CN114360298A - Low-altitude airspace ground supervision service system - Google Patents
Low-altitude airspace ground supervision service system Download PDFInfo
- Publication number
- CN114360298A CN114360298A CN202111568135.4A CN202111568135A CN114360298A CN 114360298 A CN114360298 A CN 114360298A CN 202111568135 A CN202111568135 A CN 202111568135A CN 114360298 A CN114360298 A CN 114360298A
- Authority
- CN
- China
- Prior art keywords
- navigation
- aircraft
- label information
- determining
- airplane
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000005516 engineering process Methods 0.000 claims abstract description 28
- 238000012544 monitoring process Methods 0.000 claims abstract description 24
- 230000004044 response Effects 0.000 claims abstract description 23
- 238000004891 communication Methods 0.000 claims abstract description 12
- 230000008859 change Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 5
- 238000013500 data storage Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 18
- 230000000007 visual effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 13
- 238000003860 storage Methods 0.000 description 12
- 238000004590 computer program Methods 0.000 description 9
- 230000008569 process Effects 0.000 description 8
- 230000006870 function Effects 0.000 description 6
- 238000012545 processing Methods 0.000 description 4
- 230000003287 optical effect Effects 0.000 description 3
- 238000012217 deletion Methods 0.000 description 2
- 230000037430 deletion Effects 0.000 description 2
- 238000007726 management method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000012800 visualization Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 210000004556 brain Anatomy 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Landscapes
- Traffic Control Systems (AREA)
Abstract
The embodiment of the invention provides a low-altitude airspace ground supervision service system, and belongs to the technical field of ground supervision based on Beidou communication. The method comprises the following steps: the interface display module is used for displaying a map of an area to be monitored; determining the position of the navigation airplane on the map according to the label information and displaying the label information on the position; displaying a trajectory of the navigable aircraft on the map, and enabling playback of the trajectory of the navigable aircraft in response to a selection operation by a user; the data communication module is used for determining that any one of the Beidou short message technology terminal and the Beidou RNSS and RDSS technology terminals receives the label information of the navigation airplane; the monitoring and commanding scheduling module is used for determining a recommended scheduling strategy for the navigation aircraft according to the label information of the navigation aircraft and the received environment information; and determining an actual scheduling strategy of the navigation airplane. The invention can realize the supervision and control of the navigation aircraft, realize the visual effect of the ground and ensure that the navigation aircraft completes the task.
Description
Technical Field
The invention relates to the technical field of ground supervision based on Beidou communication, in particular to a low-altitude airspace ground supervision service system.
Background
The low-altitude airspace supervision service platform based on the core technology and equipment of the domestic Beidou satellite is a set of monitoring system which adopts the integrated, standardized and modularized communication, navigation and monitoring technology, aims at a certain type of general aviation operation tasks, realizes remote command and monitoring on the affiliated airplane by a ground monitoring center, and performs unified management and scheduling so as to improve the efficiency of general aviation operation. The low-altitude airspace supervision service platform based on the core technology and equipment of the domestic Beidou satellite can comprise the Beidou satellite and a communication network thereof, a ground monitoring command center terminal and a general aircraft Beidou airborne terminal according to the composition division.
At present, the ground monitoring command center is the most important part of the platform, and is the brain for realizing the command and monitoring task of the navigation aircraft. At present, a ground monitoring center in a low-altitude airspace is always blank, so that how to ensure the efficiency of ground monitoring and ensure that a navigation aircraft completes an operation task is a problem which needs to be solved urgently in the present stage.
Disclosure of Invention
The embodiment of the invention aims to provide a low-altitude airspace ground supervision service system which can realize supervision and control of a navigation aircraft, realize a ground visualization effect and ensure that the navigation aircraft completes tasks.
In order to achieve the above object, an embodiment of the present invention provides a low-altitude airspace ground monitoring service system, where the low-altitude airspace ground monitoring service system includes:
the interface display module is used for displaying a map of an area to be monitored; wherein the map is configured to be capable of performing a hierarchical presentation in response to a user's operation; receiving label information from a navigation aircraft, determining the position of the navigation aircraft on the map according to the label information, and displaying the label information on the position; displaying a trajectory of the navigable aircraft on the map, and enabling playback of the trajectory of the navigable aircraft to be performed in response to a selection operation by a user;
the data communication module is used for determining that any one of a Beidou short message technology terminal and a Beidou RNSS and RDSS technology terminal is used for receiving the label information of the navigation airplane;
the monitoring and commanding scheduling module is used for determining a recommended scheduling strategy for the navigation aircraft according to the label information of the navigation aircraft and the received environment information; and determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user for the recommended scheduling strategy.
Preferably, the interface display module includes:
the marking sub-module is used for marking an operation target point, an operation area and a dangerous area of the navigation aircraft on the map;
the airplane label submodule is used for receiving label information of the navigable airplane and responding to selection operation of a user on a label information display control to display the selected label information of the navigable airplane on the map; the label information comprises a model, an airplane speed, a target airport, a flight type, a track number, a wake flow, an instruction height and a height change rate;
a trajectory display submodule for:
determining the track display effect of the navigation aircraft according to the judgment result of whether the flight of the navigation aircraft belongs to the traffic plan, and determining the display color of the navigation aircraft on the map according to the working state of the navigation aircraft;
determining a playback strategy for the track of the navigable aircraft in response to a user selection operation for a control of the playback track strategy.
Preferably, the playback track policy includes: a track playback strategy selected according to the aircraft track number, a track playback strategy selected according to the time period, and a track playback strategy selected according to the speed.
Preferably, the trajectory display sub-module is further configured to display a trajectory for playing back the navigable aircraft in response to a user-selected trajectory playback speed of the navigable aircraft.
Preferably, the data communication module includes:
the acquisition submodule is used for acquiring the type of the label information;
and the receiving end determining submodule is used for determining the Beidou short message technology terminal and one of the Beidou RNSS and RDSS technology terminals according to the type of the label information so as to receive the label information of the navigation airplane.
Preferably, the receiving end determining sub-module is configured to:
when the label information is airplane speed and instruction height, determining the Beidou short message technology terminal to receive the label information;
and when the label information relates to encrypted information, determining the Beidou RNSS and RDSS technology terminals to receive the label information.
Preferably, the monitoring and commanding dispatch module comprises:
the corresponding relation determining submodule is used for acquiring the corresponding relation between the label information and the environment information of the navigation aircraft and the recommended scheduling strategy;
the current strategy determining submodule is used for determining a current recommended scheduling strategy corresponding to the current label information and the received current environment information according to the corresponding relation; and
and the actual strategy determining submodule is used for responding to the selection operation of the user aiming at the current recommended scheduling strategy and determining the actual scheduling strategy of the navigation airplane.
Preferably, the policy determination sub-module is configured to, in response to a user selection operation for the currently recommended scheduling policy, determine an actual scheduling policy of the navigable aircraft, including:
the policy determination submodule is configured to:
displaying a selection display control of the current recommended scheduling strategy;
and determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user aiming at the current recommended scheduling strategy.
Preferably, the low-altitude airspace ground supervision service system further includes: and the data storage module is used for storing the label information of the navigation airplane.
Preferably, the low-altitude airspace ground supervision service system further includes: and the track prediction module is used for predicting the target track of the navigation aircraft according to the running track of the navigation aircraft.
By the technical scheme, the ground supervision service system is used for remotely commanding and monitoring the aircraft to which the ground supervision service system belongs aiming at the operation tasks of a certain type of general aviation, and unified scheduling and management are carried out on the aircraft to improve the efficiency of general aviation operation. The invention realizes the friendly display of the whole interface and the interface parameter setting thereof through the interface display module. The displayed information comprises a map, a label, track display, playback and the like, so that the ground visualization effect is realized, and the navigation aircraft is ensured to complete tasks.
Additional features and advantages of embodiments of the invention will be set forth in the detailed description which follows.
Drawings
The accompanying drawings, which are included to provide a further understanding of the embodiments of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the embodiments of the invention without limiting the embodiments of the invention. In the drawings:
FIG. 1 is a block diagram illustrating a low-altitude airspace ground surveillance service system of the present invention;
FIG. 2 is a block diagram illustrating an interface display module of the present invention;
FIG. 3 is a block diagram illustrating a data communication module of the present invention;
FIG. 4 is a block diagram illustrating a monitoring and command scheduling module of the present invention; and
fig. 5 is a flow chart illustrating a track playback process of the present invention.
