CN208076624U - space electromagnetic environment monitoring device and system - Google Patents
space electromagnetic environment monitoring device and system Download PDFInfo
- Publication number
- CN208076624U CN208076624U CN201820425931.XU CN201820425931U CN208076624U CN 208076624 U CN208076624 U CN 208076624U CN 201820425931 U CN201820425931 U CN 201820425931U CN 208076624 U CN208076624 U CN 208076624U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- electromagnetic radiation
- airborne
- electromagnetic environment
- wireless communication
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
A kind of space electromagnetic environment monitoring device of the utility model offer and system, are related to unmanned plane and electromagnetic field measurements field, there is a problem of that user experience is poor to alleviate existing space electromagnetic environment monitoring method, can improve user experience.The space electromagnetic environment monitoring device includes：Unmanned plane, airborne electromagnetic radiation monitor, on-board data Acquisition Instrument, ground data terminal；Wherein, airborne electromagnetic radiation monitor and on-board data Acquisition Instrument are arranged on unmanned plane, and airborne electromagnetic radiation monitor is connected with on-board data Acquisition Instrument, and on-board data Acquisition Instrument is connected with ground data terminal；Airborne electromagnetic radiation monitor is used to monitor the electromagnetic environment in space, obtains electromagnetic environment data；On-board data Acquisition Instrument is used to obtain the electromagnetic environment data of airborne electromagnetic radiation monitor, and by electromagnetic environment data transmission to the ground data terminal.
Description
Technical field
The utility model is related to space exploration technical fields, more particularly, to a kind of space electromagnetic environment monitoring device and sky
Between electromagnetic environment monitoring system.
Background technology
Currently, conventional electromagnetic environment monitor is to use portable electromagnetic monitoring instrument, can be reached in monitoring personnel
Place or the hand-held measurement of personnel, or tripod is set up, electromagnetic field monitoring probe is erected on tripod, is connected by optical fiber
Host is monitored, the hand-held monitoring host of monitoring personnel is read.However this monitoring can only be on the ground that monitoring personnel can reach
Side is monitored, and in the place that personnel are difficult to reach, especially AC power transmission and transformation project, intermediate waves transmitting station, mobile communication
Electromagnetic field in antenna for base station peripheral space is monitored, and existing monitoring means cannot be satisfied this requirement of user, cause
User experience is not high.
To sum up, existing electromagnetic environment monitor has that user experience is poor.
Utility model content
In view of this, the purpose of this utility model is to provide space electromagnetic environment monitoring device and system, it is existing to alleviate
With the presence of the problem that the electromagnetic environment monitor user experience in technology is poor.
In a first aspect, the utility model embodiment provides a kind of space electromagnetic environment monitoring device, the spatial electromagnetic ring
Border monitoring device includes：Unmanned plane, airborne electromagnetic radiation monitor, on-board data Acquisition Instrument, ground data terminal；
Wherein, the airborne electromagnetic radiation monitor and the on-board data Acquisition Instrument are arranged on the unmanned plane,
The airborne electromagnetic radiation monitor is connected with the on-board data Acquisition Instrument, the on-board data Acquisition Instrument and the ground
Data terminal is connected；
The airborne electromagnetic radiation monitor is used to monitor the electromagnetic environment data in space；
The on-board data Acquisition Instrument is used to obtain the electromagnetic environment data of airborne electromagnetic radiation monitor, and by the electricity
Magnetic environment data transmission is to the ground data terminal.
With reference to first aspect, the utility model embodiment provides the first possible embodiment of first aspect,
In, the ground data terminal includes remote controler and video data terminal, and the video data terminal is connected with the remote controler
It connects, the video data terminal is for showing monitoring information；The remote controler is wirelessly communicated with the unmanned plane by unmanned plane
System is communicated.
With reference to first aspect, the utility model embodiment provides second of possible embodiment of first aspect,
In, the ground data terminal includes remote controler and video data terminal, and the remote controler passes through unmanned plane with the unmanned plane
Communication system is communicated, and the on-board data Acquisition Instrument includes the first wireless communication module, and the video data terminal includes
Second wireless communication module, first wireless communication module constitute another wireless communication with second wireless communication module and are
System, the on-board data Acquisition Instrument are communicated by the wireless communication system and the video data terminal.
With reference to first aspect, the utility model embodiment provides the third possible embodiment of first aspect,
In, the airborne electromagnetic radiation monitor is arranged in the upper end at the center of unmanned aerial vehicle body.
The third possible embodiment with reference to first aspect, the utility model embodiment provide the of first aspect
Four kinds of possible embodiments, wherein the on-board data Acquisition Instrument is arranged in the upper end at the center of unmanned aerial vehicle body, and is arranged
In the lower end of the airborne electromagnetic radiation monitor；The on-board data Acquisition Instrument and the airborne electromagnetic radiation monitor pass through
Bayonet joint connects.
The possible embodiment of with reference to first aspect the first, the utility model embodiment provide the of first aspect
Five kinds of possible embodiments, wherein the unmanned plane wireless communication system includes antenna, and the antenna is arranged to non-omnidirectional antennas
Line, and, the antenna episternites is towards the center of unmanned plane main body；It is outer by unmanned plane center direction that the master of the antenna penetrates direction
Side.
With reference to first aspect, the utility model embodiment provides the 6th kind of possible embodiment of first aspect,
In, the airborne electromagnetic radiation monitor includes the power frequency electromagnet Field probe that measurement frequency is 50Hz.
With reference to first aspect, the utility model embodiment provides the 7th kind of possible embodiment of first aspect,
In, the airborne electromagnetic radiation monitor includes radio-frequency electromagnetic Field probe of the frequency range between 500kHz-3.5GHz.
With reference to first aspect, the utility model embodiment provides the 7th kind of possible embodiment of first aspect,
In, the unmanned plane uses multi-rotor unmanned aerial vehicle or fixed-wing unmanned plane.
Second aspect, the utility model embodiment also provide a kind of space electromagnetic environment monitoring system, including：Host computer and
Space electromagnetic environment monitoring device described in any one of first aspect and its possible embodiment, the host computer with it is described
Space electromagnetic environment monitoring device is connected.
The utility model embodiment brings following advantageous effect：
In space electromagnetic environment monitoring device and system that the utility model embodiment provides, it is applied to space electromagnetic environment
Monitoring, wherein the space electromagnetic environment monitoring device includes：Unmanned plane, airborne electromagnetic radiation monitor, on-board data acquisition
Instrument, ground data terminal；Wherein, airborne electromagnetic radiation monitor and on-board data Acquisition Instrument are arranged on unmanned plane, airborne
Electromagnetic radiation monitoring instrument is connected with on-board data Acquisition Instrument, and on-board data Acquisition Instrument is connected with ground data terminal；It is airborne
Electromagnetic radiation monitoring instrument is used to monitor the electromagnetic environment data in space；On-board data Acquisition Instrument is for obtaining airborne electromagnetic radiation prison
The electromagnetic environment data of instrument are surveyed, and by electromagnetic environment data transmission to ground data terminal.Therefore, the utility model embodiment carries
The technical solution of confession, be based on unmanned air vehicle technique, can alleviate electromagnetic environment monitor in the prior art there are user experience compared with
The problem of difference, improves user experience.
