CN109001669A - The method of on-air radio pyroelectric monitor - Google Patents
The method of on-air radio pyroelectric monitor Download PDFInfo
- Publication number
- CN109001669A CN109001669A CN201810706774.4A CN201810706774A CN109001669A CN 109001669 A CN109001669 A CN 109001669A CN 201810706774 A CN201810706774 A CN 201810706774A CN 109001669 A CN109001669 A CN 109001669A
- Authority
- CN
- China
- Prior art keywords
- radio
- monitoring
- threshold value
- air
- signal strength
- 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.)
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
- G01S3/04—Details
- G01S3/12—Means for determining sense of direction, e.g. by combining signals from directional antenna or goniometer search coil with those from non-directional antenna
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/0278—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves involving statistical or probabilistic considerations
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/12—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Probability & Statistics with Applications (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Present disclose provides a kind of methods of on-air radio pyroelectric monitor, specifically comprise the following steps: the frequency of targeted radio clearly monitored in the air, and confirm the corresponding position of the targeted radio;Aerial platform flies to the position of the confirmation Target Wireless electric frequency;The signal strength for the monitoring frequency that observation radio monitoring equipment receives in real time simultaneously;When monitoring that radio signal strength reaches a scheduled threshold value, direction finding and positioning are carried out to targeted radio, and fly in the position that the corresponding position of the threshold value begins around report interference source;In the flight course, then when finding identical with the predetermined threshold position of at least one monitoring signals intensity, to targeted radio progress direction finding and positioning, and recorded;It is carried out providing the maximum location point of possibility according to the signal strength of the monitoring point of determining at least two, direction finding result.The disclosure can quickly and accurately carry out the monitoring of on-air radio electricity, greatly improve the efficiency of on-air radio pyroelectric monitor.
Description
Technical field
This disclosure relates to radio art more particularly to a kind of carry out on-air radio pyroelectric monitor using airflight platform
Method.
Background technique
Radio propagation belongs to unobstructed propagation, when radio is in overland propagation, will receive the objects such as high mountain, urban high-rise building
Body blocks, and radio signal can generate diffraction, refraction and scattering phenomenon, therefore when illegal wireless electric signal is passed on ground
Sowing time uses ground stationary monitoring base station, vehicle-mounted monitoring base station and hand-held monitoring device due to these irregular propagation phenomenons
It carries out being difficult fast and accurately to carry out direction finding and positioning when terrestrial wireless pyroelectric monitor;Come radio monitoring department this year gradually to open
The monitoring begun using aerial platform progress radio, major reason are that radio propagates similar clean room, no screening in the sky
Gear, Free propagation, while aerial platform flying height are high, at the same can a wide range of test flight, therefore carried out using aerial platform
Radio air monitoring is a kind of optimal monitoring means.
Radio air monitoring is carried out using aerial platform, direction finding and positioning especially are carried out to interference signal, need sky
Middle platform carries out aerial flight according to the radio signal received, and how to carry out flight is that aerial monitoring is quick, effective
Key.
Summary of the invention
(1) technical problems to be solved
Present disclose provides a kind of methods of on-air radio pyroelectric monitor, are asked with the technology at least partly solving set forth above
Topic.
(2) technical solution
According to one aspect of the disclosure, a kind of method of on-air radio pyroelectric monitor is provided, is specifically comprised the following steps:
S1: the frequency of the clear targeted radio monitored in the air, and confirm the corresponding position of the targeted radio;
S2: aerial platform takes off and flies towards the corresponding position of the confirmation targeted radio;Observe nothing in real time simultaneously
The signal strength for the monitoring frequency that line pyroelectric monitor equipment receives;
S3: when monitoring that radio signal strength reaches a scheduled threshold value, direction finding is carried out to targeted radio and is determined
Position, and fly in the position that the corresponding position of the threshold value begins around report interference source;
S4: in the flight course, then when finding identical with the predetermined threshold position of at least one monitoring signals intensity,
Direction finding and positioning are carried out to targeted radio, and recorded;
S5: cross bearing and probable ellipse are carried out according to the signal strength of the monitoring point of determining at least two, direction finding result
Statistics, and provide the maximum location point of possibility.
