CN202068445U - Mobile monitoring system - Google Patents
Mobile monitoring system Download PDFInfo
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- CN202068445U CN202068445U CN2011201218797U CN201120121879U CN202068445U CN 202068445 U CN202068445 U CN 202068445U CN 2011201218797 U CN2011201218797 U CN 2011201218797U CN 201120121879 U CN201120121879 U CN 201120121879U CN 202068445 U CN202068445 U CN 202068445U
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Abstract
Provided is a mobile monitoring system, comprising an aerial flight monitoring platform, an earth station system, and a remote monitoring center, wherein the aerial flight monitoring platform comprises a flight module, a navigation module, a motor speed regulation module, a monitoring equipment module, and a flight wireless data transmission module; the earth station system comprises a mobile monitoring computer, a mobile power supply module, a ground network communication module, and a ground wireless data transmission module; the remote monitoring center comprises a remote computer, a monitoring display screen, and a remote network communication module; and the aerial flight monitoring platform, the earth station system, and the remote monitoring center are in communication connection. When the mobile monitoring system is in use, the aerial flight monitoring platform is in charge of data acquisition and monitoring; the earth station system is in charge of processing data and controlling the aerial flight monitoring platform; and the remote monitoring center is in charge of remote monitoring. The mobile monitoring system features complete function, great monitoring effect, high intelligent degree, and low application difficulty.
Description
Technical field
The utility model relates to a kind of supervising device, relates in particular to a kind of mobile monitoring system, specifically is applicable to the real-time monitoring in the multiple situations such as geological disaster investigation, news photography, territory exploration, the conservation of wildlife, high-tension bus-bar inspection.
Background technology
At present, along with the high speed development of society, in fields such as fire in high buildings, news photography, territory exploration, the conservation of wildlife, geological disaster investigation, forest fire protections, people are increasing to the demand of mobile monitor.
The mobile monitor device that uses in the prior art generally adds that by helicopter, fixed-wing aircraft or fire balloon a cover wireless video monitoring equipment is formed, during use, control aircraft by skilled manipulator and fly, carry out mobile monitor by aircraft simultaneously.But this kind mobile monitor device has following defective:
At first, development along with society, people need obtain more fully information to monitored object, and this has just proposed high request to monitor data, and prior art can only provide video data, can not satisfy people's monitoring needs far away, in addition, prior art can only realize the information interchange between aerial supervising device and the ground station, and can not realize remote monitoring, the realization that this has just limited monitoring effect is unfavorable for the carrying out of subsequent operation.This shows that the function of prior art is comprehensive inadequately.
Secondly, existing mobile monitor device must a plurality of skilled manipulators be controlled, and each operation of whole mobile monitor device substantially all is independent operation, carry out separately, need mutual interchange between each link operating personnel, in case a certain link goes wrong, just can't monitor smoothly, though rely on existing automatic technology, can intelligent part operation, but because majority still is in the elementary step, thus can't be real accomplish rational overall arrangement and effectively intellectuality, this just means that each link be unable to do without skilled manipulator and participates in, in case lack effectively scheduling between the manipulator, the monitoring error will occur, thereby reduce monitoring effect.This shows that the intelligent degree of prior art is lower.
The 3rd, existing mobile monitor device takes helicopter, fixed-wing aircraft or fire balloon as aircraft, and those aircraft not only can not be in flight near the ground, and with high costs, safeguards inconvenience, so be difficult to widespread usage.This shows that the application difficulty of prior art is higher.