Other feature and advantage of the utility model will illustrate in the following description, also, partly from specification
In become apparent, or understood by implementing the utility model.The purpose of this utility model and other advantages are illustrating
Specifically noted structure is realized and is obtained in book, claims and attached drawing.
To enable the above objects, features, and advantages of the utility model to be clearer and more comprehensible, preferred embodiment cited below particularly, and
The appended attached drawing of cooperation, is described in detail below.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific implementation mode or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, other drawings may also be obtained based on these drawings.
Fig. 1 is the structure diagram for the space electromagnetic environment monitoring device that the utility model embodiment provides；
Fig. 2 is a kind of schematic diagram for the space electromagnetic environment monitoring device that the utility model embodiment provides；
Fig. 3 is the outside drawing for the space electromagnetic environment monitoring device that the utility model embodiment provides；
Fig. 4 is the stereogram of unmanned plane and airborne portion that the utility model embodiment provides；
Fig. 5 is the vertical view of unmanned plane and airborne portion that the utility model embodiment provides；
Fig. 6 is another schematic diagram for the space electromagnetic environment monitoring device that the utility model embodiment provides；
Fig. 7 is the structure chart that the space electromagnetic environment that the utility model embodiment provides monitors system.
Specific implementation mode
To keep the purpose, technical scheme and advantage of the utility model embodiment clearer, below in conjunction with attached drawing to this
The technical solution of utility model is clearly and completely described, it is clear that described embodiment is that the utility model part is real
Example is applied, instead of all the embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not making
The every other embodiment obtained under the premise of creative work, shall fall within the protection scope of the present invention.
Currently, conventional electromagnetic environment monitor is to use portable electromagnetic monitoring instrument, can be reached in monitoring personnel
Place or the hand-held measurement of personnel, or tripod is set up, electromagnetic field monitoring probe is erected on tripod, is connected by optical fiber
Host is monitored, the hand-held monitoring host of monitoring personnel is read.However this monitoring can only be on the ground that monitoring personnel can reach
Side is monitored, and in the place that personnel are difficult to reach, especially AC power transmission and transformation project, intermediate waves transmitting station, mobile communication
Electromagnetic field in antenna for base station peripheral space is monitored, and existing monitoring means cannot be satisfied this requirement of user, cause
User experience is not high.To sum up, existing electromagnetic environment monitor has that user experience is poor.Based on this, this practicality
A kind of space electromagnetic environment monitoring device and system that new embodiment provides, the unmanned air vehicle technique based on rapid development can be with
Alleviate existing electromagnetic environment monitor and there is a problem of that user experience is poor, user experience can be improved.
For ease of understanding the present embodiment, first to a kind of spatial electromagnetic ring disclosed in the utility model embodiment
Border monitoring device describes in detail.
Embodiment one：
The utility model embodiment provides a kind of space electromagnetic environment monitoring device, is applied to environmental monitoring, tool
Body is monitored applied to space electromagnetic environment.
As shown in Figures 1 to 5, which includes：Unmanned plane 1, airborne electromagnetic radiation monitor
2, on-board data Acquisition Instrument 3, ground data terminal 4.
Wherein, above-mentioned airborne electromagnetic radiation monitor and above-mentioned on-board data Acquisition Instrument are arranged on above-mentioned unmanned plane,
Above-mentioned airborne electromagnetic radiation monitor is connected with above-mentioned on-board data Acquisition Instrument, above-mentioned on-board data Acquisition Instrument and above-mentioned ground
Data terminal is connected.
Above-mentioned airborne electromagnetic radiation monitor is used to monitor the electromagnetic environment data in space.Wherein, electromagnetic environment data packet
Include field strength, frequency spectrum etc..
Above-mentioned on-board data Acquisition Instrument is used to obtain the electromagnetic environment data of airborne electromagnetic radiation monitor, and by above-mentioned electricity
Magnetic environment data transmission is to above-mentioned ground data terminal.
Specifically, unmanned plane 1, airborne electromagnetic radiation monitor 2, on-board data Acquisition Instrument 3 are space electromagnetic environment prisons
Survey the unmanned plane of device and the important component of airborne portion 123.Above-mentioned unmanned plane includes unmanned plane wireless communication system 11.
Here ground data terminal is a kind of control of ground and data terminal, has the function of that flying vehicles control and data lead to
Communication function.
Specifically, above-mentioned ground data terminal 4 includes remote controler 41 and video data terminal 42, above-mentioned video data terminal
It is connected with above-mentioned remote controler.
Here remote controler, that is, flight controller is used to control the flight of unmanned plane, and, above-mentioned remote controler with it is above-mentioned nobody
Machine is communicated by unmanned plane wireless communication system.
Specifically, above-mentioned remote controler is remotely controlled unmanned plane by unmanned plane wireless communication system, (i.e. number passes, for passing
Defeated UAV Flight Control instruction and the parameter for obtaining flight), receiving the image that unmanned plane transmits, (i.e. figure passes, and is used for transmission
The realtime graphic of Airborne Camera), and, it receives data collecting instrument and passes through the remaining bandwidth for transmission of unmanned plane wireless communication system
Monitoring data (i.e. business data transmission).
Above-mentioned unmanned plane wireless communication system includes antenna.
Remote controler and video data terminal are integrated.
Above-mentioned video data terminal is a kind of data display platform, and above-mentioned video data terminal is for showing information；
Above- mentioned information includes monitoring data and monitoring result.
In the specific implementation, airborne electromagnetic radiation monitor connects on-board data Acquisition Instrument, the number of on-board data Acquisition Instrument
Monitoring data are descended into ground data terminal (ground remote control and display platform) according to the wireless communication system by unmanned plane,
Show monitoring result.
Further, above-mentioned video data terminal be additionally operable to draw monitoring data at any time, height, speed, spatial position
Curve or figure.Unmanned plane during flying instruction, the channel radio being had by oneself by unmanned plane can be edited and be arranged in video data terminal
Letter system is transferred to unmanned plane, executes automatic flight.
Specifically, unmanned controller by UAV Communication system synchronization obtain unmanned plane parameter information (including fly
Row state parameter, flight status parameter here includes time parameter, spatial positional information, elevation information, velocity information etc.) and
Monitoring data (business datum) show monitoring data on video data terminal (being provided with graphic plotting software platform), draw
Monitoring data at any time, height, speed, spatial position curve or figure.Data display platform can be edited and nobody is arranged
Machine flight directive, the wireless communication system being had by oneself by unmanned plane are transferred to unmanned plane, execute automatic flight.
Above-mentioned video data terminal uses mobile device, specifically, video data terminal is using smart mobile phone or tablet electricity
Brain.
