pre-acquired aircraft route view for early warning. Based on the solution of the present application, aiming at the problem of the lack of effective early warning means in the process of the current pilot (or unmanned), a solution that can effectively warn the navigation process of the aircraft is proposed. Early-warning judgment, generating early-warning reports and loading and displaying them in the aircraft route view, realizing timely early warning during the flight of the aircraft, and assisting the pilot to deal with various situations during the flight in time, thereby improving the safety of the aircraft's navigation process and effectively eliminating the need for Security risks.
Description
技术领域technical field
本申请涉及航空领域，尤其涉及一种飞行器预警方法、装置、终端设备以及存储介质。The present application relates to the field of aviation, and in particular, to an aircraft early warning method, device, terminal device and storage medium.
背景技术Background technique
目前，在民航飞机的航行过程中，飞行员主要依靠仪表显控和空管系统的辅助来驾驶飞机。当航行过程中出现一些突发的状况(如飞机偏航、异常天气、空管临时调度、空域临时管制等)时，飞行员需要依靠自己的经验来判断飞行器的当前航行状况。由于缺乏可靠的预警系统，使得航行中的安全保障极大地依赖于飞行员的个人经验和个人素质，导致航行中出现了不可控的因素，产生了一定的安全隐患。At present, during the navigation of civil aircraft, pilots mainly rely on the assistance of instrument display and control and air traffic control system to fly the aircraft. When some emergencies occur during the flight (such as aircraft yaw, abnormal weather, temporary air traffic control, temporary airspace control, etc.), pilots need to rely on their own experience to judge the current flight status of the aircraft. Due to the lack of a reliable early warning system, the safety guarantee during the flight is greatly dependent on the personal experience and personal quality of the pilot, resulting in uncontrollable factors during the flight, resulting in certain safety hazards.
因此，有必要提出一种能够在飞行器航行中进行有效预警判断，从而帮助飞行员安全驾驶的技术方案。Therefore, it is necessary to propose a technical solution that can effectively make early warning and judgment during the flight of the aircraft, thereby helping pilots to drive safely.
发明内容SUMMARY OF THE INVENTION
本申请的主要目的在于提供一种飞行器预警方法、装置、终端设备以及存储介质，旨在解决由于由于缺乏可靠的预警系统所存在的安全隐患。The main purpose of the present application is to provide an aircraft early warning method, device, terminal device and storage medium, aiming to solve the potential safety hazards due to the lack of a reliable early warning system.
为实现上述目的，本申请提供一种飞行器预警方法，飞行器预警方法包括：In order to achieve the above purpose, the present application provides a method for early warning of an aircraft, and the method for early warning of an aircraft includes:
获取飞行器的航行信息；Obtain the navigation information of the aircraft;
基于飞行器的航行信息进行预警判断，得到预警报告；Based on the navigation information of the aircraft, make an early warning judgment and obtain an early warning report;
将所述预警报告加载至预先获取的飞行器航线视景中进行预警。The early warning report is loaded into the pre-acquired aircraft route view for early warning.
可选的，飞行器的航行信息包括：飞行器航线信息、飞行器高度信息、域内飞行器态势信息中的一种或多种，所述预警报告包括：航线边界预警报告、飞行器高度预警报告、域内飞行器态势预警报告中的一种或多种，所述基于所述飞行器的信息进行预警判断，得到预警报告的步骤包括：Optionally, the navigation information of the aircraft includes one or more of: aircraft route information, aircraft altitude information, and intra-domain aircraft situation information, and the early warning report includes: route boundary early warning report, aircraft altitude early warning report, and intra-domain aircraft situation warning. One or more of the reports, the step of performing an early warning judgment based on the information of the aircraft, and obtaining the early warning report includes:
基于所述飞行器航线信息进行预警判断，得到所述航线边界预警报告；和/或Carry out an early warning judgment based on the aircraft route information, and obtain the route boundary early warning report; and/or
基于所述飞行器高度信息进行预警判断，得到所述航线高度预警报告；和/或Perform early warning judgment based on the aircraft altitude information, and obtain the route altitude early warning report; and/or
基于所述域内飞行器态势信息进行预警判断，得到所述域内飞行器态势预警报告。Early warning judgment is performed based on the situation information of the aircraft in the domain, and an early warning report of the situation of the aircraft in the domain is obtained.
可选的，基于所述飞行器航线信息进行预警判断，得到所述航线边界预警信息的步骤包括：Optionally, the early warning judgment is performed based on the aircraft route information, and the step of obtaining the route boundary early warning information includes:
基于所述飞行器航线信息，提取航线宽度边界值；extracting a route width boundary value based on the aircraft route information;
基于所述航线宽度边界值，设置飞行边界线；setting a flight boundary line based on the route width boundary value;
若所述飞行器偏离所述飞行边界线，则发出所述航线边界预警报告。If the aircraft deviates from the flight boundary line, the route boundary warning report is issued.
可选的，基于所述飞行器高度信息进行预警判断，得到所述飞行器高度预警报告的步骤包括：Optionally, the step of performing an early warning judgment based on the aircraft altitude information, and obtaining the aircraft altitude warning report includes:
获取预设距离内的最高物体高度信息；Get the height information of the highest object within the preset distance;
基于所述飞行器高度信息，计算所述飞行器与预设距离内最高物体的高度差；Calculate the height difference between the aircraft and the tallest object within a preset distance based on the aircraft altitude information;
若所述高度差小于预设的报警值，则发出所述飞行器高度预警报告。If the height difference is smaller than a preset alarm value, the aircraft height warning report is issued.
可选的，基于所述域内飞行器态势信息进行预警判断，得到所述域内飞行器态势预警报告的步骤包括：Optionally, the step of performing early warning and judgment based on the situation information of the aircraft in the domain, and obtaining the early warning report of the situation of the aircraft in the domain includes:
基于所述域内飞行器态势信息，计算域内其他飞行器与本飞行器发生碰撞的概率；Calculate the probability of collision between other aircraft in the domain and the aircraft based on the situation information of the aircraft in the domain;
若所述碰撞的概率超过预设碰撞概率，则发出所述域内飞行器态势预警报告。If the probability of the collision exceeds the preset probability of collision, a situational warning report of the aircraft in the domain is issued.
可选的，飞行器的航行信息还包括飞行器机身宽度，所述将所述预警信息加载至预先获取的航线视景中进行预警的步骤之前包括：Optionally, the navigation information of the aircraft further includes the width of the fuselage of the aircraft, and the step of loading the early warning information into the pre-acquired route view for early warning includes:
基于所述飞行器机身宽度，计算得到所述飞行器的边界线；Calculate the boundary line of the aircraft based on the fuselage width of the aircraft;
将所述飞行器的边界线加载到所述航线视景中，以显示所述飞行器在所述航线视景中的相对位置。A boundary line of the aircraft is loaded into the route view to display the relative position of the aircraft in the route view.
