CN105151309A - Unmanned aerial vehicle achieving positioning and landing through image recognition - Google Patents
Unmanned aerial vehicle achieving positioning and landing through image recognition Download PDFInfo
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- CN105151309A CN105151309A CN201510600158.7A CN201510600158A CN105151309A CN 105151309 A CN105151309 A CN 105151309A CN 201510600158 A CN201510600158 A CN 201510600158A CN 105151309 A CN105151309 A CN 105151309A
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Abstract
An unmanned aerial vehicle achieving positioning and landing through image recognition is characterized by comprising a vehicle body, electric rotor wings, a flight state computer control system, a remote controller and a ground control center; one or more shooting devices are arranged at the bottom of the vehicle body, and the shooting device is in signal connection with a host of the flight state computer control system; and the flight state computer control system carries out the comparison analysis on pictures provided by the shooting device in real time and picture information in a database, and a flight instruction is given comprehensively to control the unmanned aerial vehicle to fly and land. For a remote control aircraft only executing the flight task in the small space range, positioning of the remote control aircraft can be well achieved through image recognition, and aircraft explosion is avoided. Under the situation, the number of needed software and hardware resources is not large. The communication secrecy performance is good through communication optical fibers or power transmission lines. An external power source can prolong the hang time of the unmanned aerial vehicle.
Description
Technical field
The present invention relates to the unmanned plane relying on image recognition location and landing.
Background technology
Existing a kind of remotely-piloted vehicle can position by satellite positioning-terminal, and it can perform aerial mission at various complex condition.But when person who is ambitious or tenacious of purpose adopts false satellite positioning signal to cheat it, it likely can be infected and drop to the place of mistake.Further, the remotely-piloted vehicle utilizing satellite positioning-terminal to locate is easy to aircraft bombing and namely falls near high building, it is said that high building has blocked satellite-signal and/or the reflection of high building to radio signal causes.Remotely-piloted vehicle of the present invention and unmanned plane are same things.
Summary of the invention
The object of the invention is to provide a kind of new remotely-piloted vehicle location technology.
The present invention realizes the technical scheme of its object: manufacture the unmanned plane that relies on image recognition location and landing, comprise fuselage, electronic rotor, state of flight computer control system and remote controller, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module; Contain more than one picture pick-up device at fuselage bottom, picture pick-up device is connected with state of flight computer control system host signal; State of flight computer control system, by carrying out analyzing and processing to the picture that picture pick-up device provides in real time, comprises and comparing with the pictorial information of data bank, comprehensively goes out flight directive and controls unmanned plane during flying landing.
Also can adopt the power transmission line be connected with external power supply, external power supply supplies unmanned plane continuously by power transmission line.
Also can adopt a power line communication module, utilize power line communication module and power transmission line to realize the communication with ground.
Can also adopt a communication optical fiber, unmanned plane utilizes communication optical fiber to realize the communication with ground.
Beneficial effect: at least, for the remotely-piloted vehicle only performing aerial mission a little spatial dimension, relies on image recognition technology not only can realize the location of remotely-piloted vehicle well, avoids aircraft bombing, can also realize accurate landing; And the software and hardware resources in the case, required for it is also few.Communication optical fiber or power transmission line is utilized to realize communication security performance good.External power supply can extend the hang time of unmanned plane.
Accompanying drawing explanation
Fig. 1 is a unmanned plane fundamental diagram at the scene relying on image recognition location and landing.
Fig. 2 is the amplification feature of shaft in Fig. 1 and poroid thing.
In figure, 1. unmanned plane; 2. fuselage; 3. electronic rotor; 4. remote controller; 5. ground control center; 6. picture pick-up device; 8. external power supply; 9. power transmission line; 10. logistics car; 11. power line communication modules; 14. shut down cooperation interface; 15. vehicle bodies; 16. carrier aircrafts coordinate interface; 17. shafts; 18. poroid things; 19. grooves; 22. through holes; 23. dead bolts.
Detailed description of the invention
Fig. 1 provides embodiment 1.