The communication modes that a UAV Communication system is only arranged in whole device have the following advantages：Flight control and data
It is more convenient when flight control is observed the same staff with data on the same platform, improve the effect of detection
Rate.It, can be to avoid separately building the nothing of a set of data collecting instrument furthermore with the unmanned plane wireless communication system that unmanned plane is had by oneself
The cost of line communication module also avoids the emc issue between two kinds of wireless communication systems, the own nothing of unmanned plane
Man-machine wireless communication system is Specialty Design, communication efficiency performance and stability higher.
From the point of view of unmanned plane electromagnetic environment monitor, main radiation source (base station, power transmission and transformation line and radio and television hair
Penetrate facility) all it is to be located in the air, if airborne electromagnetic radiation monitor (i.e. airborne electromagnetic radiation monitor) is mounted on unmanned plane
The lower part of fuselage then will appear the problem of signal is blocked before reaching airborne electromagnetic radiation monitor by unmanned aerial vehicle body, and
And in underbelly, the antenna of distance wireless communication system closer to, it is easier to be interfered.
Further, the airborne electromagnetic radiation monitor of the present embodiment is arranged in the upper end of unmanned aerial vehicle body.
It is normally on several support arms of unmanned plane in view of the antenna of multi-rotor unmanned aerial vehicle, how to reduce unmanned plane certainly
The interference of body electromagnetism, further, airborne electromagnetic radiation monitor are arranged at the center of unmanned aerial vehicle body.
I.e. airborne electromagnetic radiation monitor is arranged in the upper end at the center of unmanned aerial vehicle body.
In order to be further reduced the interference of unmanned plane self electromagnetism, further, unmanned plane wireless communication system includes day
The antenna of line, the UAV Communication system is arranged to non-omnidirectional antenna, and, above-mentioned antenna episternites is towards in unmanned plane main body
The heart；It is outwardly directed by unmanned plane center that the master of above-mentioned antenna penetrates direction.The antenna for reducing unmanned plane (is installed to unmanned plane center
Have airborne electromagnetic radiation monitoring instrument position) emission probability.
Further, the measurement lower limit requirement of above-mentioned airborne electromagnetic radiation monitor is field strength≤0.5V/m.
In order to reduce windage as far as possible, further, above-mentioned airborne electromagnetic radiation monitor shape is designed as bottom surface half
The top of the diameter cylinder bigger than top surface radius, above-mentioned cylinder is hemispherical.
Consider how to reduce the interference signal of unmanned plane itself, further, above-mentioned airborne electromagnetic spoke to greatest extent
The Sensor section (probe) for penetrating monitor is arranged far from the side of unmanned aerial vehicle body, it is preferred that airborne electromagnetic Radiation monitoring
The top in instrument is arranged in the probe (no matter power frequency or radio frequency) of instrument, as far as possible far from fuselage, and wireless communication system
The antenna of system, to reduce the interference of unmanned plane.
In view of unmanned plane is after being equipped with airborne electromagnetic radiation monitor and data collecting instrument, how to keep unmanned plane whole
The balance of body, further, above-mentioned on-board data Acquisition Instrument are arranged at the center of unmanned aerial vehicle body.
The whole structure and stress about center all directions of unmanned plane is all symmetrical in this way, to keep unmanned plane by
The balance of power.
In view of being provided with image collecting device below unmanned aerial vehicle body, the finiteness of underlying space is further, above-mentioned
On-board data Acquisition Instrument is arranged in the upper end of unmanned aerial vehicle body.
In this way, above-mentioned airborne electromagnetic radiation monitor and above-mentioned on-board data Acquisition Instrument are arranged in unmanned aerial vehicle body
The upper end of the heart.I.e. above-mentioned airborne electromagnetic radiation monitor and above-mentioned on-board data Acquisition Instrument are arranged in unmanned aerial vehicle body
The heart, and it is respectively positioned on the upper end of unmanned aerial vehicle body.
In view of the convenience that on-board data Acquisition Instrument is connect with airborne electromagnetic radiation monitor, shorten wire length, side
Just in-site installation, the cross-interference issue for also avoiding long cable tie from, further, above-mentioned on-board data Acquisition Instrument are arranged in unmanned plane
The upper end at the center of fuselage, and be arranged in the lower end of above-mentioned airborne electromagnetic radiation monitor；Above-mentioned on-board data Acquisition Instrument and upper
Airborne electromagnetic radiation monitor is stated to connect by bayonet joint.
Further, above-mentioned airborne electromagnetic radiation monitor is counted by hard grafting adaptor cup jointing in on-board data Acquisition Instrument
Pass through screw connection according to Acquisition Instrument and unmanned plane.
Here by the way that airborne electromagnetic radiation monitor and above-mentioned on-board data Acquisition Instrument are arranged at unmanned aerial vehicle body
The upper end at center improves the flying quality (such as wind resistance and stability) of unmanned plane entirety.
In order to further reduce windage, and reduce the torque of stress.Further, above-mentioned airborne electromagnetic radiation monitor
The sum of the height of height and above-mentioned data collecting instrument be less than the 1/2 of unmanned plane wheelbase.
In order to realize product lightness and improve the cruising ability of the device, further, above-mentioned on-board data Acquisition Instrument
With above-mentioned airborne electromagnetic radiation monitor by the battery powered of unmanned plane, weight mounted is reduced, continuation of the journey energy is improved
Power.
Further, above-mentioned unmanned plane uses multi-rotor unmanned aerial vehicle or fixed-wing unmanned plane.That is, it is above-mentioned nobody
Machine can be multi-rotor unmanned aerial vehicle, can also be fixed-wing unmanned plane.
Airborne electromagnetic radiation monitor and on-board data Acquisition Instrument are arranged on unmanned plane, are gone up to the air using UAV flight,
Airborne electromagnetic radiation monitor is used to monitor the electromagnetic environment data in space, and on-board data Acquisition Instrument obtains airborne electromagnetic radiation prison
The electromagnetic environment data for surveying instrument are controlled to ground by wireless real-time transmission and data terminal (ground data terminal).
Specifically, the unmanned plane in the present embodiment uses quadrotor drone.
It should be noted that as an alternative, above-mentioned unmanned plane can even is that ascending balloon or other liters
Empty device, it is contemplated that electromagnetic field monitor (probe) is fixed on ascending balloon, the side stored by the way that automatic collection is arranged
Method exports monitoring data after the completion of monitoring.This method the problem is that：It 1) can only be in the reached position of monitoring personnel
The overhead set is monitored, and cannot be monitored according to specified track and route；2) monitoring data cannot be monitoring people in real time
Member is grasped；3) efficiency monitored is low, of high cost.Therefore, unmanned plane is preferably used in the present embodiment.
Further, in some embodiments, above-mentioned airborne electromagnetic radiation monitor includes the work that measurement frequency is 50Hz
Frequency electromagnetic field is popped one's head in, and the field strength of power frequency (50Hz) can be directly obtained, and avoids the frequency range of motor interference.
Specifically, the power frequency electromagnet Field probe that frequency is 50Hz can obtain or pass through center using spectrum analysis function
Frequency is that 50Hz narrow band filters obtain.
In the present embodiment, airborne electromagnetic radiation monitor includes the power frequency electromagnet Field probe that frequency is 50Hz and center frequency
Rate is 50Hz narrow band filters.