In some embodiments of the disclosure, in the step S1, it is disturbed report by described, determines targeted radio
Frequency, and the position for providing report interference source is reported according to being disturbed, determine the position of aerial monitoring respective frequencies radio.
In some embodiments of the disclosure, the position of the report interference source provided includes longitude and latitude, height.
In some embodiments of the disclosure, in the step S3, the scheduled threshold value is preset before flight, or is being flown
It is configured during row according to the Strength Changes of the signal monitored in the air.
In some embodiments of the disclosure, in the step S3, the scheduled threshold value is according to the signal monitored in the air
Strength Changes setting.
In some embodiments of the disclosure, in the step S3, when aerial platform reaches the position of the threshold value, around report
The position flight for accusing interference source includes: according to the point that can obtain at least one radio signal strength again as scheduled threshold value
Flight path flight.
In some embodiments of the disclosure, in the step S3, the flight path include round, rectangular, triangular form or
It turns back and flies.
In some embodiments of the disclosure, in the step S3, the flight path is circle, and the center of circle being diversion, which takes, to be reported
Accuse the position of interference source.
In some embodiments of the disclosure, in the step S5, when finding a monitoring signals intensity and predetermined threshold phase
With position when, according to the direction finding of the result of record corresponding with predetermined threshold first point record and location data realization to mesh
Mark radio is positioned.
In some embodiments of the disclosure, in the step S5, when finding multiple monitoring signals intensity and predetermined threshold phase
With position when, cross bearing and probable ellipse are carried out according to the signal strength of multiple points, direction finding result and counted, possibility is obtained
Maximum location point.
(3) beneficial effect
It can be seen from the above technical proposal that the method for disclosure on-air radio pyroelectric monitor at least has the advantages that
One of them:
(1) according to the characteristics of radio and the characteristics of aerial platform, airflight platform is utilized to carry out on-air radio electricity prison
It surveys, designs an exact flying method, can quickly and accurately carry out the monitoring of on-air radio electricity, greatly improve sky
The efficiency of middle radio monitoring;
(2) on-air radio pyroelectric monitor is carried out using aerial platform, can really restores the case where aviation radio interferes, is
Civil aviaton's flight provides aviation radio effective guarantee.
Detailed description of the invention
Fig. 1 is the flow chart of the method for embodiment of the present disclosure on-air radio pyroelectric monitor.
Fig. 2 is position of the flight position of embodiment of the present disclosure aerial platform relative to report interference source and actual signal source
Schematic diagram.
Fig. 3 is the specific flight profile, mission profile schematic diagram of embodiment of the present disclosure aerial platform.
Fig. 4 is the specific flight profile, mission profile schematic diagram of the another aerial platform of the embodiment of the present disclosure.
Fig. 5, which is the embodiment of the present disclosure, to carry out equal strength to echo signal and is diversion the schematic diagram of measurement.
Fig. 6 is the schematic diagram of a specific embodiment of the flying method of embodiment of the present disclosure on-air radio pyroelectric monitor.
Specific embodiment
Present disclose provides a kind of methods of on-air radio pyroelectric monitor.Because radio is Free propagation in the sky, do not have
One determining flying method is difficult to execute airflight monitoring task, due to carry out to unknown radio emitting source
Lateral and positioning, therefore just need to design an exact flying method according to the characteristics of radio and the characteristics of aerial platform,
To improve the efficiency of airflight monitoring.
Disclosure some embodiments will be done referring to appended attached drawing in rear and more comprehensively describe to property, some of but not complete
The embodiment in portion will be shown.In fact, the various embodiments of the disclosure can be realized in many different forms, and should not be construed
To be limited to this several illustrated embodiment;Relatively, these embodiments are provided so that the disclosure meets applicable legal requirement.
