CN203773355U - Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device - Google Patents

Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device Download PDF

Info

Publication number
CN203773355U
CN203773355U CN201320789437.9U CN201320789437U CN203773355U CN 203773355 U CN203773355 U CN 203773355U CN 201320789437 U CN201320789437 U CN 201320789437U CN 203773355 U CN203773355 U CN 203773355U
Authority
CN
China
Prior art keywords
unit
real
big dipper
unmanned plane
unmanned aerial
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.)
Expired - Fee Related
Application number
CN201320789437.9U
Other languages
Chinese (zh)
Inventor
梁谋强
Original Assignee
梁谋强
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 梁谋强 filed Critical 梁谋强
Priority to CN201320789437.9U priority Critical patent/CN203773355U/en
Application granted granted Critical
Publication of CN203773355U publication Critical patent/CN203773355U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model relates to a three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device and belongs to the unmanned aerial vehicle flight monitoring management system technical filed. A ground monitoring integrated information processing unit is connected with a ground monitoring wireless mobile communication unit, a Beidou communication unit, a data sharing communication unit, a display control unit and a terminal positioning unit respectively. According to the three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device, a three-dimensional multi-image layer type unmanned aerial vehicle dynamic real-time monitoring and management mode is adopted. The three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device can be connected into third-party map data such as Google, so that three-dimensional multi-image layer three-dimensional overlapping display from different data sources and flight real-time dynamic monitoring of an unmanned aerial vehicle simulation three-dimensional model can be realized. The three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device is advantageous in high accuracy, intuitiveness, convenience, high integration, powerful function, efficiency monitoring and no positioning blind area. With the three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device adopted, multi-unmanned aerial vehicle cooperative monitoring, high-precision, real-time, continuous and seamless positioning of whole airspace-covering flight, real-time and continuous communication between unmanned aerial vehicles and a ground monitoring terminal, and whole-airspace coverage can be realized, and high reliability and strong stability of a system can be realized.

