CN206411519U - A kind of UAS of video control landing - Google Patents
A kind of UAS of video control landing Download PDFInfo
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- CN206411519U CN206411519U CN201720007841.4U CN201720007841U CN206411519U CN 206411519 U CN206411519 U CN 206411519U CN 201720007841 U CN201720007841 U CN 201720007841U CN 206411519 U CN206411519 U CN 206411519U
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Abstract
The utility model discloses a kind of UAS of video control landing, including remote control terminal, unmanned plane and its flight control system, processor, also image module, communication module and the UWB modules of connection on a processor are also associated with flight control system；Unmanned plane opens image module when according to the control of remote control terminal flight to specified touchdown area, the ambient image of landing field around unmanned plane is sent to remote control terminal by processor, communication module, remote control terminal selects suitable landing point according to the ambient image received, control signal control UWB modules are sent to position the point that lands, location information is sent to processor after UWB completion positioning, processor controls flight control system to complete UAV Landing according to location information.The utility model has the advantages that：Unmanned plane is in circumstances not known landing strong adaptability, and reliability is high.
Description
Technical field
The utility model is related to a kind of unmanned plane landing system, and in particular to a kind of unmanned plane system of video control landing
System.
Background technology
Location technology, refers to the technology for entering row positional information measure to measurement target.With the development of science and technology, in each neck
, it is necessary to which the target being accurately positioned is more and more in domain, especially dynamic mobile target is accurately positioned, has been increasingly becoming each
The key issue of industry concern.UWB location technologies have high bandwidth, low-power consumption, strong antijamming capability, transmission rate height, frequency spectrum
The features such as utilization rate is high, power system capacity is big, multi-path resolved rate is high, can in real time be positioned to dynamic object, and can ensure positioning
Precision, to realize that the automatic management that material factory goods is loaded provides reliable technical support.
The accuracy method of depopulated helicopter generally has two kinds.One is under the instruction of GPS geo-location system, it is real
Existing accuracy.Helicopter landing is guided using GPS, is current most common method.However, because gps signal penetration power is poor,
Easily influenceed and failed by above ground structure and grove.In addition, GPS can also be lost under special circumstances by US military control
Effect.Therefore, there is drawback and hidden danger using GPS guiding helicopter landings.The second is using vision guided navigation device, according to prior paving
If the instruction of signal cloth on the ground, helicopter landing is guided.Because vision guided navigation must realize identification using optical signalling, and
The optical signalling of signal cloth is very big by surrounding environment influence.Therefore, in the case where illumination is not enough, the identification of vision guided navigation device
Rate can be reduced seriously, or even None- identified signal cloth.Especially at night, vision guided navigation device must by external light source irradiation
Could normal work.Further, since signal cloth is generally laid before helicopter landing, and can not in the landing mission of helicopter
It is mobile.The landing position of depopulated helicopter according to real flight conditions, can not be thus changed in real time.Therefore, both the above method
There is a certain degree of deficiency.
Because GPS guiding can not be positioned to mobile platform exactly by US military control, and GPS guiding, simultaneously
Battlefield surroundings are complicated and changeable, and information progress is landed according to the map, and danger is higher, and continuing one kind can be flexible according to surrounding environment
Select the UAS of landing point.
Utility model content
Technical problem to be solved in the utility model is flexibly to select landing point to aid in unmanned plane according to landing field environment
Land, it is therefore intended that a kind of UAS of video control landing is provided, solve because GPS guiding is by US military control,
And GPS guiding can not be positioned to mobile platform exactly, while battlefield surroundings are complicated and changeable, information is carried out according to the map
Land is dangerous higher, continues a kind of the problem of the UAS of landing point can be flexibly selected according to surrounding environment.
The utility model is achieved through the following technical solutions：
A kind of UAS of video control landing, including remote control terminal, unmanned plane and its flight control system, fly control system
Processor, also image module, communication module and the UWB modules of connection on a processor are also associated with system；
Processor：The ambient image that image module is sent is received, ambient image is sent to communication module；Receive long-range control
The control signal that end processed is sent, sends control signals to UWB modules after processing；The location information that UWB modules are sent is received, according to
Location information is controlled to flight control system；
Image module：The ambient image around unmanned plane is gathered, image information is sent to processor；
Communication module：The ambient image that reception processing device is sent, remote control terminal is sent to by ambient image；Receive long-range
The control signal that control end is sent, sends control signals to processor；
UWB modules：The control signal that reception processing device is sent, transmitting UWB is positioned, and location information is sent into processing
Device.Unmanned plane opens image module when according to the control of remote control terminal flight to specified touchdown area, around unmanned plane
The ambient image of landing field is sent to remote control terminal by processor, communication module, and remote control terminal is according to the ring received
The suitable landing point of border image selection, sends control signal control UWB modules and the point that lands is positioned, UWB is completed after positioning
Location information is sent to processor, processor controls flight control system to complete UAV Landing according to location information.