In first exemplary embodiment of the disclosure, a kind of method of on-air radio pyroelectric monitor is provided.Fig. 1 is this
The flow chart of the method for open first embodiment on-air radio pyroelectric monitor.As shown in Figure 1, the side of disclosure on-air radio pyroelectric monitor
Method specifically comprises the following steps:
S1: the frequency of the clear targeted radio monitored in the air, and confirm the corresponding position of the targeted radio;
In the step S1, targeted radio can be interference signal, in order to exclude the targeted radio of above-mentioned interference, need
Lateral and positioning is carried out to it.In general, the department for receiving Target Wireless electrical interference can provide and be disturbed report, pass through institute
State and be disturbed report, determine the frequency of targeted radio, and according to the position for being disturbed report and providing report interference source: for example through
Latitude, height etc. determine the position of aerial monitoring respective frequencies radio.It is general that report interference source can provide targeted radio
Orientation, but its actual position needs further measurement.
S2: aerial platform takes off and flies towards the corresponding position of targeted radio (such as report interference source);It is real simultaneously
When the signal strength of monitoring frequency that receives of observation radio monitoring equipment.
The flight position of aerial platform is as shown in Figure 2 relative to the position of report interference source and actual signal source.Carry out
When monitoring, aerial platform first flies according to the position of report interference source as a purpose, and the position of targeted radio, i.e.,
Actual interference position is located near report interference source.
The specific flight profile, mission profile of aerial platform is as shown in Figure 3 and Figure 4, the position in actual interference source it can be seen from Fig. 3 and Fig. 4
Set may than report interference source position is farther or the position in actual interference source is likely located to fly to and reports the way of interference source
In, and there is also differences for the height in actual interference source and the height of report interference source.
S3: when monitoring that radio signal strength reaches a scheduled threshold value, direction finding is carried out to targeted radio and is determined
Position, and fly in the position that the corresponding position of the threshold value begins around report interference source.
The scheduled threshold value can select a moderate threshold value according to the Strength Changes of the signal monitored in the air);Example
Such as: 20dB, 50dB.
When aerial platform reaches the position of the threshold value, start to be diversion around report interference source.In some implementations
In example, the center of circle being diversion is taken on the straight line of course line, the position near report interference source, at this time can be with the threshold value
Round tangent line is done in position, is that 500 meters, 1000 meters, 2000 meters or larger radius are diversion with radius, as shown in Figure 5;It is preferred that
Ground, the center of circle being diversion take in the position of report interference source.
In different embodiments, the position flight around report interference source can also use other tracks, such as just
Shape, triangular form or flight etc. of turning back.It is that finding other radio signal strengths is scheduled threshold value around the purpose of flight
Point, any available radio signal strength of the flight path used is the flight path of the point of scheduled threshold value.
S4: in the flight course, then when finding identical with the predetermined threshold position of at least one monitoring signals intensity,
Direction finding and positioning are carried out to targeted radio, and recorded.
When finding identical with the predetermined threshold position of two monitoring signals intensity, similarly targeted radio is surveyed
To and positioning, therefore the intersection point of the straight line in the targeted radio direction obtained according to the direction finding of two points be possible target without
The position of line electricity.
When finding identical with the predetermined threshold position of more than two monitoring signals intensity, similarly to targeted radio into
The probability firmware to Target Wireless electric position may be implemented according to the direction finding of multiple spot in row direction finding and positioning.
S5: cross bearing and probable ellipse are carried out according to the signal strength of the monitoring point of determining at least two, direction finding result
Statistics, and provide the maximum location point of possibility.
When finding identical with the predetermined threshold position of a monitoring signals intensity, according to the result and predetermined threshold of record
The direction finding of corresponding first point record and location data can be realized and be positioned to targeted radio.
When finding identical with the predetermined threshold position of multiple monitoring signals intensity, according to the signal strength of multiple points, survey
Cross bearing and probable ellipse statistics, the available maximum location point of possibility are carried out to result.
Using the flying method, can the fast and accurate monitoring for carrying out on-air radio electricity, greatly improve on-air radio
The efficiency and result of pyroelectric monitor.
For the purposes, technical schemes and advantages of the disclosure are more clearly understood, below in conjunction with specific embodiment, and reference
The disclosure is further described in attached drawing.
Embodiment
Using Civil Aviation ATM receive AIRLINE & AIRPORT airliner pilot report aerial noise spot as example, when Civil Aviation ATM portion
Door receives unit after B point (longitude and latitude, height) receives the reporting of interference, and sets out monitoring helicopter and execute interference and search to appoint
Business, as shown in Figure 6:
Aerial monitoring helicopter takes off, and from takeoff point A point rectilinear flight, flies towards reporting point B point;
As point of arrival C0, discovery monitored signal intensity reaches preset threshold value 30dB, records the longitude and latitude of the point, high
Degree, the measurement direction of signal strength and targeted radio;
Fixed lower signal strength is carried out equal strength to echo signal and is diversion measurement, monitored helicopter in the air, started with C0 point
It carries out using B point as the circular flight in the center of circle;
When flying to C1 point, signal strength is as preset threshold value, the monitoring system registers longitude and latitude, height, letter
The measurement direction of number intensity and targeted radio;
When continuing flight to C2, signal strength is the same with threshold value, the monitoring system registers longitude and latitude, height, and signal is strong
The measurement direction of degree and targeted radio;
According to the measurement result of tri- points of C0, C1, C2, cross bearing calculates the position of measured signal, and on map
It carries out drawing out specific location.
According to the multi-point signal situation tested, the probable ellipse and maximum probability positioning T point of noise spot appearance are provided.
So far, attached drawing is had been combined the embodiment of the present disclosure is described in detail.It should be noted that in attached drawing or saying
In bright book text, the implementation for not being painted or describing is form known to a person of ordinary skill in the art in technical field, and
It is not described in detail.In addition, the above-mentioned definition to each element and method be not limited in mentioning in embodiment it is various specific
Structure, shape or mode, those of ordinary skill in the art simply can be changed or be replaced to it.
It should also be noted that, the direction term mentioned in embodiment, for example, "upper", "lower", "front", "rear", " left side ",
" right side " etc. is only the direction with reference to attached drawing, not is used to limit the protection scope of the disclosure.Through attached drawing, identical element by
Same or similar appended drawing reference indicates.When may cause understanding of this disclosure and cause to obscure, conventional structure will be omitted
Or construction.
And the shape and size of each component do not reflect actual size and ratio in figure, and only illustrate the embodiment of the present disclosure
Content.In addition, in the claims, any reference symbol between parentheses should not be configured to the limit to claim
System.
It unless there are known entitled phase otherwise anticipates, the numerical parameter in this specification and appended claims is approximation, energy
Enough bases pass through the resulting required characteristic changing of content of this disclosure.Specifically, all be used in specification and claim
The middle content for indicating composition, the number of reaction condition etc., it is thus understood that repaired by the term of " about " in all situations
Decorations.Under normal circumstances, the meaning expressed refers to include by specific quantity ± 10% variation in some embodiments, some
± 5% variation in embodiment, ± 1% variation in some embodiments, in some embodiments ± 0.5% variation.
Furthermore word "comprising" does not exclude the presence of element or step not listed in the claims.It is located in front of the element
Word "a" or "an" does not exclude the presence of multiple such elements.
In addition, unless specifically described or the step of must sequentially occur, there is no restriction in the above institute for the sequence of above-mentioned steps
Column, and can change or rearrange according to required design.And above-described embodiment can be based on the considerations of design and reliability, that
This mix and match is used using or with other embodiments mix and match, i.e., the technical characteristic in different embodiments can be freely combined
Form more embodiments.
Those skilled in the art will understand that can be carried out adaptively to the module in the equipment in embodiment
Change and they are arranged in one or more devices different from this embodiment.It can be the module or list in embodiment
Member or component are combined into a module or unit or component, and furthermore they can be divided into multiple submodule or subelement or
Sub-component.Other than such feature and/or at least some of process or unit exclude each other, it can use any
Combination is to all features disclosed in this specification (including adjoint claim, abstract and attached drawing) and so disclosed
All process or units of what method or apparatus are combined.Unless expressly stated otherwise, this specification is (including adjoint power
Benefit require, abstract and attached drawing) disclosed in each feature can carry out generation with an alternative feature that provides the same, equivalent, or similar purpose
It replaces.Also, in the unit claims listing several devices, several in these devices can be by same hard
Part item embodies.
Similarly, it should be understood that in order to simplify the disclosure and help to understand one or more of each open aspect,
Above in the description of the exemplary embodiment of the disclosure, each feature of the disclosure is grouped together into single implementation sometimes
In example, figure or descriptions thereof.However, the disclosed method should not be interpreted as reflecting the following intention: i.e. required to protect
The disclosure of shield requires features more more than feature expressly recited in each claim.More precisely, as following
Claims reflect as, open aspect is all features less than single embodiment disclosed above.Therefore,
Thus the claims for following specific embodiment are expressly incorporated in the specific embodiment, wherein each claim itself
All as the separate embodiments of the disclosure.
Particular embodiments described above has carried out further in detail the purpose of the disclosure, technical scheme and beneficial effects
Describe in detail it is bright, it is all it should be understood that be not limited to the disclosure the foregoing is merely the specific embodiment of the disclosure
Within the spirit and principle of the disclosure, any modification, equivalent substitution, improvement and etc. done should be included in the guarantor of the disclosure
Within the scope of shield.
Claims (10)
1. a kind of method of on-air radio pyroelectric monitor, specifically comprises the following steps:
S1: the frequency of the clear targeted radio monitored in the air, and confirm the corresponding position of the targeted radio;
S2: aerial platform takes off and flies towards the corresponding position of the confirmation targeted radio;Observe radio in real time simultaneously
The signal strength for the monitoring frequency that monitoring device receives;
S3: when monitoring that radio signal strength reaches a scheduled threshold value, carrying out direction finding and positioning to targeted radio, and
It flies in the position that the corresponding position of the threshold value begins around report interference source;
S4: in the flight course, then when finding identical with the predetermined threshold position of at least one monitoring signals intensity, to mesh
It marks radio and carries out direction finding and positioning, and recorded;
S5: the system of cross bearing and probable ellipse is carried out according to the signal strength of the monitoring point of determining at least two, direction finding result
Meter, and provide the maximum location point of possibility.
2. according to the method described in claim 1, being disturbed report in the step S1 by described, determining targeted radio
Frequency determine the position of aerial monitoring respective frequencies radio and according to the position for being disturbed report and providing report interference source.
3. according to the method described in claim 1, the position of the report interference source provided includes longitude and latitude, height.
4. according to the method described in claim 3, the scheduled threshold value is preset before flight, Huo Zhe in the step S3
It is configured in flight course according to the Strength Changes of the signal monitored in the air.
5. according to the method described in claim 4, the scheduled threshold value is according to the signal monitored in the air in the step S3
Strength Changes setting.
6. according to the method described in claim 3, when aerial platform reaches the position of the threshold value, being surrounded in the step S3
The position flight of report interference source includes: according to the point that can obtain at least one radio signal strength again as scheduled threshold value
Flight path flight.
7. according to the method described in claim 6, in the step S3, the flight path include round, rectangular, triangular form or
It turns back and flies.
8. according to the method described in claim 6, the flight path is circle, and the center of circle being diversion takes in the step S3
Report the position of interference source.