The Chinese patent Granted publication number is CN201753105U, Granted publication day is that the utility model patent on March 2nd, 2011 discloses a kind of aerial supervising device, it comprises unmanned vehicle, the bottom of unmanned vehicle is provided with frame, frame is provided with camera, frame comprises pair of rotary axes pedestal and a pair of motor base, be provided with rotation axis between the two rotation axis pedestals, the rotation axis two ends are rotationally connected with two rotation axis pedestals respectively, the footpath of rotation axis upwards is fixed with second drive link, camera is arranged on the rotation axis, be provided with stepping motor between two motor bases, stepping motor is fixed on the motor base, the output shaft of stepping motor and another motor base are rotationally connected, the footpath of output shaft upwards is fixed with first drive link, is provided with connecting rod between first drive link and second drive link, and the connecting rod two ends are hinged with first drive link and second drive link respectively.Though this utility model can not only be reached the spot fast, and can aloft hover and at length understand field condition, and can pass through camera omnibearing stereo floor picture, but it can only give ground station by transmitting video data, not only data are not abundant, and can not remote monitoring, thereby its function be incomplete.
Summary of the invention
The purpose of this utility model be overcome incomplete, the intelligent degree of the function that exists in the prior art lower, use higher defective and the problem of difficulty, provide more complete, the intelligent degree of a kind of function higher, use the lower mobile monitoring system of difficulty.
For realizing above purpose, technical solution of the present utility model is: a kind of mobile monitoring system, comprise airflight monitor supervision platform and earth station system, described airflight monitor supervision platform comprises flight module, watch-dog module and flight wireless data transfer module, earth station system comprises mobile monitor computer and terrestrial wireless data transmission module, terrestrial wireless data transmission module and the wireless connections of flight wireless data transfer module;
Described mobile monitoring system also comprises remote monitoring center, and remote monitoring center is connected with the earth station system network; Described airflight monitor supervision platform also comprises navigation module and electric machine speed regulation module, navigation module, electric machine speed regulation module, watch-dog module, flight wireless data transfer module all are connected with the flight module, and the flight module comprises flight controller and goes up 3-axis acceleration sensor, atmospheric pressure transducer and three axis angular rate sensors that are provided with.
Described navigation module comprises electronic compass, navigation controller and GPS positioner.
One end of described electric machine speed regulation module is connected with flight controller, and the other end is connected with brshless DC motor, and the other end of brshless DC motor is connected with screw.
Described electric machine speed regulation module is connected with flight controller by the I2C bus.
Described watch-dog module comprises video camera, infrared thermoviewer, camera or gas sensor.
Described earth station system also comprises ground network communication module and portable power source system, ground network communication module, portable power source system, terrestrial wireless data transmission module all are connected with the mobile monitor computer, described remote monitoring center comprises remote computer, monitoring display screen and remote network communication module, and the remote network communication module is connected with ground network communication module network.
Described mobile monitor computer comprises monitoring software, historical data base, man-machine interface and numerical map.
Described portable power source system comprises storage battery and inverter.
Described remote network communication module is carried out network by 3G network or cable broadband with the ground network communication module and is connected.
Compared with prior art, the beneficial effects of the utility model are:
1, because a kind of mobile monitoring system of the utility model comprises the airflight monitor supervision platform, earth station system and remote monitoring center, wherein, flight wireless data transfer module in the airflight monitor supervision platform and the terrestrial wireless data transmission module wireless connections in the earth station system, earth station system is connected with the remote monitoring center network, this design has not only realized the information interchange between airflight monitor supervision platform and the earth station system, and remote monitoring center and airflight monitor supervision platform have been realized, information interchange between the earth station system makes to the utlity model has remote control function; In addition, watch-dog module in the airflight monitor supervision platform comprises video camera, infrared thermoviewer, camera and gas sensor, navigation module comprises electronic compass, navigation controller and GPS positioner, these instruments provide abundanter information can for earth station system, remote monitoring center, are convenient to improve monitoring effect.Therefore not only function is more complete for the utility model, and monitoring effect is better.