Description

3 D stereo multi-layer image formula unmanned plane is located maintenance device in real time
Technical field:
The utility model relates to unmanned plane during flying monitoring management system technical field, relates in particular to a kind of 3 D stereo multi-layer image formula unmanned plane and locates in real time maintenance device.
Background technology:
Along with each fields such as mapping, exploration, the condition of a disaster prevention, environmental monitoring, agricultural irrigation, emergency processing, forest fire protection, electric power line walking, aeroplane photography continue to bring out out the active demand to new technical means, unmanned plane relies on that it is with low cost, maneuverability, can all weather operations etc. advantage and being used widely in these fields.Meanwhile, how to improve the monitoring unmanned efficiency of management in operation process, guarantee that the safe flight operation of the full spatial domain of unmanned plane is most important comprehensively, could meet the present situation demand of diversified flight range operation.
At present, what the product of monitoring unmanned management both at home and abroad extensively adopted is the X-Y scheme monitoring management pattern based on two-dimensional digital map, show unmanned plane during flying track with two-dimensional curve, flight attitude shows with a large amount of unmanned plane kinematic parameters, exist supervision intuitive, accuracy poor, professional too strong, use inconvenient, be prone to the shortcomings such as erroneous judgement; Aspect real-time location, adopt single gps satellite positioning system to carry out location, position, if GPS application is restricted or disturbs, there is blind area, will cause system to locate, have a strong impact on aloft unmanned plane Real-time Monitor Management; Simultaneously, in communication aspects, only adopt mobile radio networks to carry out data message transmission, run into the communication blind district without network signal, will lose the Real-time Monitor Management ability to unmanned plane during flying, by greatly increasing the incidence of the aberdeen cutlets such as unmanned plane loss or shock, just can not ensure in the flight safety of blind area unmanned plane.Due to the existence of above all drawbacks, therefore existing monitoring management system cannot meet the real demand of multiple UAVs in the safe flight monitoring operation management of full spatial domain at all.
And, along with the increase of the unmanned plane of aerial work, user needs the demand of multiple UAVs real-time monitoring in spatial domain day by day to be highlighted simultaneously, but traditional product is still confined to the regulatory format of " one to one ", cannot meet the demand of multi-machine collaborative flight supervision; What is more important, the increase of aerial work unmanned plane, under same spatial domain, multiple UAVs is carried out operation simultaneously, certainly will cause the anxiety of spatial domain resource, bring potential collision threat particularly to manned airline carriers of passengers, traditional product provides an adequate solution method cannot to blank pipe department.
At present, on market, existing nothing enters machine monitoring management system (as intelligent bird SUAV (small unmanned aerial vehicle) ground monitoring system, boat letter unmanned aerial vehicle station navigation monitoring system), all adopt X-Y scheme monitoring management pattern, realize the flight path of unmanned plane is shown, two-dimensional digital map shows unmanned plane during flying track with two-dimensional curve as a setting.The flight path of two-dimensional curve is only made up of longitude and latitude, can not embody intuitively flying height, therefore in the time that the longitude and latitude of two airplane present positions is identical, on two-dimensional map, the overlapped state of two airplanes will be shown as, the erroneous judgement of very easily bringing aircraft collision to monitoring management personnel.What is more important, flight attitude shows with real-time, a large amount of unmanned plane kinematic parameters, can only, by monitoring management personnel by these kinematic parameters are comprehensively analyzed, judged, just can draw unmanned plane during flying attitude situation, specialization is too strong, intuitive is poor; And this mode is had relatively high expectations to monitoring management personnel's professional skill, tend to because the deficiency of specialty flight knowledge and experience, cause misjudgment, obtain incorrect flight attitude result, this will bring serious consequence to unmanned plane during flying monitoring management and flight safety.In summary, this series products is poor to monitoring management intuitive, the accuracy of unmanned plane during flying track and attitude, it is convenient not to use, be prone to erroneous judgement, cause monitoring management efficiency low, cannot meet the present situation demand of unmanned plane fast development now, the efficient monitoring management of safe flight, diversified hazardous flight region operation at all.
Utility model content:
The purpose of this utility model is to provide 3 D stereo multi-layer image formula unmanned plane and locates in real time maintenance device, it adopts brand-new 3 D stereo multi-layer image formula unmanned plane dynamic real-time monitor management mode, by third party's map datums such as access google, realize from the three-dimensional Overlapping display of three-dimensional multi-layer image in different pieces of information source and unmanned plane emulation three-dimensional model the real-time dynamic supervision that flies, accurately, intuitively, convenient, product height is integrated, powerful, supervision is efficient, non-blind area, system location, realize the collaborative monitoring of multiple no-manned plane, continuous seamless location while covering the high-precision real flying in full spatial domain, unmanned plane and ground monitoring terminal room real-time continuous uninterrupted communication also cover the feature in full spatial domain, system operation reliability is high and stability is strong.
In order to solve the existing problem of background technology, the utility model is by the following technical solutions: it comprises airborne positioning and communicating device 1, ground monitoring communicator 2, mobile radio networks 3, big-dipper satellite 4 and gps satellite 5, wherein airborne positioning and communicating device 1 comprises airborne integrated information processing unit 6, flying data collector unit 7, airborne wireless mobile comm unit 8, Big Dipper communication unit 9 and Big Dipper GPS double star data fusion positioning unit 10, ground monitoring communicator 2 comprises ground monitoring wireless mobile communications unit 11, Big Dipper communication unit 12, data sharing communication unit 13, ground monitoring integrated information processing unit 14, indicative control unit 15 and terminal positioning unit 16, airborne integrated information processing unit 6 respectively with flying data collector unit 7, airborne wireless mobile comm unit 8, Big Dipper communication unit 9 and Big Dipper GPS double star data fusion positioning unit 10 interconnect, mobile radio networks 3 interconnects with airborne wireless mobile comm unit 8 and ground monitoring wireless mobile communications unit 11 respectively, big-dipper satellite 4 interconnects with Big Dipper communication unit 9 and Big Dipper communication unit 12 respectively, gps satellite 5 interconnects with Big Dipper GPS double star data fusion positioning unit 10, Big Dipper GPS double star data fusion positioning unit 10 is connected with big-dipper satellite 4, ground monitoring integrated information processing unit 14 respectively with ground monitoring wireless mobile communications unit 11, Big Dipper communication unit 12, data sharing communication unit 13, indicative control unit 15 and terminal positioning unit 16 interconnect.