可选的，将所述预警信息加载至预先获取的所述飞行器的航线视景中进行预警显示的步骤之后还包括：Optionally, after the step of loading the early warning information into the pre-acquired route view of the aircraft for early warning display, the method further includes:
若所述飞行器接收到紧急预警信息，则在所述飞行器的航线视景中进行应急航线显示，具体包括：If the aircraft receives the emergency warning information, it will display the emergency route in the route view of the aircraft, which specifically includes:
基于所述临时预警信息，计算得到所述应急航线；Calculate the emergency route based on the temporary early warning information;
基于所述应急航线，调整所述飞行器的航线视景，以将所述应急航线显示在所述飞行器的航线视景中。Based on the emergency route, the aircraft's route view is adjusted to display the emergency route in the aircraft's route view.
此外，为实现上述目的，本申请实施例还提出一种飞行器预警装置，所述飞行器预警装置包括：In addition, in order to achieve the above purpose, an embodiment of the present application also proposes an aircraft early warning device, and the aircraft early warning device includes:
信息获取模块，用于获取飞行器的航行信息；The information acquisition module is used to acquire the navigation information of the aircraft;
预警判断模块，用于基于所述飞行器的航行信息，进行预警判断，得到预警报告；an early warning judgment module, configured to perform early warning judgment based on the navigation information of the aircraft, and obtain an early warning report;
预警显示模块，用于将所述预警报告加载至预先获取的飞行器航线视景中进行预警。The early warning display module is used for loading the early warning report into the pre-acquired aircraft route view for early warning.
此外，为实现上述目的，本申请实施例还提出一种终端设备，所述终端设备包括存储器、处理器及存储在所述存储器上并可在所述处理器上运行的飞行器预警程序，所述飞行器预警程序被所述处理器执行时实现如上所述的飞行器预警方法的步骤。In addition, in order to achieve the above purpose, an embodiment of the present application further proposes a terminal device, the terminal device includes a memory, a processor, and an aircraft early warning program stored in the memory and running on the processor, the When the aircraft early warning program is executed by the processor, the steps of the above-mentioned aircraft early warning method are implemented.
此外，为实现上述目的，本申请实施例还提出一种计算机可读存储介质，所述计算机可读存储介质上存储有飞行器预警程序，所述飞行器预警程序被处理器执行时实现如上所述的飞行器预警方法的步骤。In addition, in order to achieve the above purpose, an embodiment of the present application further proposes a computer-readable storage medium, where an aircraft early warning program is stored on the computer-readable storage medium, and the aircraft early warning program is executed by a processor to achieve the above-mentioned The steps of the aircraft early warning method.
本申请提出的飞行器预警方法、装置、终端设备以及存储介质，通过获取飞行器的航行信息；基于所述飞行器的航行信息进行预警判断，得到预警报告；将所述预警报告加载至预先获取的飞行器航线视景中进行预警。基于本申请方案，针对当下飞行员(或无人驾驶)的过程中缺乏有效预警手段的问题，提出了一种能够对飞行器的航行过程进行有效预警的方案，通过对飞行器的各种信息进行预警判断，生成预警报告并在飞行器航线视景中加载显示，实现了航行中的及时预警，能够辅助飞行员处理航行中的各种情况，从而提高了飞行器航行过程的安全性，有效消除了安全隐患。The aircraft early warning method, device, terminal device and storage medium proposed in the present application obtain the navigation information of the aircraft; make early warning judgment based on the navigation information of the aircraft, and obtain the early warning report; and load the early warning report to the pre-acquired aircraft route Warning in sight. Based on the solution of the present application, aiming at the problem of lack of effective early warning means in the process of current pilots (or unmanned pilots), a scheme that can effectively give early warning to the navigation process of the aircraft is proposed. , generate an early warning report and display it in the aircraft's route view, which realizes timely early warning during navigation, and can assist pilots in handling various situations during navigation, thereby improving the safety of the aircraft's navigation process and effectively eliminating potential safety hazards.
附图说明Description of drawings
图1为本申请飞行器预警装置所属终端设备的功能模块示意图；Fig. 1 is the functional module schematic diagram of the terminal equipment to which the aircraft early warning device of the application belongs;
图2为本申请飞行器预警方法第一实施例的流程示意图；FIG. 2 is a schematic flowchart of the first embodiment of the aircraft early warning method of the application;
图3为本申请飞行器预警方法第一实施例关于步骤S20的细化流程示意图；FIG. 3 is a schematic flow chart of the refinement of step S20 according to the first embodiment of the aircraft early warning method of the present application;
图4为本申请飞行器预警方法第一实施例关于步骤S20的又一细化流程示意图；FIG. 4 is a schematic flow chart of another refinement of step S20 according to the first embodiment of the aircraft early warning method of the present application;
图5为本申请飞行器预警方法第一实施例关于步骤S20的又一细化流程示意图；FIG. 5 is a schematic flow chart of another refinement of step S20 according to the first embodiment of the aircraft early warning method of the present application;
图6为本申请飞行器预警方法第二实施例的流程示意图；6 is a schematic flowchart of the second embodiment of the aircraft early warning method of the application;
图7为本申请飞行器预警方法第三实施例的流程示意图。FIG. 7 is a schematic flowchart of a third embodiment of an aircraft early warning method of the present application.
本申请目的的实现、功能特点及优点将结合实施例，参照附图做进一步说明。The realization, functional characteristics and advantages of the purpose of the present application will be further described with reference to the accompanying drawings in conjunction with the embodiments.
具体实施方式Detailed ways
应当理解，此处所描述的具体实施例仅仅用以解释本申请，并不用于限定本申请。It should be understood that the specific embodiments described herein are only used to explain the present application, but not to limit the present application.
本申请实施例的主要解决方案是：获取飞行器的航行信息；基于所述飞行器的航行信息进行预警判断，得到预警报告；将所述预警报告加载至预先获取的飞行器航线视景中进行预警。本申请考虑到，如果飞行员只能依靠自身的经验和简单的操作设备来对飞行器进行驾驶，不确定性因素太多(如飞行员状态、经验不足)，导致航行中出现了不可控的因素，安全性难以得到较高低保障。因此，本申请方案提出了对飞行器的各种信息进行预警判断，帮助飞行员驾驶的方法，经过实践证明，本方案能够有效地辅助飞行员(或无人驾驶系统)，有效消除安全隐患，还可用于飞行员(或无人驾驶系统)的训练。The main solutions of the embodiments of the present application are: acquiring the navigation information of the aircraft; performing early warning judgment based on the navigation information of the aircraft, and obtaining an early warning report; and loading the early warning report into a pre-acquired aircraft route view for early warning. This application considers that if pilots can only rely on their own experience and simple operating equipment to drive the aircraft, there are too many uncertain factors (such as pilot status, lack of experience), resulting in uncontrollable factors during navigation, safety Sex is difficult to obtain higher and lower protection. Therefore, the solution of this application proposes a method for early warning and judgment of various information of the aircraft to help pilots to drive. It has been proved by practice that this solution can effectively assist pilots (or unmanned systems), effectively eliminate potential safety hazards, and can also be used for Training of pilots (or unmanned systems).
本申请实施例涉及的技术术语：Technical terms involved in the embodiments of this application:
航线，即飞机飞行的路线，也被称为空中交通线，简称航线。飞机的航线不仅确定了飞机飞行具体方向、起讫点和经停点，而且还根据空中交通管制的需要，规定了航线的宽度和飞行高度，以维护空中交通秩序，保证飞行安全。Route, that is, the route that the aircraft flies, also known as the air traffic line, referred to as the route. The flight route of an aircraft not only determines the specific direction, origin, destination and stop point of the aircraft's flight, but also specifies the width and flight height of the flight route according to the needs of air traffic control, so as to maintain air traffic order and ensure flight safety.