9. according to the method described in claim 6, in the step S5, when finding a monitoring signals intensity and predetermined threshold phase
With position when, according to the direction finding of the result of record corresponding with predetermined threshold first point record and location data realization to mesh
Mark radio is positioned.
10. according to the method described in claim 6, in the step S5, when finding multiple monitoring signals intensity and predetermined threshold
When identical position, cross bearing is carried out according to the signal strength of multiple points, direction finding result and probable ellipse counts, obtains possibility
The maximum location point of property.
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CN201810706774.4A CN109001669A (en) | 2018-06-29 | 2018-06-29 | The method of on-air radio pyroelectric monitor |
CN202211002532.XA CN115372889A (en) | 2018-06-29 | 2018-06-29 | Method for over-the-air radio monitoring |
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CN201810706774.4A CN109001669A (en) | 2018-06-29 | 2018-06-29 | The method of on-air radio pyroelectric monitor |
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CN201810706774.4A Pending CN109001669A (en) | 2018-06-29 | 2018-06-29 | The method of on-air radio pyroelectric monitor |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113110541A (en) * | 2021-04-15 | 2021-07-13 | 浙江大学 | Radio frequency spectrum monitoring and positioning device and method based on unmanned aerial vehicle and mobile ground station |
CN114035150A (en) * | 2021-07-28 | 2022-02-11 | 中国电子科技集团公司第二十九研究所 | Radio frequency source direction finding device and positioning method based on unmanned aerial vehicle lift-off platform |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2500743A1 (en) * | 2011-03-16 | 2012-09-19 | Exelis Inc. | System and method for three-dimensional geolocation of emitters based on energy measurements |
CN104155981A (en) * | 2014-06-30 | 2014-11-19 | 成都点阵科技有限公司 | Air radio monitoring system based on ground remote control of multi-rotor robot |
CN104320208A (en) * | 2014-11-11 | 2015-01-28 | 西华大学 | Air radio monitoring method |
CN204203456U (en) * | 2014-11-11 | 2015-03-11 | 西华大学 | For the aerial intelligent robot of radio monitoring |
CN106301623A (en) * | 2016-09-09 | 2017-01-04 | 成都定为电子技术有限公司 | The interference source detection identification method of a kind of spectrum monitoring unmanned plane and device thereof |
-
2018
- 2018-06-29 CN CN202211002532.XA patent/CN115372889A/en active Pending
- 2018-06-29 CN CN201810706774.4A patent/CN109001669A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2500743A1 (en) * | 2011-03-16 | 2012-09-19 | Exelis Inc. | System and method for three-dimensional geolocation of emitters based on energy measurements |
CN104155981A (en) * | 2014-06-30 | 2014-11-19 | 成都点阵科技有限公司 | Air radio monitoring system based on ground remote control of multi-rotor robot |
CN104320208A (en) * | 2014-11-11 | 2015-01-28 | 西华大学 | Air radio monitoring method |
CN204203456U (en) * | 2014-11-11 | 2015-03-11 | 西华大学 | For the aerial intelligent robot of radio monitoring |
CN106301623A (en) * | 2016-09-09 | 2017-01-04 | 成都定为电子技术有限公司 | The interference source detection identification method of a kind of spectrum monitoring unmanned plane and device thereof |
Non-Patent Citations (1)
Title |
---|
刘益君: ""空中无线电监测测向系统研究"", 《中国优秀博硕士学位论文全文数据库(硕士) 信息科技辑》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113110541A (en) * | 2021-04-15 | 2021-07-13 | 浙江大学 | Radio frequency spectrum monitoring and positioning device and method based on unmanned aerial vehicle and mobile ground station |
CN114035150A (en) * | 2021-07-28 | 2022-02-11 | 中国电子科技集团公司第二十九研究所 | Radio frequency source direction finding device and positioning method based on unmanned aerial vehicle lift-off platform |
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CN115372889A (en) | 2022-11-22 |
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