Further, in other embodiments, above-mentioned airborne electromagnetic radiation monitor includes that frequency range exists
Radio-frequency electromagnetic Field probe between 500kHz-3.5GHz.
Specifically, in the present embodiment, above-mentioned airborne electromagnetic radiation monitor includes the radio frequency that lower-frequency limit is 500kHz
Emf probe can improve the rejection ability to unmanned plane motor interference signal, while the frequency of the radio-frequency electromagnetic Field probe
The upper limit is 3.5GHz, to avoid the interference of unmanned plane wireless communication system (when unmanned plane wireless communication frequency is 5.8GHz).
It should be noted that the lower-frequency limit and upper frequency limit of radio-frequency electromagnetic Field probe are with specific reference to practical measurement demand
(such as according to frequency of the communication frequency of unmanned plane and measurement object) is chosen or is designed and produced, and the basic principle of selection is：
Reduce the interference signal (unmanned plane motor or UAV Communication system) for even avoiding unmanned plane itself in measurement process.On
It is a kind of preferred embodiment to state numerical value, is not construed as limitations of the present invention.For example, radio frequency electromagnetic field is visited
The lower-frequency limit of head may be 30MHz (model probe needs special design), the upper frequency limit of radio-frequency electromagnetic Field probe
Can be 5.2GHz.
It is pointed out that the sensing of power frequency electromagnet Field probe or radio-frequency electromagnetic Field probe as electromagnetic radiation monitoring instrument
Device component needs to be arranged on the top for recording electromagnetic radiation monitoring instrument, and far from unmanned aerial vehicle body and wireless communication system
Antenna；In other words, the probe of airborne electromagnetic radiation monitor should be as far as possible far from fuselage, to reduce the interference of unmanned plane.
In space electromagnetic environment monitoring device and system that the utility model embodiment provides, it is applied to space electromagnetic environment
Monitoring, wherein the space electromagnetic environment monitoring device includes：Unmanned plane, airborne electromagnetic radiation monitor, on-board data acquisition
Instrument, ground data terminal；Wherein, airborne electromagnetic radiation monitor and on-board data Acquisition Instrument are arranged on unmanned plane, airborne
Electromagnetic radiation monitoring instrument is connected with on-board data Acquisition Instrument, and on-board data Acquisition Instrument is connected with ground data terminal；It is airborne
Electromagnetic radiation monitoring instrument is used to monitor the electromagnetic environment data in space；On-board data Acquisition Instrument is for obtaining airborne electromagnetic radiation prison
The electromagnetic environment data of instrument are surveyed, and by electromagnetic environment data transmission to ground data terminal.Therefore, the utility model embodiment carries
The technical solution of confession, be based on unmanned air vehicle technique, can alleviate electromagnetic environment monitor in the prior art there are user experience compared with
The problem of difference, improves user experience.
Embodiment two：
As shown in fig. 6, the utility model embodiment provides another space electromagnetic environment monitoring device, the spatial electromagnetic
Environment monitoring device includes：Unmanned plane 1, airborne electromagnetic radiation monitor 2, on-board data Acquisition Instrument 3, ground data terminal 4.Tool
Body, unmanned plane 1, airborne electromagnetic radiation monitor 2, on-board data Acquisition Instrument 3 are the nothings of the space electromagnetic environment monitoring device
Man-machine and airborne portion 123 important component.Above-mentioned unmanned plane includes unmanned plane wireless communication system 11.
Difference lies in, above-mentioned ground data terminal include remote controler 41 and video data terminal 42 with embodiment one, on
Remote controler is stated to be communicated by UAV Communication system 11 with above-mentioned unmanned plane.
Specifically, above-mentioned remote controler carries out no-manned machine distant control and figure with above-mentioned unmanned plane by UAV Communication system 11
It passes.
Above-mentioned on-board data Acquisition Instrument includes the first wireless communication module 31, and above-mentioned video data terminal includes second wireless
Communication module 32, above-mentioned first wireless communication module constitute another wireless communication system (again with above-mentioned second wireless communication module
Referred to as business datum communication system, is exclusively used in business data transmission), above-mentioned on-board data Acquisition Instrument is by above-mentioned wireless communication
System is communicated (business data transmission) with above-mentioned video data terminal.
Specifically, the first wireless communication module 31, the second wireless communication module 32 are all made of ZIGBEE modules.
In the present embodiment, remote controler and video data terminal are separation, and the two is individually independent equipment, and connectionless
Relationship, so that flight control and business data transmission respectively obtain control.
Above-mentioned video data terminal uses mobile terminal, specifically, video data terminal is using portable computer or puts down
Plate computer (PAD).
Embodiment two and embodiment one the difference is that, first that on-board data Acquisition Instrument is equipped on unmanned plane is wireless
Communication module, built in video data terminal on the ground or external second wireless communication module, on-board data Acquisition Instrument obtain
Monitoring data (business datum) the second wireless communication module radioed to by the first wireless communication module to reach data aobvious
Show terminal.Original unmanned plane is kept to wirelessly communicate between the remote controler and unmanned plane of unmanned plane.The present embodiment is provided with two sets
Independent wireless communication system, a set of to be passed for no-manned machine distant control and figure, a set of transmission for business datum realizes flight
The independence that control and data are shown.
The present embodiment be arranged two sets of independent wireless communication systems the advantages of be：Flight control and data, which are shown, to be separated, when
When flight remote control manipulator and data Observation personnel are different personnel, remote control distributor personnel can be absorbed in the flight control of unmanned plane
System, improves the safety of flight, and the personnel by addition paying close attention to monitoring data observe data in video data terminal.And embodiment one
Flight control and data are shown as identical platform, it has not been convenient to be carried out at the same time flight control and data observation.
It should be pointed out that for the convenience that data are shown, at least one embodiment, above-mentioned on-board data Acquisition Instrument
It is also communicated, the parameter information for obtaining unmanned plane with unmanned plane (particularly with the main control module of unmanned plane), and will
System is transferred to video data terminal to above-mentioned parameter information by radio communication；Above-mentioned parameter information include longitude and latitude, height, when
Between, battery capacity, drone status and state of flight.
By the above-mentioned means, video data terminal is facilitated also to grasp the state of unmanned plane in time, facilitate video data terminal
Curve or figure are drawn based on unmanned plane parameter and electromagnetic field monitoring parameters, for example draws song of the monitoring data with height change
Line draws the curve that monitoring data change over time, and draws the distribution map etc. of monitoring data in space.In addition, data are shown
The automatic flight control instruction (being preset with control software) of unmanned plane can also be worked out and be arranged to terminal, pass through the second radio communication mold
Block is wirelessly uploaded to the first wireless communication module, reaches on-board data Acquisition Instrument, and on-board data Acquisition Instrument sends instructions to nothing
It is man-machine.Unmanned plane can automatically be flown according to the instruction.
Embodiment three：
The design scheme of the utility model is described in detail by taking common UAV system as an example below：
Unmanned plane is divided into aircraft section and ground flying remote control, and aircraft and ground flying remote control are equipped with channel radio
Letter system is wirelessly communicated between aircraft section and ground flying remote control, such as is transmitted image, data and flown
Row control instruction etc..