按照飞机飞行的起讫点，航线可分为国际航线、国内航线和地区航线三大类：国际航线是指飞行路线连接两个或两个以上国家的航线；国内航线是指在一个国家内部的航线，它又可分为干线、支线和地方航线三大类；地区航线指在一国之内，连接普通地区和特殊地区的航线，如中国内地与港、澳、台地区之间的航线。另外，航线还可分为固定航线和临时航线，临时航线通常不得与航路、固定航线交叉或是通过飞行频繁的机场上空。According to the origin and destination of aircraft flight, routes can be divided into three categories: international routes, domestic routes and regional routes: international routes refer to routes connecting two or more countries; domestic routes refer to routes within a country , it can be divided into three categories: trunk lines, branch lines and local routes; regional routes refer to routes within a country that connect ordinary regions and special regions, such as routes between mainland China and Hong Kong, Macao and Taiwan regions. In addition, routes can also be divided into fixed routes and temporary routes. Temporary routes are usually not allowed to intersect with air routes or fixed routes or pass over airports with frequent flights.
本申请实施例考虑到，在飞行器的航行中，如果飞行员单纯借助仪表显控和空管系统来驾驶飞机，需要依靠自己的经验来判断飞行器当前状态。这样一来，当航行中出现一些突发状况(如飞机偏航、异常天气、空管临时调度、空域临时管制等)时，飞行员的自身素质将间接决定整个飞行器的安危，导致航行过程中出现了不可控的因素，产生了一定的安全隐患。The embodiments of the present application consider that, during the flight of the aircraft, if the pilot simply uses the instrument display and control system and the air traffic control system to fly the aircraft, he needs to rely on his own experience to judge the current state of the aircraft. In this way, when some emergencies occur during the flight (such as aircraft yaw, abnormal weather, temporary air traffic control, temporary airspace control, etc.), the pilot's own quality will indirectly determine the safety of the entire aircraft, resulting in the occurrence of accidents during the flight. Uncontrollable factors have caused certain security risks.
因此，本申请实施例方案从飞行员缺乏有效预警手段这一问题出发，通过获取飞行器的信息并进行各项预警判断，将生成的预警报告加载到航线视景中显示，飞行员可借助包含有预警报告的视景画面驾驶飞行器，提高了航行中的安全性。Therefore, the solution of the embodiment of the present application starts from the problem that the pilot lacks effective early warning means. By acquiring the information of the aircraft and making various early warning judgments, the generated early warning report is loaded into the route view for display, and the pilot can use the information contained in the early warning report. The visual picture of flying the aircraft improves the safety during navigation.
具体地，参照图1，图1为本申请飞行器预警装置所属终端设备的功能模块示意图。该飞行器预警装置可以为独立于终端设备的、能够对飞行器的信息进行预警判断并结合航线视景画面显示的装置，其可以通过硬件或软件的形式承载于终端设备上。该终端设备可以为手机、平板电脑等具有数据处理功能的智能移动终端，还可以为具有数据处理功能的固定终端设备或服务器等。Specifically, referring to FIG. 1 , FIG. 1 is a schematic diagram of functional modules of a terminal device to which the aircraft early warning device of the present application belongs. The aircraft early warning device may be a device independent of the terminal equipment, capable of performing early warning judgment on the information of the aircraft and displaying it in combination with the route view screen, which can be carried on the terminal equipment in the form of hardware or software. The terminal device may be an intelligent mobile terminal with a data processing function, such as a mobile phone or a tablet computer, or a fixed terminal device or a server with a data processing function.
在本实施例中，该飞行器预警装置所属终端设备至少包括输出模块110、处理器120、存储器130以及通信模块140。In this embodiment, the terminal device to which the aircraft early warning apparatus belongs at least includes an
存储器130中存储有操作系统以及飞行器预警程序，飞行器预警装置可以将获取的飞行器的信息；基于所述飞行器的信息进行预警判断得到的预警报告等信息存储于该存储器130中；输出模块110可为显示屏等。通信模块140可以包括WIFI模块、移动通信模块以及蓝牙模块等，通过通信模块140与外部设备或服务器进行通信。An operating system and an aircraft early warning program are stored in the
其中，存储器130中的飞行器预警程序被处理器执行时实现以下步骤：Wherein, when the aircraft early warning program in the
获取飞行器的航行信息；Obtain the navigation information of the aircraft;
基于所述飞行器的航行信息进行预警判断，得到预警报告；Carry out early warning judgment based on the navigation information of the aircraft, and obtain an early warning report;
将所述预警报告加载至预先获取的飞行器航线视景中进行预警。The early warning report is loaded into the pre-acquired aircraft route view for early warning.
进一步地，存储器130中的飞行器预警程序被处理器执行时还实现以下步骤：Further, when the aircraft early warning program in the
基于所述飞行器航线信息进行预警判断，得到所述航线边界预警报告；Carry out early warning judgment based on the aircraft route information, and obtain the route boundary early warning report;
基于所述飞行器高度信息进行预警判断，得到所述航线高度预警报告；Perform early warning judgment based on the aircraft altitude information, and obtain the route altitude early warning report;
基于所述域内飞行器态势信息进行预警判断，得到所述域内飞行器态势预警报告。Early warning judgment is performed based on the situation information of the aircraft in the domain, and an early warning report of the situation of the aircraft in the domain is obtained.
进一步地，存储器130中的飞行器预警程序被处理器执行时还实现以下步骤：Further, when the aircraft early warning program in the
基于所述飞行器航线信息，提取航线宽度边界值；extracting a route width boundary value based on the aircraft route information;
基于所述航线宽度边界值，设置飞行边界线；setting a flight boundary line based on the route width boundary value;
若所述飞行器偏离所述飞行边界线，则发出所述航线边界预警报告。If the aircraft deviates from the flight boundary line, the route boundary warning report is issued.
进一步地，存储器130中的飞行器预警程序被处理器执行时还实现以下步骤：Further, when the aircraft early warning program in the
获取预设距离内的最高物体高度信息；Get the height information of the highest object within the preset distance;
基于所述飞行器高度信息，计算所述飞行器与预设距离内最高物体的高度差；Calculate the height difference between the aircraft and the tallest object within a preset distance based on the aircraft altitude information;
若所述高度差小于预设的报警值，则发出所述飞行器高度预警报告。If the height difference is smaller than a preset alarm value, the aircraft height warning report is issued.
进一步地，存储器130中的飞行器预警程序被处理器执行时还实现以下步骤：Further, when the aircraft early warning program in the
基于所述域内飞行器态势信息，对其他域内飞行器的飞行态势进行分级；Based on the situation information of the aircraft in the domain, classify the flying situation of the aircraft in other domains;
基于分级后的飞行态势，计算所述其他域内飞行器与本飞行器发生碰撞的概率；Calculate the probability of collision between the aircraft in the other domain and the aircraft based on the classified flight situation;
若存在与所述本飞行器达到预设碰撞概率的其他域内飞行器，则发出所述域内飞行器态势预警报告。If there are other aircraft in the domain that reach the preset probability of collision with the aircraft, a situational warning report of the aircraft in the domain is issued.