The UWB modules include UWB transmitter modules and UWB receiving modules；
UWB transmitter modules：The control signal sent according to processor irradiates UWB to appointed place；
UWB receiving modules：The UWB points of irradiation on ground are detected, point of irradiation is positioned, location information is sent to place
Manage device.UWB transmitter modules to expecting after landing point irradiation UWB, Airborne UWB receiving module on unmanned plane according to TOA, TDOA,
RSS and AOA technologies determine the position relationship of point of irradiation and unmanned plane.During UAV Landing, remote control terminal is more
After the point of irradiation for changing UWB transmitter, the expectation landing point of unmanned plane is also changed to new point of irradiation immediately.In the landing of helicopter
During, it is possible to use UWB transmitter modules easily change target position, after the point of irradiation for changing UWB transmitter modules, nothing
Airborne UWB receiving module on man-machine captures new point of irradiation, and processor is output signals to according to new point of irradiation.
Described image module uses high-definition camera.It is easy to gather unmanned function collection using high-definition camera apparent
Ambient image, is easy to remote control terminal to select suitable landing point.
The communication module is communicated using TD-LTE.TD-LTE is used as the important opportunity of communications industry Transformation Period, bag
It is leading by China containing a large amount of Chinese patents, while having obtained extensive international support, become international standard；While upper network speed
Degree is fast, can reach tens times of TD-SCDMA technology, makes it possible ubiquitous high speed Internet access, is convenient for high definition figure
The data transfer of picture.
The utility model compared with prior art, has the following advantages and advantages：
1st, a kind of UAS of video control landing of the utility model, what remote control terminal can be passed back according to unmanned plane
Image remote controls UAV Landing, strong adaptability；
2nd, a kind of UAS of video control landing of the utility model, is guided, reliability is high using UWB.
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the utility model embodiment, constitutes the one of the application
Part, does not constitute the restriction to the utility model embodiment.In the accompanying drawings：
Fig. 1 is the utility model system structure diagram.
Embodiment
For the purpose of this utility model, technical scheme and advantage is more clearly understood, with reference to embodiment and accompanying drawing,
The utility model is described in further detail, and exemplary embodiment of the present utility model and its explanation are only used for explaining this
Utility model, is not intended as limiting of the present utility model.
Embodiment
As shown in figure 1, a kind of UAS of video of the utility model control landing, including remote control terminal, nobody
Processor, also image module, the communication module of connection on a processor are also associated with machine and its flight control system, flight control system
With UWB modules, the processor uses S12MagniV；Unmanned plane is according to the control of remote control terminal flight to specified landing
Image module is opened during region, the ambient image of landing field around unmanned plane is sent to remotely by processor, communication module
Control end, remote control terminal selects suitable landing point according to the ambient image received, sends control signal control UWB modules
To landing, point is positioned, and location information is sent into processor after UWB completion positioning, and processor controls to fly according to location information
Control system completes UAV Landing.The UWB modules include UWB transmitter modules and UWB receiving modules, and UWB sending modules are used
FREESCALE XS110, UWB receiving module are using the serial radars of NOVELDA 6100；UWB transmitter modules shine to expectation landing point
Penetrate after UWB, the Airborne UWB receiving module on unmanned plane determines point of irradiation and nobody according to TOA, TDOA, RSS and AOA technology
The position relationship of machine.During UAV Landing, after the point of irradiation of remote control terminal change UWB transmitter, unmanned plane
It is expected that landing point is also changed to new point of irradiation immediately.In the landing mission of helicopter, it is possible to use UWB transmitter modules are convenient
After ground change target position, the point of irradiation for changing UWB transmitter modules, the Airborne UWB receiving module capture on unmanned plane is new
Point of irradiation, processor is output signals to according to new point of irradiation.Described image module uses high-definition camera.Taken the photograph using high definition
As head is easy to gather the apparent ambient image of unmanned function collection, it is easy to remote control terminal to select suitable landing point.It is described
Communication module is communicated using TD-LTE.TD-LTE as communications industry Transformation Period important opportunity, comprising a large amount of Chinese
Patent, it is leading by China, while having obtained extensive international support, become international standard；Networking speed is fast simultaneously, can reach
Tens times of TD-SCDMA technology, make it possible ubiquitous high speed Internet access, are convenient for the data transfer of high-definition image.
Processor：The ambient image that image module is sent is received, ambient image is sent to communication module；Receive long-range control
The control signal that end processed is sent, sends control signals to UWB modules after processing；The location information that UWB modules are sent is received, according to
Location information is controlled to flight control system；
Image module：The ambient image around unmanned plane is gathered, image information is sent to processor；
Communication module：The ambient image that reception processing device is sent, remote control terminal is sent to by ambient image；Receive long-range
The control signal that control end is sent, sends control signals to processor；
UWB modules：The control signal that reception processing device is sent, transmitting UWB is positioned, and location information is sent into processing
Device；
UWB transmitter modules：The control signal sent according to processor irradiates UWB to appointed place；
UWB receiving modules：The UWB points of irradiation on ground are detected, point of irradiation is positioned, location information is sent to place
Manage device.
Above-described embodiment, is entered to the purpose of this utility model, technical scheme and beneficial effect
One step is described in detail, be should be understood that and be the foregoing is only embodiment of the present utility model, is not used to limit
Fixed protection domain of the present utility model, all any modifications within spirit of the present utility model and principle, made, is equally replaced
Change, improve, should be included within protection domain of the present utility model.
Claims (4)
1. a kind of UAS of video control landing, including remote control terminal, unmanned plane and its flight control system, its feature exist
In, be also associated with processor in flight control system, connection on a processor also have image module, communication module and UWB modules；
Processor：The ambient image that image module is sent is received, ambient image is sent to communication module；Receive remote control terminal
UWB modules are sent control signals to after the control signal of transmission, processing；The location information that UWB modules are sent is received, according to positioning
Information is controlled to flight control system；
Image module：The ambient image around unmanned plane is gathered, image information is sent to processor；
Communication module：The ambient image that reception processing device is sent, remote control terminal is sent to by ambient image；Receive remote control
The control signal sent is held, processor is sent control signals to；
UWB modules：The control signal that reception processing device is sent, transmitting UWB is positioned, and location information is sent into processor.
2. a kind of UAS of video control landing according to claim 1, it is characterised in that the UWB modules
Including UWB transmitter modules and UWB receiving modules；
UWB transmitter modules：The control signal sent according to processor irradiates UWB to appointed place；
UWB receiving modules：The UWB points of irradiation on ground are detected, point of irradiation is positioned, location information is sent to processing
Device.
3. a kind of UAS of video control landing according to claim 1, it is characterised in that described image module
Using high-definition camera.
4. a kind of UAS of video control landing according to claim 1, it is characterised in that the communication module
Communicated using TD-LTE.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720007841.4U CN206411519U (en) | 2017-01-04 | 2017-01-04 | A kind of UAS of video control landing |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720007841.4U CN206411519U (en) | 2017-01-04 | 2017-01-04 | A kind of UAS of video control landing |
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| Publication Number | Publication Date |
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| CN206411519U true CN206411519U (en) | 2017-08-15 |
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| CN201720007841.4U Expired - Fee Related CN206411519U (en) | 2017-01-04 | 2017-01-04 | A kind of UAS of video control landing |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106681356A (en) * | 2017-01-04 | 2017-05-17 | 四川克瑞斯航空科技有限公司 | Unmanned aerial vehicle system for guiding landing through remote control over UWB |
| CN108008739A (en) * | 2017-12-28 | 2018-05-08 | 南京航空航天大学 | A kind of unmanned plane tracking of mobile target and landing system and method |
| CN108088699A (en) * | 2017-12-15 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of unmanned unit of gobi soil sampling |
| CN108226913A (en) * | 2017-12-23 | 2018-06-29 | 成都汇蓉国科微系统技术有限公司 | A kind of full resolution pricture navigation system for second-mission aircraft All Weather Landing |
| CN108945491A (en) * | 2018-04-08 | 2018-12-07 | 北京领航智能科技发展有限公司 | Unmanned plane based on UWB precisely guides and automatic landing method |
| CN109460047A (en) * | 2018-10-23 | 2019-03-12 | 昆山优尼电能运动科技有限公司 | The unmanned plane autonomous hierarchical landing method and system of view-based access control model navigation |
-
2017
- 2017-01-04 CN CN201720007841.4U patent/CN206411519U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106681356A (en) * | 2017-01-04 | 2017-05-17 | 四川克瑞斯航空科技有限公司 | Unmanned aerial vehicle system for guiding landing through remote control over UWB |
| CN108088699A (en) * | 2017-12-15 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of unmanned unit of gobi soil sampling |
| CN108226913A (en) * | 2017-12-23 | 2018-06-29 | 成都汇蓉国科微系统技术有限公司 | A kind of full resolution pricture navigation system for second-mission aircraft All Weather Landing |
| CN108008739A (en) * | 2017-12-28 | 2018-05-08 | 南京航空航天大学 | A kind of unmanned plane tracking of mobile target and landing system and method |
| CN108945491A (en) * | 2018-04-08 | 2018-12-07 | 北京领航智能科技发展有限公司 | Unmanned plane based on UWB precisely guides and automatic landing method |
| CN109460047A (en) * | 2018-10-23 | 2019-03-12 | 昆山优尼电能运动科技有限公司 | The unmanned plane autonomous hierarchical landing method and system of view-based access control model navigation |
| CN109460047B (en) * | 2018-10-23 | 2022-04-12 | 昆山优尼电能运动科技有限公司 | Unmanned aerial vehicle autonomous graded landing method and system based on visual navigation |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20170815 Termination date: 20210104 |