Described airborne positioning and communicating device 1 is mainly according to ground steering order, unmanned plane real-time flight status data to be collected, and transfers to ground monitoring communicator 2.
Described ground monitoring communicator 2 has been mainly the functions such as sending controling instruction, the real-time analysis of unmanned plane during flying status data and demonstration, flight path real-time follow-up, multi-machine collaborative flight supervision, the police of collision intelligent forecasting.
Described airborne integrated information processing unit 6 is mainly used in receiving and responding the steering order of ground monitor terminal, and receive unmanned plane real-time flight status data and preserve, whether the base station signal strength that simultaneously judges the land that airborne wireless mobile comm unit receives can proper communication, if can proper communication, start airborne wireless mobile communications unit 8, born and the function of the two-way communication of ground monitoring terminal by airborne wireless mobile comm unit 8, if can not proper communication, start Big Dipper communication unit 9, born and the function of ground monitoring terminal two-way communication by Big Dipper communication unit 9, guarantee the real-time continuous uninterrupted communication of unmanned plane and ground monitoring terminal room.
Described flying data collector unit 7 is mainly used in other flying quality sensors, as gyroscope, three-dimensional acceleration sensor, omnidirectional's magnetic field sensor, static pressure altitude gauge etc., the related data simultaneously sensor being gathered, be unmanned plane during flying attitude data, be sent to airborne integrated information processing unit 6.
Described Big Dipper communication unit 9 comprises Big Dipper communication antenna and Big Dipper transceiver, Big Dipper communication unit 9 and airborne wireless mobile comm unit 8 are respectively by the two-way communication of Beidou satellite communication system and the realization of civilian mobile radio networks and ground monitoring terminal, by the real-time flight status data of unmanned plane, comprise longitude and latitude, highly, flight attitude data etc., be transmitted to ground monitoring terminal and maybe the steering orders such as the request location of the ground monitoring terminal of reception be transmitted to airborne integrated information processing unit 6.
Described Big Dipper GPS double star data fusion positioning unit 10 comprises satellite signal receiving antenna, double star data fusion positioning chip and data processing module, continuous seamless location the information such as locator data longitude and latitude, height are passed to airborne integrated information processing unit or received the request positioning instruction that airborne integrated information processing unit transmits during for the high-precision real of unmanned plane.
The two-way communication that real-time stabilization is set up with airborne wireless mobile comm unit 8 and Big Dipper communication unit 9 respectively in described ground monitoring wireless mobile communications unit 11.
Described data sharing communication unit 13 is mainly used in downloading from data sharing platform the real-time locator data of adjacent unmanned plane of obtaining required spatial domain, meanwhile, under the condition allowing, the own current real-time locator data of unmanned plane is uploaded to shared platform in authority.
Described ground monitoring integrated information processing unit 14 is as the data processing centre (DPC) of ground based terminal, be mainly used in realizing the transmitted in both directions of information between indicative control unit 15 and ground monitoring wireless mobile communications unit 14 or Big Dipper communication unit 12, judge whether ground monitoring wireless mobile communications unit can be realized and being connected of specific sequence number airborne wireless mobile comm unit, if can connect, born and the function of the two-way communication of above-mentioned airborne positioning and communicating device 1 by ground monitoring wireless mobile communications unit 14, if can not connect, born and the function of the unmanned plane two-way communication of above-mentioned airborne positioning and communicating device 1 by Beidou satellite communication system by Big Dipper communication unit 12, simultaneously, ground monitoring integrated information processing unit 14 is by the real-time locator data of other unmanned plane in the same spatial domain receiving, target Unmanned Aerial Vehicle Data knot combined analysis with native system supervision, set up the unit decomposition of mission area, airborne sensor, network service is at the model of interior each element, the control of unmanned plane collective motion is provided, multiple no-manned plane keeps away barrier planning and multiple no-manned plane Cooperative Area monitors strategy three large function supports, simultaneously, identify the potential unmanned plane with certain collision threat and provide anti-collision warning information between unmanned plane to indicative control unit 15.
Described indicative control unit 15 is made up of three-dimensional map display module, unmanned plane state processing module and terminal control module three parts, be used for providing inputting interface for user's input control information and show unmanned plane real-time flight state, show that with trivector curve unmanned plane during flying track, unmanned plane emulation three-dimensional model show flight attitude, steering order information etc., monitor earthward integrated information processing unit sending controling instruction or receive the unmanned plane real-time flight status data that integrated information processing unit is sent.
Principle of work of the present utility model: ground monitoring communicator 2 first by steering order by being distributed in the civilian mobile radio networks on land or passing to the unmanned plane that is equipped with airborne positioning and communicating device 1 by Beidou satellite communication system, unmanned plane is received after steering order, enter real-time locating and monitoring state, start Big Dipper GPS double star data fusion positioning unit 10 and collect the data such as real-time flight attitude, then above unmanned plane real-time flight status data is passed to and is equipped with above-mentioned ground monitoring communicator 2 by mobile radio networks 3 or Beidou satellite communication system, finally by emulation electronic three-dimensional map and the unmanned plane emulation three-dimensional model of indicative control unit 15, Real time dynamic display monitoring management unmanned plane, simultaneously, have flight path real-time follow-up concurrently, the globalize of the multiple UAVs that same user is let fly away based on same monitor terminal synchronously supervised, between unmanned plane, collide intelligent forecasting alert etc. multi-functional in one.
The utility model adopts based on Virtual Globe d engine technology, and in conjunction with google two-dimensional/three-dimensional map datum interface, build innovatively 3 D stereo multi-layer image formula unmanned plane dynamic real-time monitor management mode, thoroughly solve under the graphical monitoring management pattern of conventional two-dimensional, intuitive to unmanned plane during flying track and attitude Real-time Monitor Management and the drawback that convenience is poor, accuracy is low, significantly improve the monitoring unmanned efficiency of management.