进一步地，存储器130中的飞行器预警程序被处理器执行时还实现以下步骤：Further, when the aircraft early warning program in the
基于所述飞行器机身宽度，计算得到所述飞行器的边界线；Calculate the boundary line of the aircraft based on the fuselage width of the aircraft;
将所述飞行器的边界线加载到所述航线视景中，以显示所述飞行器在所述航线视景中的相对位置。A boundary line of the aircraft is loaded into the route view to display the relative position of the aircraft in the route view.
进一步地，存储器130中的飞行器预警程序被处理器执行时还实现以下步骤：Further, when the aircraft early warning program in the
若所述飞行器接收到紧急预警信息，则在所述飞行器的航线视景中进行应急航线显示，具体包括：If the aircraft receives the emergency warning information, it will display the emergency route in the route view of the aircraft, which specifically includes:
基于所述临时预警信息，计算得到所述应急航线；Calculate the emergency route based on the temporary early warning information;
基于所述应急航线，调整所述飞行器的航线视景，以将所述应急航线显示在所述飞行器的航线视景中。Based on the emergency route, the aircraft's route view is adjusted to display the emergency route in the aircraft's route view.
本实施例通过上述方案，具体通过获取飞行器的航行信息；基于所述飞行器的航行信息进行预警判断，得到预警报告；将所述预警报告加载至预先获取的飞行器航线视景中进行预警。基于本申请方案，针对当下飞行员(或无人驾驶)的过程中缺乏有效预警手段的问题，提出了一种能够对飞行器的航行过程进行有效预警的方案，通过对飞行器的各种信息进行预警判断，生成预警报告并在飞行器航线视景中加载显示，实现了航行中的及时预警，能够辅助飞行员处理航行中的各种情况，从而提高了飞行器航行过程的安全性，有效消除了安全隐患。This embodiment uses the above solution, specifically by acquiring the navigation information of the aircraft; performing early warning judgment based on the navigation information of the aircraft, and obtaining an early warning report; and loading the early warning report into the pre-acquired aircraft route view for early warning. Based on the solution of the present application, aiming at the problem of lack of effective early warning means in the process of current pilots (or unmanned pilots), a scheme that can effectively give early warning to the navigation process of the aircraft is proposed. , generate an early warning report and display it in the aircraft's route view, which realizes timely early warning during navigation, and can assist pilots in handling various situations during navigation, thereby improving the safety of the aircraft's navigation process and effectively eliminating potential safety hazards.
基于上述终端设备架构但不限于上述架构，提出本申请方法实施例。Based on the above-mentioned terminal device architecture but not limited to the above-mentioned architecture, the method embodiments of the present application are proposed.
参照图2，图2为本申请飞行器预警方法第一实施例的流程示意图。所述飞行器预警方法包括：Referring to FIG. 2 , FIG. 2 is a schematic flowchart of the first embodiment of the aircraft early warning method of the present application. The aircraft early warning method includes:
步骤S10，获取飞行器的航行信息；Step S10, obtaining the navigation information of the aircraft;
具体地，本实施例辅助飞行员进行飞行器预警的过程，是通过对获取飞行器的信息并进行预警判断实现的。因此，本步骤要首先获取飞行器的信息，以在后续步骤中进行分析判断。通常情况下，飞行器的空管系统中存储有关于当前飞行器的各种信息，因此本步骤中获取飞行器的信息这一流程也可借助上述飞管系统来完成。作为一种实施方式，本申请的实施人员能够理解，本实施例及后续实施例的执行主体可以为一种加载了飞行器预警程序的空管系统，上述飞行器预警程序能够完全实现本申请所提出的飞行器预警方案，之后，通过与上述空管系统的交互可以更加便捷地实现本方案。为了方便起见，在后续的说明中，均以上述加载了飞行器预警程序的空管系统作为本方案的默认执行主体。Specifically, the process of assisting the pilot to carry out the aircraft early warning in this embodiment is realized by acquiring the information of the aircraft and performing early warning judgment. Therefore, in this step, the information of the aircraft should be obtained first, so as to analyze and judge in the subsequent steps. Usually, various information about the current aircraft is stored in the air traffic control system of the aircraft, so the process of acquiring the information of the aircraft in this step can also be completed with the aid of the above-mentioned flight control system. As an implementation manner, practitioners of the present application can understand that the execution body of this embodiment and subsequent embodiments may be an air traffic control system loaded with an aircraft early warning program, and the above aircraft early warning program can fully realize the proposed Aircraft early warning scheme, after that, this scheme can be more conveniently implemented by interacting with the above-mentioned air traffic control system. For the sake of convenience, in the subsequent descriptions, the above-mentioned air traffic control system loaded with the aircraft early warning program is used as the default execution body of this scheme.
更为具体地，上述飞行器的航行信息具体包括：More specifically, the navigation information of the above-mentioned aircraft specifically includes:
飞行器航线信息，包含有飞行器在此次航行中的航线的信息，如航线的方向、路径等信息；Aircraft route information, including the route information of the aircraft in this voyage, such as the direction and path of the route;
飞行器高度信息，即本飞行器的当前飞行高度；Aircraft altitude information, that is, the current flight altitude of the aircraft;
域内飞行器态势信息，即在一个约定的空域内，其他所有飞行器的信息。The situation information of aircraft in the domain, that is, the information of all other aircraft in a predetermined airspace.
步骤S20，基于所述飞行器的航行信息进行预警判断，得到预警报告；Step S20, performing an early warning judgment based on the navigation information of the aircraft, and obtaining an early warning report;
参照上述步骤S10，飞行器的信息包括飞行器航线信息、飞行器高度信息、域内飞行器态势信息，对应飞行器的信息，飞行器的预警报告包括航线边界预警报告、飞行器高度预警报告、域内飞行器态势预警报告，具体地，上述基于所述飞行器的信息进行预警判断，得到预警报告的步骤具体包括：Referring to the above step S10, the information of the aircraft includes aircraft route information, aircraft altitude information, aircraft situation information in the domain, and the information of the corresponding aircraft, and the early warning report of the aircraft includes the route boundary warning report, the aircraft altitude warning report, and the aircraft situation warning report in the domain. Specifically , the above-mentioned steps of performing an early warning judgment based on the information of the aircraft, and obtaining an early warning report specifically include:
基于所述飞行器航线信息进行预警判断，得到所述航线边界预警报告；Carry out early warning judgment based on the aircraft route information, and obtain the route boundary early warning report;
具体地，参照图3，图3为本申请飞行器预警方法第一实施例关于步骤S20的细化流程示意图，所述基于所述飞行器航线信息进行预警判断，得到所述航线边界预警报告的步骤包括：Specifically, referring to FIG. 3 , FIG. 3 is a schematic flow chart of the refinement of step S20 in the first embodiment of the aircraft early warning method of the present application. The step of performing early warning judgment based on the aircraft route information and obtaining the route boundary early warning report includes the following steps: :
步骤A10，基于所述飞行器航线信息，提取航线宽度边界值；Step A10, based on the aircraft route information, extract the route width boundary value;
步骤A20，基于所述航线宽度边界值，设置飞行边界线；Step A20, setting a flight boundary line based on the route width boundary value;
更为具体地，飞行器的航线信息中包含有飞行器此次航线的所有信息，借助该飞行器航线信息，可以对当前飞行器是否偏航做出判断。航线宽度边界值为航线的左右宽度边界值，该值能直观地表示出当前航线的方向范围，当飞行器的航行方向超出航线的左右宽度边界值时，即可认为飞行器偏航。More specifically, the route information of the aircraft includes all the information of the current route of the aircraft. With the aid of the route information of the aircraft, it is possible to judge whether the current aircraft is yaw. The route width boundary value is the left and right width boundary value of the route, which can intuitively indicate the direction range of the current route. When the flight direction of the aircraft exceeds the left and right width boundary value of the route, the aircraft can be considered to be yaw.