2, because a kind of mobile monitoring system of the utility model comprises the airflight monitor supervision platform, earth station system and remote monitoring center, wherein, the airflight monitor supervision platform comprises the flight module, navigation module, the electric machine speed regulation module, watch-dog module and flight wireless data transfer module, earth station system comprises the mobile monitor computer, the portable power source system, ground network communication module and terrestrial wireless data transmission module, remote monitoring center comprises remote computer, monitoring display screen and remote network communication module, during use, each module image data and monitoring by the airflight monitor supervision platform, and be transferred to earth station system, be transferred to remote monitoring center then, the airflight monitor supervision platform is controlled according to data by the operator again, this control both can directly be made by earth station system, also can make by remote monitoring center, very convenient, and do not need as prior art, each link all must be equipped with operating personnel, not only saved manpower greatly, and overall arrangement and intelligent effect have been improved, especially being furnished with monitoring display when remote monitoring center shields, earth station system is furnished with monitoring software, historical data base, when man-machine interface and numerical map, operation will be simpler and easy, degree directly perceived will be stronger, thereby further reduce manpower, improve monitoring effect.Therefore the not only intelligent degree of the utility model is higher, and monitoring effect is better.
3, because the airflight monitor supervision platform that uses in a kind of mobile monitoring system of the utility model, earth station system and remote monitoring center all are made of various modules, not only easy to use, help improving data acquisition, signal transmission and control effect, even when a certain module goes wrong, also can directly replace and work on, greatly reduce maintenance difficulties, in addition, the airflight monitor supervision platform that the utility model is taked is with brshless DC motor, screw provides flying power, not only volume is less, and cost is lower, and flying height easy to control, suitable high suitable low, have than wide applications.Therefore application difficulty of the present utility model is lower.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the structural representation of aerial flight monitor supervision platform among Fig. 1.
Fig. 3 is the structural representation of earth station system among Fig. 1.
Fig. 4 is the structural representation of Fig. 1 medium-long range Surveillance center.
Among the figure: airflight monitor supervision platform 1, earth station system 2, remote monitoring center 3, remote computer 31, monitoring display screen 32, remote network communication module 33, flight module 4, flight controller 41,3-axis acceleration sensor 42, atmospheric pressure transducer 43, three axis angular rate sensors 44, watch-dog module 5, video camera 51, infrared thermoviewer 52, camera 53, gas sensor 54, mobile monitor computer 6, monitoring software 61, historical data base 62, man-machine interface 63, digitally Figure 64, navigation module 7, electronic compass 71, navigation controller 72, GPS positioner 73, electric machine speed regulation module 8, brshless DC motor 81, screw 82, portable power source system 9, flight wireless data transfer module 10, terrestrial wireless data transmission module 11, ground network communication module 12.
Embodiment
Below in conjunction with description of drawings and embodiment the utility model is described in further detail.
Referring to figure 1 – Fig. 4, a kind of mobile monitoring system, comprise airflight monitor supervision platform 1 and earth station system 2, described airflight monitor supervision platform 1 comprises flight module 4, watch-dog module 5 and flight wireless data transfer module 10, earth station system 2 comprises mobile monitor computer 6 and terrestrial wireless data transmission module 11, terrestrial wireless data transmission module 11 and 10 wireless connections of flight wireless data transfer module;
Described mobile monitoring system also comprises remote monitoring center 3, and remote monitoring center 3 is connected with earth station system 2 networks; Described airflight monitor supervision platform 1 also comprises navigation module 7 and electric machine speed regulation module 8, navigation module 7, electric machine speed regulation module 8, watch-dog module 5, flight wireless data transfer module 10 all are connected with flight module 4, and flight module 4 comprises flight controller 41 and goes up 3-axis acceleration sensor 42, atmospheric pressure transducer 43 and three axis angular rate sensors 44 that are provided with.
Described navigation module 7 comprises electronic compass 71, navigation controller 72 and GPS positioner 73.Effect when wherein, navigation controller 72 is selected the ARM9 main control chip is preferable.
One end of described electric machine speed regulation module 8 is connected with flight controller 41, and the other end is connected with brshless DC motor 81, and the other end of brshless DC motor 81 is connected with screw 82.