Ground flying remote control includes the remote controler of flight and video data terminal (is usually smart mobile phone or tablet electricity
Brain).
The data (business datum) for the airborne electromagnetic radiation monitor that on-board data Acquisition Instrument obtains will pass through wireless side
Formula is transmitted back to the data platform on ground, realizes real-time data acquisition and display.
There are two types of the wireless data communication schemes for realizing above-mentioned on-board data Acquisition Instrument and ground data terminal：
Scheme one：The unmanned plane wireless communication system carried using unmanned aerial vehicle platform transmits airborne data collecting instrument acquisition
Electromagnetic field data to ground data terminal, at this moment ground control terminal (remote controler) and video data terminal be it is integrated (i.e.
Face data terminal, what the remote controler and video data terminal were connected to connect).Conventional unmanned plane is equipped with wireless figure and passes and count biography
System, figure pass the realtime graphic for being used for transmission Airborne Camera, and number, which passes to be used for transmission UAV Flight Control instruction and obtain, to fly
Capable parameter, the Data transfer system have remaining bandwidth that can transmit additional business datum, therefore certainly using unmanned aerial vehicle platform
The unmanned plane wireless communication system of band transmits the monitoring data of airborne data collecting instrument.
Airborne airborne electromagnetic radiation monitor connects on-board data Acquisition Instrument, and the data of data collecting instrument pass through unmanned plane
Monitoring data are descended into ground data terminal (ground remote control display platform) by wireless communication system, show monitoring result.
Scheme two：Without using the wireless communication system that unmanned plane is had by oneself, on-board data Acquisition Instrument uses independent channel radio
Letter scheme increases by the first wireless communication module in unmanned plane and airborne portion to on-board data Acquisition Instrument, in ground surface end, setting
One independent video data terminal (built-in or external second wireless communication module), the airborne electricity of on-board data Acquisition Instrument acquisition
Module is wirelessly transmitted to the video data terminal on ground to the monitoring data of magnetic radiation monitor by radio communication.
Scheme two and scheme one difference lies in：There are two sets of independent wireless communication systems, it is a set of to be used for no-manned machine distant control
It is passed with figure, a set of transmission for business datum, flight control platform and video data terminal separation.
The advantages of scheme one is：Flight control and data are on the same platform, when flight control and data are observed together
It is more convenient when one people, improve the efficiency of detection.It, can be to avoid another furthermore with the wireless communication system that unmanned plane is had by oneself
Row builds the cost of the wireless communication module of a set of data collecting instrument, and the electromagnetism also avoided between two kinds of wireless communication systems is simultaneous
Capacitive problem, the own wireless communication system of unmanned plane are Specialty Design, communication efficiency performance and stability higher.
The advantages of scheme two is：Flight control and data, which are shown, to be separated, when flight remote control manipulator and data Observation personnel are
When different personnel, remote control distributor personnel can be absorbed in the flight control of unmanned plane, the safety of flight be improved, by addition paying close attention to
The personnel of monitoring data observe data in video data terminal.And the flight of scheme one control and data are identical platform, it has not been convenient to
It is carried out at the same time flight control and data observation.
For the unmanned plane of external electromagnetic field measuring and design：Electromagnetic radiation measuring instrument will measure the electromagnetic field signal in space,
Avoid the electromagnetic interference that unmanned plane itself generates to the measurement of electromagnetic field, there are mainly two types of interference for unmanned plane：1) unmanned electromechanical
The interference that machine (for multi-rotor unmanned aerial vehicle) generates when working；2) communication interference of unmanned plane wireless communication system.
The interference of unmanned plane motor work, frequency is usually hundreds of Hz to more than ten kHz, and the main positions of interference source are more
At the motor of rotor wing unmanned aerial vehicle, and it is transmitted to by power cable and controlling cable etc. the multiple portions of unmanned plane；Unmanned plane without
The usually used industry science of line communication system cures frequency range, and common communication frequency is 2.45GHz frequency ranges or 5.8GHz frequency ranges.Due to
Fly the needs of remote control, and wireless communication system needs the transmitting of normality, thus cannot by close wireless communication system or
Wirelessly communicate it is idle in the case of carry out electromagnetic field monitoring.
One, the design of airborne electromagnetic radiation monitor：For airborne electromagnetic radiation monitor usually there are two types of type, one kind is work
Frequency airborne electromagnetic radiation monitor, another kind are the airborne electromagnetic radiation monitoring instrument of radio frequency.
A can not have to the wireless communication system interference for worrying unmanned plane for power frequency airborne electromagnetic radiation monitor, because
Frequency phase-difference it is distant, wireless communication system does not affect the measurement of power frequency electromagnetic field.But the interfering frequency of motor is fallen
In the frequency range (5Hz-100kHz) of conventional power frequency airborne electromagnetic radiation monitor.Solution is：Using with
The power frequency electromagnet Field probe that 50Hz points electricity frequency measures function (is obtained using spectrum analysis function or is 50Hz by centre frequency
Narrow band filter obtains), this power frequency electromagnet Field probe can directly obtain the field strength of power frequency (50Hz), and avoid motor interference
Frequency range.Since the low frequency electromagnetic measurement demand of the overwhelming majority is in power domain, it is power frequency to need the frequency measured
(50Hz), therefore this scheme can solve the problems, such as this.
For B for the airborne electromagnetic radiation monitoring instrument of radio frequency, common electromagnetic measurement frequency range is 100kHz-6GHz, this
A frequency range is three dB bandwidth, but for the electric field of more than ten kHz frequency ranges, rejection ability limited (being usually 20dB) or energy
Induction, although smaller.But the interference field strength that generates of motor it is bigger such as common reached more than ten V/m, can be apparent
Influence emf probe measurement lower limit, and interference field strength caused by this motor is related with motor operating power
, that is to say, that it is interfered when motor speed is high big, interferes small when rotating speed is low, therefore cannot simply deduct interference
Signal.For this solution to the problem：Using the higher radio-frequency electromagnetic Field probe of measurement frequency lower limit, under measurement frequency
500kHz or measurement frequency lower limit are limited to as the radio-frequency electromagnetic Field probe of 30MHz (model probe needs special design).
At this moment 40dB or more can be reached for the rejection ability of the motor interference signal of more than ten kHz by popping one's head in.
