CN201176264Y - Aerial mobile semi-intelligent electronic eye - Google Patents
Aerial mobile semi-intelligent electronic eye Download PDFInfo
- Publication number
- CN201176264Y CN201176264Y CNU2008200453603U CN200820045360U CN201176264Y CN 201176264 Y CN201176264 Y CN 201176264Y CN U2008200453603 U CNU2008200453603 U CN U2008200453603U CN 200820045360 U CN200820045360 U CN 200820045360U CN 201176264 Y CN201176264 Y CN 201176264Y
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Abstract
The utility model aims to provide a semi-intelligent auto-control aerial electronic eye which can fly in the sky, wherein a GPS positioning system, a light sense balanced system, a video emission system and an automatic operation system are connected on a remote control flying model, and a receiving antenna, a device electrical control system and a remote controller are arranged on the ground. The utility model has the beneficial effect that the aerial electronic eye can be widely applied on the natural disaster monitoring, ground environment protection, large-scale activity monitoring, and searches on the land or in the sea, and the independent flying system as the main carrier of the aerial electronic eye can be applied in the insecticide spraying in high altitude, artificial rain and acid rain neutralization, etc.
Description
Technical field
The utility model relates to a kind of electronic eyes of airflight, more particularly, and the electronic eyes that relates to a kind of airflight and have semi-intelligent chemical control system system.
Background technology
Find that in news report the environment monitoring personnel and the reporter that have are stopped in outdoors, the reporter's pick up camera that has is fallen, personnel are beaten, and what inconvenience was worked carries out; Present safety traffic checks that major part is by the patrol of traffic constable steering vehicle, but sometimes because traffic jam is difficult to institute's occurrence is carried out overall monitor, in time makes resolution; The still the most traditional personal monitoring of most of risk of forest fire monitorings is because personnel's deficiency causes some fire can not in time obtain finding, thereby leads to serious consequence; The marine instruments such as will setting out helicopter sometimes of searching spends huge; Super-huge activity also exists the difficult problem of surrounding environment monitoring.So, need a kind of can flight aloft, and can the automatically controlled electronic eyes.
Summary of the invention
But the purpose of this utility model provides a kind of aerial electronic eyes of semi-intelligent automatically controlled of flight aloft.
For achieving the above object, the utility model is taked following technical scheme:
The aerial semi-intelligent electronic eyes that moves, on the remote control distributor model, GPS position fixing system, light sensation balanced system, video transmission system are connected with automatic operation system respectively; Be provided with signal receiving antenna, equipment electric-control system and remote controller on ground.
The GPS position fixing system is used to gather the air position data of aircraft, and used as the required flight parameter of automatic operation system.The light sensation balanced system is used for the aerial statue information acquisition of aircraft automatic control process.Autonomous cruise speed system is the core of control, and it focuses on the data of GPS position fixing system and the data of light sensation balanced system, writes down and carry out written program in advance, is the core of whole automatic control process.The video transmission system is used for the video image that camera photographs is sent to signal receiving antenna by wireless mode.Remote controller is used for manually carrying out taking off of aircraft and lands, so this electronic eyes is the semi-intelligent electronic eyes.
Described GPS position fixing system, light sensation balanced system, video transmission system, automatic operation system, signal receiving antenna, equipment electric-control system and remote controller all can adopt prior art.
The beneficial effects of the utility model are: it can apply to the disaster monitoring widely, ground environmental protection, traffic, large-scale activity monitoring, in land, the marine search, its main carrier autonomous flight system can also be used for spraying insecticide in the high-altitude, rainmaking, acid rain and etc.
Description of drawings
Fig. 1 is the system construction drawing of the utility model embodiment;
Fig. 2 is the upward view of the model aircraft of the utility model embodiment.
Description of reference numerals: 1-model aircraft; The 2-GPS position fixing system; 3-light sensation balanced system; 4-video transmission system; The 5-autonomous cruise speed system; The 6-signal receiving antenna; 7-equipment electric-control system; The 8-remote controller.
The specific embodiment
Below in conjunction with drawings and Examples content of the present invention is described further.