Described electric machine speed regulation module 8 is connected with flight controller 41 by the I2C bus.Wherein, electric machine speed regulation module 8 mainly is made up of microprocessor and field effect transistor.
Described watch-dog module 5 comprises video camera 51, infrared thermoviewer 52, camera 53 or gas sensor 54.
Described earth station system 2 also comprises ground network communication module 12 and portable power source system 9, ground network communication module 12, portable power source system 9, terrestrial wireless data transmission module 11 all are connected with mobile monitor computer 6, described remote monitoring center 3 comprises remote computer 31, monitoring display screen 32 and remote network communication module 33, and remote network communication module 33 is connected with ground network communication module 12 networks.
Described mobile monitor computer 6 comprises monitoring software 61, historical data base 62, man-machine interface 63 and Figure 64 digitally.
Described portable power source system 9 comprises storage battery and inverter.
Described remote network communication module 33 is carried out network by 3G network or cable broadband with ground network communication module 12 and is connected.
During use, the automatic cruising path of airflight monitor supervision platform 1 is set on digitally Figure 64 of earth station system 2 earlier, allow airflight monitor supervision platform 1 implement mobile monitor then along the route of setting, also can fly by remote manual control airflight monitor supervision platform 1, when 1 flight of airflight monitor supervision platform, the 3-axis acceleration sensor 42 that is provided with on it, atmospheric pressure transducer 43, three axis angular rate sensors 44, gas sensor 54, electronic compass 71, navigation controller 72, GPS positioner 73 can be gathered the real-time flying quality of airflight monitor supervision platform 1, as the attitude parameter that flies, longitude and latitude, highly, electric weight, flying speed etc., simultaneously, the video camera 51 that is provided with on the watch-dog module 5, infrared thermoviewer 52 or camera 53 can be gathered the video of monitored object, monitor datas such as image, monitor data of being gathered and flying quality will be by flight wireless data transfer modules 10, wireless connections between the terrestrial wireless data transmission module 11 send the mobile monitor computer 6 in the earth station system 2 to, show by man-machine interface 63 again, and handle by 61 pairs of data that send of monitoring software, simultaneously, every data when historical data base 62 meeting record airflight monitor supervision platforms 1 are executed the task each time, comprise video image, the flight attitude parameter, longitude and latitude, highly, electric weight, flying speed etc., after the operator handles by 63 pairs of data of man-machine interface, again processing signals is fed back to the flight controller 41 in the airflight monitor supervision platform 1, control by 41 pairs of airflight monitor supervision platforms 1 of flight controller then, as: by the I2C bus, machine governor module 8 changes the pwm signal duty ratio, thereby changes brshless DC motor 81, the rotating speed of screw 82; Generate an optimal route and send to flight controller 41 by navigation module 7, and in flight course, constantly proofread and correct, promptly gather the instantaneous value of current flight by GPS positioner 73 and electronic compass 71, do a comparison with the route of setting again and whether depart from the route that sets to draw, thereby realize a closed-loop control, and then finish the go home route of function of automatic cruising, a key and set.In addition, can also pass through remote network communication module 33, ground network communication module 12 and realize that earth station systems 2 are connected with network between the remote monitoring center 3, connect or the cable broadband connection as 3G network, thereby realization remote monitoring function, be about to real-time Data Transmission to remote computer 31, and on monitoring display screen 32, show, the user just can have a real-time understanding to flight monitoring situation in remote monitoring center 3, and can on network, pass through cryptographic acess earth station system 2, and it is carried out remote control.
In use, the portable power source system 9 that is made up of a jumbo storage battery, inverter is responsible for giving earth station system 2 power supplies and charges for airflight monitor supervision platform 1.It at least can be for earth station system 2 continuous operations more than 50 hours, and simultaneously, when airflight monitor supervision platform 1 electric weight was not enough, its earth station system 2 that can fly back carried out supply.This portable power source system 9 adopts lithium battery equilibrium charging technology, can protect the electric power system of earth station system 2 to a greater extent.
