CN107861519A - A kind of unmanned plane landing control system - Google Patents
A kind of unmanned plane landing control system Download PDFInfo
- Publication number
- CN107861519A CN107861519A CN201711078714.4A CN201711078714A CN107861519A CN 107861519 A CN107861519 A CN 107861519A CN 201711078714 A CN201711078714 A CN 201711078714A CN 107861519 A CN107861519 A CN 107861519A
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- Prior art keywords
- unmanned plane
- control system
- landing
- wireless
- information
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- 238000004891 communication Methods 0.000 claims abstract description 7
- 238000012937 correction Methods 0.000 claims abstract description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 4
- 230000010365 information processing Effects 0.000 claims description 3
- 238000012856 packing Methods 0.000 claims description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of unmanned plane landing control system, including wireless locating base station, terrestrial wireless control system and at least two unmanned plane, it is characterised in that：3G communication modules, identification radio frequency encoding, wireless location label, position correction module and time block are integrated in the flight-control computer that the unmanned plane includes.The present invention solves unmanned plane landing phases, the technical problem of position inaccurate, and between automatically controlling at the beginning of the landing of each unmanned plane, when making multiple unmanned plane needs be landed, landed according to set order, cost is low, strong applicability, strong antijamming capability, accurate positioning.
Description
Technical field
The present invention relates to unmanned plane field, in particular to a kind of unmanned plane landing control system.
Background technology
The flight of unmanned plane generally comprise take off, airline operation and landing three phases, it is most at present it is civilian nobody
Machine is all using location navigation modes such as GPS or big-dipper satellites, and precision is typically in 5m~10m or so, and these three stages make
With this positioning method.Because course sector is relatively spacious, thus in the airline operation stage of centre, it is allowed to 5m~10m be present
Position error, and in landing phases, course line is relatively busy, it is necessary to accurately drop to specified point and will be according to set priority
Order is landed.But existing positioning precision is difficult to ensure that unmanned plane lands in specified point, and nobody can not be automatically controlled
The beginning landing time of machine so that drifted off the course during landing.
The content of the invention
In order to solve the above technical problems, The present invention provides a kind of unmanned plane landing control system, including wireless location
Base station, terrestrial wireless control system and at least two unmanned plane, 3G is integrated in the flight-control computer that the unmanned plane includes
Communication module, identification radio frequency encoding, wireless location label, position correction module and time block；
The identification radio frequency encoding sends the unique identification coding of unmanned plane；
The 3G communication modules are used to be communicated with terrestrial wireless control system；
The wireless location label receives the positioning radio wave that terrestrial wireless control system is sent and replys wireless pulses
Signal；
The wireless locating base station catches the wireless pulse signals, and by wireless pulse signals and its information at time point
Send to terrestrial wireless control system；
The terrestrial wireless control, the wireless pulse signals are processed into the three-dimensional coordinate information of unmanned plane, by described in
Landing timing information of the information processing at time point into unmanned plane；And by the three-dimensional coordinate information and landing timing information according to
The unique identification coding information carries out data packing, is sent to the unmanned plane of response；
The position correction module, the position of unmanned plane is modified according to the three-dimensional coordinate information；
The time block opens landing according to the landing timing information after the specified time.
Further, the terrestrial wireless control system also includes alarm module and manual rectification module；
The alarm module deviates preset coordinate threshold range in unmanned plane and does not press the landing sequential in unmanned plane
When information is landed, alarmed, and start position automatically amendment and landing sequential correct automatically；
The manual rectification module, in unmanned plane forfeiture position during automatic capability for correcting, aligning is carried out to it.
Compared with prior art, the beneficial effects of the invention are as follows：
The present invention solves unmanned plane landing phases, the technical problem of position inaccurate, and can automatically control it is each nobody
Machine land at the beginning of between, when multiple unmanned plane needs is landed, landed according to set order, cost is low, suitable
With property is strong, strong antijamming capability, accurate positioning.
Brief description of the drawings
The accompanying drawing of the present invention is used for providing further understanding of the present application, forms the part of the application, attached at these
Same or analogous part is represented in figure using identical reference number, in the accompanying drawings：
Fig. 1 is the circuit theory schematic diagram of the present invention.
Embodiment
To make the purpose, technical scheme and advantage of the application clearer, below in conjunction with drawings and the specific embodiments, to this
Application is described in further detail, and the schematic description and description of the application is used to explain the application, composition pair
The improper restriction of the application.
As shown in figure 1, a kind of unmanned plane landing control system of the present embodiment, a kind of unmanned plane landing control system, bag
Wireless locating base station, terrestrial wireless control system and at least two unmanned plane are included, in the flight-control computer that unmanned plane includes
Integrated 3G communication modules, identification radio frequency encoding, wireless location label, position correction module and time block.Identification
Radio frequency encoding sends the unique identification coding of unmanned plane；3G communication modules are used to be communicated with terrestrial wireless control system；Nothing
Line positioning label receives the positioning radio wave that terrestrial wireless control system is sent and replys wireless pulse signals；Wireless location base
Stand and catch wireless pulse signals, and the information of wireless pulse signals and its time point is sent to terrestrial wireless control system；Ground
Face controlled in wireless, wireless pulse signals are processed into the three-dimensional coordinate information of unmanned plane, by the information processing at time point into nobody
The landing timing information of machine；And three-dimensional coordinate information and landing timing information are subjected to data according to unique identification coding information and beaten
Bag, it is sent to the unmanned plane of response；Position correction module, the position of unmanned plane is modified according to three-dimensional coordinate information；It is fixed
When module according to landing timing information landing is opened after the specified time.