As shown in Figure 1 and Figure 2, GPS position fixing system 2, light sensation balanced system 3, video transmission system 4 and autonomous cruise speed system 5 are set on model aircraft 1.GPS position fixing system 2 is installed in the fuselage; Light sensation balanced system 3 is installed on the fuselage; Video transmission system 4 is installed under the fuselage; Autonomous cruise speed system 5 is arranged in the fuselage, and is connected with GPS position fixing system 2, light sensation balanced system 3, video transmission system 4 respectively.On the ground, signal receiving antenna 6 is connected with equipment electric-control system 7, and remote controller 8 is used for taking off of telecontrolled aircraft model 1 and lands.
According to relevant place shown longitude and latitude coding on the GPS position fixing system, be allowed to condition at the course line instruction that ground station sets, 100 meters to 2000 meters height in radius 5-10 kilometer range realize that nobody controls flight or spirals.By controlling on the ground command system of staff in 10 kilometer range, be allowed to condition at the high-altitude and follow the trail of the objective, return automatically by Departure times on reverse, the place set at last.It is recorded a video the surface state of institute's route via, take pictures, synchronously with video transmission to ground receiving system, people can monitor the surface state of respective point at a distance in real time.
Operate with remote controller when model aircraft takes off, after it was elevated to certain altitude, nobody controlled flight according to instruction voluntarily.Its flight path and spatial domain all are to set according to appointed place shown longitude and latitude data on GPS, the attitude of airborne aircraft is controlled by the light sensation balancing device, and the height of airflight and the size of power are to set according to the situation of landform, depth of building and wind-force, wind direction in advance.Last it get back to the predetermined point sky according to the Departure times on reverse of setting, command its landing or allow its vertical landing that releases a parachute automatically by remote controller.
What this specification sheets was enumerated is better embodiment of the present invention only, and all equivalent technologies conversion of being done under principle of work of the present invention and thinking all are considered as protection scope of the present invention.
Claims (1)
1, the aerial semi-intelligent electronic eyes that moves, it is characterized in that: on the remote control distributor model, GPS position fixing system, light sensation balanced system, video transmission system are connected with automatic operation system respectively; Be provided with signal receiving antenna, equipment electric-control system and remote controller on ground.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008200453603U CN201176264Y (en) | 2008-03-25 | 2008-03-25 | Aerial mobile semi-intelligent electronic eye |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008200453603U CN201176264Y (en) | 2008-03-25 | 2008-03-25 | Aerial mobile semi-intelligent electronic eye |
Publications (1)
Publication Number | Publication Date |
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CN201176264Y true CN201176264Y (en) | 2009-01-07 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CNU2008200453603U Expired - Fee Related CN201176264Y (en) | 2008-03-25 | 2008-03-25 | Aerial mobile semi-intelligent electronic eye |
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CN (1) | CN201176264Y (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103657110A (en) * | 2013-12-15 | 2014-03-26 | 苏州市峰之火数码科技有限公司 | Remote control aircraft toy |
CN104061910A (en) * | 2014-07-04 | 2014-09-24 | 南京森林警察学院 | Forest burning point positioning method based on GPS receiver and two cameras |
CN104608935A (en) * | 2015-03-09 | 2015-05-13 | 杨文昊 | Model aircraft |
CN108996650A (en) * | 2018-07-12 | 2018-12-14 | 上海雁阁机电科技有限公司 | A kind of device for administering acid rain using aircraft |
-
2008
- 2008-03-25 CN CNU2008200453603U patent/CN201176264Y/en not_active Expired - Fee Related
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103657110A (en) * | 2013-12-15 | 2014-03-26 | 苏州市峰之火数码科技有限公司 | Remote control aircraft toy |
CN104061910A (en) * | 2014-07-04 | 2014-09-24 | 南京森林警察学院 | Forest burning point positioning method based on GPS receiver and two cameras |
CN104061910B (en) * | 2014-07-04 | 2016-08-24 | 南京森林警察学院 | Forest fire independent positioning method based on gps receiver and twin camera |
CN104608935A (en) * | 2015-03-09 | 2015-05-13 | 杨文昊 | Model aircraft |
CN108996650A (en) * | 2018-07-12 | 2018-12-14 | 上海雁阁机电科技有限公司 | A kind of device for administering acid rain using aircraft |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090107 |