In embodiment 1, manufacture the unmanned plane 1 that relies on image recognition location and landing, comprise fuselage 2, electronic rotor 3, state of flight computer control system and remote controller 4, and adopt a ground control center 5; State of flight computer control system is connected with ground control center 5 signal and accepts the control of ground control center 5; State of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module; Containing more than one picture pick-up device 6 bottom fuselage 2, picture pick-up device 6 is connected with state of flight computer control system host signal; State of flight computer control system is compared by the pictorial information of the picture that provides in real time picture pick-up device 6 and data bank, comprehensively goes out flight directive and controls unmanned plane during flying landing.
And adopting external power supply 8 and a power transmission line 9 be connected with external power supply 8, external power supply 8 supplies unmanned plane 1 continuously by power transmission line 9.External power supply 8 is arranged at ground control center 5 place, comprises and being loaded on a logistics car 10.
Unmanned plane 1 and ground control center 5 respectively adopt a power line communication module 11, and power line communication module 11 is connected with power transmission line 9 signal, and unmanned plane 1 utilizes power line communication module 11 and power transmission line 9 to realize the communication with ground control center 5.
Fuselage 2 comprises one and shuts down cooperation interface 14, and logistics car 10 comprises vehicle body 15, and the top of vehicle body 15 comprises a carrier aircraft and coordinates interface 16.
Shut down and coordinate interface 14 to comprise two or more shaft 17; Carrier aircraft coordinates interface 16 to comprise the poroid thing 18 of two or more, and each shaft 17 can realize plug-in type with each poroid thing 18 and be connected.
The end of shaft 17 is wedge shape, and shaft 17 is containing a groove 19; A through hole 22 is contained in the side of poroid thing 18, arranges a dead bolt 23 in through hole 22, and dead bolt 23 can move along through hole 22, and time in the groove 19 of the shaft 18 that dead bolt 23 deeply falls, shaft 17 is locked.
Shut down the design coordinating interface to coordinate the form at interface to adopt other different as required from carrier aircraft.
Embodiment 1 can also be done like this: do not use power line communication module, but makes unmanned plane and ground control center respectively adopt an optical fiber communication modules and adopt a communication optical fiber; Unmanned plane and ground control center respectively adopt an optical fiber communication modules and adopt a communication optical fiber; Communication optical fiber connects unmanned plane 1 and ground control center 5, and optical fiber communication modules is connected with communication optical fiber signal, and unmanned plane 1 utilizes optical fiber communication modules and communication optical fiber to realize the communication with ground control center 5.
Insulating barrier or the communication optical fiber of communication optical fiber embedding power transmission line 9 are connected together with power transmission line 9.The transfer rate that communication optical fiber provides is high.
Claims (6)
1. rely on the unmanned plane of image recognition location and landing, it is characterized in that comprising fuselage, electronic rotor, state of flight computer control system and remote controller; Fuselage is provided with more than one picture pick-up device, and picture pick-up device is connected with state of flight computer control system host signal; State of flight computer control system, by carrying out analyzing and processing to the picture that picture pick-up device provides in real time, comprehensively goes out flight directive and controls unmanned plane during flying landing.
2., according to the unmanned plane that dependence image recognition according to claim 1 is located and landed, it is characterized in that comprising external power supply and a power transmission line be connected with external power supply, external power supply supplies unmanned plane continuously by power transmission line.
3. according to the unmanned plane that dependence image recognition according to claim 2 is located and landed, it is characterized in that also comprising ground control center, unmanned plane and ground control center respectively adopt a power line communication module, power line communication module is connected with powerline signal, and unmanned plane utilizes power line communication module and power transmission line to realize the communication with ground control center.
4., according to the unmanned plane that dependence image recognition according to claim 2 is located and landed, it is characterized in that also comprising a communication optical fiber, unmanned plane and ground control center respectively adopt an optical fiber communication modules and adopt a communication optical fiber; Communication optical fiber connects unmanned plane and ground control center, and optical fiber communication modules is connected with communication optical fiber signal, and unmanned plane utilizes optical fiber communication modules and communication optical fiber to realize the communication with ground control center.
5., according to the unmanned plane that the dependence image recognition described in claims 1 or 2 is located and landed, it is characterized in that comprising fuselage comprises a shutdown cooperation interface, shuts down cooperation interface and coordinates interface fit to be connected with the carrier aircraft in the external world.