Wherein, terrestrial wireless control system also includes alarm module and manual rectification module；Alarm module is inclined in unmanned plane
From preset coordinate threshold range and when unmanned plane is not landed by landing timing information, alarmed, and start position
Automatic amendment and landing sequential is corrected automatically；Manual rectification module, in unmanned plane forfeiture position during automatic capability for correcting, it is entered
Row aligning.
The present embodiment describes more specific and detailed, also gives some advantageous measures of embodiment, still, the implementation
Example and advantageous measure can not be used as limitation of the present invention, when those skilled in the art sees the program, make other
Deformation and the replacement of equivalent arrangements, all should be within protection scope of the present invention.
Claims (2)
- The control system 1. a kind of unmanned plane lands, including wireless locating base station, terrestrial wireless control system and at least two nobody Machine, it is characterised in that：3G communication modules are integrated in the flight-control computer that the unmanned plane includes, identification radio frequency is compiled Code, wireless location label, position correction module and time block；The identification radio frequency encoding sends the unique identification coding of unmanned plane；The 3G communication modules are used to be communicated with terrestrial wireless control system；The wireless location label receives the positioning radio wave that terrestrial wireless control system is sent and replys wireless pulse signals；The wireless locating base station catches the wireless pulse signals, and wireless pulse signals and its information at time point are sent To terrestrial wireless control system；The terrestrial wireless control, the wireless pulse signals are processed into the three-dimensional coordinate information of unmanned plane, by the time Landing timing information of the information processing of point into unmanned plane；And by the three-dimensional coordinate information and landing timing information according to described Unique identification coding information carries out data packing, is sent to the unmanned plane of response；The position correction module, the position of unmanned plane is modified according to the three-dimensional coordinate information；The time block opens landing according to the landing timing information after the specified time.
- A kind of 2. unmanned plane landing control system according to claim 1, it is characterised in that：The terrestrial wireless control system System also includes alarm module and manual rectification module；The alarm module deviates preset coordinate threshold range in unmanned plane and does not press the landing timing information in unmanned plane When being landed, alarmed, and start position automatically amendment and landing sequential correct automatically；The manual rectification module, in unmanned plane forfeiture position during automatic capability for correcting, aligning is carried out to it.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711078714.4A CN107861519A (en) | 2017-11-06 | 2017-11-06 | A kind of unmanned plane landing control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711078714.4A CN107861519A (en) | 2017-11-06 | 2017-11-06 | A kind of unmanned plane landing control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107861519A true CN107861519A (en) | 2018-03-30 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201711078714.4A Withdrawn CN107861519A (en) | 2017-11-06 | 2017-11-06 | A kind of unmanned plane landing control system |
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| CN (1) | CN107861519A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108829135A (en) * | 2018-07-28 | 2018-11-16 | 深圳市烽焌信息科技有限公司 | Unmanned plane charging base station with high recharge efficiency |
| CN109446955A (en) * | 2018-10-17 | 2019-03-08 | 南京理工大学泰州科技学院 | A kind of image processing method, device, unmanned plane and server |
| CN111368971A (en) * | 2020-02-19 | 2020-07-03 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned aerial vehicle cluster cooperative landing sequencing method and system |
| CN114137569A (en) * | 2021-09-26 | 2022-03-04 | 碧空环境科技有限公司 | Pollution traceability system based on laser radar and unmanned aerial vehicle combination |
| CN114935946A (en) * | 2022-07-21 | 2022-08-23 | 浙江这里飞科技有限公司 | Unmanned aerial vehicle landing method and device |
| CN116996105A (en) * | 2023-07-03 | 2023-11-03 | 中国舰船研究设计中心 | Aircraft correction instruction transmission link design method based on radio frequency integration |
-
2017
- 2017-11-06 CN CN201711078714.4A patent/CN107861519A/en not_active Withdrawn
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108829135A (en) * | 2018-07-28 | 2018-11-16 | 深圳市烽焌信息科技有限公司 | Unmanned plane charging base station with high recharge efficiency |
| CN109446955A (en) * | 2018-10-17 | 2019-03-08 | 南京理工大学泰州科技学院 | A kind of image processing method, device, unmanned plane and server |
| CN111368971A (en) * | 2020-02-19 | 2020-07-03 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned aerial vehicle cluster cooperative landing sequencing method and system |
| CN111368971B (en) * | 2020-02-19 | 2021-01-08 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned aerial vehicle cluster cooperative landing sequencing method and system |
| CN114137569A (en) * | 2021-09-26 | 2022-03-04 | 碧空环境科技有限公司 | Pollution traceability system based on laser radar and unmanned aerial vehicle combination |
| CN114935946A (en) * | 2022-07-21 | 2022-08-23 | 浙江这里飞科技有限公司 | Unmanned aerial vehicle landing method and device |
| CN116996105A (en) * | 2023-07-03 | 2023-11-03 | 中国舰船研究设计中心 | Aircraft correction instruction transmission link design method based on radio frequency integration |
| CN116996105B (en) * | 2023-07-03 | 2024-05-14 | 中国舰船研究设计中心 | Aircraft correction instruction transmission link design method based on radio frequency integration |
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| Date | Code | Title | Description |
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| PB01 | Publication | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180330 |
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| WW01 | Invention patent application withdrawn after publication |