为了使预警报告更有价值，本实施例还在航线宽度边界值的基础上设置了飞行边界线，该飞行边界线可以按照实际需求设置一定(可考虑根据飞行器的性能、飞管系统的操作延迟等因素确定)的约束余量，使得飞行边界线比真实的航线宽度边界值要小，这样一来，可以在飞行器偏航之前就发出偏航预警，防患于未然，让预警更有价值。In order to make the early warning report more valuable, this embodiment also sets a flight boundary line on the basis of the route width boundary value. and other factors), so that the flight boundary line is smaller than the actual route width boundary value, so that the yaw warning can be issued before the aircraft yaw, preventing problems before they occur, and making the warning more valuable.
步骤A30，若所述飞行器偏离所述飞行边界线，则发出所述航线边界预警报告。Step A30, if the aircraft deviates from the flight boundary line, issue the route boundary warning report.
更为具体地，根据上述步骤中设置的飞行边界线，并通过空管系统实时确定本飞行器的当前位置，判断飞行器是否偏离上述飞行边界线，如果偏离，则会发出航线边界预警的报告，后续步骤中可以根据此报告在飞行器的航线视景画面中以声光报警的形式提醒飞行员(或无人驾驶系统，后文不再赘述)，并发出修正指令。关于判断飞行器是否偏离飞行边界线的过程，本申请的实施人员可以选择任意一种方式来实现判断的目的，本实施例不再赘述。More specifically, according to the flight boundary line set in the above steps, the current position of the aircraft is determined in real time through the air traffic control system, and it is judged whether the aircraft deviates from the above-mentioned flight boundary line. In the step, according to the report, the pilot (or the unmanned system, which will not be described in detail below) can be reminded in the form of sound and light alarm in the route view screen of the aircraft, and a correction instruction can be issued. Regarding the process of judging whether the aircraft deviates from the flight boundary line, the implementer of the present application may choose any method to achieve the purpose of judgment, which will not be repeated in this embodiment.
基于所述飞行器高度信息进行预警判断，得到所述航线高度预警报告；Perform early warning judgment based on the aircraft altitude information, and obtain the route altitude early warning report;
具体地，参照图4，图4为本申请飞行器预警方法第一实施例关于步骤S20的又一细化流程示意图，所述基于所述飞行器高度信息进行预警判断，得到所述航线高度预警报告的步骤具体包括：Specifically, referring to FIG. 4 , FIG. 4 is another detailed flow chart of step S20 of the first embodiment of the aircraft early warning method of the present application, wherein the early warning judgment is performed based on the aircraft altitude information, and the route altitude early warning report is obtained. The steps include:
步骤A100，获取预设航线距离内的最高物体高度信息；Step A100, obtaining the height information of the highest object within the preset route distance;
步骤A200，基于所述飞行器高度信息，计算所述飞行器与预设距离内最高物体的高度差；Step A200, based on the height information of the aircraft, calculate the height difference between the aircraft and the highest object within a preset distance;
更为具体地，前述飞行器飞行高度信息可以通过飞行器上的信息采集载荷(如高度表或大气数据计算机等方式)获得，预设距离内的最高物体高度信息可以通过雷达或导航卫星的数据获得，此处的预设距离内的最高物体值山峰、大楼等较高的物体。为了确保飞行器航行中不会碰撞到地面的物体，此处将飞行器高度信息和预设距离内的最高物体高度信息进行高差比对，计算二者的高度差，并在后续步骤中判断次高度差是否会造成影响。为了保证飞行员有足够的时间修正飞行器的高度，预设距离的选取可以考虑飞行器的拉起时间以及其他因素，选取一个较为安全的范围，以保证飞行员收到预警报告后有足够的时间升高飞行器的高度。More specifically, the aforementioned aircraft flight height information can be obtained through the information collection load on the aircraft (such as an altimeter or an atmospheric data computer, etc.), and the height information of the highest object within a preset distance can be obtained through radar or navigation satellite data, The highest object values within the preset distance here are tall objects such as mountains and buildings. In order to ensure that the aircraft does not collide with objects on the ground, the height difference between the aircraft height information and the height information of the highest object within the preset distance is compared, and the height difference between the two is calculated, and the next height is determined in the subsequent steps. Whether the difference will have an impact. In order to ensure that the pilot has enough time to correct the altitude of the aircraft, the selection of the preset distance can consider the pull-up time of the aircraft and other factors, and select a relatively safe range to ensure that the pilot has enough time to raise the aircraft after receiving the warning report. the height of.
步骤A300，若所述高度差小于预设的报警值，则发出所述飞行器高度预警报告。Step A300, if the height difference is less than a preset alarm value, issue an altitude warning report of the aircraft.
更为具体地，预设的报警值可以结合上述预设距离来确定，使得高差小于报警值时，飞行员能够迅速采取措施修正飞行器的高度。在后续步骤中，所得到的的飞行器高度预警报告被发送给空管系统后，空管系统将在航线视景中以一种较为明显的方式显示此预警报告，在此不再赘述。More specifically, the preset alarm value can be determined in combination with the above-mentioned preset distance, so that when the height difference is smaller than the alarm value, the pilot can quickly take measures to correct the altitude of the aircraft. In the subsequent steps, after the obtained aircraft altitude warning report is sent to the air traffic control system, the air traffic control system will display the early warning report in a more obvious way in the route view, which will not be repeated here.
基于所述域内飞行器态势信息进行预警判断，得到所述域内飞行器态势预警报告。Early warning judgment is performed based on the situation information of the aircraft in the domain, and an early warning report of the situation of the aircraft in the domain is obtained.