According to measurement demand, the demand of most of unmanned plane spatial electromagnetic field measurement comes from mobile communication base station (frequency
Range 800MHz-2.7GHz), broadcast and TV radiating station (working frequency 500kHz-800MHz), for wireless communication system
Interference, can design for the frequency of test object, and the wireless communication system interfering frequency exclusion of unmanned plane itself is being surveyed
It measures except frequency.It is designed according to communication frequency used in unmanned plane；1) unmanned plane wireless communication frequency is 5.8GHz, is adopted
It is 5.2GHz or the measurement frequency upper limit for example, by using upper frequency limit with the lower radio-frequency electromagnetic Field probe of the measurement frequency upper limit
For the emf probe of 3.5GHz.To avoid the interference of unmanned plane wireless communication system.2) for measurand working frequency
It is close with wireless communication frequency, can not be come effective the case where distinguishing, such as wireless communication frequency by Frequency Band Selection of popping one's head in
The unmanned plane of 2.45GHz, measurand are mobile communication base station (working frequency 800MHz-2.7GHz), it is difficult to from the frequency of probe
It is distinguished in rate selection, at this moment, following measures can be taken：If the antenna of multi-rotor unmanned aerial vehicle is normally at unmanned plane
On dry support arm, therefore by airborne electromagnetic radiation monitor, it is mounted on unmanned plane center, the upside of main part.It can incite somebody to action
The communication antenna designs of unmanned plane repack non-omnidirectional antenna into：It allows the master of unmanned plane antenna to penetrate direction to be designed as by unmanned plane
The heart is outwardly directed, and antenna episternites is made to reduce unmanned plane antenna to unmanned plane center (installation airborne electromagnetic towards unmanned plane center
Radiation monitor position) transmitting.
In this way, can usually make the interference field strength measured at airborne electromagnetic radiation monitor from original antenna (without setting
Meter or the omnidirectional antenna of repacking) interference field strength (1-2) V/m, (0.2-0.5) V/ is being dropped to using interference field strength after the program
M or less.Even the interference outside band, this is acceptable for electromagnetic environment measurement, radiates and supervises generally for airborne electromagnetic
The measurement lower limit requirement for surveying instrument is≤0.5V/m.
In summary it requires：Frequency for unmanned plane probe is preferably 500kHz-3.5GHz.
Two, airborne electromagnetic radiation monitor designs：1) there are two types of installation of the airborne electromagnetic radiation monitor on unmanned plane
Selection, one is mounted in the top of unmanned aerial vehicle body (main body), and one is mounted in the lower part of unmanned aerial vehicle body, but from unmanned plane
The angle of electromagnetic environment monitor, main radiation source (base station, power transmission and transformation line and radio and television launch facility) are all to be located in the air,
If mounted on the lower part of unmanned aerial vehicle body, it will appear signal before reaching airborne electromagnetic radiation monitor by unmanned plane machine
The problem of body blocks, and in underbelly, distance wireless communication system antenna closer to, it is easier to be interfered.Therefore will
Airborne electromagnetic radiation monitor is mounted on the top of unmanned plane；2) knot of airborne airborne electromagnetic radiation monitor and data collecting instrument
Structure designs, and after being equipped with airborne electromagnetic radiation monitor and data collecting instrument, unmanned plane should integrally keep the balance of stress, to the greatest extent
It is possible to reduce plus windage, however unmanned plane entirety flying quality (wind resistance, cruising ability and keep stability) can seriously by
It influences.Therefore following measures are taken：The airborne airborne electromagnetic radiation monitor shapes of a are designed as circle more slightly wider than top below
Column, top are hemispherical, reduce windage；B data collecting instruments and airborne electromagnetic radiation monitor are placed in unmanned aerial vehicle body
The heart, from horizontal direction on, whole structure and stress about unmanned plane center all directions is all symmetrical, keep unmanned plane by
The balance of power；The height of c airborne electromagnetic radiation monitors is less than the 1/2 of unmanned plane wheelbase plus the height of data collecting instrument, with
It reduces and adds windage, and reduce the torque of stress；The Sensor section of d airborne electromagnetic radiation monitors is located at the top of instrument
(antenna far from fuselage and wireless communication system as far as possible, to reduce the interference of unmanned plane), data collecting instrument is located at machine
Electromagnetic radiation monitoring instrument lower end is carried, unmanned aerial vehicle body upper end uses bayonet joint between each other, and line is short, facilitates live peace
Dress, the cross-interference issue for also avoiding long cable tie from.E product light designs, airborne electromagnetic radiation monitor and data collecting instrument make
It is powered with the battery of unmanned plane, reduces weight mounted.
The space electromagnetic environment monitoring device of the present embodiment design has following major advantage：
1) the electromagnetic environment measuring system of first UAV flight realizes electromagnetic environment in convenient and mobility space
Monitoring；
2) it takes airborne electromagnetic radiation monitor and measures frequency range optimization design, interference signal inhibition interference protection measure and nothing
Man-machine radio antenna directional diagram optimization design etc. reduces or the motor of unmanned plane itself is avoided to interfere and wirelessly communicate and does
It disturbs.The required accuracy of measurement for measuring electromagnetic field is ensured.
3) data collecting instrument of carrying and the structure design of electromagnetic field measurements probe are optimized, small size, windage are taken
Small, symmetry, light-weighted design have ensured that the unmanned plane after carrying keeps good performance, including balance, stability,
Wind resistance, persistence of work etc..
4) two kinds of radio communication systems according to demand, are devised, using unmanned plane from wire/wireless communication system and in addition
The wireless communication module of a set of data collecting instrument is built, the former simple system, no-manned machine distant control and data display platform one, side
Just single manipulation and monitoring；The latter's no-manned machine distant control and video data terminal separation, facilitate aircrew to be absorbed in flight, remaining people
The demand of member's observation data.
5) realize that automatic flight and automatic electromagnetic monitoring environmental data, monitoring data return ground display terminal in real time.
Based on above-mentioned design philosophy, small-sized quadrotor (is preferably selected using the M100 types unmanned plane of XX companies here as platform
Unmanned plane, interference is small, small to the influence for being tested electromagnetic environment), it designs one and measures broadcast and TV radiating station, mobile communication base station
Electromagnetic radiation measuring unmanned plane.
The working frequency 515kHz-800MHz of broadcast and TV radiating station, the working frequency 800MHz- of mobile communication base station
2.7GHz。
The motor interfering frequency of M100 type unmanned planes is 11kHz or so (by test), unmanned plane wireless communication system
The working frequency of system is that 2.45GHz/5.8GHz frequency ranges are optional.
Measurement lower limit is 0.5V/m；
UAV system weight≤1kg；
It is required that flight control platform (remote controler) is detached with video data terminal；
Flight time 20min-30min.
Design scheme is as follows：
Single unit system includes unmanned generator terminal and ground surface end, wherein unmanned generator terminal includes unmanned plane, on-board data Acquisition Instrument, machine
Carry electromagnetic radiation monitoring instrument；Ground surface end includes unmanned controller, video data terminal.
The frequency range 500kHz-3.5GHz of rf electric field probe, for the 40dB that is suppressed to of 11kHz interference signals, electricity
Interference level≤0.1V/m caused by machine interference.
Unmanned plane wireless communication frequency is selected as 5.8GHz, while being carried out to the transmitting antenna of unmanned plane wireless communication system
The Curve guide impeller transmitting towards unmanned plane center of omnidirectional antenna (such as shielding), main direction of penetrating are airborne towards outside unmanned plane
Electromagnetic radiation monitoring instrument is located at the episternites of antenna.So that interference field strength≤0.2V/m at airborne electromagnetic radiation monitor.
