CN113406679A - Airborne equipment positioning device based on ADS-B signal - Google Patents

Airborne equipment positioning device based on ADS-B signal Download PDF

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Publication number
CN113406679A
CN113406679A CN202110527119.4A CN202110527119A CN113406679A CN 113406679 A CN113406679 A CN 113406679A CN 202110527119 A CN202110527119 A CN 202110527119A CN 113406679 A CN113406679 A CN 113406679A
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China
Prior art keywords
module
ads
signal
flying
driving device
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Pending
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CN202110527119.4A
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Chinese (zh)
Inventor
梁玉谊
罗喜伶
许乙付
罗亨
王珺珺
刘宏
邵斌
王彦双
王朝斌
王奇
梁永福
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CHINA EXPRESS CO LTD
Hangzhou Innovation Research Institute of Beihang University
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CHINA EXPRESS CO LTD
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Priority to CN202110527119.4A priority Critical patent/CN113406679A/en
Publication of CN113406679A publication Critical patent/CN113406679A/en
Pending legal-status Critical Current

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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
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/421—Determining position by combining or switching between position solutions or signals derived from different satellite radio beacon positioning systems; by combining or switching between position solutions or signals derived from different modes of operation in a single system
    • G01S19/425—Determining position by combining or switching between position solutions or signals derived from different satellite radio beacon positioning systems; by combining or switching between position solutions or signals derived from different modes of operation in a single system by combining or switching between signals derived from different satellite radio beacon positioning systems
    • A—HUMAN NECESSITIES
    • A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M29/00—Scaring or repelling devices, e.g. bird-scaring apparatus
    • A01M29/16—Scaring or repelling devices, e.g. bird-scaring apparatus using sound waves
    • A01M29/18—Scaring or repelling devices, e.g. bird-scaring apparatus using sound waves using ultrasonic signals
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • 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
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
    • G01S19/10—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing dedicated supplementary positioning signals
    • G01S19/12—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing dedicated supplementary positioning signals wherein the cooperating elements are telecommunication base stations
    • 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
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/428—Determining position using multipath or indirect path propagation signals in position determination
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01W—METEOROLOGY
    • G01W1/00—Meteorology
    • G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0095—Devices specially adapted to avoid bird strike

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Environmental Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • Birds (AREA)
  • Pest Control & Pesticides (AREA)
  • Wood Science & Technology (AREA)
  • Zoology (AREA)
  • Insects & Arthropods (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Atmospheric Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Ecology (AREA)
  • Toys (AREA)

Abstract

The invention provides an airborne equipment positioning device based on ADS-B signals, which comprises an airborne box, wherein a positioning system is welded in the airborne box, a flying device is connected on the airborne box, when the device works, the device can be used for monitoring the ground in an aviation manner and monitoring wind speed, distance, temperature, humidity and the like through the positioning system, the situations of field installation, arrangement, operation, carrying, flying test and the like of the aviation flying equipment are facilitated, when the aviation flying equipment flies, a flying animal can be encountered, when the flying animal is detected through a detector in a long distance, an ultrasonic driving device sends ultrasonic waves to drive the flying animal, if the driving is not in time, when the flying animal flies to the aviation flying equipment, the flying animal tends to light to work, the flying animal is attracted, under the action of a translation plate, the flight animal falls into and holds the intracavity, prevents that flight animal and aviation flight equipment from directly bumping.