Therefore the utility model is not only multiple functional, monitoring effect is better, and intelligent degree is higher, it is lower to use difficulty.
Claims (8)
1. mobile monitoring system, comprise airflight monitor supervision platform (1) and earth station system (2), described airflight monitor supervision platform (1) comprises flight module (4), watch-dog module (5) and flight wireless data transfer module (10), earth station system (2) comprises mobile monitor computer (6) and terrestrial wireless data transmission module (11), terrestrial wireless data transmission module (11) and the wireless connections of flight wireless data transfer module (10) is characterized in that:
Described mobile monitoring system also comprises remote monitoring center (3), and remote monitoring center (3) is connected with earth station system (2) network; Described airflight monitor supervision platform (1) also comprises navigation module (7) and electric machine speed regulation module (8), navigation module (7), electric machine speed regulation module (8), watch-dog module (5), flight wireless data transfer module (10) all are connected with flight module (4), and flight module (4) comprises flight controller (41) and goes up 3-axis acceleration sensor (42), the atmospheric pressure transducer (43) and three axis angular rate sensors (44) that is provided with.
2. a kind of mobile monitoring system according to claim 1 is characterized in that: described navigation module (7) comprises electronic compass (71), navigation controller (72) and GPS positioner (73).
3. a kind of mobile monitoring system according to claim 1, it is characterized in that: an end of described electric machine speed regulation module (8) is connected with flight controller (41), the other end is connected with brshless DC motor (81), and the other end of brshless DC motor (81) is connected with screw (82).
4. a kind of mobile monitoring system according to claim 3 is characterized in that: described electric machine speed regulation module (8) is connected with flight controller (41) by the I2C bus.
5. a kind of mobile monitoring system according to claim 1 is characterized in that: described watch-dog module (5) comprises video camera (51), infrared thermoviewer (52), camera (53) or gas sensor (54).
6. a kind of mobile monitoring system according to claim 1, it is characterized in that: described earth station system (2) also comprises ground network communication module (12) and portable power source system (9), ground network communication module (12), portable power source system (9), terrestrial wireless data transmission module (11) all are connected with mobile monitor computer (6), described remote monitoring center (3) comprises remote computer (31), monitoring display screen (32) and remote network communication module (33), and remote network communication module (33) is connected with ground network communication module (12) network.
7. a kind of mobile monitoring system according to claim 6 is characterized in that: described portable power source system (9) comprises storage battery and inverter.
8. a kind of mobile monitoring system according to claim 6 is characterized in that: described remote network communication module (33) is carried out network by 3G network or cable broadband with ground network communication module (12) and is connected.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201218797U CN202068445U (en) | 2011-04-23 | 2011-04-23 | Mobile monitoring system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN2011201218797U CN202068445U (en) | 2011-04-23 | 2011-04-23 | Mobile monitoring system |
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| CN202068445U true CN202068445U (en) | 2011-12-07 |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102984207A (en) * | 2012-11-06 | 2013-03-20 | 太仓市同维电子有限公司 | Method for achieving remote monitoring information communication |