Comprehensive unmanned plane motor interference and wireless communication system interference, interference field strength≤0.3V/m, unmanned plane measure system
The measurement lower limit of system is less than or equal to 0.5V/m, meets design requirement.
Airborne electromagnetic radiation monitor shape is cylinder, and following slightly wider, top is slightly narrow, and top is hemispherical, below gradually
Change is square, i.e. the structure of airborne electromagnetic radiation monitor is as follows：Main body is at cylinder, and the bottom surface radius of the cylinder is big
It is hemispherical end cap in the top of top surface radius, aforementioned body, the lower end of main body is square pedestal, aforementioned body, end cap, bottom
Seat is in integrated molding, and square base and the size of on-board data Acquisition Instrument are adapted, and are just socketed in on-board data acquisition
On instrument, specifically, airborne electromagnetic radiation monitor is connect with on-board data Acquisition Instrument by hard grafting connector, it is aided with four hands and twists
Screw is fixed on on-board data Acquisition Instrument.On-board data Acquisition Instrument is screwed with unmanned plane, is accepted and is placed on transport
It is also what on-board data Acquisition Instrument was fixed together in case, and airborne electromagnetic radiation monitor can disassemble.It is airborne
Electromagnetic radiation monitoring instrument is mounted on the top of unmanned aerial vehicle body, the position of centre.
The height of airborne electromagnetic radiation monitor is 25cm, and the height of on-board data Acquisition Instrument is 5cm, and entire length is
30cm is less than the 1/2 of unmanned plane wheelbase 65cm.
Airborne electromagnetic radiation monitor and on-board data Acquisition Instrument are powered using the battery of unmanned plane.
First wireless communication module built in on-board data Acquisition Instrument, such as ZIGBEE modules (antenna of multiplexing unmanned plane, work
Frequency 2.45GHz), communication distance is up to 2 kilometers.
The total weight of airborne electromagnetic radiation monitor and on-board data Acquisition Instrument is about 850g.
On-board data Acquisition Instrument is communicated with unmanned plane, obtain the longitude and latitude of unmanned plane, height, battery capacity, speed,
Time, flight parameter and state of flight etc. are transferred to the platform on ground by the first wireless communication module.
On-board data Acquisition Instrument acquires the monitoring data of airborne electromagnetic radiation monitoring instrument in real time, and wirelessly passes down
To the video data terminal on ground.It is 1s that data, which acquire transmission frequency, i.e., monitoring per second simultaneously transmits one group of data.
In ground surface end, in addition to remote controler, one portable computer of configuration is wireless as video data terminal, external second
Communication module (such as ZIGBEE modules), computer obtain the monitoring data of data collecting instrument, and the instruction flown automatically is passed through
Second wireless communication module is sent to on-board data Acquisition Instrument.Flight directive is sent to unmanned plane, unmanned plane by data collecting instrument
It is flown automatically according to these instructions.
The Specifeca tion speeification of the integral type unmanned plane is as follows：
Measurement frequency range：500kHz-3.5GHz.
Measuring range：0.5V/m-400V/m.
Measurement error：≤3dB.
Flight time：25min.
Flight (communication) distance：2000m.
Example IV：
As shown in fig. 7, the utility model embodiment additionally provides a kind of space electromagnetic environment monitoring system, the system packet
It includes：The space electromagnetic environment monitoring device 700 that host computer 600 and previous embodiment refer to, above-mentioned host computer and above-mentioned space electricity
Magnetic environment monitoring device is connected.
Host computer can carry out telecommunication with the video data terminal of space electromagnetic environment monitoring device, such as remotely obtain
Monitoring data are taken either remotely to send control instruction or control parameter etc..
The space electromagnetic environment that the utility model embodiment provides monitors system, the spatial electromagnetic provided with above-described embodiment
Environment monitoring device technical characteristic having the same reaches identical technique effect so can also solve identical technical problem.
It should be noted that the above-mentioned unmanned plane of the application includes unmanned plane main control module, it is not shown in figure.
In addition, in the description of the utility model embodiment unless specifically defined or limited otherwise, term " installation ",
" connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally connect
It connects；It can be mechanical connection, can also be electrical connection；It can be directly connected, can also indirectly connected through an intermediary, it can
To be the connection inside two elements.For the ordinary skill in the art, it can understand above-mentioned term with concrete condition
Concrete meaning in the present invention.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.In addition, term " the
One ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
Finally it should be noted that：Above above-described embodiment, only specific embodiment of the present utility model, to illustrate this
The technical solution of utility model, rather than its limitations, the scope of protection of the utility model is not limited thereto, although with reference to aforementioned
The utility model is described in detail in embodiment, it will be understood by those of ordinary skill in the art that：It is any to be familiar with this skill
The technical staff in art field within the technical scope disclosed by the utility model, still can be to the skill recorded in previous embodiment
Art scheme modify or can readily occur in variation or equivalent replacement of some of the technical features；And these modifications,
Variation is replaced, the spirit and model of the utility model embodiment technical solution that it does not separate the essence of the corresponding technical solution
It encloses, should be covered within the scope of the utility model.Therefore, the scope of protection of the utility model is answered above-mentioned is wanted with right
Subject to the protection domain asked.
Claims (10)
1. a kind of space electromagnetic environment monitoring device, which is characterized in that the space electromagnetic environment monitoring device includes：Unmanned plane,
Airborne electromagnetic radiation monitor, on-board data Acquisition Instrument, ground data terminal；
Wherein, the airborne electromagnetic radiation monitor and the on-board data Acquisition Instrument are arranged on the unmanned plane, described
Airborne electromagnetic radiation monitor is connected with the on-board data Acquisition Instrument, the on-board data Acquisition Instrument and the ground data
Terminal is connected；
The airborne electromagnetic radiation monitor is used to monitor the electromagnetic environment in space, obtains electromagnetic environment data；
The on-board data Acquisition Instrument is used to obtain the electromagnetic environment data of airborne electromagnetic radiation monitor, and by the electromagnetism ring
Border data transmission is to the ground data terminal.
2. space electromagnetic environment monitoring device according to claim 1, which is characterized in that the ground data terminal includes
Remote controler and video data terminal, the video data terminal are connected with the remote controler, and the video data terminal is used for
Show information；The remote controler is communicated with the unmanned plane by unmanned plane wireless communication system.
3. space electromagnetic environment monitoring device according to claim 1, which is characterized in that the ground data terminal includes
Remote controler and video data terminal, the remote controler are communicated with the unmanned plane by UAV Communication system, the machine
It includes the first wireless communication module to carry data collecting instrument, and the video data terminal includes the second wireless communication module, and described the
One wireless communication module constitutes another wireless communication system with second wireless communication module, and the on-board data Acquisition Instrument is logical
The wireless communication system is crossed to be communicated with the video data terminal.
4. space electromagnetic environment monitoring device according to claim 1, which is characterized in that the airborne electromagnetic Radiation monitoring
The upper end at the center of unmanned aerial vehicle body is arranged in instrument.