The utility model adopts Big Dipper GPS double star data fusion positioning technology chip, continuous seamless location when having designed and Implemented innovatively unmanned plane and covering the high-precision real of full spatial domain flight, take the lead in reaching non-blind area, system location, effectively stability and the reliability of raising system location, at monitoring unmanned management domain, breakthrough realization is without can be to extreme low-altitude in conjunction with the visual of supervisor, valley, backer, the unmanned plane of traditional high-risk flight range flights such as high building is other is accurate in real time, remote monitoring and administration, realize the supervision method design of " one-to-many ", taking the lead in easily realizing the globalize of the multiple UAVs that same user is let fly away based on same monitor terminal synchronously supervises.
The utility model adopts the unmanned plane perception based on locator data information sharing and evades technology, realize innovatively and between unmanned plane, collided the alert function of intelligent forecasting, effectively evade the generation of midair collision risk between the unmanned plane flying in same spatial domain, the intellectuality of monitoring unmanned management system has been mentioned to higher level.
The communication mode that the utility model adopts mobile radio networks to combine with Big Dipper communication network, the breakthrough real-time continuous uninterrupted communication of realizing unmanned plane and ground monitoring terminal room, efficiently solves that traditional product cannot be communicated by letter in mobile radio networks blind area and realistic problem that cannot Real-time Monitor Management.
The utility model adopts Miniaturization Design, and system self poisoning information is added in map, can realize at vehicle and dispose terminal, completes in real time unmanned plane supervision operation in movement.
The utility model adopts brand-new 3 D stereo multi-layer image formula unmanned plane dynamic real-time monitor management mode, by third party's map datums such as access google, realize from the three-dimensional Overlapping display of three-dimensional multi-layer image in different pieces of information source and unmanned plane emulation three-dimensional model the real-time dynamic supervision that flies, accurately, intuitively, convenient, product height is integrated, powerful, supervision is efficient, non-blind area, system location, realize the collaborative monitoring of multiple no-manned plane, continuous seamless location while covering the high-precision real flying in full spatial domain, unmanned plane and ground monitoring terminal room real-time continuous uninterrupted communication also cover the feature in full spatial domain, system operation reliability is high and stability is strong.
Brief description of the drawings:
Fig. 1 is structural representation of the present utility model;
Fig. 2 is system architecture schematic diagram of the present utility model.
Embodiment:
With reference to Fig. 1, Fig. 2, this embodiment by the following technical solutions: it comprises airborne positioning and communicating device 1, ground monitoring communicator 2, mobile radio networks 3, big-dipper satellite 4 and gps satellite 5, wherein airborne positioning and communicating device 1 comprises airborne integrated information processing unit 6, flying data collector unit 7, airborne wireless mobile comm unit 8, Big Dipper communication unit 9 and Big Dipper GPS double star data fusion positioning unit 10, ground monitoring communicator 2 comprises ground monitoring wireless mobile communications unit 11, Big Dipper communication unit 12, data sharing communication unit 13, ground monitoring integrated information processing unit 14, indicative control unit 15 and terminal positioning unit 16, airborne integrated information processing unit 6 respectively with flying data collector unit 7, airborne wireless mobile comm unit 8, Big Dipper communication unit 9 and Big Dipper GPS double star data fusion positioning unit 10 interconnect, mobile radio networks 3 interconnects with airborne wireless mobile comm unit 8 and ground monitoring wireless mobile communications unit 11 respectively, big-dipper satellite 4 interconnects with Big Dipper communication unit 9 and Big Dipper communication unit 12 respectively, gps satellite 5 interconnects with Big Dipper GPS double star data fusion positioning unit 10, Big Dipper GPS double star data fusion positioning unit 10 is connected with big-dipper satellite 4, ground monitoring integrated information processing unit 14 respectively with ground monitoring wireless mobile communications unit 11, Big Dipper communication unit 12, data sharing communication unit 13, indicative control unit 15 and terminal positioning unit 16 interconnect.
Described airborne positioning and communicating device 1 is mainly according to ground steering order, unmanned plane real-time flight status data to be collected, and transfers to ground monitoring communicator 2.
Described ground monitoring communicator 2 has been mainly the functions such as sending controling instruction, the real-time analysis of unmanned plane during flying status data and demonstration, flight path real-time follow-up, multi-machine collaborative flight supervision, the police of collision intelligent forecasting.
Described airborne integrated information processing unit 6 is mainly used in receiving and responding the steering order of ground monitor terminal, and receive unmanned plane real-time flight status data and preserve, whether the base station signal strength that simultaneously judges the land that airborne wireless mobile comm unit receives can proper communication, if can proper communication, start airborne wireless mobile communications unit 8, born and the function of the two-way communication of ground monitoring terminal by airborne wireless mobile comm unit 8, if can not proper communication, start Big Dipper communication unit 9, born and the function of ground monitoring terminal two-way communication by Big Dipper communication unit 9, guarantee the real-time continuous uninterrupted communication of unmanned plane and ground monitoring terminal room.
Described flying data collector unit 7 is mainly used in other flying quality sensors, as gyroscope, three-dimensional acceleration sensor, omnidirectional's magnetic field sensor, static pressure altitude gauge etc., the related data simultaneously sensor being gathered, be unmanned plane during flying attitude data, be sent to airborne integrated information processing unit 6.
Described Big Dipper communication unit 9 comprises Big Dipper communication antenna and Big Dipper transceiver, Big Dipper communication unit 9 and airborne wireless mobile comm unit 8 are respectively by the two-way communication of Beidou satellite communication system and the realization of civilian mobile radio networks and ground monitoring terminal, by the real-time flight status data of unmanned plane, comprise longitude and latitude, highly, flight attitude data etc., be transmitted to ground monitoring terminal and maybe the steering orders such as the request location of the ground monitoring terminal of reception be transmitted to airborne integrated information processing unit 6.
Described Big Dipper GPS double star data fusion positioning unit 10 comprises satellite signal receiving antenna, double star data fusion positioning chip and data processing module, continuous seamless location the information such as locator data longitude and latitude, height are passed to airborne integrated information processing unit or received the request positioning instruction that airborne integrated information processing unit transmits during for the high-precision real of unmanned plane.