具体地，参照图5，图5为本申请飞行器预警方法第一实施例关于步骤S20的又一细化流程示意图，所述基于所述域内飞行器态势信息进行预警判断，得到所述域内飞行器态势预警报告的步骤具体包括：Specifically, referring to FIG. 5 , FIG. 5 is another detailed flow chart of step S20 of the first embodiment of the aircraft early warning method of the present application. The early warning judgment is performed based on the situation information of the aircraft in the domain, and the situation warning of the aircraft in the domain is obtained. The steps to report include:
步骤A1000，基于所述域内飞行器态势信息，计算域内其他飞行器与本飞行器发生碰撞的概率；Step A1000, based on the situation information of the aircraft in the domain, calculate the probability of collision between other aircraft in the domain and this aircraft;
更为具体地，在前述步骤中获取域内飞行器态势信息时，可以通过飞管系统接收(如通过ADS-B广播接收或其他接收途径)约定空域内其他飞行器的位置信息，并进行态势感知。之后，可继续借助空管系统计算其他域内飞行器与本飞行器发生碰撞的概率。关于碰撞概率计算的方式，本申请的实施人员可以查阅资料，选择任意一种现有飞行器碰撞概率计算的方案来实现，本实施例对此不做限定，达到碰撞概率计算的目的即可。More specifically, when the situation information of the aircraft in the domain is obtained in the foregoing steps, the position information of other aircraft in the agreed airspace can be received through the flight control system (eg, through ADS-B broadcast reception or other receiving methods), and situational awareness can be performed. After that, you can continue to use the air traffic control system to calculate the probability of collision between aircraft in other domains and this aircraft. Regarding the method of collision probability calculation, the implementer of the present application can consult the data and choose any existing aircraft collision probability calculation scheme to realize it, which is not limited in this embodiment, as long as the purpose of collision probability calculation is achieved.
步骤A2000，若所述碰撞的概率超过预设碰撞概率，则发出所述域内飞行器态势预警报告。Step A2000, if the probability of collision exceeds a preset probability of collision, issue a situational warning report of the aircraft in the domain.
更为具体地，本申请实施人员可以根据飞行器的参数，以及同一航线内其他飞行器的参数来提前设定一个碰撞概率，当本飞行器与其他飞行器的碰撞概率超出此预设碰撞概率时，认为飞行器在当前路线下有可能发生碰撞事故，发出域内飞行器态势预警报告，以提醒飞行员注意域内飞行器的动向，在可能有意外碰撞时及时作出修正。More specifically, the practitioner of the present application can set a collision probability in advance according to the parameters of the aircraft and the parameters of other aircraft in the same route. When the collision probability between the aircraft and other aircraft exceeds this preset collision probability, it is considered that the aircraft A collision accident may occur under the current route, and an early warning report of the aircraft situation in the domain is issued to remind the pilot to pay attention to the movement of the aircraft in the domain, and make timely corrections in the event of a possible accidental collision.
步骤S30，将所述预警报告加载至预先获取的飞行器航线视景中进行预警。Step S30, loading the early warning report into a pre-acquired aircraft route view for early warning.
具体地，根据上述步骤中所得到的航线边界预警报告、航线高度预警报告、域内飞行器态势预警报告，将这些预警报告记载到预先获取的飞行器航线视景中以对飞行员进行对应的预警显示，包括：航线边界预警显示、航线高度预警显示、域内飞行器态势预警显示，以提醒飞行员及时处理或修正。飞行器航线视景是包含有飞行器当前位置信息、飞行器的航线信息、地图信息的视景画面，通过飞行器航线视景显示出预警报告，可以更加形象地给飞行员以提示的效果。Specifically, according to the route boundary warning report, the route altitude warning report, and the aircraft situation warning report in the domain obtained in the above steps, these warning reports are recorded in the pre-obtained aircraft route view to display the corresponding warning to the pilot, including: : Route boundary warning display, route altitude warning display, and aircraft situation warning display in the domain to remind pilots to deal with or make corrections in time. The aircraft route view is a visual screen that includes the current position information of the aircraft, the route information of the aircraft, and the map information. The early warning report is displayed through the aircraft route view, which can give the pilot the effect of prompting more vividly.
更为具体地，预警的方式可以为声光报警，即通过声音和光线来发出警报。对于航线边界预警显示，空管系统会在飞行器航线视景中强化(可以通过颜色渲染的形式)显示出边界预警线，并发出预警声音，即警告当前飞行航线超出了飞行边界线，提醒飞行员进行偏航修正，修正结束后，若当前飞行航线不再超过飞行边界线，停止报警显示。More specifically, the way of early warning can be sound and light alarm, that is, sound and light are used to issue an alarm. For the route boundary warning display, the air traffic control system will strengthen the aircraft route view (in the form of color rendering) to display the boundary warning line, and issue a warning sound, that is, to warn that the current flight route exceeds the flight boundary line, and remind the pilot to carry out Yaw correction, after the correction is completed, if the current flight route no longer exceeds the flight boundary line, the alarm display will stop.
对于航线高度预警显示，一旦受到航线高度的预警报告，则空管系统会在本飞行器的航线视景画面中显示预警提示，并采用声光报警的方式下发修正指令，提醒飞行员增加航行高度，修正结束后，若航行高度与上述预设距离内的最高物体高度差大于报警值，停止报警显示。For the route altitude warning display, once the warning report of the route altitude is received, the air traffic control system will display the warning prompt on the route view screen of the aircraft, and issue a correction instruction by means of sound and light alarm to remind the pilot to increase the sailing altitude. After the correction is completed, if the difference between the sailing altitude and the height of the highest object within the above preset distance is greater than the alarm value, the alarm display will be stopped.
对于域内飞行器态势预警显示，一旦本飞行器与域内其他飞行器的碰撞概率达到预设值，则空管系统会在飞行器航线视景画面中显示出其他飞行器，并给这些可能发生碰撞的飞行器添加预警显示(如给这些飞行器的图像加颜色框、着重闪烁这些飞行器等)，并采用声光报警的方式下发修正指令，提醒飞行员注意这些飞行器的动向，避免意外碰撞。For the situational warning display of aircraft in the domain, once the collision probability between this aircraft and other aircraft in the domain reaches the preset value, the air traffic control system will display other aircraft in the aircraft's route view screen, and add early warning display to these aircraft that may collide (such as adding color boxes to the images of these aircraft, focusing on flashing these aircraft, etc.), and using sound and light alarms to issue correction instructions to remind pilots to pay attention to the movements of these aircraft and avoid accidental collisions.
本实施例通过上述方案，具体通过获取飞行器的信息；基于所述飞行器的信息进行预警判断，得到预警报告；将所述预警报告加载至预先获取的飞行器航线视景中进行预警。本实施例中的预警报告包括航线边界预警报告、飞行器高度预警报告、域内飞行器态势预警报告，通过这些预警报告对当前飞行器的信息进行全面的预警判断，以辅助飞行员安全驾驶，使得飞行器的安全航行不再只能依靠飞行员的个人经验和个人素质，提高了飞行器航行中的安全性。This embodiment uses the above solution, specifically by acquiring information of the aircraft; performing early warning judgment based on the information of the aircraft, and obtaining an early warning report; and loading the early warning report into a pre-acquired aircraft route view for early warning. The early warning report in this embodiment includes a route boundary early warning report, an aircraft altitude early warning report, and an aircraft situation early warning report in the domain. Through these early warning reports, a comprehensive early warning judgment is made on the information of the current aircraft, so as to assist the pilot to drive safely and ensure the safe navigation of the aircraft. It is no longer necessary to rely on the personal experience and personal quality of the pilot, which improves the safety of the aircraft during navigation.