5. space electromagnetic environment monitoring device according to claim 4, which is characterized in that the on-board data Acquisition Instrument is set
The upper end at the center of unmanned aerial vehicle body is set, and is arranged in the lower end of the airborne electromagnetic radiation monitor；The on-board data
Acquisition Instrument is connected with the airborne electromagnetic radiation monitor by bayonet joint.
6. space electromagnetic environment monitoring device according to claim 2, which is characterized in that unmanned plane wireless communication system
System includes antenna, and the antenna is arranged to non-omnidirectional antenna, and, the antenna episternites is towards the center of unmanned plane main body；It is described
It is outwardly directed by unmanned plane center that the master of antenna penetrates direction.
7. space electromagnetic environment monitoring device according to claim 1, which is characterized in that the airborne electromagnetic Radiation monitoring
Instrument includes the power frequency electromagnet Field probe that measurement frequency is 50Hz.
8. space electromagnetic environment monitoring device according to claim 1, which is characterized in that the airborne electromagnetic Radiation monitoring
Instrument includes radio-frequency electromagnetic Field probe of the frequency range between 500kHz-3.5GHz.
9. space electromagnetic environment monitoring device according to claim 1, which is characterized in that the unmanned plane uses more rotors
Unmanned plane or fixed-wing unmanned plane.
10. a kind of space electromagnetic environment monitors system, which is characterized in that including：Described in host computer and claim any one of 1-9
Space electromagnetic environment monitoring device, the host computer is connected with the space electromagnetic environment monitoring device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820425931.XU CN208076624U (en) | 2018-03-27 | 2018-03-27 | space electromagnetic environment monitoring device and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820425931.XU CN208076624U (en) | 2018-03-27 | 2018-03-27 | space electromagnetic environment monitoring device and system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208076624U true CN208076624U (en) | 2018-11-09 |
Family
ID=64042079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820425931.XU Active CN208076624U (en) | 2018-03-27 | 2018-03-27 | space electromagnetic environment monitoring device and system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208076624U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108303598A (en) * | 2018-03-27 | 2018-07-20 | 北京科环世纪电磁兼容技术有限责任公司 | Space electromagnetic environment monitoring device and system |
| CN112821967A (en) * | 2021-01-07 | 2021-05-18 | 同方电子科技有限公司 | Handheld wide-band electromagnetic environment monitoring device |
| CN113834972A (en) * | 2020-06-23 | 2021-12-24 | 广东省环境辐射监测中心 | Remote control's anti-interference on-vehicle electromagnetic radiation monitoring system |
| RU2777985C2 (en) * | 2019-08-02 | 2022-08-12 | Общество с ограниченной ответственностью "СТАТУС КОНСАЛТ" | Method for measurement of maximum density of energy flow of electromagnetic field at points in vicinity of axis of main emission of cellular communication antenna, using unmanned aerial vehicle of helicopter type |
| SE2150951A1 (en) * | 2021-07-16 | 2023-01-17 | Emc Mapping Sweden Ab C/O Bergloef | Method and system for mapping electronic environment with an unmanned aerial system |
| SE2350028A1 (en) * | 2023-01-13 | 2024-03-05 | EMC Mapping Sweden AB | Methods and systems for determining electromagnetic compatibility for a target electrical device by an unmanned aerial system |
-
2018
- 2018-03-27 CN CN201820425931.XU patent/CN208076624U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108303598A (en) * | 2018-03-27 | 2018-07-20 | 北京科环世纪电磁兼容技术有限责任公司 | Space electromagnetic environment monitoring device and system |
| RU2777985C2 (en) * | 2019-08-02 | 2022-08-12 | Общество с ограниченной ответственностью "СТАТУС КОНСАЛТ" | Method for measurement of maximum density of energy flow of electromagnetic field at points in vicinity of axis of main emission of cellular communication antenna, using unmanned aerial vehicle of helicopter type |
| CN113834972A (en) * | 2020-06-23 | 2021-12-24 | 广东省环境辐射监测中心 | Remote control's anti-interference on-vehicle electromagnetic radiation monitoring system |
| CN112821967A (en) * | 2021-01-07 | 2021-05-18 | 同方电子科技有限公司 | Handheld wide-band electromagnetic environment monitoring device |
| SE2150951A1 (en) * | 2021-07-16 | 2023-01-17 | Emc Mapping Sweden Ab C/O Bergloef | Method and system for mapping electronic environment with an unmanned aerial system |
| WO2023287342A1 (en) * | 2021-07-16 | 2023-01-19 | Grundbulten 101770 Ab Unä Emc Sky Mapping Ab | Method and system for mapping electronic environment with an unmanned aerial system |
| SE2350028A1 (en) * | 2023-01-13 | 2024-03-05 | EMC Mapping Sweden AB | Methods and systems for determining electromagnetic compatibility for a target electrical device by an unmanned aerial system |
| SE545884C2 (en) * | 2023-01-13 | 2024-03-05 | EMC Mapping Sweden AB | Methods and systems for determining electromagnetic compatibility for a target electrical device by an unmanned aerial system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208076624U (en) | space electromagnetic environment monitoring device and system | |
| CN108303598A (en) | Space electromagnetic environment monitoring device and system | |
| EP3104184B1 (en) | Method and apparatus for locating faults in overhead power transmission lines | |
| CN206004706U (en) | A kind of data collecting system | |
| CN103175789B (en) | Water quality hyperspectral air remote sensing system based on many rotor wing unmanned aerial vehicles | |
| CN202068445U (en) | Mobile monitoring system | |
| CN106296871B (en) | Unmanned aerial vehicle supervision method and system | |
| CN203217082U (en) | Remotely-controlled flight GPS geographic information collection system | |
| WO2015188464A1 (en) | Agricultural remote sensing system | |
| CN102114635A (en) | Intelligent controller of inspection robot | |
| CN206515700U (en) | A kind of UAV Flight Control System based on smart mobile phone | |
| CN109901124A (en) | A kind of on-air radio electrical signal detection and analysis system | |
| CN108845587A (en) | Unmanned plane real-time control system and unmanned plane | |
| CN204258162U (en) | Helicopter in electric inspection process system | |
| CN203673535U (en) | Power line inspection device and system | |
| CN108803633A (en) | A kind of unmanned plane low latitude monitoring system based on mobile communications network | |
| CN113148156A (en) | Many rotor unmanned aerial vehicle with barrier function is kept away to laser intelligence | |
| CN207663283U (en) | A kind of unmanned plane vision guided navigation test system | |
| CN111142115A (en) | Intelligent distance measurement system and method based on unmanned aerial vehicle technology | |
| CN207000827U (en) | Aircraft, earth station and RF detection system | |
| CN203289564U (en) | Power line patrol system | |
| CN211427155U (en) | Based on unmanned aerial vehicle supervision integrated control system | |
| CN215932111U (en) | Aeromagnetic total field and horizontal gradient measuring system of multi-rotor unmanned aerial vehicle | |
| CN106864763A (en) | It is a kind of to aid in being accurately positioned and fixing device for unmanned plane landing | |
| CN207926581U (en) | A kind of environmental monitoring system and wireless communication module |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |