CN204856925U - Low -latitude flying ware developments monitoring system - Google Patents
Low -latitude flying ware developments monitoring system Download PDFInfo
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- CN204856925U CN204856925U CN201520560545.8U CN201520560545U CN204856925U CN 204856925 U CN204856925 U CN 204856925U CN 201520560545 U CN201520560545 U CN 201520560545U CN 204856925 U CN204856925 U CN 204856925U
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Abstract
An embodiment of the utility model discloses a low -latitude flying ware developments monitoring system, include: positioner for send positioning data to the aircraft, airborne terminal for utilize positioner to confirm its exact position, through the flight information of radio communication net to surface equipment broadcasting aircraft, and the data of receiving other aircraft that surface equipment sent, analyze the data of receiving, surface equipment for the control of real -time situation is carried out to the aircraft to the information that the airborne terminal that receives each aircraft sent, and the possible flight risk of analysis goes upward the broadcasting issue and provides and prevents bumping against alarm information, the machine carries mutual equipment for connect with airborne terminal, show the real -time situation data and the alarm information of each aircraft. Through the utility model discloses, be favorable to the management of proper implementation airspace management and flow, improve operational economy, improve the airspace utilization efficiency to fundamentally has improved navigation flight safety nature.
Description
Technical field
The utility model relates to monitoring field, particularly relates to a kind of low flyer dynamic surveillance system.
Background technology
Along with the development of technology, the application of General Aviation also more comes also extensive, and General Aviation Development, spatial domain opening is crucial.Spatial domain not opening, general-purpose aircraft just cannot go up to the air flight smoothly, and the work in every of General Aviation also just cannot advance.The main difficulty that current low altitude airspace administrative reform faces is: the open contradiction in air defence safety and low latitude, spatial domain MRP on the open impact of low altitude airspace, legal liabilities define exist lack, operational management system is unsound, fly and serve guarantee condition imperfection.Different from external General Aviation operation monitoring pattern, China is the country highly set up defences, and surrounding enviroment are complicated, and there is again numerous important restricted areas some areas, the pressure of air defence safety is very large, and the monitoring of low, slow, the little airbound target of General Aviation is most important to aviation safety.In general, air traffic control means are also relatively backward, therefore, explore the scientific and effective navigation regulatory format building and be applicable to, by Erecting and improving statutory standard, carry out general aviation aircraft and airborne equipment mechanism of permitting the entrance, and set up automatic real time monitoring mechanism, set up the oversight mechanism of effective air defence safety and flight safety, be very important.
Utility model content
In view of this, the utility model discloses a kind of low flyer dynamic surveillance system, improve spatial domain utilization ratio, improve Flight security.
The utility model discloses a kind of low flyer dynamic surveillance system, comprising:
Locating device, for sending locator data to aircraft;
Airborne Terminal, for utilizing locating device to determine its exact position, by the flight information of wireless communication networks device broadcasts aircraft earthward, and receiving the data of other aircraft that uphole equipment sends, resolving the data received;
Uphole equipment, the information that the Airborne Terminal for receiving each aircraft sends, carry out real-time situation monitoring to aircraft, analyze possible flight risk, upstream broadcast is issued and is provided anti-collision warning message;
The real-time situation data of each aircraft and warning message, for being connected with Airborne Terminal, are shown by airborne interactive device.
Optionally, described Airborne Terminal periodically sends apply for information, closes on the position of aircraft, orientation, relative height and distance in order to inquiry, and according to close on the position of aircraft, orientation, relative height and distance calculate close on aircraft close on value;
When described close on value be less than predetermined threshold value time, described Airborne Terminal sends alerting signal.
Optionally, described locating device is big-dipper satellite positioning system or gps satellite positioning system.
Optionally, described Airborne Terminal is ADS-B equipment, and described ADS-B equipment is determined the accurate location on its aloft/ground, in conjunction with after other data, positional information sent to operational support and service centre by aviation wireless private network after receiving the Big Dipper/gps signal.
Optionally, the flight information of described aircraft comprises: the flight path of the height of the position of aircraft, the flying speed of aircraft, aircraft, the flight trend of aircraft, aircraft.
Optionally, described uphole equipment comprises cloud computing center, and described cloud computing center can carry out real-time multidimensional space data and calculate, and the result that data calculate is used for immediately adjusting foundation for the aircraft of each course movement provides.