Description

Airborne equipment positioning device based on ADS-B signal
Technical Field
The invention belongs to the technical field of ADS-B, and particularly relates to an airborne equipment positioning device based on ADS-B signals.
Background
The ADS-B is a broadcast type automatic relevant monitoring, as the name suggests, namely, the information such as the position, the height, the speed, the course, the identification number and the like of the airplane can be automatically acquired from relevant airborne equipment without manual operation or inquiry, so that a controller can monitor the state of the airplane, the airborne equipment is equipment for measuring, processing, transmitting, displaying and controlling various information, instructions and operations in the flying process of the airplane, and when the aviation flying equipment works, the aviation flying equipment is easy to collide with flying animals, so that the flying animals are prevented from being touched, the flying animals are prevented from being accidentally injured, and the airplane is prevented from being damaged.
Disclosure of Invention
The invention aims to provide an airborne equipment positioning device based on ADS-B signals, so as to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: an airborne equipment positioning device based on ADS-B signals comprises an airborne box, wherein a positioning system is welded in the airborne box, and a flying device is connected to the airborne box;
the flight device is including driving device and nearly device of tending far away, nearly device of tending is located device one side of driving far away, the device of driving far away includes the battery, the detector, the ultrasonic wave drives the ware, control panel, rotating device and reflecting plate, the battery respectively with the detector, ultrasonic wave drives ware and control panel, rotating device electric connection, the detector, ultrasonic wave drives ware and rotating device respectively with control panel electric connection, the battery, the detector, the ultrasonic wave drives the ware, control panel is located the rotating device inboard, the last reflecting plate of installing of rotating device, rotating device drives the reflecting plate and is the circular type motion.
As optimizing, nearly trend device is including trend light, translation board, holding the chamber, holds chamber side-mounting and has the translation board, and translation board opposite side is located and holds the intracavity, holds intracavity portion and installs trend light, and trend light runs through and holds the chamber, means that trend light can illuminate and hold the chamber.
Preferably, the number of the reflecting plates is two or more, and the reflecting plates are located around the rotating device.
Preferably, the reflection angle of the ultrasonic driver is different relative to each reflection plate.
Preferably, the widths of the two or more reflection plates are different.
Preferably, the ultrasonic wave driving device comprises a first frequency band ultrasonic wave driving device, a second frequency band ultrasonic wave driving device and a third frequency band ultrasonic wave driving device.
As optimization, the translation plate is provided with filter holes.
As optimization, the positioning system comprises a power module, a GNSS module, a data processing module, an ADS-B signal module, a sensor module, a communication module and a control terminal, wherein the power module respectively provides power for the GNSS module, the data processing module, the ADS-B signal module, the sensor module and the communication module;
the GNSS module transmits the received information to the control terminal after processing the received information by the data processing module; the ADS-B signal module transmits the received signals to the control terminal after the received signals are processed by the data processing module; the communication module transmits the received communication information to the data processing module in real time and transmits the communication information to the control terminal after the communication information is processed.
For optimization, the control terminal sends out corresponding command information which is processed by the data processing module and then is respectively transmitted to the GNSS module, the data processing module, the ADS-B signal module, the sensor module and the communication module, the GNSS module, the data processing module, the ADS-B signal module, the sensor module and the communication module send out received signals and send the signals to satellites, base stations and the like, the sensor module sends the received signals to the control terminal after the received signals are processed by the data processing module, the target signals are GNSS (Global Navigation Satellite System) Satellite positioning signals, radar inquiry signals received and identified by a transponder, ADS-B (Automatic Dependent Surveillance-Broadcast) signals sent by the ground or an aircraft, data communication signals and flight service signals sent by a ground server, and the like;
the power supply module provides power for the GNSS module, the data processing module, the ADS-B signal module, the sensor module and the communication module; the GNSS generally refers to a global navigation satellite system, and comprises GPS positioning, Beidou positioning and the like, and at present, the domestic production is advocated domestically, and a GNSS module is recommended to use a Beidou satellite navigation system; the GNSS module transmits the received information to the control terminal after processing the received information by the data processing module; the ADS-B signal module transmits the received signals to the control terminal after the received signals are processed by the data processing module; the communication module transmits the received communication information to the data processing module in real time, processes the communication information and transmits the processed communication information to the control terminal (the communication module is connected with the communication base station through wireless, and the communication base station is connected with the communication satellite through wireless signals); the module information transmission is reversible, or the control terminal can send out corresponding command information to the data processing module for processing, then transmit the processed command information to each module, then send the processed command information to the satellite, the base station and the like, and transmit the processed command information to the control terminal after the sensor module (wind speed, distance, temperature, humidity and the like) processes the received command information to the data processing module.
Compared with the prior art, the invention has the beneficial effects that: according to the invention, the positioning system can be used for aerial monitoring the ground, and can also be used for monitoring wind speed, distance, temperature, humidity and the like, so that the conditions of field installation, arrangement, operation, carrying, flight test and the like of the aerial flight equipment are facilitated, the flying device can be arranged to repel flying animals, the flying animals which cannot be repelled are driven, the approaching flying animals are attracted by the approaching device, and then the accommodating cavity is introduced, so that the flying animals are prevented from colliding with the aerial flight equipment.
Drawings
FIG. 1 is a schematic view of an overall structure of an ADS-B signal-based airborne equipment positioning device according to the present invention;
FIG. 2 is a schematic diagram of a positioning system according to the present invention;
FIG. 3 is a schematic structural view of the remote driving apparatus according to the present invention;
fig. 4 is a schematic structural diagram of the accommodating chamber of the present invention.
In the figure: the system comprises a 1-airborne box, a 2-positioning system, a 21-power supply module, a 22-GNSS module, a 23-data processing module, a 24-ADS-B signal module, a 25-sensor module, a 26-communication module, a 27-control terminal, a 3-flight device, a 4-far driving device, a 41-storage battery, a 42-detector, a 43-ultrasonic driving device, a 44-control panel, a 45-rotating device, a 46-reflecting plate, a 5-near trend device, a 51-trend light, a 52-translation plate and a 53-containing cavity.
Detailed Description
The present invention will be further illustrated with reference to the accompanying drawings and specific embodiments, which are to be understood as merely illustrative of the invention and not as limiting the scope of the invention. It should be noted that the terms "front," "back," "left," "right," "upper" and "lower" used in the following description refer to directions in the drawings, and the terms "inner" and "outer" refer to directions toward and away from, respectively, the geometric center of a particular component.
Referring to fig. 1-4, an ADS-B signal-based airborne equipment positioning device comprises an airborne box 1, a positioning system 2 is welded inside the airborne box 1, and a flying device 3 is connected to the airborne box 1;
the flying device 3 comprises a far driving device 4 and a near driving device 5, the near driving device 5 is positioned at one side of the far driving device 4, the far driving device 4 comprises a storage battery 41, a detector 42, an ultrasonic driving device 43, a control panel 44, a rotating device 45 and a reflecting plate 46, the storage battery 41 is respectively and electrically connected with the detector 42, the ultrasonic driving device 43, the control panel 44 and the rotating device 45, the detector 42, the ultrasonic driving device 43 and the rotating device 45 are respectively and electrically connected with the control panel 44, the storage battery 41, the detector 42, the ultrasonic driving device 43 and the control panel 44 are positioned at the inner side of the rotating device 45, the reflecting plate 46 is installed on the rotating device 45, the rotating device 45 drives the reflecting plate 46 to do circular motion, the storage battery 41 is for example a storage battery with the model of XKD-150W, the detector 42 is for example a detector with the model of RX-40QZ, for example, the control panel 44 is a control panel of FR-4 type manufactured by shenzhen china electronics limited company, and the rotating device 45 includes a circular plate, a support plate and a motor, the motor is fixedly mounted on the airborne box 1, the support plate is fixedly mounted at the output end of the motor, the circular plate is fixedly mounted at the outer side of the support plate, the motor rotates to drive the circular plate to rotate, so as to drive the reflection plate to do circular motion, and the support plate and the circular plate are similar to a steering wheel on an automobile.
The approach device 5 comprises an approach light 51, a translation plate 52 and an accommodating cavity 53, wherein the translation plate 52 is arranged on the side surface of the accommodating cavity 53, the other side of the translation plate 52 is positioned in the accommodating cavity 53, the approach light 51 is arranged in the accommodating cavity 53, the light of the approach light 51 penetrates through the accommodating cavity 53, and the accommodating cavity 53 is Z-shaped, for example.
The reflecting plates 46 are provided in two or more numbers, and the reflecting plates 46 are located around the rotating device 45.
The reflection angle of the ultrasonic driver 43 with respect to each of the reflection plates 46 is different.
The widths of two or more reflection plates 46 are different.
The ultrasonic driving device 43 comprises a first frequency band ultrasonic driving device, a second frequency band ultrasonic driving device and a third frequency band ultrasonic driving device, wherein the ultrasonic driving device 43 is a driving device with the model of s60, for example, manufactured by a factory of an amurless county high-energy power equipment sales center company.
The translating plate 52 is provided with filter holes.
The positioning system 2 comprises a power module 21, a GNSS module 22, a data processing module 23, an ADS-B signal module 24, a sensor module 25, a communication module 26 and a control terminal 27, wherein the power module 21 respectively provides power for the GNSS module 22, the data processing module 23, the ADS-B signal module 24, the sensor module 25 and the communication module 26, the power module 21 selects a power module with model number WRB2405MH-10W, the GNSS module 22 selects a module with model number L76X, the data processing module 23 selects a siemens data processing module with model number JRTH424D, the ADS-B signal module 24 and the sensor module 25 select a module with model number JRTH424D, and the communication module 26 selects a communication module with model number B7600C 1;
the GNSS module 22 processes the received information through the data processing module 23 and transmits the processed information to the control terminal 27; the ADS-B signal module 24 will process the received signal through the data processing module 23 and transmit the processed signal to the control terminal 27; the communication module 26 transmits the received communication information to the data processing module 23 in real time, and then transmits the processed communication information to the control terminal 27, the communication module 26 is connected with a communication base station through wireless, and the communication base station is connected with a communication satellite through wireless signals.
The control terminal 27 sends out corresponding command information, the command information is processed by the data processing module 23 and then is respectively transmitted to the GNSS module 22, the data processing module 23, the ADS-B signal module 24, the sensor module 25 and the communication module 26, the GNSS module 22, the data processing module 23, the ADS-B signal module 24, the sensor module 25 and the communication module 26 send out received signals and send the signals to satellites, base stations and the like, and the sensor module 25 (the sensor module comprises wind speed, distance, temperature, humidity and the like) transmits the received signals to the control terminal 27 after being processed by the data processing module 23.
The working principle is as follows: an airborne equipment positioning device based on ADS-B signals comprises an airborne box 1, a positioning system 2 is welded in the airborne box 1, a flying device 3 is connected on the airborne box 1, when the device works, the device can be used for aerial monitoring the ground through the positioning system 2 and can also monitor wind speed, distance, temperature, humidity and the like, the conditions of field installation, arrangement, operation, carrying, flying test and the like of the aerial flying equipment are facilitated, when the aerial flying equipment flies, a flying animal can be encountered, when the aerial flying equipment is far away, when the flying animal is detected through a detector 42, an ultrasonic wave driving device 43 sends ultrasonic waves to drive the flying animal, if the flying animal is too late to be driven, when the flying animal flies to the aerial flying equipment, the flying animal tends to light 51 to work, the flying animal is attracted, under the action of a translation plate 52, the flight animal falls into the accommodation cavity 53, and the flight animal and the aviation flight equipment are prevented from directly colliding.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents, and it is intended that the described embodiments of the invention be construed as merely a subset of the embodiments of the invention and not as a whole. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Claims (9)