The two-way communication that real-time stabilization is set up with airborne wireless mobile comm unit 8 and Big Dipper communication unit 9 respectively in described ground monitoring wireless mobile communications unit 11.
Described data sharing communication unit 13 is mainly used in downloading from data sharing platform the real-time locator data of adjacent unmanned plane of obtaining required spatial domain, meanwhile, under the condition allowing, the own current real-time locator data of unmanned plane is uploaded to shared platform in authority.
Described ground monitoring integrated information processing unit 14 is as the data processing centre (DPC) of ground based terminal, be mainly used in realizing the transmitted in both directions of information between indicative control unit 15 and ground monitoring wireless mobile communications unit 14 or Big Dipper communication unit 12, judge whether ground monitoring wireless mobile communications unit can be realized and being connected of specific sequence number airborne wireless mobile comm unit, if can connect, born and the function of the two-way communication of above-mentioned airborne positioning and communicating device 1 by ground monitoring wireless mobile communications unit 14, if can not connect, born and the function of the unmanned plane two-way communication of above-mentioned airborne positioning and communicating device 1 by Beidou satellite communication system by Big Dipper communication unit 12, simultaneously, ground monitoring integrated information processing unit 14 is by the real-time locator data of other unmanned plane in the same spatial domain receiving, target Unmanned Aerial Vehicle Data knot combined analysis with native system supervision, set up the unit decomposition of mission area, airborne sensor, network service is at the model of interior each element, the control of unmanned plane collective motion is provided, multiple no-manned plane keeps away barrier planning and multiple no-manned plane Cooperative Area monitors strategy three large function supports, simultaneously, identify the potential unmanned plane with certain collision threat and provide anti-collision warning information between unmanned plane to indicative control unit 15.
Described indicative control unit 15 is made up of three-dimensional map display module, unmanned plane state processing module and terminal control module three parts, be used for providing inputting interface for user's input control information and show unmanned plane real-time flight state, show that with trivector curve unmanned plane during flying track, unmanned plane emulation three-dimensional model show flight attitude, steering order information etc., monitor earthward integrated information processing unit sending controling instruction or receive the unmanned plane real-time flight status data that integrated information processing unit is sent.
The principle of work of this embodiment: ground monitoring communicator 2 first by steering order by being distributed in the civilian mobile radio networks on land or passing to the unmanned plane that is equipped with airborne positioning and communicating device 1 by Beidou satellite communication system, unmanned plane is received after steering order, enter real-time locating and monitoring state, start Big Dipper GPS double star data fusion positioning unit 10 and collect the data such as real-time flight attitude, then above unmanned plane real-time flight status data is passed to and is equipped with above-mentioned ground monitoring communicator 2 by mobile radio networks 3 or Beidou satellite communication system, finally by emulation electronic three-dimensional map and the unmanned plane emulation three-dimensional model of indicative control unit 15, Real time dynamic display monitoring management unmanned plane, simultaneously, have flight path real-time follow-up concurrently, the globalize of the multiple UAVs that same user is let fly away based on same monitor terminal synchronously supervised, between unmanned plane, collide intelligent forecasting alert etc. multi-functional in one.
This embodiment adopts based on Virtual Globe d engine technology, and in conjunction with google two-dimensional/three-dimensional map datum interface, build innovatively 3 D stereo multi-layer image formula unmanned plane dynamic real-time monitor management mode, thoroughly solve under the graphical monitoring management pattern of conventional two-dimensional, intuitive to unmanned plane during flying track and attitude Real-time Monitor Management and the drawback that convenience is poor, accuracy is low, significantly improve the monitoring unmanned efficiency of management.
This embodiment adopts Big Dipper GPS double star data fusion positioning technology chip, continuous seamless location when having designed and Implemented innovatively unmanned plane and covering the high-precision real of full spatial domain flight, take the lead in reaching non-blind area, system location, effectively stability and the reliability of raising system location, at monitoring unmanned management domain, breakthrough realization is without can be to extreme low-altitude in conjunction with the visual of supervisor, valley, backer, the unmanned plane of traditional high-risk flight range flights such as high building is other is accurate in real time, remote monitoring and administration, realize the supervision method design of " one-to-many ", taking the lead in easily realizing the globalize of the multiple UAVs that same user is let fly away based on same monitor terminal synchronously supervises.
This embodiment adopts the unmanned plane perception based on locator data information sharing and evades technology, realize innovatively and between unmanned plane, collided the alert function of intelligent forecasting, effectively evade the generation of midair collision risk between the unmanned plane flying in same spatial domain, the intellectuality of monitoring unmanned management system has been mentioned to higher level.
The communication mode that this embodiment adopts mobile radio networks to combine with Big Dipper communication network, the breakthrough real-time continuous uninterrupted communication of realizing unmanned plane and ground monitoring terminal room, efficiently solves that traditional product cannot be communicated by letter in mobile radio networks blind area and realistic problem that cannot Real-time Monitor Management.
This embodiment adopts Miniaturization Design, and system self poisoning information is added in map, can realize at vehicle and dispose terminal, completes in real time unmanned plane supervision operation in movement.
This embodiment adopts brand-new 3 D stereo multi-layer image formula unmanned plane dynamic real-time monitor management mode, by third party's map datums such as access google, realize from the three-dimensional Overlapping display of three-dimensional multi-layer image in different pieces of information source and unmanned plane emulation three-dimensional model the real-time dynamic supervision that flies, accurately, intuitively, convenient, product height is integrated, powerful, supervision is efficient, non-blind area, system location, realize the collaborative monitoring of multiple no-manned plane, continuous seamless location while covering the high-precision real flying in full spatial domain, unmanned plane and ground monitoring terminal room real-time continuous uninterrupted communication also cover the feature in full spatial domain, system operation reliability is high and stability is strong.

Claims (4)

1. 3 D stereo multi-layer image formula unmanned plane is located maintenance device in real time, it is characterized in that it comprises airborne positioning and communicating device (1), ground monitoring communicator (2), mobile radio networks (3), big-dipper satellite (4) and gps satellite (5), wherein airborne positioning and communicating device (1) comprises airborne integrated information processing unit (6), flying data collector unit (7), airborne wireless mobile comm unit (8), Big Dipper communication unit (9) and Big Dipper GPS double star data fusion positioning unit (10), ground monitoring communicator (2) comprises ground monitoring wireless mobile communications unit (11), Big Dipper communication unit (12), data sharing communication unit (13), ground monitoring integrated information processing unit (14), indicative control unit (15) and terminal positioning unit (16), airborne integrated information processing unit (6) respectively with flying data collector unit (7), airborne wireless mobile comm unit (8), Big Dipper communication unit (9) and Big Dipper GPS double star data fusion positioning unit (10) interconnect, mobile radio networks (3) interconnects with airborne wireless mobile comm unit (8) and ground monitoring wireless mobile communications unit (11) respectively, big-dipper satellite (4) interconnects with Big Dipper communication unit (9) and Big Dipper communication unit (12) respectively, gps satellite (5) interconnects with Big Dipper GPS double star data fusion positioning unit (10), Big Dipper GPS double star data fusion positioning unit (10) is connected with big-dipper satellite (4), ground monitoring integrated information processing unit (14) respectively with ground monitoring wireless mobile communications unit (11), Big Dipper communication unit (12), data sharing communication unit (13), indicative control unit (15) and terminal positioning unit (16) interconnect.
2. 3 D stereo multi-layer image formula unmanned plane according to claim 1 is located maintenance device in real time, it is characterized in that described Big Dipper communication unit (9) comprises Big Dipper communication antenna and Big Dipper transceiver.
3. 3 D stereo multi-layer image formula unmanned plane according to claim 1 is located maintenance device in real time, it is characterized in that described Big Dipper GPS double star data fusion positioning unit (10) comprises satellite signal receiving antenna, double star data fusion positioning chip and data processing module.
4. 3 D stereo multi-layer image formula unmanned plane according to claim 1 is located maintenance device in real time, it is characterized in that described indicative control unit (15) is made up of three-dimensional map display module, unmanned plane state processing module and terminal control module three parts.
CN201320789437.9U 2013-12-05 2013-12-05 Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device Expired - Fee Related CN203773355U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320789437.9U CN203773355U (en) 2013-12-05 2013-12-05 Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320789437.9U CN203773355U (en) 2013-12-05 2013-12-05 Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device

Publications (1)

Publication Number Publication Date
CN203773355U true CN203773355U (en) 2014-08-13

Family

ID=51290523

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320789437.9U Expired - Fee Related CN203773355U (en) 2013-12-05 2013-12-05 Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device

Country Status (1)

Country Link
CN (1) CN203773355U (en)

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104503460A (en) * 2014-12-05 2015-04-08 电子科技大学 Ground station control system for universal unmanned aerial vehicle
CN104750111A (en) * 2015-03-09 2015-07-01 王琪杰 Flying monitoring system of unmanned aerial vehicle
CN105096661A (en) * 2015-06-29 2015-11-25 中国民用航空厦门空中交通管理站 Air traffic flow management system based on vertical profile view and method
CN105739516A (en) * 2016-05-09 2016-07-06 王彦成 Unmanned plane management and control device and corresponding system
CN106301623A (en) * 2016-09-09 2017-01-04 成都定为电子技术有限公司 The interference source detection identification method of a kind of spectrum monitoring unmanned plane and device thereof
CN106339003A (en) * 2016-10-09 2017-01-18 北京国泰北斗科技有限公司 Barrier-avoiding method, airspace management system and unmanned aerial vehicle
CN106454209A (en) * 2015-08-06 2017-02-22 航天图景(北京)科技有限公司 Unmanned aerial vehicle emergency quick action data link system and unmanned aerial vehicle emergency quick action monitoring method based on spatial-temporal information fusion technology
CN106444842A (en) * 2016-11-30 2017-02-22 浙江大学 Novel flight positioning control system for four-axis aircraft
CN106569504A (en) * 2015-10-09 2017-04-19 内蒙古信源信息技术有限公司 Apparatus for realizing device information acquisition in remote area through Beidou unmanned gyroplanes and data exchanging method
CN106713344A (en) * 2017-01-10 2017-05-24 深圳高科新农技术有限公司 Unmanned aerial vehicle (UAV) supervision and management device and method
US9852642B2 (en) 2016-03-08 2017-12-26 International Business Machines Corporation Drone air traffic control and flight plan management
US9950791B2 (en) 2016-03-08 2018-04-24 International Business Machines Corporation Drone receiver
US10013886B2 (en) 2016-03-08 2018-07-03 International Business Machines Corporation Drone carrier
US10062292B2 (en) 2016-03-08 2018-08-28 International Business Machines Corporation Programming language for execution by drone
US10417917B2 (en) 2016-03-08 2019-09-17 International Business Machines Corporation Drone management data structure
CN110365397A (en) * 2019-06-24 2019-10-22 天津天航智远科技有限公司 The TT&C system of load-carrying dirigible
CN110574437A (en) * 2017-05-03 2019-12-13 高通股份有限公司 Exchanging messages comprising capability information coupled with a drone between a user equipment coupled with the drone and a component of a terrestrial wireless communications user network
US10689107B2 (en) 2017-04-25 2020-06-23 International Business Machines Corporation Drone-based smoke detector
CN111739349A (en) * 2020-07-28 2020-10-02 北京环境特性研究所 Unmanned aerial vehicle comprehensive management and control system for petroleum and petrochemical field
CN111819610A (en) * 2018-03-06 2020-10-23 Dfs德国空管有限公司 Air situation information and traffic management system for unmanned aerial vehicles and manned aircraft
CN112185177A (en) * 2020-09-29 2021-01-05 深圳天鹰兄弟无人机创新有限公司 Big data management and analysis system and method based on Internet of things
WO2021013228A1 (en) * 2019-07-24 2021-01-28 深圳市道通智能航空技术有限公司 Wireless communication method and device, unmanned aerial vehicle, and unmanned aerial vehicle control system
CN112509381A (en) * 2020-10-16 2021-03-16 广州飞图信息科技有限公司 Visual display method and device for unmanned aerial vehicle route signal blind area
CN113359834A (en) * 2021-06-22 2021-09-07 中国民用航空总局第二研究所 Unmanned aerial vehicle operation monitoring method, system and monitoring platform
CN114088131A (en) * 2020-08-24 2022-02-25 北京市安全生产科学技术研究院 Monitoring modeling device and forest emergency fire-fighting monitoring system