6., according to the unmanned plane that dependence image recognition according to claim 5 is located and landed, it is characterized in that shutting down cooperation interface comprises two or more shaft; Carrier aircraft coordinates interface to comprise the poroid thing of two or more, and described shaft and poroid thing can realize plug-in type and be connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510600158.7A CN105151309A (en) | 2015-09-18 | 2015-09-18 | Unmanned aerial vehicle achieving positioning and landing through image recognition |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201510600158.7A CN105151309A (en) | 2015-09-18 | 2015-09-18 | Unmanned aerial vehicle achieving positioning and landing through image recognition |
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| CN105151309A true CN105151309A (en) | 2015-12-16 |
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| CN201510600158.7A Withdrawn CN105151309A (en) | 2015-09-18 | 2015-09-18 | Unmanned aerial vehicle achieving positioning and landing through image recognition |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105857630A (en) * | 2016-03-30 | 2016-08-17 | 乐视控股（北京）有限公司 | Parking apron device, aircraft and aircraft parking system |
| CN106054918A (en) * | 2016-05-30 | 2016-10-26 | 北京小米移动软件有限公司 | Method and device for providing information of unmanned aerial vehicle |
| CN106355866A (en) * | 2016-11-14 | 2017-01-25 | 徐志勇 | Unmanned aerial vehicle detection image storage analytic system |
| CN106628211A (en) * | 2017-03-16 | 2017-05-10 | 山东大学 | Ground guiding type unmanned aerial vehicle flying landing system and method based on LED dot matrix |
| CN107140145A (en) * | 2017-04-27 | 2017-09-08 | 上海大学 | A kind of unmanned boat folding and unfolding unmanned plane device |
| WO2018024069A1 (en) * | 2016-08-04 | 2018-02-08 | 北京京东尚科信息技术有限公司 | Method, device and system for guiding unmanned aerial vehicle to land |
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| US20040239561A1 (en) * | 2003-04-03 | 2004-12-02 | Durban Jack P. | Automated portable remote robotic transceiver with directional antenna |
| WO2010048919A1 (en) * | 2008-10-31 | 2010-05-06 | Lfk-Lenkflugkörpersysteme Gmbh | Multi-functional servicing and test unit for unmanned flying objects |
| CN102417037A (en) * | 2010-09-28 | 2012-04-18 | 株式会社拓普康 | Automatic taking-off and landing system |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857630A (en) * | 2016-03-30 | 2016-08-17 | 乐视控股（北京）有限公司 | Parking apron device, aircraft and aircraft parking system |
| CN106054918A (en) * | 2016-05-30 | 2016-10-26 | 北京小米移动软件有限公司 | Method and device for providing information of unmanned aerial vehicle |
| WO2018024069A1 (en) * | 2016-08-04 | 2018-02-08 | 北京京东尚科信息技术有限公司 | Method, device and system for guiding unmanned aerial vehicle to land |
| US11383857B2 (en) | 2016-08-04 | 2022-07-12 | Beijing Jingdong Qianshi Technology Co., Ltd. | Method, device and system for guiding unmanned aerial vehicle to land |
| CN106355866A (en) * | 2016-11-14 | 2017-01-25 | 徐志勇 | Unmanned aerial vehicle detection image storage analytic system |
| CN106628211A (en) * | 2017-03-16 | 2017-05-10 | 山东大学 | Ground guiding type unmanned aerial vehicle flying landing system and method based on LED dot matrix |
| CN106628211B (en) * | 2017-03-16 | 2019-02-26 | 山东大学 | Ground control formula unmanned plane during flying landing system and method based on LED dot matrix |
| CN107140145A (en) * | 2017-04-27 | 2017-09-08 | 上海大学 | A kind of unmanned boat folding and unfolding unmanned plane device |
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Address after: Taizhou City, Zhejiang province 317500 Wenling City Taiping Street South Road 109 Lane 9 Applicant after: Shi Guoliang Address before: 200335 Changning District, Gan Xi Road, Lane 100, room 30, No. 502, room Applicant before: Shi Guoliang |
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20151216 |
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| WW01 | Invention patent application withdrawn after publication |