CN105270602A - Method and device for realizing direction finding and positioning of radio signals by multi-rotor (multi-shaft) aircraft - Google Patents
Method and device for realizing direction finding and positioning of radio signals by multi-rotor (multi-shaft) aircraft Download PDFInfo
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- CN105270602A CN105270602A CN201410226468.2A CN201410226468A CN105270602A CN 105270602 A CN105270602 A CN 105270602A CN 201410226468 A CN201410226468 A CN 201410226468A CN 105270602 A CN105270602 A CN 105270602A
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Abstract
The invention relates to a method and device for realizing direction finding and positioning of radio signals by a multi-rotor (multi-shaft) aircraft. The invention aims to realize direction finding and positioning of radio signals from the air, utilizes the structural features of the multi-rotor (multi-shaft) aircraft, mounts direction-finding antennas on the rotor arms to compose a direction-finding antenna array, thus realizing the direction finding and positioning method and device of radio signals.
Description
One, technical field
The invention belongs to radio monitoring and direction-finding field, make full use of many rotors (multiaxis) Flight Vehicle Structure feature, direction-finder antenna be arranged on horn, composition direction estimation antenna array, realizes the DF and location of radio signal.
Two, background technology
Along with developing rapidly of China's urban construction and increasing of all kinds of radio facility, normal communication also increases increasingly by the event of radio interference.Radiowave when ground propagation, can because the refraction of all media, reflection and become disorderly and unsystematic; And when aloft propagating, almost do not reflect, there is through property.This feature make to monitor in the air the position of interference source that obtains and direction be almost the most truly, information the most accurately.In addition, the aircraft speed implementing aerial monitoring is very fast, and can be flown to rapidly another point by a point, carry out grade separation multipoint positioning, therefore, the position of interference source accuracy rate obtained is very high.
The direction finding of on-air radio pyroelectric monitor supplements as the one of traditional monitoring pattern, existing monitoring net can be formed the multi-function modern three-dimensional monitoring nets such as Long-distance Control, associating direction finding, emphasis monitoring, can realize covering institute's administrative area full frequency band, full-service, all the period of time, omnibearing monitoring, thus General Promotion technology management level.
1. explanation of nouns
1). radio direction finding
According to character and the propagation characteristic of radiowave, use specialized instrument and equipment, measure the process of radio arrival bearing.
2). channels watcher
Measure the specialized instrument and equipment of radiowave arrival bearing.Generally include four parts: direction-finder antenna, Input matching crosspoint, receiver, direction information processes and displays (instruction) unit.
3). radio monitoring
For obtaining frequency spectrum, frequency, signal information or being acquisition radio intelligence information in military struggle in radio spectrum management, and the technological means implemented.Which includes the sport technique segments such as monitoring, direction finding, identification, building database.
4). wireless monitoring
For obtaining radio target frequency bands signal, the relevant information of echo signal, the technological means such as the reception taked, monitoring, identification, analysis, record.
5) many rotors (multiaxis) aircraft
Multi-rotor aerocraft is also Multi-axis aircraft, by the flying platform organized power system more and form, generally common are four rotors, six rotors, eight rotors ... 18 rotors, even more rotor compositions.Electronic multi-rotor aerocraft drives screw propeller to form single group rotor power system, by inertial navigation system, flight control system, navigationsystem, electronic governor composition control drive part by brushless motor.Aircraft can carry the lift-offs such as imaging equipment, Communication Equipment, collection equipment, special equipment as flight carrier, can reach the height (0-500 rice) of traditional approach out of reach.
Multi-rotor aerocraft is different from the feature of other aircraft:
A) multi-rotor aerocraft has obvious advantage with the structure of its uniqueness with succinct system architecture compared with conventional aircraft.
B) move aircraft using Hi cell as energy with oil compared with noise lower, low-latitude flying can be realized and not easily discover.
C) vertical takeoff and landing can just can stabilized flight at comparatively narrow space, and determines to have not by the advantage that place limits compared with rotor aircraft.