Optionally, the result that described data calculate is used for immediately adjusting foundation for the aircraft of each course movement provides, and comprising:
For the landing of aircraft under bad weather condition provides safe basis; And
For flight path and the backup flight path of the foggy regional aircraft calculation optimization in many mountains.
Optionally, described system also comprises low latitude integrated supervision unit, and described low latitude integrated supervision unit is made up of one or more subfilter and a fusion center;
Described subfilter receives all kinds of monitoring data, and adopts Kalman filtering to carry out filtering process to every class monitoring data, forms local tracks;
Described fusion center receives the local tracks after each subfilter process, and adopts without resetting federal blending algorithm, forms system flight path.
Optionally, described system also comprises ADS-B land station, and described ADS-B land station is made up of ADS-B receiver hardware module, signal processing software module and network management system three part;
Described ADS-B land station is the network architecture of all-IP, utilize modular design, double reception passage, Hot Spare mode improve stiffness of system, remote network management is adopted to realize remote radio frequency self-inspection, the Long-distance Control of ADS-B land station, to realize ADS-B land station unmanned.
Optionally, described airborne interactive device is connected with airborne wireless communication terminal, for General Aviation mobile interchange, information interaction by wireless or wired mode;
Described airborne interactive device has supervision navigation, integrated information service, flight planning service, weather information, value-added service function.
By low flyer dynamic surveillance system of the present utility model, the information such as the identification number of aircraft, position, trend, flight path can be sent to operational support and service centre by Airborne Terminal in real time.Compare conventional radar to monitor, General Aviation wireless private network in the utility model can provide supervision target and report refresh rate faster, the flight path of location/velocity information more accurately, be conducive to larger lifting track Calculation degree of accuracy, be supplied to controller's more exact trajectory display, for the decision-making of controller provides strong support, ensure the security in field, low latitude.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
The structural drawing of a kind of low flyer dynamic surveillance system that Fig. 1 provides for the utility model embodiment;
The General Aviation private network function that Fig. 2 provides for the utility model embodiment and structural representation;
The structural drawing of the mobile system that Fig. 3 provides for the utility model embodiment;
The low latitude integrated supervision cell data processing flow chart that Fig. 4 provides for the utility model embodiment.
Embodiment
Below in conjunction with accompanying drawing, the utility model embodiment is described in detail.
Should be clear and definite, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making other embodiments all obtained under creative work prerequisite, all belong to the scope of the utility model protection.
The structural drawing of a kind of low flyer dynamic surveillance system that Fig. 1 provides for the utility model embodiment.This dynamic surveillance system comprises locating device, Airborne Terminal, uphole equipment and airborne interactive device.
Locating device, for sending locator data to aircraft, positioning system can ensure at any time, and on the earth, any point can observe satellite simultaneously, to ensure that satellite can collect longitude and latitude and the height of this observation station, to realize the functions such as navigation, location, time service.This can be used for vector aircraft safety, exactly along selected route, arrive punctually at the destination.
Locating device can provide following information: (1) coordinate (Coordinate), has two and three dimensions two kinds of representations; (2) road sign (Landmarkorwaypoint), this is a coordinate figure of GPS internal memory; (3) route (Route), route is the one group of data stored in GPS internal memory, comprises the coordinate of a starting point and a terminal, can also comprise the coordinate of some intermediate points, and the line segment between every two coordinates is one leg; (4) working direction (Heading), GPS does not have the function of north arrow, does not know direction during transfixion; (5) (Bearing) is led; (6) sun set/raise time (Sunset/raisetime); (7) plot trail (Plottrail).Aircraft can receive above-mentioned information, and completes the functions such as location, navigation based on above-mentioned information.
Locating device comprises and being not limited to: GPS (GPS), glonass system, Galileo system, dipper system.
Airborne Terminal, for utilizing locating device to determine its exact position, by the flight information of wireless communication networks device broadcasts aircraft earthward, and receiving the data of other aircraft that uphole equipment sends, resolving the data received.
Airborne Terminal, primarily of the part such as broadband wireless communications unit, the Big Dipper/GPS navigation unit composition, supports that external audio frequency exports and display device.Airborne Terminal basic composition block diagram as shown in Figure 2.
As an embodiment, Airborne Terminal has following characteristic:
(1) environmental suitability, reliability, Electro Magnetic Compatibility etc. follow DO160G standard, need by the test of coherent detection mechanism;
(2) internal integration 1 1800M5M terminal, maximum traffic handling capacity 10bps;
(3) terminal uses the high-power transmitter module of 40dBm, meets vacant lot and covers demand at a distance;
(4) terminal can utilize the Big Dipper/GPS to provide position, velocity information are carried out Doppler shift estimation, auxiliaryly to be switched;
(5) pps pulse per second signal that terminal utilizes the Big Dipper/GPS to provide is calibrated local crystal oscillator frequency drift;
(6) use two higher width antennas of front and back isolation ratio to point to former and later two directions respectively, switch by antenna and reduce non-direct projection footpath energy, improve co-channel interference, improve performance of handoffs etc.
Uphole equipment, the information that the Airborne Terminal for receiving each aircraft sends, carry out real-time situation monitoring to aircraft, analyze possible flight risk, upstream broadcast is issued and is provided anti-collision warning message;
The airborne locating information of uphole equipment by receiving, and carry out fuzzy matching with flight planning, accurate grasp thru-flight device situation, real-time situation supervision is carried out to Flight device, meets monitoring side and the real-time flight situation of common aero vehicle is carried out monitoring to ensure air defence security needs.
The real-time situation data of each aircraft and warning message, for being connected with Airborne Terminal, are shown by airborne interactive device.
Airborne interactive device is display and the interactive device of Airborne Terminal, can be connected by wireless and wired two kinds of modes with Airborne Terminal.Equipment, based on intelligent operating system platform, can meet General Aviation mobile interchange, requirements analysis, is the comprehensive carrier monitoring the application platforms such as navigation, integrated information service, flight planning service, weather information, value-added service.
As an embodiment, airborne interactive device comprises following characteristic: have dual core processor, 4G internal memory, 4 external USBs, 4 inputs and 2 outputs 429 buses (optional high, low speed), Large Copacity solid state hard disc, ethernet port, 28 volts of direct current inputs, machine power source, ni-mh reserve battery, avoids FAA to the misgivings of elemental lithium, by DO-160F standard, wireless WiFi supports.
As an embodiment, based on ADS-B and Big Dipper technology, by the integration of wireless communication technology and ADS-B land station, the reception to the ADS-BOUT information that other aircrafts send can be realized, simultaneously in conjunction with the own location information that the Big Dipper provides, thus realize showing air traffic information in real time on airborne interactive device, meet the requirement of aircraft traffic navigation.System possesses initiatively interrogation function, can provide alarm for parameters such as closing on the position of aircraft, orientation, relative height and distance
Described Airborne Terminal is ADS-B equipment, and described ADS-B equipment is determined the accurate location on its aloft/ground, in conjunction with after other data, positional information sent to operational support and service centre by aviation wireless private network after receiving the Big Dipper/gps signal.
For kind and the business characteristic of General Aviation weather data, notice to navigator information, by the further investigation of the data class that relates to General Aviation Flight information, feature, source and update mechanism, absolutely empty, the Air-Ground data being applicable to China's Flight data management feature in conjunction with technical design such as ADS-B, Data-Link, air communications nets is collected, the operational support of integrated and management and service centre, realizes the information fusion of multi-source aviation flight data efficient and integrated process.Related keyword information is as follows:
To aircraft: GNSS positional information, highly, speed, flight posture, type, identification code etc.
To crew: spatial domain demand, flight planning etc.
To ground blank pipe: spatial domain situation, spatial domain draw establish, plan reply, flight before data bulletin, chart information, meteorologic information, navigational intelligence etc.
Real-time information (voice/data) alternately to lifting spatial domain utilization ratio and traffic administration efficiency most important.By the aviation private network based on wireless communication technology, operational support and service centre can provide real-time flight service support to aircraft, self flying quality also can be sent to operational support and service centre by aircraft in real time, finally realize the real-time, interactive of vacant lot information, under supporting unmanned situation fast automatic complete General Aviation Flight information issue and the flight information service such as alternately.
Operational support and service centre are unified network platforms, and supervision, communication, navigation and traffic management information all should converge to a unified network platform, carry out unified data processing and demand response.
According to demand General Aviation target being implemented to reliable surveillance, realize Multiple Information Sources (multi-source monitoring data, air traffic control radar, flight planning, real-time weather information etc.) heterogeneous data merge, the Track In Track of General Aviation target and prediction, comprehensive warning (low clearance alarm, collision alert, repeated code, non-adimission area invades alarm), develop distributed General Aviation information service and flight planning overall treatment software platform, possess heterogeneous data to merge, flight visual simulation, the record and review of system running state, system synthesis flight path exports, integrated information is issued, flight plan management with the function such as automatically to examine.
The unified platform will provide high-quality and data timely for numerous user and application.By reducing interface and system quantity and type, the unified platform, by reducing unnecessary information redundancy, facilitates the information sharing of multimachine structure better.
The flight information of aircraft comprises: the flight path of the height of the position of aircraft, the flying speed of aircraft, aircraft, the flight trend of aircraft, aircraft.
Uphole equipment comprises cloud computing center, and described cloud computing center can carry out real-time multidimensional space data and calculate, and the result that data calculate is used for immediately adjusting foundation for the aircraft of each course movement provides.
The management in spatial domain has relied on the Coordination Decision of wide area to support coordination technique to a great extent, along with the raising of aircraft independent navigation performance and the development of Ground-to-Air Data Link, and with the combination of the infotecies such as cloud computing, realize air defence to monitor, the collaborative of flight safety management, information-based, merge becoming a business and technology height and the application of intersecting, deeply carrying out operation flow research and running on the basis of conceptual design, the combination of airspace management and cloud computing technology, the ability of system process complexity can be significantly improved, user therefrom can obtain very large value, there is wide promotion prospect.
Cloud computing center can provide the powerful information-based operational management ability of real-time calculating navigation for ground supervisory systems, the algorithm of various complexity can be allowed (to comprise spatial domain in hyperspace, position of aircraft, aircraft performance, aircraft wish, multi-aircraft mutual relationship) calculate, to for provide at the aircraft of each course movement real time monitoring with immediately adjust; For the landing under bad weather condition provides safe basis, be flight path and the backup flight path of the foggy regional aircraft calculation optimization in many mountains.
Described system also comprises low latitude integrated supervision unit, and low latitude integrated supervision disposal system is arranged on each flight service terminal, also can be described as low latitude integrated supervision service terminal.Comprehensive monitoring system is a basic support system in General Aviation Flight service station.This system is made up of different function units module, according to different area monitoring calling hierarchies or level of integrated system, for concrete navigation regional traffic density, visibility and infrastructure condition, monitor navigation aircraft safety, move in an orderly manner, thus improve the efficiency of management.Because the degree of perfection of the scale on different airport, runlevel, air traffic flow, layout and existing operational support system, OSS is different, therefore, for different targeted surveillance regions, the composition of surveillance, function, system integration mode also will there are differences.At present, because the height of empty flying activity is lower, first and second radar cannot reach and cover completely, and the impact of low-altitude surveillance also by landform and barrier is comparatively large, simultaneously also comparatively serious by meteorological factor influence.So low latitude integrated supervision unit should be designed to low cost all standing comprehensive monitoring system (ADS-B, MLAT etc.) according to navigable condition, this comprehensive monitoring system has the function of foreign peoples's Multiple Source Sensor data fusion.This system can provide intelligentized, unattended, with low cost, visual remote tower system for navigation airport, navigation airport and all moving targets of low altitude airspace can be monitored, also can provide position and the relevant information of accurate, real-time, that turnover rate is high low altitude airspace moving target for low latitude integrated supervision unit.
Low latitude integrated supervision unit can receive and resolve ADS-B data, and data layout is in accordance with the regulation of ASTERIXCAT021; Low latitude integrated supervision unit can receive and resolve MLAT data, and data layout is in accordance with the regulation of ASTERIXCAT020; Low latitude integrated supervision unit carries out fusion treatment to the polynary monitoring data such as ADS-B, MLAT, and can provide system flight path synthesis display and the display of single channel monitoring data.
Low latitude integrated supervision unit adopts without resetting federal blending algorithm, is made up of some subfilters and a fusion center.Subfilter receives all kinds of monitoring datas such as ADS-BMLAT, and adopts Kalman filtering to carry out filtering process to every class monitoring data, forms local tracks.Fusion center receives the local tracks after each subfilter process, and adopts without resetting federal blending algorithm, forms system flight path, as shown in Figure 4.
System also comprises ADS-B land station, and described ADS-B land station is made up of ADS-B receiver hardware module, signal processing software module and network management system three part.
Described ADS-B land station is the network architecture of all-IP, utilize modular design, double reception passage, Hot Spare mode improve stiffness of system, remote network management is adopted to realize remote radio frequency self-inspection, the Long-distance Control of ADS-B land station, to realize ADS-B land station unmanned.
ADS-B land station adopts modular design, considers opening, extendability, intelligent simultaneously; According to the use scenes of product, while meeting user function demand, also consider the shielding of product and Electro Magnetic Compatibility, portable soundness and attractive in appearance and easy to use intelligent and be convenient to safeguard.
ADS-B land station supports RTCADO260 series standard, provides the ether interface of standard to be connected with air traffic control system, adopts double antenna channel hot standby part to ensure the reliability of product; Support gps signal, for user provides time scale information; ADS-B earth station equipment administrative center is adopted to manage one or more ADS-B land station.
ADS-B land station leading indicator is as follows:
Receive frequency: 1090 ± 1MHz;
Sensitivity :-85dBm;
Dynamic range: >65dB;
Reliability: MTBF>20000 hour;
Maintainable: MTTR is no more than 30 minutes;
Environmental suitability requires: meet RTCADO-160D regulation;
Lightning protection: grade reaches 20kA (8/20us);
Electromagnetic compatibility: meet RTCADO-160D regulation;
Serviceability temperature :-35 ° of C are to+65 ° of C;
Interface: base-T100;
With air traffic control system interface protocol: ASTERIXCategory21;
Radio frequency interface: N-type;
Covering radius: be not less than 200 nautical miles;
Track following capacity: 500;
Power supply: AC and DC is powered support
Ground base station adopts 1800MHz fiber optic stretch base station, and principal feature is as follows:
(1) adopt the advanced 4G gordian technique such as CS-OFDMA, Adaptive Modulation, dynamic channel allocation, fast joint detection, the availability of frequency spectrum is high, and message transmission rate is high, wide coverage;
(2) adopt advanced enhanced smart antenna technology, antijamming capability is strong, supports identical networking;
(3) base station maximum transmission power 40dbm, meets vacant lot and covers demand at a distance;
(4) support terminal high-speed mobile, supports that the business across base station switches;
(5) supporting business merges, and realizes the business such as point-to-point voice, cluster voice, wideband data, video monitoring, video dispatching and video conference;
(6) the Access Control measure such as support equipment authentication, subscription authentication, business authentication, security is high;
(7) realize whole IP group network, the network architecture is simple;
(8) processing power is strong, and service concurrence number is high.
Described airborne interactive device is connected with airborne wireless communication terminal, for General Aviation mobile interchange, information interaction by wireless or wired mode; Described airborne interactive device has supervision navigation, integrated information service, flight planning service, weather information, value-added service function.
One of ordinary skill in the art will appreciate that all or part of flow process realized in above-described embodiment method, that the hardware that can carry out instruction relevant by computer program has come, described program can be stored in a computer read/write memory medium, this program, when performing, can comprise the flow process of the embodiment as above-mentioned each side method.Wherein, described storage medium can be magnetic disc, CD, read-only store-memory body (Read-OnlyMemory, ROM) or random store-memory body (RandomAccessMemory, RAM) etc.
The above; be only embodiment of the present utility model; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; the change that can expect easily or replacement, all should be encompassed within protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain of claim.
Claims (10)
1. a low flyer dynamic surveillance system, is characterized in that, comprising:
Locating device, for sending locator data to aircraft;
Airborne Terminal, for utilizing locating device to determine its exact position, by the flight information of wireless communication networks device broadcasts aircraft earthward, and receiving the data of other aircraft that uphole equipment sends, resolving the data received;
Uphole equipment, the information that the Airborne Terminal for receiving each aircraft sends, carry out real-time situation monitoring to aircraft, analyze possible flight risk, upstream broadcast is issued and is provided anti-collision warning message;
The real-time situation data of each aircraft and warning message, for being connected with Airborne Terminal, are shown by airborne interactive device.
2. system according to claim 1, is characterized in that,
Described Airborne Terminal periodically sends apply for information, closes on the position of aircraft, orientation, relative height and distance in order to inquiry, and according to close on the position of aircraft, orientation, relative height and distance calculate close on aircraft close on value;
When described close on value be less than predetermined threshold value time, described Airborne Terminal sends alerting signal.
3. system according to claim 1, is characterized in that,
Described locating device is big-dipper satellite positioning system or gps satellite positioning system.
4. system according to claim 2, is characterized in that,
Described Airborne Terminal is ADS-B equipment, and described ADS-B equipment is determined the accurate location on its aloft/ground, in conjunction with after other data, positional information sent to operational support and service centre by aviation wireless private network after receiving the Big Dipper/gps signal.
5. system according to claim 1, is characterized in that,
The flight information of described aircraft comprises: the flight path of the height of the position of aircraft, the flying speed of aircraft, aircraft, the flight trend of aircraft, aircraft.