Cited By (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104503460A (en) * 2014-12-05 2015-04-08 电子科技大学 Ground station control system for universal unmanned aerial vehicle
CN104750111A (en) * 2015-03-09 2015-07-01 王琪杰 Flying monitoring system of unmanned aerial vehicle
CN104750111B (en) * 2015-03-09 2019-02-22 王琪杰 A kind of unmanned plane during flying monitoring system
CN105096661A (en) * 2015-06-29 2015-11-25 中国民用航空厦门空中交通管理站 Air traffic flow management system based on vertical profile view and method
CN105096661B (en) * 2015-06-29 2017-12-05 中国民用航空厦门空中交通管理站 Air traffic Workflow Management System and method based on vertical sectional view
CN106454209B (en) * 2015-08-06 2019-08-06 航天图景(北京)科技有限公司 The fast anti-data link system of unmanned plane emergency and method based on TEMPORAL-SPATIAL INFORMATION FUSION
CN106454209A (en) * 2015-08-06 2017-02-22 航天图景(北京)科技有限公司 Unmanned aerial vehicle emergency quick action data link system and unmanned aerial vehicle emergency quick action monitoring method based on spatial-temporal information fusion technology
CN106569504A (en) * 2015-10-09 2017-04-19 内蒙古信源信息技术有限公司 Apparatus for realizing device information acquisition in remote area through Beidou unmanned gyroplanes and data exchanging method
US10417917B2 (en) 2016-03-08 2019-09-17 International Business Machines Corporation Drone management data structure
US11217106B2 (en) 2016-03-08 2022-01-04 International Business Machines Corporation Drone air traffic control and flight plan management
US10922983B2 (en) 2016-03-08 2021-02-16 International Business Machines Corporation Programming language for execution by drone
US9852642B2 (en) 2016-03-08 2017-12-26 International Business Machines Corporation Drone air traffic control and flight plan management
US9950791B2 (en) 2016-03-08 2018-04-24 International Business Machines Corporation Drone receiver
US10013886B2 (en) 2016-03-08 2018-07-03 International Business Machines Corporation Drone carrier
US10062292B2 (en) 2016-03-08 2018-08-28 International Business Machines Corporation Programming language for execution by drone
US10540900B2 (en) 2016-03-08 2020-01-21 International Business Machines Corporation Drone air traffic control and flight plan management
US10081425B2 (en) 2016-03-08 2018-09-25 International Business Machines Corporation Drone receiver
US11151885B2 (en) 2016-03-08 2021-10-19 International Business Machines Corporation Drone management data structure
US11183072B2 (en) 2016-03-08 2021-11-23 Nec Corporation Drone carrier
US10899444B2 (en) 2016-03-08 2021-01-26 International Business Machines Corporation Drone receiver
CN105739516A (en) * 2016-05-09 2016-07-06 王彦成 Unmanned plane management and control device and corresponding system
CN106301623A (en) * 2016-09-09 2017-01-04 成都定为电子技术有限公司 The interference source detection identification method of a kind of spectrum monitoring unmanned plane and device thereof
CN106301623B (en) * 2016-09-09 2018-09-18 成都定为电子技术有限公司 A kind of the interference source detection identification method and its device of spectrum monitoring unmanned plane
CN106339003A (en) * 2016-10-09 2017-01-18 北京国泰北斗科技有限公司 Barrier-avoiding method, airspace management system and unmanned aerial vehicle
CN106444842B (en) * 2016-11-30 2019-06-11 浙江大学 A kind of flight positioning control system of novel four-axle aircraft
CN106444842A (en) * 2016-11-30 2017-02-22 浙江大学 Novel flight positioning control system for four-axis aircraft
CN106713344B (en) * 2017-01-10 2019-12-27 深圳高科新农技术有限公司 Unmanned aerial vehicle supervision device and method
CN106713344A (en) * 2017-01-10 2017-05-24 深圳高科新农技术有限公司 Unmanned aerial vehicle (UAV) supervision and management device and method
US10689107B2 (en) 2017-04-25 2020-06-23 International Business Machines Corporation Drone-based smoke detector
US11438760B2 (en) 2017-05-03 2022-09-06 Qualcomm Incorporated Exchanging a message including an in-flight status indicator between a drone-coupled user equipment and a component of a terrestrial wireless communication subscriber network
CN110574437A (en) * 2017-05-03 2019-12-13 高通股份有限公司 Exchanging messages comprising capability information coupled with a drone between a user equipment coupled with the drone and a component of a terrestrial wireless communications user network
CN111819610A (en) * 2018-03-06 2020-10-23 Dfs德国空管有限公司 Air situation information and traffic management system for unmanned aerial vehicles and manned aircraft
CN110365397A (en) * 2019-06-24 2019-10-22 天津天航智远科技有限公司 The TT&C system of load-carrying dirigible
WO2021013228A1 (en) * 2019-07-24 2021-01-28 深圳市道通智能航空技术有限公司 Wireless communication method and device, unmanned aerial vehicle, and unmanned aerial vehicle control system
CN111739349A (en) * 2020-07-28 2020-10-02 北京环境特性研究所 Unmanned aerial vehicle comprehensive management and control system for petroleum and petrochemical field
CN114088131A (en) * 2020-08-24 2022-02-25 北京市安全生产科学技术研究院 Monitoring modeling device and forest emergency fire-fighting monitoring system
CN112185177A (en) * 2020-09-29 2021-01-05 深圳天鹰兄弟无人机创新有限公司 Big data management and analysis system and method based on Internet of things
CN112509381A (en) * 2020-10-16 2021-03-16 广州飞图信息科技有限公司 Visual display method and device for unmanned aerial vehicle route signal blind area
CN113359834A (en) * 2021-06-22 2021-09-07 中国民用航空总局第二研究所 Unmanned aerial vehicle operation monitoring method, system and monitoring platform
CN113359834B (en) * 2021-06-22 2022-06-10 中国民用航空总局第二研究所 Unmanned aerial vehicle operation monitoring method, system and monitoring platform

Similar Documents

Publication Publication Date Title
CN203773355U (en) Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device
CN104808682B (en) Small-sized rotor wing unmanned aerial vehicle automatic obstacle avoiding flight control method
CN105388907B (en) Multiple no-manned plane low latitude monitoring system based on mobile communications network
CN105119650B (en) Signal relay system and its signal trunking method based on unmanned vehicle
CN104318809B (en) Portable ADS-B mobile system with 3g function
CN205540284U (en) A joint control system for unmanned aerial vehicle
US20180046177A1 (en) Motion Sensing Flight Control System Based on Smart Terminal and Terminal Equipment
CN103927906B (en) The method of Big Dipper independent navigation based on Big Dipper short message and 4G communication pattern
US20150260824A1 (en) Unmanned aerial system drone situational awareness flight safety and tracking system
CN103592948B (en) Unmanned plane flight collision avoidance method
CN202694592U (en) Comprehensive management network platform of civil unmanned aerial vehicle
CN103472847B (en) Unmanned plane power circuit polling flight path method for supervising and system
CN105676249B (en) A kind of navigation aircraft communication navigation observ and method based on 4G/3G/BDS
CN106919183B (en) unified control's multi-functional unmanned aerial vehicle group
CN105913692A (en) Flight monitoring service method and system thereof
CN104503460A (en) Ground station control system for universal unmanned aerial vehicle
CN106210627A (en) A kind of unmanned plane fire dispatch system
CN201597755U (en) Fire early warning airplane
Lu et al. Toward uav-based airborne computing
CN206741310U (en) Multiple no-manned plane communication control system
CN103076810A (en) Portable miniature ground mobile workstation for unmanned aerial vehicle
CN104501828B (en) A kind of General Aviation airborne surveillance system
CN207367056U (en) A kind of fire-fighting unmanned plane based on Mega2560
CN1393682A (en) Real-time flight simulation monitor system
CN204906394U (en) Signal relay system based on unmanned vehicles

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140813

Termination date: 20161205