D) (only motor bearings the is mechanical part) maintenance compared with conventional helicopters (having more complicated mechanical part and drive mechanism) of simple mechanical part composition is quite simple.
E) clear superiority that volume is little, lightweight, load-carrying is greatly multi-rotor aerocraft, by FHP-Z617, aircraft deadweight 2kg, can carry and comprise the weight of battery pack up to 4kg, load-carrying ability is 2 times of own wt.And development size is less than a sq m, the portable transportation case of 70*65*35 after folding, easily can be received into together with accessory device.
F) complete machine all-electronin increases steady, simple to operate.Autonomous navigation can realize full automaticity flight.The power system of excellent performance provides the flight attitude of maneuverability, and wind loading rating is strong.
Many rotor flyings system can be widely used in agriculture low-to-medium altitude and sow seeds, sprays insecticide, the supervision of security monitoring, forest extinguishing, the condition of a disaster, emergency communication, electric power application, marine applications, weather monitoring, aerial survey of taking photo by plane, also will be developed further to the application of more than 30 the industry aspects such as aerial exploration, noiseless investigation, border patrol, nuclear radiation detection, mineral exploration aviation, traffic patrolling in addition.
2. utilize many rotors (multiaxis) aircraft to carry out the current situation and problem of direction finding
There is no the correlation technique and the report that utilize many rotors (multiaxis) aircraft to carry out radio direction finding at present.
Three, summary of the invention:
The object of the invention is to realize from carrying out DF and location to radio signal in the air, utilize many rotors (multiaxis) Flight Vehicle Structure feature, direction-finder antenna be arranged on horn, composition direction estimation antenna array, realizes the DF and location method and apparatus of radio signal.
The object of the invention is to be achieved through the following technical solutions:
Many rotors (multiaxis) aircraft realizes radio-signal direction finding localization method, it is characterized in that by astronomical cycle on many rotors (multiaxis) aircraft rotor support arm, and composition aerial system, reaches the object of DF and location.
Many rotors (multiaxis) aircraft realizes radio-signal direction finding localization method, it is characterized in that installing radio signal reception direction finding apparatus on many rotors (multiaxis) aircraft.
Many rotors (multiaxis) aircraft realizes radio-signal direction finding localization method, it is characterized in that being arranged on by directional antenna on many rotors (multiaxis) aircraft.
Many rotors (multiaxis) aircraft realizes radio-signal direction finding registration device, it is characterized in that by astronomical cycle on many rotors (multiaxis) aircraft rotor support arm, and composition aerial system, reaches the object of DF and location.
Many rotors (multiaxis) aircraft realizes radio-signal direction finding registration device, it is characterized in that comprising many rotors (multiaxis) aircraft, receiver, direction finding treater, antenna, wireless transmission unit.
Many rotors (multiaxis) aircraft realizes radio-signal direction finding registration device, it is characterized in that comprising directional antenna.
Four, beneficial effect:
The present invention contrasts prior art and has following innovative point:
1, many rotors (multiaxis) aircraft of selected technology maturation.
2, make full use of many rotors (multiaxis) Flight Vehicle Structure feature, direction-finder antenna is arranged on horn, composition direction estimation antenna array.The present invention contrasts prior art and has following remarkable advantage:
1, many rotors (multiaxis) vehicle technology is ripe, with low cost, simple to operate, has been widely used in taking photo by plane, agricultural, forestry, sea-freight, the fields such as traffic.
2, make full use of many rotors (multiaxis) Flight Vehicle Structure feature, do not break and change aircraft integral structure and load-carrying balance, direction-finder antenna is arranged on horn, composition direction estimation antenna array.
3, easy to use, namely can fly empty use, also can many rotors (multiaxis) aircraft being provided with direction finding apparatus is placed on the fastenings such as tripod, use as fixing direction finding apparatus.
4, equipment is light, is convenient to install erection and use.
Five, accompanying drawing explanation
Fig. 1 is the schematic diagram of the inventive method;
Fig. 2 is the schematic diagram of apparatus of the present invention 1;
Fig. 3 is the schematic diagram of the embodiment of the present invention;
Wherein: 101-1# antenna, 102-2# antenna, 103-3# antenna, 104-4# antenna, the many rotors of 105-(multiaxis) aircraft, 106-direction finding apparatus, 107-tripod.
Six, detailed description of the invention
Below in conjunction with accompanying drawing 3 and embodiment, the invention will be further described.
Basic thought of the present invention is that many rotors (multiaxis) vehicle technology adopted is ripe, with low cost, simple to operate, make full use of many rotors (multiaxis) Flight Vehicle Structure feature, do not break and change aircraft integral structure and load-carrying balance, direction-finder antenna be arranged on horn, composition direction estimation antenna array, completes on-air radio electric signal DF and location, monitoring analysis.
Embodiment:
Adopt Foxtech8 rotor craft (105), direction finding apparatus DF3301 (106), the antenna DAT2030 (101 of Chengdu Zerosoft Technology Co., Ltd. are installed thereon, 102,103,104 ...) be arranged on aircraft rotor support arm, composition direction estimation antenna array, realizes Aerial Direction Finding location; The aircraft installing direction finding apparatus additional also can be arranged on tripod (on 107), realizes the direction finding of fixed ground.
Below by reference to the accompanying drawings the specific embodiment of the present invention is described; but these explanations can not be understood to limit scope of the present invention; protection scope of the present invention is limited by the claims of enclosing, and any change on the claims in the present invention basis is all protection scope of the present invention.
Claims (9)
1. rotor more than (multiaxis) aircraft realizes radio-signal direction finding localization method, it is characterized in that by astronomical cycle on many rotors (multiaxis) aircraft rotor support arm or its extended position, and composition aerial system, reaches the object of DF and location.
2. many rotors (multiaxis) aircraft according to right 1 realizes radio-signal direction finding localization method, it is characterized in that installing radio signal reception direction finding apparatus on many rotors (multiaxis) aircraft.
3. many rotors (multiaxis) aircraft according to right 1 realizes radio-signal direction finding localization method, it is characterized in that antenna is collapsible.
4. many rotors (multiaxis) aircraft according to right 1 realizes radio-signal direction finding localization method, it is characterized in that being arranged on by directional antenna on many rotors (multiaxis) aircraft.
5. many rotors (multiaxis) aircraft according to right 1 realizes radio-signal direction finding localization method, it is characterized in that many rotors (multiaxis) aircraft being provided with direction finding apparatus to be placed on the fastenings such as tripod, use as fixing direction finding apparatus.
6. rotor more than (multiaxis) aircraft realizes radio-signal direction finding registration device, it is characterized in that by astronomical cycle on many rotors (multiaxis) aircraft rotor support arm or its extended position, and composition aerial system, reaches the object of DF and location.
7. many rotors (multiaxis) aircraft according to right 4 realizes radio-signal direction finding registration device, it is characterized in that comprising many rotors (multiaxis) aircraft, receiver, direction finding treater, antenna, wireless transmission unit.
8. many rotors (multiaxis) aircraft according to right 4 realizes radio-signal direction finding registration device, it is characterized in that comprising directional antenna.