进一步地，参照图6，图6为本申请飞行器预警方法第二实施例的流程示意图。基于上述图2所示实施例的步骤S30，所述将所述预警报告加载至预先获取的航线视景中进行预警的步骤之前包括：Further, referring to FIG. 6 , FIG. 6 is a schematic flowchart of the second embodiment of the aircraft early warning method of the present application. Based on the step S30 of the embodiment shown in FIG. 2, the step of loading the early warning report into the pre-acquired route view for early warning includes:
步骤S301，获取所述飞行器的机身宽度信息；Step S301, obtaining the fuselage width information of the aircraft;
步骤S302，基于所述机身宽度信息，计算得到所述飞行器的边界线；Step S302, calculating the boundary line of the aircraft based on the fuselage width information;
具体地，飞行器的空管系统中存储有飞行器的参数，根据该参数可以获取飞行器的机身宽度信息，根据此机身宽度信息进行计算、比例尺缩小和比对航线宽度，可以得到飞行器的机翼(或整个机体，根据实际需要选择)的最左侧和最右侧的边界线，此边界线是对整个飞行器的实际模型所做的抽象，即只考虑飞行器的左右宽度计算得到，通过此边界线，可以直观地反映出飞行器在固定平面内的情况。Specifically, the parameters of the aircraft are stored in the air traffic control system of the aircraft. According to the parameters, the fuselage width information of the aircraft can be obtained. According to the fuselage width information, calculation, scale reduction and comparison of the route width can be performed to obtain the wings of the aircraft. (or the entire body, selected according to actual needs) the leftmost and rightmost boundary lines, this boundary line is an abstraction of the actual model of the entire aircraft, that is, only the left and right widths of the aircraft are calculated, and through this boundary line, which can intuitively reflect the situation of the aircraft in a fixed plane.
步骤S303，将所述飞行器的边界线加载到所述航线视景中，以显示所述飞行器在所述航线视景中的位置。Step S303, loading the boundary line of the aircraft into the route view to display the position of the aircraft in the route view.
具体地，关于飞行器航线视景的具体内容，可以参照上述图2所示实施例中的说明。在通过上述步骤得到飞行器的边界线之后，可以将此边界线模拟现实在航线视景的航线层中，从而直观显现飞行器整个机身在本航线视景中的相对位置，帮助飞行员实时观察本飞行器的航行情况，以更好地根据接收到的各种预警报告对飞行器进行修正。Specifically, for the specific content of the route view of the aircraft, reference may be made to the description in the above-mentioned embodiment shown in FIG. 2 . After the boundary line of the aircraft is obtained through the above steps, the boundary line can be simulated in the route layer of the route view, so that the relative position of the entire fuselage of the aircraft in the route view can be visually displayed, helping the pilot to observe the aircraft in real time. navigation conditions in order to better make corrections to the aircraft based on the various early warning reports received.
本实施例通过上述方案，具体通过获取所述飞行器的机身宽度信息；基于所述机身宽度信息，计算得到所述飞行器的边界线；将所述飞行器的边界线加载到所述航线视景中，以显示所述飞行器在所述航线视景中的位置。相比于上述实施例，本实施例还提出了一种在飞行器的航线视景中显示出飞行器整个机身的方案，帮助飞行员直观地判断飞行器的当前位置，从而进一步提高了本申请方案的安全性，扩充了本申请方案的应用场景，增强了本申请方案的适用范围。This embodiment adopts the above solution, specifically by acquiring the fuselage width information of the aircraft; calculating the boundary line of the aircraft based on the fuselage width information; loading the boundary line of the aircraft into the route view to display the position of the aircraft in the route view. Compared with the above-mentioned embodiment, this embodiment also proposes a scheme of displaying the entire fuselage of the aircraft in the route view of the aircraft, which helps the pilot to intuitively judge the current position of the aircraft, thereby further improving the safety of the scheme of the present application. properties, expand the application scenarios of the solution of the present application, and enhance the scope of application of the solution of the present application.
进一步地，参照图7，图7为本申请飞行器预警方法第三实施例的流程示意图。基于上述图2所示实施例的步骤S30，所述将所述预警报告加载至预先获取的所述飞行器的航线视景中进行预警显示的步骤之后还包括：Further, referring to FIG. 7 , FIG. 7 is a schematic flowchart of the third embodiment of the aircraft early warning method of the present application. Based on step S30 of the embodiment shown in FIG. 2, the step of loading the early warning report into the pre-acquired route view of the aircraft for early warning display further includes:
步骤S40，若所述飞行器接收到紧急预警信息，则在所述飞行器的航线视景中进行应急航线显示，具体包括：Step S40, if the aircraft receives the emergency warning information, display the emergency route in the route view of the aircraft, which specifically includes:
基于所述临时预警信息，计算得到所述应急航线；Calculate the emergency route based on the temporary early warning information;
基于所述应急航线，调整所述飞行器的航线视景，以将所述应急航线显示在所述飞行器的航线视景中。Based on the emergency route, the aircraft's route view is adjusted to display the emergency route in the aircraft's route view.
具体地，飞行器在航行中难以避免遇到一些紧急情况，本步骤中所指的紧急预警信息包括这些紧急情况，如空管临时调度、前方地面施工干扰、空域临时管制等情况，当发生这类紧急情况时，飞管系统会计算并规划制定最有利的航线指引，即得到应急航线。一旦该应急航线出现后，原有航线视景中的其他元素会根据此应急航线做响应调整，突出显示应急航线。飞管系统还会根据此应急航线引导飞行器进行避障、避害或临时备降等方案，确保飞行器的安全。Specifically, it is difficult for the aircraft to avoid encountering some emergency situations during navigation. The emergency warning information referred to in this step includes these emergency situations, such as temporary air traffic control dispatch, ground construction interference ahead, temporary airspace control, etc. In an emergency, the flight control system will calculate and plan the most favorable route guidance, that is, an emergency route. Once the emergency route appears, other elements in the original route view will be adjusted according to the emergency route, and the emergency route will be highlighted. The flight control system will also guide the aircraft to avoid obstacles, avoid hazards or make temporary backups according to the emergency route to ensure the safety of the aircraft.
本实施例通过上述方案，在飞行器的航线视景中进行应急航线显示，具体通过基于紧急预警信息，计算得到所述应急航线；基于所述应急航线，调整所述飞行器的航线视景，以将所述应急航线显示在所述飞行器的航线视景中。相较于上述实施例，本实施例提出了针对紧急预警信息采取应急航线显示的方案，进一步扩展了本申请方案的应用场景，进一步保障飞行器航行安全，增强了本申请方案的适用性。In this embodiment, through the above solution, the emergency route is displayed in the route view of the aircraft. Specifically, the emergency route is obtained by calculating based on the emergency warning information; based on the emergency route, the route view of the aircraft is adjusted so as to The emergency route is displayed in the aircraft's route view. Compared with the above-mentioned embodiments, the present embodiment proposes a solution for displaying emergency flight routes for emergency warning information, which further expands the application scenarios of the solution of the present application, further ensures the safety of aircraft navigation, and enhances the applicability of the solution of the present application.
此外，本申请实施例还提出一种飞行器预警装置，所述飞行器预警装置包括：In addition, the embodiment of the present application also proposes an aircraft early warning device, and the aircraft early warning device includes:
信息获取模块，用于获取飞行器的航行信息；The information acquisition module is used to acquire the navigation information of the aircraft;
预警判断模块，用于基于所述飞行器的航行信息，进行预警判断，得到预警报告；an early warning judgment module, configured to perform early warning judgment based on the navigation information of the aircraft, and obtain an early warning report;
预警显示模块，用于将所述预警报告加载至预先获取的飞行器航线视景中进行预警。The early warning display module is used for loading the early warning report into the pre-acquired aircraft route view for early warning.