6. system according to claim 1, is characterized in that,
Described uphole equipment comprises cloud computing center, and described cloud computing center can carry out real-time multidimensional space data and calculate, and the result that data calculate is used for immediately adjusting foundation for the aircraft of each course movement provides.
7. system according to claim 6, is characterized in that, the result that described data calculate is used for immediately adjusting foundation for the aircraft of each course movement provides, and comprising:
For the landing of aircraft under bad weather condition provides safe basis; And
For flight path and the backup flight path of the foggy regional aircraft calculation optimization in many mountains.
8. system according to claim 1, is characterized in that,
Described system also comprises low latitude integrated supervision unit, and described low latitude integrated supervision unit is made up of one or more subfilter and a fusion center;
Described subfilter receives all kinds of monitoring data, and adopts Kalman filtering to carry out filtering process to every class monitoring data, forms local tracks;
Described fusion center receives the local tracks after each subfilter process, and adopts without resetting federal blending algorithm, forms system flight path.
9. system according to claim 1, is characterized in that,
Described system also comprises ADS-B land station, and described ADS-B land station is made up of ADS-B receiver hardware module, signal processing software module and network management system three part;
Described ADS-B land station is the network architecture of all-IP, utilize modular design, double reception passage, Hot Spare mode improve stiffness of system, remote network management is adopted to realize remote radio frequency self-inspection, the Long-distance Control of ADS-B land station, to realize ADS-B land station unmanned.
10. system according to claim 1, is characterized in that,
Described airborne interactive device is connected with airborne wireless communication terminal, for General Aviation mobile interchange, information interaction by wireless or wired mode;
Described airborne interactive device has supervision navigation, integrated information service, flight planning service, weather information, value-added service function.
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105070105A (en) * | 2015-07-29 | 2015-11-18 | 重庆赛乐威航空科技有限公司 | Low-altitude aircraft dynamic monitoring system |
| CN106887055A (en) * | 2017-01-23 | 2017-06-23 | 广州博进信息技术有限公司 | Flight is jolted method for early warning and its system |
| CN106950990A (en) * | 2017-04-26 | 2017-07-14 | 安阳全丰航空植保科技股份有限公司 | A kind of long-range airborne UAV Flight Control System and method |
| CN107439004A (en) * | 2016-08-11 | 2017-12-05 | 深圳市道通智能航空技术有限公司 | One kind tracking and knowledge method for distinguishing, system and aircraft |
| CN109254288A (en) * | 2018-10-19 | 2019-01-22 | 北京东进航空科技股份有限公司 | Method and system for low slow bug monitoring, early warning |
| CN110689763A (en) * | 2019-09-20 | 2020-01-14 | 中国飞行试验研究院 | Airborne auxiliary navigation method, device and system based on wireless reception |
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2015
- 2015-07-29 CN CN201520560545.8U patent/CN204856925U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105070105A (en) * | 2015-07-29 | 2015-11-18 | 重庆赛乐威航空科技有限公司 | Low-altitude aircraft dynamic monitoring system |
| CN107439004A (en) * | 2016-08-11 | 2017-12-05 | 深圳市道通智能航空技术有限公司 | One kind tracking and knowledge method for distinguishing, system and aircraft |
| CN107439004B (en) * | 2016-08-11 | 2020-04-10 | 深圳市道通智能航空技术有限公司 | Tracking and identifying method, system and aircraft |
| CN106887055A (en) * | 2017-01-23 | 2017-06-23 | 广州博进信息技术有限公司 | Flight is jolted method for early warning and its system |
| CN106887055B (en) * | 2017-01-23 | 2020-07-14 | 中国民航科学技术研究院 | Early warning method and system for flying bump |
| CN106950990A (en) * | 2017-04-26 | 2017-07-14 | 安阳全丰航空植保科技股份有限公司 | A kind of long-range airborne UAV Flight Control System and method |
| CN106950990B (en) * | 2017-04-26 | 2020-06-16 | 安阳全丰航空植保科技股份有限公司 | Remote airborne unmanned aerial vehicle flight control system and method |
| CN109254288A (en) * | 2018-10-19 | 2019-01-22 | 北京东进航空科技股份有限公司 | Method and system for low slow bug monitoring, early warning |
| CN110689763A (en) * | 2019-09-20 | 2020-01-14 | 中国飞行试验研究院 | Airborne auxiliary navigation method, device and system based on wireless reception |
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