| CN103002012A (en) * | 2012-11-06 | 2013-03-27 | 太仓市同维电子有限公司 | Method for implementing remote communication of monitoring information |
| CN104700576A (en) * | 2015-03-27 | 2015-06-10 | 徐州飞梦电子科技有限公司 | Quick water rescuing system and method |
| CN104811674A (en) * | 2015-05-22 | 2015-07-29 | 郑君雄 | Prison intelligent security device based on multi-rotor unmanned aerial vehicle |
| CN105699599A (en) * | 2016-03-01 | 2016-06-22 | 徐海慧 | Air quality detection device used in infectious disease isolation room |
| CN106162050A (en) * | 2015-03-25 | 2016-11-23 | 宇瞻科技股份有限公司 | Indoor monitoring system and method thereof |
| CN106200667A (en) * | 2016-09-05 | 2016-12-07 | 南京理工大学 | Petrochemical iy produced site intelligent cruising inspection system |
| CN106325300A (en) * | 2016-10-21 | 2017-01-11 | 广东容祺智能科技有限公司 | Remote condition monitoring and controlling system of unmanned aerial vehicle based on GSM-4G communication |
| CN106341587A (en) * | 2016-10-26 | 2017-01-18 | 许云龙 | Simple yet highly effective VR recorder |
| CN106507049A (en) * | 2016-11-18 | 2017-03-15 | 河南中医药大学 | A kind of remote wireless monitoring system based on GIS-Geographic Information System |
| CN106803938A (en) * | 2017-03-01 | 2017-06-06 | 张琛 | A kind of no worker monitor aircraft |
| CN106899836A (en) * | 2017-03-31 | 2017-06-27 | 大庆安瑞达科技开发有限公司 | The air-ground integrated maneuvering platform of alert enterprise's linkage |
| CN106909169A (en) * | 2017-03-30 | 2017-06-30 | 广东容祺智能科技有限公司 | A kind of full automatic power patrol UAV system |
| CN106989728A (en) * | 2017-03-21 | 2017-07-28 | 广东容祺智能科技有限公司 | A kind of building ground mapping system based on unmanned plane |
-
2011
- 2011-04-23 CN CN2011201218797U patent/CN202068445U/en not_active Expired - Fee Related
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102984207A (en) * | 2012-11-06 | 2013-03-20 | 太仓市同维电子有限公司 | Method for achieving remote monitoring information communication |
| CN103002012A (en) * | 2012-11-06 | 2013-03-27 | 太仓市同维电子有限公司 | Method for implementing remote communication of monitoring information |
| CN106162050A (en) * | 2015-03-25 | 2016-11-23 | 宇瞻科技股份有限公司 | Indoor monitoring system and method thereof |
| CN104700576A (en) * | 2015-03-27 | 2015-06-10 | 徐州飞梦电子科技有限公司 | Quick water rescuing system and method |
| CN104811674A (en) * | 2015-05-22 | 2015-07-29 | 郑君雄 | Prison intelligent security device based on multi-rotor unmanned aerial vehicle |
| CN105699599A (en) * | 2016-03-01 | 2016-06-22 | 徐海慧 | Air quality detection device used in infectious disease isolation room |
| CN106200667A (en) * | 2016-09-05 | 2016-12-07 | 南京理工大学 | Petrochemical iy produced site intelligent cruising inspection system |
| CN106325300A (en) * | 2016-10-21 | 2017-01-11 | 广东容祺智能科技有限公司 | Remote condition monitoring and controlling system of unmanned aerial vehicle based on GSM-4G communication |
| CN106341587A (en) * | 2016-10-26 | 2017-01-18 | 许云龙 | Simple yet highly effective VR recorder |
| CN106507049A (en) * | 2016-11-18 | 2017-03-15 | 河南中医药大学 | A kind of remote wireless monitoring system based on GIS-Geographic Information System |
| CN106803938A (en) * | 2017-03-01 | 2017-06-06 | 张琛 | A kind of no worker monitor aircraft |
| CN106989728A (en) * | 2017-03-21 | 2017-07-28 | 广东容祺智能科技有限公司 | A kind of building ground mapping system based on unmanned plane |
| CN106909169A (en) * | 2017-03-30 | 2017-06-30 | 广东容祺智能科技有限公司 | A kind of full automatic power patrol UAV system |
| CN106899836A (en) * | 2017-03-31 | 2017-06-27 | 大庆安瑞达科技开发有限公司 | The air-ground integrated maneuvering platform of alert enterprise's linkage |
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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: 20111207 Termination date: 20140423 |