9. many rotors (multiaxis) aircraft according to right 4 realizes radio-signal direction finding registration device, comprise tripod, many rotors (multiaxis) aircraft being provided with direction finding apparatus is placed on the fastenings such as tripod, uses as fixing direction finding apparatus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410226468.2A CN105270602A (en) | 2014-05-27 | 2014-05-27 | Method and device for realizing direction finding and positioning of radio signals by multi-rotor (multi-shaft) aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410226468.2A CN105270602A (en) | 2014-05-27 | 2014-05-27 | Method and device for realizing direction finding and positioning of radio signals by multi-rotor (multi-shaft) aircraft |
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| CN105270602A true CN105270602A (en) | 2016-01-27 |
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| CN201410226468.2A Pending CN105270602A (en) | 2014-05-27 | 2014-05-27 | Method and device for realizing direction finding and positioning of radio signals by multi-rotor (multi-shaft) aircraft |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107108009A (en) * | 2016-09-05 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and its frame, frame assembling external member |
| CN107672803A (en) * | 2017-09-14 | 2018-02-09 | 青岛四合信息科技有限公司 | A kind of technology and device of the automatic detection calibration radio guard of unmanned plane |
| CN109216873A (en) * | 2016-11-23 | 2019-01-15 | 深圳市大疆创新科技有限公司 | Rack, unmanned vehicle and the antenna switching method of unmanned vehicle |
| EP3835804A1 (en) * | 2019-12-10 | 2021-06-16 | Rohde & Schwarz GmbH & Co. KG | Unmanned aerial vehicle as well as direction finding system |
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| DE102008024308A1 (en) * | 2008-05-20 | 2009-12-03 | Eads Deutschland Gmbh | Method for detecting non-cooperative air traffic on-board of aircraft, involves calculating distance or position of target on both blades of aircraft from angles by two sensors |
| CN202471957U (en) * | 2012-03-30 | 2012-10-03 | 成都九华圆通科技发展有限公司 | Unmanned airborne radio monitoring direction-finding system |
| CN103402225A (en) * | 2013-08-20 | 2013-11-20 | 成都零点科技有限公司 | Method and device for supervising radio relay station |
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2014
- 2014-05-27 CN CN201410226468.2A patent/CN105270602A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008024308A1 (en) * | 2008-05-20 | 2009-12-03 | Eads Deutschland Gmbh | Method for detecting non-cooperative air traffic on-board of aircraft, involves calculating distance or position of target on both blades of aircraft from angles by two sensors |
| CN202471957U (en) * | 2012-03-30 | 2012-10-03 | 成都九华圆通科技发展有限公司 | Unmanned airborne radio monitoring direction-finding system |
| CN103402225A (en) * | 2013-08-20 | 2013-11-20 | 成都零点科技有限公司 | Method and device for supervising radio relay station |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107108009A (en) * | 2016-09-05 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and its frame, frame assembling external member |
| WO2018040116A1 (en) * | 2016-09-05 | 2018-03-08 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, and rack and rack assembly kit thereof |
| CN109216873A (en) * | 2016-11-23 | 2019-01-15 | 深圳市大疆创新科技有限公司 | Rack, unmanned vehicle and the antenna switching method of unmanned vehicle |
| CN109216873B (en) * | 2016-11-23 | 2020-11-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle frame, unmanned aerial vehicle and antenna switching method |
| CN107672803A (en) * | 2017-09-14 | 2018-02-09 | 青岛四合信息科技有限公司 | A kind of technology and device of the automatic detection calibration radio guard of unmanned plane |
| EP3835804A1 (en) * | 2019-12-10 | 2021-06-16 | Rohde & Schwarz GmbH & Co. KG | Unmanned aerial vehicle as well as direction finding system |
| CN113044209A (en) * | 2019-12-10 | 2021-06-29 | 罗德施瓦兹两合股份有限公司 | Unmanned aerial vehicle and direction finding system |
| US11754657B2 (en) | 2019-12-10 | 2023-09-12 | Rohde & Schwarz Gmbh & Co. Kg | Unmanned aerial vehicle as well as direction finding system |
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Addressee: Chengdu Zero Technology Co., Ltd. Document name: Notification of Publication and of Entering the Substantive Examination Stage of the Application for Invention |
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Address after: West high tech Zone Fucheng Road in Chengdu city of Sichuan province 610000 No. 399 Tianfu New Valley No. 8 unit 1 Building No. 1701 Applicant after: Chengdu Zero Technology Co., Ltd. Address before: West high tech Zone Fucheng Road in Chengdu city of Sichuan province 610000 No. 399 Tianfu New Valley Building No. 5 room 1206 Applicant before: Chengdu Zero Technology Co., Ltd. |
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Application publication date: 20160127 |