Detailed Description
The following detailed description of embodiments of the invention refers to the accompanying drawings. It should be understood that the detailed description and specific examples, while indicating embodiments of the invention, are given by way of illustration and explanation only, not limitation.
Fig. 1 is a block diagram of a low-altitude airspace ground supervision service system according to the present invention, and as shown in fig. 1, the low-altitude airspace ground supervision service system includes:
the interface display module is used for displaying a map of an area to be monitored; wherein the map is configured to be capable of performing a hierarchical presentation in response to a user's operation; receiving label information from a navigation aircraft, determining the position of the navigation aircraft on the map according to the label information, and displaying the label information on the position; displaying a trajectory of the navigable aircraft on the map, and enabling playback of the trajectory of the navigable aircraft to be performed in response to a selection operation by a user; the interface display module can realize friendly display of the whole interface, interface parameter setting and the like, including whole map display, airplane label information, track display, playback and the like. On the interface, a map of the whole situation of china needs to be displayed, but since aerial surveillance of a navigation plane is different from general land vehicle surveillance, a simple map is often needed, and therefore, it is considered that a specific functional structure of the map is drawn by itself by means of OPENGL drawing technology as shown in fig. 2.
1) The normal display of the map initially comprises names of 34 provinces and autonomous regions in China;
2) in order to make the display of the map more standard and be used as a basic reference of the flight position of the navigation airplane in the flight process, some basic China urban and rural position points need to be set, and layered display is realized as a selectable item for displaying selectively at any time;
3) besides normal display, the map also needs to be capable of realizing basic operation on the map, and the rolling of a mouse can realize enlargement, reduction, dragging or addition and deletion of graphic elements;
4) in addition, marks need to be made on the operating target point, the operating area and the dangerous area of the navigation aircraft, such as text editing addition, flag special marks, straight lines, circles, solid circles, circular arcs, squares, triangles and the like, and the functions require that the graphic mark data addition, the data backup and storage, the data deletion, the graphic display and temporary hiding and the like are realized.
The data communication module is used for determining that any one of a Beidou short message technology terminal and a Beidou RNSS and RDSS technology terminal is used for receiving the label information of the navigation airplane;
the monitoring and commanding scheduling module is used for determining a recommended scheduling strategy for the navigation aircraft according to the label information of the navigation aircraft and the received environment information; and determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user for the recommended scheduling strategy.
Preferably, as shown in fig. 2, the interface display module includes:
the marking sub-module is used for marking an operation target point, an operation area and a dangerous area of the navigation aircraft on the map;
the airplane label submodule is used for receiving label information of the navigable airplane and responding to selection operation of a user on a label information display control to display the selected label information of the navigable airplane on the map; the label information comprises a model, an airplane speed, a target airport, a flight type, a track number, a wake flow, an instruction height and a height change rate;
in order to better and intuitively view simple information for monitoring a navigable aircraft on an operator interface of a ground command center system, the aircraft label information is generally provided on an air traffic control system. Such information includes the information described above.
1) The airplane signage information is displayed on a map, typically in a rectangular box with a border comprising the information described above. The navigation aircraft track symbol can be moved along with the navigation aircraft when new position information of the navigation aircraft is received;
2) in order to prevent the overlap of the navigation track symbols, the airplane label can move freely, and the method is generally realized by clicking a right mouse button and dragging the airplane label;
3) the types of airplane label display are set and are divided into standard types and expansibility. The standard type comprises a track number or a national registration number, a wake flow, an altitude change prompt, a real-time altitude, a command altitude, an airplane speed and extended type information, and the standard type comprises all information of the standard type, a landing airport and a airplane type. The sign guiding line is a connecting line between the navigation track symbol and the airplane sign. The system is provided with three types, namely a short type, a Chinese type and a long type, and the length is 2, 4 and 6 in sequence, and the unit is centimeter.
A trajectory display submodule for:
determining the track display effect of the navigation aircraft according to the judgment result of whether the flight of the navigation aircraft belongs to the traffic plan, and determining the display color of the navigation aircraft on the map according to the working state of the navigation aircraft;
determining a playback strategy for the track of the navigable aircraft in response to a user selection operation for a control of the playback track strategy.
In the invention, for the sake of simplicity, the problem of complex airplane flight attitude is not considered, the airplane track is only displayed on the two-dimensional map, and the simpler basic graph is adopted as the flight track symbol of the navigation airplane in the flight process. The tracklets are represented by filled triangles at the initial stage of the navigation of the aircraft, i.e., when no correlation from the basic flight plan information is made to the aircraft; the hollow square representation is adopted when the flight plan of the navigation aircraft is related manually or automatically by the system in the ground command and monitoring system. Meanwhile, due to the superior-inferior relation of the sun shading of the commanding machine and the civil air defense handset, the ground commanding and monitoring system is called to monitor the subordinate navigation aircraft. Thus, a navigable aircraft has only three basic states: the method comprises the steps of initial, task execution and task completion, wherein the three states correspond to yellow, magenta and cyan one by one.
The basic requirement of track playback is to enable the monitoring decision-making personnel to call the track number before at any time to reproduce the flight process of the navigation airplane for the reference of the decision-making personnel. More specifically, different monitoring environments and monitoring entities need to be considered.
Preferably, the playback track policy includes: a track playback strategy selected according to the aircraft track number, a track playback strategy selected according to the time period, and a track playback strategy selected according to the speed.
Preferably, the trajectory display sub-module is further configured to display a trajectory for playing back the navigable aircraft in response to a user-selected trajectory playback speed of the navigable aircraft. The flow of the track playback is shown in fig. 5.
1) According to the number of airplanes: the number of the navigation airplanes can be selectively selected according to the airplane track number; and full selection, namely carrying out aircraft playback on all airplanes under the commander, and carrying out playback operation on single-gate aircrafts and multiple-selection aircrafts.
2) Playback according to time: the time playback is to select a certain time period required for the track playback in a manner of year, month, day, hour, minute and second.
3) Playback in speed: and inquiring historical track data according to a certain flight speed, and then reproducing the track on the electronic map.
In addition, the flying speed can be selected according to 1, 2, 3, 5 and 10 times.
Preferably, as shown in fig. 3, the data communication module includes: the acquisition submodule is used for acquiring the type of the label information; and the receiving end determining submodule is used for determining the Beidou short message technology terminal and one of the Beidou RNSS and RDSS technology terminals according to the type of the label information so as to receive the label information of the navigation airplane.
The Beidou short message technology is adopted to encode information such as airplane speed, command altitude and the like into a special position information message pattern, and then the position information message pattern is directly transmitted to the commander through a Beidou first-generation passing satellite.
The Beidou RDSS + RNSS technologies can form a subordinate membership relationship through a specific IC card of the Beidou system. It is this membership that makes the system simple in solving the information reception problem. Generally, after the commander and the airborne Beidou terminal are provided with the Beidou IC card, the ID written in the IC card forms the superior-inferior relation between the card and the card.
Preferably, the receiving end determining sub-module is configured to:
when the label information is airplane speed and instruction height, determining the Beidou short message technology terminal to receive the label information;
and when the label information relates to encrypted information, determining the Beidou RNSS and RDSS technology terminals to receive the label information.
Preferably, as shown in fig. 4, the monitoring and commanding scheduling module includes: the corresponding relation determining submodule is used for acquiring the corresponding relation between the label information and the environment information of the navigation aircraft and the recommended scheduling strategy; the current strategy determining submodule is used for determining a current recommended scheduling strategy corresponding to the current label information and the received current environment information according to the corresponding relation; and the actual strategy determination submodule is used for determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user aiming at the current recommended scheduling strategy.
The invention realizes the dispatching and commanding functions of the navigation aircraft cluster, and comprehensively considers the factors of the task state, the flight range, the maintenance fault, the oil quantity, the number of people on board, the type, the weather and the like of the current aircraft. And determining a reasonable model or a navigation plane to execute the task according to the playing relation between the environment information and the sign information and the recommended scheduling strategy.
Preferably, the policy determination sub-module is configured to, in response to a user selection operation for the currently recommended scheduling policy, determine an actual scheduling policy of the navigable aircraft, including:
the policy determination submodule is configured to:
displaying a selection display control of the current recommended scheduling strategy;
and determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user aiming at the current recommended scheduling strategy.
Preferably, the low-altitude airspace ground supervision service system further includes: and the data storage module is used for storing the label information of the navigation airplane.
Preferably, the low-altitude airspace ground supervision service system further includes: and the track prediction module is used for predicting the target track of the navigation aircraft according to the running track of the navigation aircraft.
As will be appreciated by one skilled in the art, embodiments of the present application may be provided as a method, system, or computer program product. Accordingly, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present application may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
The present application is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the application. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
In a typical configuration, a computing device includes one or more processors (CPUs), input/output interfaces, network interfaces, and memory.
The memory may include forms of volatile memory in a computer readable medium, Random Access Memory (RAM) and/or non-volatile memory, such as Read Only Memory (ROM) or flash memory (flash RAM). The memory is an example of a computer-readable medium.
Computer-readable media, including both non-transitory and non-transitory, removable and non-removable media, may implement information storage by any method or technology. The information may be computer readable instructions, data structures, modules of a program, or other data. Examples of computer storage media include, but are not limited to, phase change memory (PRAM), Static Random Access Memory (SRAM), Dynamic Random Access Memory (DRAM), other types of Random Access Memory (RAM), Read Only Memory (ROM), Electrically Erasable Programmable Read Only Memory (EEPROM), flash memory or other memory technology, compact disc read only memory (CD-ROM), Digital Versatile Discs (DVD) or other optical storage, magnetic cassettes, magnetic tape magnetic disk storage or other magnetic storage devices, or any other non-transmission medium that can be used to store information that can be accessed by a computing device. As defined herein, a computer readable medium does not include a transitory computer readable medium such as a modulated data signal and a carrier wave.
It should also be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in the process, method, article, or apparatus that comprises the element.
As will be appreciated by one skilled in the art, embodiments of the present application may be provided as a method, system, or computer program product. Accordingly, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present application may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
The above are merely examples of the present application and are not intended to limit the present application. Various modifications and changes may occur to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the scope of the claims of the present application.
Claims (10)
1. A low-altitude airspace ground supervision service system, comprising:
the interface display module is used for displaying a map of an area to be monitored; wherein the map is configured to be capable of performing a hierarchical presentation in response to a user's operation; receiving label information from a navigation aircraft, determining the position of the navigation aircraft on the map according to the label information, and displaying the label information on the position; displaying a trajectory of the navigable aircraft on the map, and enabling playback of the trajectory of the navigable aircraft to be performed in response to a selection operation by a user;
the data communication module is used for determining that any one of a Beidou short message technology terminal and a Beidou RNSS and RDSS technology terminal is used for receiving the label information of the navigation airplane;
the monitoring and commanding scheduling module is used for determining a recommended scheduling strategy for the navigation aircraft according to the label information of the navigation aircraft and the received environment information; and determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user for the recommended scheduling strategy.
2. The low-altitude airspace ground supervision service system according to claim 1, wherein the interface display module includes:
the marking sub-module is used for marking an operation target point, an operation area and a dangerous area of the navigation aircraft on the map;
the airplane label submodule is used for receiving label information of the navigable airplane and responding to selection operation of a user on a label information display control to display the selected label information of the navigable airplane on the map; the label information comprises a model, an airplane speed, a target airport, a flight type, a track number, a wake flow, an instruction height and a height change rate;
a trajectory display submodule for:
determining the track display effect of the navigation aircraft according to the judgment result of whether the flight of the navigation aircraft belongs to the traffic plan, and determining the display color of the navigation aircraft on the map according to the working state of the navigation aircraft;
determining a playback strategy for the track of the navigable aircraft in response to a user selection operation for a control of the playback track strategy.
3. The low-altitude airspace ground administration service system according to claim 2, wherein the playback trajectory policy includes: a track playback strategy selected according to the aircraft track number, a track playback strategy selected according to the time period, and a track playback strategy selected according to the speed.
4. The low-altitude airspace ground surveillance service system of claim 2, wherein the trajectory display sub-module is further configured to show a trajectory for playing back the navigable aircraft in response to a user-selected trajectory playback speed of the navigable aircraft.
5. The low-altitude airspace ground supervision service system according to claim 1, wherein the data communication module includes:
the acquisition submodule is used for acquiring the type of the label information;
and the receiving end determining submodule is used for determining the Beidou short message technology terminal and one of the Beidou RNSS and RDSS technology terminals according to the type of the label information so as to receive the label information of the navigation airplane.
6. The low-altitude airspace ground supervision service system according to claim 5, wherein the receiving end determination submodule is configured to:
when the label information is airplane speed and instruction height, determining the Beidou short message technology terminal to receive the label information;
and when the label information relates to encrypted information, determining the Beidou RNSS and RDSS technology terminals to receive the label information.
7. The low-altitude airspace ground supervision service system according to claim 1, wherein the monitoring and commanding scheduling module includes:
the corresponding relation determining submodule is used for acquiring the corresponding relation between the label information and the environment information of the navigation aircraft and the recommended scheduling strategy;
the current strategy determining submodule is used for determining a current recommended scheduling strategy corresponding to the current label information and the received current environment information according to the corresponding relation; and
and the actual strategy determining submodule is used for responding to the selection operation of the user aiming at the current recommended scheduling strategy and determining the actual scheduling strategy of the navigation airplane.
8. The low-altitude airspace ground surveillance service system of claim 7, wherein the policy determination sub-module, in response to a user selection operation for the current recommended scheduling policy, is configured to determine an actual scheduling policy of the navigable aircraft including:
the policy determination submodule is configured to:
displaying a selection display control of the current recommended scheduling strategy;
and determining the actual scheduling strategy of the navigation airplane in response to the selection operation of the user aiming at the current recommended scheduling strategy.
9. The low-altitude airspace ground supervision service system according to claim 1, wherein the low-altitude airspace ground supervision service system further includes: and the data storage module is used for storing the label information of the navigation airplane.
10. The low-altitude airspace ground supervision service system according to claim 1, wherein the low-altitude airspace ground supervision service system further includes: and the track prediction module is used for predicting the target track of the navigation aircraft according to the running track of the navigation aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111568135.4A CN114360298A (en) | 2021-12-21 | 2021-12-21 | Low-altitude airspace ground supervision service system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111568135.4A CN114360298A (en) | 2021-12-21 | 2021-12-21 | Low-altitude airspace ground supervision service system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114360298A true CN114360298A (en) | 2022-04-15 |
Family
ID=81100749
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111568135.4A Pending CN114360298A (en) | 2021-12-21 | 2021-12-21 | Low-altitude airspace ground supervision service system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114360298A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114842679A (en) * | 2022-04-20 | 2022-08-02 | 中国民用航空总局第二研究所 | Recording and playback method and system for airport scene track data |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103578300A (en) * | 2013-11-06 | 2014-02-12 | 华北计算技术研究所 | Network-oriented low-altitude flight dynamically monitoring system |
| CN103809600A (en) * | 2014-03-04 | 2014-05-21 | 北京航空航天大学 | Human-machine interaction control system of unmanned airship |
| CN203786910U (en) * | 2014-04-29 | 2014-08-20 | 北京威胜通达科技有限公司 | Beidou low-altitude flight monitoring system |
| CN105676249A (en) * | 2016-04-20 | 2016-06-15 | 中国民航大学 | Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS |
| CN107356940A (en) * | 2017-08-11 | 2017-11-17 | 四川联丰云网科技有限公司 | Low-altitude surveillance system based on Beidou satellite communication |
| CN107591035A (en) * | 2017-09-15 | 2018-01-16 | 山东东进航空科技有限公司 | Aircraft based on digital identity identification integrates management and control system and method |
| CN107808551A (en) * | 2017-10-30 | 2018-03-16 | 中国民航大学 | A kind of General Aviation operation monitoring system and its monitoring method based on the Big Dipper |
| CN207652583U (en) * | 2017-12-11 | 2018-07-24 | 西安航空电子科技有限公司 | A kind of low-altitude surveillance system |
| CN110060515A (en) * | 2019-04-19 | 2019-07-26 | 中国航空无线电电子研究所 | A kind of aircraft monitoring system and method based on GNSS |
-
2021
- 2021-12-21 CN CN202111568135.4A patent/CN114360298A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103578300A (en) * | 2013-11-06 | 2014-02-12 | 华北计算技术研究所 | Network-oriented low-altitude flight dynamically monitoring system |
| CN103809600A (en) * | 2014-03-04 | 2014-05-21 | 北京航空航天大学 | Human-machine interaction control system of unmanned airship |
| CN203786910U (en) * | 2014-04-29 | 2014-08-20 | 北京威胜通达科技有限公司 | Beidou low-altitude flight monitoring system |
| CN105676249A (en) * | 2016-04-20 | 2016-06-15 | 中国民航大学 | Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS |
| CN107356940A (en) * | 2017-08-11 | 2017-11-17 | 四川联丰云网科技有限公司 | Low-altitude surveillance system based on Beidou satellite communication |
| CN107591035A (en) * | 2017-09-15 | 2018-01-16 | 山东东进航空科技有限公司 | Aircraft based on digital identity identification integrates management and control system and method |
| CN107808551A (en) * | 2017-10-30 | 2018-03-16 | 中国民航大学 | A kind of General Aviation operation monitoring system and its monitoring method based on the Big Dipper |
| CN207652583U (en) * | 2017-12-11 | 2018-07-24 | 西安航空电子科技有限公司 | A kind of low-altitude surveillance system |
| CN110060515A (en) * | 2019-04-19 | 2019-07-26 | 中国航空无线电电子研究所 | A kind of aircraft monitoring system and method based on GNSS |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114842679A (en) * | 2022-04-20 | 2022-08-02 | 中国民用航空总局第二研究所 | Recording and playback method and system for airport scene track data |
| CN114842679B (en) * | 2022-04-20 | 2023-03-03 | 中国民用航空总局第二研究所 | Recording and playback method and system for airport scene track data |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11024181B2 (en) | Systems and methods for generating avionic displays including forecast overpressure event symbology | |
| EP3144638B1 (en) | Flight deck display systems and methods for generating cockpit displays including dynamic taxi turnoff icons | |
| US8209122B2 (en) | System and method for rendering visible features of a target location on a synthetic flight display | |
| CN102682628B (en) | General aviation operation monitoring system | |
| US7742847B2 (en) | Method and system for context sensitive aircraft navigation | |
| US9153137B2 (en) | Temporally based weather symbology | |
| US9041560B2 (en) | System and method of displaying a runway temporarily displaced threshold and an aircraft landing aiming point | |
| US20160232797A1 (en) | Methods and systems for dynamically providing contextual weather information | |
| US20170183105A1 (en) | Display of meteorological data in aircraft | |
| US8660719B2 (en) | Four-dimensional flyable area display system for aircraft | |
| CN103714719B (en) | Based on the Flight navigational system of Beidou satellite navigation | |
| CN105448138B (en) | Aircraft system and method for displaying spacing information | |
| CN111781951A (en) | Industrial park monitoring and data visualization system based on cluster unmanned aerial vehicle | |
| EP2821752B1 (en) | System and method for producing and submitting a pirep | |
| US20120035849A1 (en) | Data Driven Route Strip | |
| CN105890622A (en) | Cockpit display systems and methods for generating navigation displays including landing diversion symbology | |
| US9168859B2 (en) | System and method for displaying visual flight reference points | |
| CN105139606A (en) | Low-altitude aircraft information interaction system | |
| US9875659B2 (en) | System and method for exocentric display of integrated navigation | |
| CN114360298A (en) | Low-altitude airspace ground supervision service system | |
| US20220383761A1 (en) | Dynamic navigation procedures | |
| US20230230490A1 (en) | System and method for better determining path parameters of aircrafts | |
| EP3940673A1 (en) | Systems and methods for presenting environment information on a mission timeline | |
| JP2024045933A (en) | Flight information presentation system, flight information presentation method and program | |
| Farrell Jr et al. | 14 th ICCRTS C2 and Agility Weather Effects Embedded within Net-Centric C2 System Workflows |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20220415 |