本实施例实现飞行器预警的原理及实施过程，请参照上述各实施例，在此不再赘述。For the principle and implementation process of implementing the aircraft early warning in this embodiment, please refer to the above-mentioned embodiments, which will not be repeated here.
此外，本申请实施例还提出一种终端设备，所述终端设备包括存储器、处理器及存储在所述存储器上并可在所述处理器上运行的飞行器预警程序，所述飞行器预警程序被所述处理器执行时实现如上所述的飞行器预警方法的步骤。In addition, an embodiment of the present application also proposes a terminal device, the terminal device includes a memory, a processor, and an aircraft early warning program stored on the memory and executable on the processor, the aircraft early warning program being The steps of implementing the above-mentioned aircraft early warning method when the processor is executed.
由于本飞行器预警程序被处理器执行时，采用了前述所有实施例的全部技术方案，因此至少具有前述所有实施例的全部技术方案所带来的所有有益效果，在此不再一一赘述。Since the aircraft early warning program is executed by the processor, it adopts all the technical solutions of the foregoing embodiments, and therefore at least has all the beneficial effects brought by all the technical solutions of the foregoing embodiments, and will not be repeated here.
此外，本申请实施例还提出一种计算机可读存储介质，所述计算机可读存储介质上存储有飞行器预警程序，所述飞行器预警程序被处理器执行时实现如上所述的飞行器预警方法的步骤。In addition, an embodiment of the present application also proposes a computer-readable storage medium, where an aircraft early warning program is stored on the computer-readable storage medium, and when the aircraft early warning program is executed by a processor, the steps of the above-mentioned aircraft early warning method are implemented .
由于本飞行器预警程序被处理器执行时，采用了前述所有实施例的全部技术方案，因此至少具有前述所有实施例的全部技术方案所带来的所有有益效果，在此不再一一赘述。Since the aircraft early warning program is executed by the processor, it adopts all the technical solutions of the foregoing embodiments, and therefore at least has all the beneficial effects brought by all the technical solutions of the foregoing embodiments, and will not be repeated here.
为了解决当前飞行员驾驶过程中缺乏有效预警系统的问题，本申请实施例提出的飞行器预警方法、装置、终端设备以及存储介质，通过获取飞行器的航行信息；基于所述飞行器的航行信息进行预警判断，得到预警报告；将所述预警报告加载至预先获取的飞行器航线视景中进行预警。基于本申请方案，针对当下飞行员(或无人驾驶)的过程中缺乏有效预警手段的问题，提出了一种能够对飞行器的航行过程进行有效预警的方案，通过对飞行器的各种信息进行预警判断，生成预警报告并在飞行器航线视景中加载显示，实现了航行中的及时预警，能够辅助飞行员处理航行中的各种情况，从而提高了飞行器航行中的安全性。In order to solve the problem of the lack of an effective early warning system in the current pilot's driving process, the aircraft early warning method, device, terminal device and storage medium proposed in the embodiments of the present application obtain the navigation information of the aircraft; make early warning judgment based on the navigation information of the aircraft, Obtain an early warning report; load the early warning report into the pre-acquired aircraft route vision for early warning. Based on the solution of the present application, aiming at the problem of lack of effective early warning means in the process of current pilots (or unmanned pilots), a scheme that can effectively give early warning to the navigation process of the aircraft is proposed. , generate an early warning report and display it in the aircraft route view, which realizes the timely early warning during the flight, and can assist the pilot to deal with various situations during the flight, thereby improving the safety of the aircraft during the flight.
需要说明的是，在本文中，术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含，从而使得包括一系列要素的过程、方法、物品或者系统不仅包括那些要素，而且还包括没有明确列出的其他要素，或者是还包括为这种过程、方法、物品或者系统所固有的要素。在没有更多限制的情况下，由语句“包括一个……”限定的要素，并不排除在包括该要素的过程、方法、物品或者系统中还存在另外的相同要素。It should be noted that, herein, the terms "comprising", "comprising" or any other variation thereof are intended to encompass non-exclusive inclusion, such that a process, method, article or system comprising a series of elements includes not only those elements, It also includes other elements not expressly listed or inherent to such a process, method, article or system. Without further limitation, an element qualified by the phrase "comprising a..." does not preclude the presence of additional identical elements in the process, method, article or system that includes the element.
上述本申请实施例序号仅仅为了描述，不代表实施例的优劣。The above-mentioned serial numbers of the embodiments of the present application are only for description, and do not represent the advantages or disadvantages of the embodiments.
通过以上的实施方式的描述，本领域的技术人员可以清楚地了解到上述实施例方法可借助软件加必需的通用硬件平台的方式来实现，当然也可以通过硬件，但很多情况下前者是更佳的实施方式。基于这样的理解，本申请的技术方案本质上或者说对现有技术做出贡献的部分可以以软件产品的形式体现出来，该计算机软件产品存储在如上的一个存储介质(如ROM/RAM、磁碟、光盘)中，包括若干指令用以使得一台终端设备(可以是手机，计算机，服务器，被控终端，或者网络设备等)执行本申请每个实施例的方法。From the description of the above embodiments, those skilled in the art can clearly understand that the method of the above embodiment can be implemented by means of software plus a necessary general hardware platform, and of course can also be implemented by hardware, but in many cases the former is better implementation. Based on such understanding, the technical solutions of the present application can be embodied in the form of software products in essence or the parts that make contributions to the prior art, and the computer software products are stored in the above storage medium (such as ROM/RAM, magnetic CD, CD), including several instructions to make a terminal device (which may be a mobile phone, a computer, a server, a controlled terminal, or a network device, etc.) to execute the method of each embodiment of the present application.
以上仅为本申请的优选实施例，并非因此限制本申请的专利范围，凡是利用本申请说明书及附图内容所作的等效结构或等效流程变换，或直接或间接运用在其他相关的技术领域，均同理包括在本申请的专利保护范围内。The above are only the preferred embodiments of the present application, and are not intended to limit the patent scope of the present application. Any equivalent structure or equivalent process transformation made by using the contents of the description and drawings of the present application, or directly or indirectly applied in other related technical fields , are similarly included within the scope of patent protection of this application.
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| CN115435776A (en) * | 2022-11-03 | 2022-12-06 | 成都沃飞天驭科技有限公司 | Method and device for displaying three-dimensional airway route, aircraft and storage medium |
| CN115440091A (en) * | 2022-11-03 | 2022-12-06 | 成都沃飞天驭科技有限公司 | Method and device for displaying route switching views, aircraft and storage medium |
| CN115440092A (en) * | 2022-11-03 | 2022-12-06 | 成都沃飞天驭科技有限公司 | Navigation information display method, device, aircraft and storage medium |
| CN115691230A (en) * | 2022-11-03 | 2023-02-03 | 成都沃飞天驭科技有限公司 | Flight display method and device, aircraft and storage medium |
| CN116052482A (en) * | 2023-04-03 | 2023-05-02 | 中航信移动科技有限公司 | Method, electronic device and storage medium for early warning of aircraft trajectory deviation |
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