1. The utility model provides an airborne equipment positioner based on ADS-B signal which characterized in that: the airborne equipment positioning device based on the ADS-B signal comprises an airborne box (1), a positioning system (2) is welded in the airborne box (1), and a flying device (3) is connected to the airborne box (1);
the flight device (3) comprises a far driving device (4) and a near driving device (5), the near driving device (5) is located on one side of the far driving device (4), the far driving device (4) comprises a storage battery (41), a detector (42), an ultrasonic driving device (43), a control panel (44), a rotating device (45) and a reflecting plate (46), the storage battery (41) is respectively electrically connected with the detector (42), the ultrasonic driving device (43), the control panel (44) and the rotating device (45), the detector (42), the ultrasonic driving device (43) and the rotating device (45) are respectively electrically connected with the control panel (44), the storage battery (41), the detector (42), the ultrasonic driving device (43) and the control panel (44) are located on the inner side of the rotating device (45), and the reflecting plate (46) is installed on the rotating device (45), the rotating device (45) drives the reflecting plate (46) to do circular motion.
2. The ADS-B signal based airborne equipment positioning device of claim 1, wherein: nearly trend device (5) including trend light (51), translation board (52), hold chamber (53), it has translation board (52) to hold chamber (53) side-mounting, translation board (52) opposite side is located hold chamber (53) in, it has trend light (51) to hold chamber (53) internally mounted, trend light (51) light runs through hold chamber (53).
3. The ADS-B signal based airborne equipment positioning device of claim 1, wherein: the reflecting plates (46) are arranged in two or more numbers, and the reflecting plates (46) are located on the periphery of the rotating device (45).
4. The ADS-B signal based airborne equipment positioning device of claim 1, wherein: the reflection angle of the ultrasonic wave repeller (43) is different relative to each reflection plate (46).
5. The ADS-B signal based airborne equipment positioning device of claim 1, wherein: the widths of two or more of the reflecting plates (46) are different.
6. The ADS-B signal based airborne equipment positioning device of claim 1, wherein: the ultrasonic driving device (43) comprises a first frequency band ultrasonic driving device, a second frequency band ultrasonic driving device and a third frequency band ultrasonic driving device.
7. The ADS-B signal based airborne equipment positioning device of claim 2, wherein: the translation plate (52) is provided with filter holes.
8. The ADS-B signal based airborne equipment positioning device of claim 1, wherein: the positioning system (2) comprises a power supply module (21), a GNSS module (22), a data processing module (23), an ADS-B signal module (24), a sensor module (25), a communication module (26) and a control terminal (27), wherein the power supply module (21) respectively provides power for the GNSS module (22), the data processing module (23), the ADS-B signal module (24), the sensor module (25) and the communication module (26);
the GNSS module (22) processes the received information through the data processing module (23) and then transmits the processed information to the control terminal (27); the ADS-B signal module (24) transmits the received signals to the control terminal (27) after being processed by the data processing module (23); the communication module (26) transmits the received communication information to the data processing module (23) in real time for processing and then transmits the processed communication information to the control terminal (27).
9. The ADS-B signal based airborne equipment positioning device of claim 8, wherein: control terminal (27) send corresponding command information and handle the back through data processing module (23) and transmit respectively for GNSS module (22), data processing module (23), ADS-B signal module (24), sensor module (25) and communication module (26), GNSS module (22), data processing module (23), ADS-B signal module (24), sensor module (25) and communication module (26) send received signal, send for the satellite, base station etc, sensor module (25) can transmit the signal of receiving for control terminal (27) after data processing module (23) is handled.
CN202110527119.4A 2021-05-14 2021-05-14 Airborne equipment positioning device based on ADS-B signal Pending CN113406679A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114509871A (en) * 2022-04-19 2022-05-17 亿慧云智能科技（深圳）股份有限公司 Multifunctional handheld low-light-level night vision device and using method thereof

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203467518U (en) * 2013-10-06 2014-03-12 邢台学院 Full-intelligent ultrasonic bird dispeller
CN104115818A (en) * 2014-08-10 2014-10-29 哈尔滨理工大学 Acousto-optic composite bird repelling system composed of vertical-axis draught fan
CN104851323A (en) * 2015-06-11 2015-08-19 张迪 Real-time monitoring system of safe rising and landing of airplane based on Beidou
CN105785360A (en) * 2014-12-17 2016-07-20 陕西大拙智能科技有限公司 Aviation safety bird repelling radar device
US9856020B1 (en) * 2016-07-27 2018-01-02 International Business Machines Corporation Drone-based mosquito amelioration based on risk analysis and pattern classifiers
CN108069026A (en) * 2016-11-18 2018-05-25 天津毅搏云山科技有限公司 A kind of new unmanned plane
CN207764625U (en) * 2018-01-08 2018-08-24 四川德科信息技术有限公司 A kind of airborne bird feelings monitoring system
CN109195865A (en) * 2016-05-28 2019-01-11 余绍炽 Insect trap
CN208818836U (en) * 2018-08-27 2019-05-03 京信通信系统（中国）有限公司 Positioning device and positioning system
CN209527639U (en) * 2019-02-19 2019-10-25 深圳市联奕实业有限公司 Mosquito killer lamp
CN110679584A (en) * 2019-10-31 2020-01-14 中国民航科学技术研究院 Automatic bird repelling device and method
CN110754463A (en) * 2019-11-29 2020-02-07 天门元淼农业产业化发展有限公司 Agricultural is with driving birds device
CN110908403A (en) * 2019-12-09 2020-03-24 国家电网有限公司 Automatic fixed-point landing device and method for electric power line patrol unmanned aerial vehicle
CN210865505U (en) * 2019-11-18 2020-06-26 韩忠强 Novel navigation alarm
CN211033051U (en) * 2019-09-29 2020-07-17 申坤 Agricultural is with having multi-functional unmanned aerial vehicle who drives bird effect
CN212845944U (en) * 2020-07-16 2021-03-30 安徽新锐激光科技有限公司 Radar system for driving birds
CN212877281U (en) * 2020-08-10 2021-04-06 本基科技(云南)有限公司 Three-dimensional multifunctional pest trapper

Patent Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203467518U (en) * 2013-10-06 2014-03-12 邢台学院 Full-intelligent ultrasonic bird dispeller
CN104115818A (en) * 2014-08-10 2014-10-29 哈尔滨理工大学 Acousto-optic composite bird repelling system composed of vertical-axis draught fan
CN105785360A (en) * 2014-12-17 2016-07-20 陕西大拙智能科技有限公司 Aviation safety bird repelling radar device
CN104851323A (en) * 2015-06-11 2015-08-19 张迪 Real-time monitoring system of safe rising and landing of airplane based on Beidou
CN109195865A (en) * 2016-05-28 2019-01-11 余绍炽 Insect trap
US9856020B1 (en) * 2016-07-27 2018-01-02 International Business Machines Corporation Drone-based mosquito amelioration based on risk analysis and pattern classifiers
CN108069026A (en) * 2016-11-18 2018-05-25 天津毅搏云山科技有限公司 A kind of new unmanned plane
CN207764625U (en) * 2018-01-08 2018-08-24 四川德科信息技术有限公司 A kind of airborne bird feelings monitoring system
CN208818836U (en) * 2018-08-27 2019-05-03 京信通信系统（中国）有限公司 Positioning device and positioning system
CN209527639U (en) * 2019-02-19 2019-10-25 深圳市联奕实业有限公司 Mosquito killer lamp
CN211033051U (en) * 2019-09-29 2020-07-17 申坤 Agricultural is with having multi-functional unmanned aerial vehicle who drives bird effect
CN110679584A (en) * 2019-10-31 2020-01-14 中国民航科学技术研究院 Automatic bird repelling device and method
CN210865505U (en) * 2019-11-18 2020-06-26 韩忠强 Novel navigation alarm
CN110754463A (en) * 2019-11-29 2020-02-07 天门元淼农业产业化发展有限公司 Agricultural is with driving birds device
CN110908403A (en) * 2019-12-09 2020-03-24 国家电网有限公司 Automatic fixed-point landing device and method for electric power line patrol unmanned aerial vehicle
CN212845944U (en) * 2020-07-16 2021-03-30 安徽新锐激光科技有限公司 Radar system for driving birds
CN212877281U (en) * 2020-08-10 2021-04-06 本基科技(云南)有限公司 Three-dimensional multifunctional pest trapper

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114509871A (en) * 2022-04-19 2022-05-17 亿慧云智能科技（深圳）股份有限公司 Multifunctional handheld low-light-level night vision device and using method thereof

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