CN112666577A - Searching device of accident-losing unmanned aerial vehicle - Google Patents
Searching device of accident-losing unmanned aerial vehicle Download PDFInfo
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- CN112666577A CN112666577A CN202011329088.3A CN202011329088A CN112666577A CN 112666577 A CN112666577 A CN 112666577A CN 202011329088 A CN202011329088 A CN 202011329088A CN 112666577 A CN112666577 A CN 112666577A
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 21
- 238000004804 winding Methods 0.000 claims description 6
- 238000005516 engineering process Methods 0.000 abstract description 3
- 238000004891 communication Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
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Abstract
The invention discloses a searching device of a wreck unmanned aerial vehicle, which comprises: the beacon is fixedly connected with the unmanned aerial vehicle through a rope, and the unmanned aerial vehicle can float on the water surface when falling into the water; the satellite positioning system receiver is hermetically arranged in the beacon and is used for receiving signals of the satellite positioning system; and the radio station is hermetically arranged in the beacon and is used for sending the radio station signal to the ground end receiving equipment. The invention utilizes the GNSS positioning system and the beacon communication technology arranged on the unmanned aerial vehicle to quickly lock the unmanned aerial vehicle in trouble, thereby realizing the search of the unmanned aerial vehicle in trouble.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle positioning, in particular to a searching device of a wrecking unmanned aerial vehicle.
Background
With the rapid development of marine industry, the related technologies of maritime search and rescue are also developing towards diversification. The unmanned aerial vehicle is searched for andd rescue and is transported to the beginning, and compared with conventional ships, airplanes, helicopters and motorboats, the unmanned aerial vehicle has the advantages of good mobility, flexible control and the like. The rescue target can be quickly positioned, and people can be replaced to execute high-risk tasks under the condition of marine disaster weather or polluted environment. The unmanned aerial vehicle has small size, light weight, high safety and flexible control, can freely and vertically take off and land, roll, hover, turn and transversely fly at any angle in narrow and complicated flight environments, is widely applied to the fields of maritime search and rescue, security and protection investigation and the like, is engaged in various dangerous works, and brings numerous convenience to the life of people.
Considering uncertainty factors, once the unmanned aerial vehicle is in danger in maritime search and rescue, the unmanned aerial vehicle loses itself, and the corresponding operation activities are also affected by inconvenience, so how to quickly find the unmanned aerial vehicle with lost functions becomes a technical problem to be solved urgently in the field.
Disclosure of Invention
The invention aims to provide a searching device of a wrecking unmanned aerial vehicle, which can be used for quickly locking the wrecking unmanned aerial vehicle by utilizing a GNSS positioning system and a beacon communication technology arranged on the unmanned aerial vehicle so as to realize searching of the wrecking unmanned aerial vehicle.
In order to achieve the above object, the present invention provides a searching apparatus for a crashed unmanned aerial vehicle, the searching apparatus comprising:
the beacon is fixedly connected with the unmanned aerial vehicle through a rope, and the unmanned aerial vehicle can float on the water surface when falling into the water;
the satellite positioning system receiver is hermetically arranged in the beacon and is used for receiving signals of the satellite positioning system;
and the radio station is hermetically arranged in the beacon and is used for sending the radio station signal to the ground end receiving equipment.
Optionally, the buoyancy of water to beacon production is greater than the difference of unmanned aerial vehicle gravity and unmanned aerial vehicle buoyancy in water.
Optionally, the searching device further comprises a mounting plate, and the mounting plate is connected to the top of the rotor head of the unmanned aerial vehicle; the beacon is mounted on the mounting plate.
Optionally, the searching apparatus further comprises a beacon chamber fixedly connected to the mounting plate, and the beacon is mounted in the beacon chamber.
Optionally, the searching device further comprises a roller for winding the rope, and the roller is installed in the beacon cabin and located at the bottom of the beacon.
Optionally, the searching device further comprises a beacon bin fixedly connected to the top of the rotor head of the unmanned aerial vehicle; the beacon is mounted within the beacon bin.
Optionally, the searching device further comprises a roller for winding the rope, and the roller is fixedly connected to the unmanned aerial vehicle.
Optionally, the gyro wheel is fixed in unmanned aerial vehicle rotor head top.
Optionally, the beacon is a hemisphere, and a recess for accommodating the roller is formed in the round bottom surface of the beacon.
Optionally, the beacon is mounted on the drone fuselage.
According to the specific embodiment provided by the invention, the invention discloses the following technical effects: the searching device of the accident unmanned aerial vehicle is characterized in that a beacon with a satellite positioning system receiver and a radio station is connected to the unmanned aerial vehicle through a rope, the satellite positioning system receiver in the beacon receives signals by using the satellite positioning system when the unmanned aerial vehicle is in danger and falls into the sea, lakes, rivers and the like, the beacon floats to the water surface, and then the radio station arranged in the beacon sends the signals to ground end receiving equipment, so that the accident unmanned aerial vehicle can be accurately positioned, and then ships are dispatched to realize quick searching and salvaging of the unmanned aerial vehicle.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
Fig. 1 is a structural diagram of a searching apparatus of a crash unmanned aerial vehicle according to embodiment 1 of the present invention;
fig. 2 is a schematic view of a search device fishing of a wreck unmanned aerial vehicle according to embodiment 1 of the present invention;
fig. 3 is a schematic view of a mounting plate connected to an unmanned aerial vehicle in embodiment 1 of the present invention;
FIG. 4 is a structural view of a mounting plate in embodiment 1 of the invention;
fig. 5 is a schematic diagram of beacon bin connection in embodiment 1 of the present invention;
FIG. 6 is a schematic view of a roller connection according to embodiment 1 of the present invention;
FIG. 7 is a schematic diagram showing that the beacon did not float out in example 1 of the present invention;
fig. 8 is a structural diagram of a searching apparatus of a wreck unmanned aerial vehicle according to embodiment 2 of the present invention.
Reference numerals: 1-a beacon; 2-a rope; 3-a ship anchor; 4-mounting a plate; 5-a screw; 6-bolt; 7-beacon bin; 8-a roller; 9-rotor head.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. 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.
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in further detail below.
Example 1
As shown in fig. 1, the searching apparatus of the wreck unmanned aerial vehicle provided in this embodiment 1 includes:
the beacon 1 is fixedly connected with the unmanned aerial vehicle through a rope 2, and can separate from the unmanned aerial vehicle and float on the water surface when the unmanned aerial vehicle falls into the water;
the satellite positioning system receiver is hermetically arranged in the beacon 1 and used for receiving signals of the satellite positioning system;
and the radio station is hermetically arranged in the beacon 1 and used for sending a radio station signal to the ground end receiving equipment.
In the embodiment, the satellite positioning system adopts a GNSS positioning system, the satellite positioning system receiver adopts a receiver corresponding to the GNSS positioning system, and the GNSS positioning system (global navigation satellite system) is an air-based radio navigation positioning system which can provide all-weather 3-dimensional coordinates and speed and time information for a user at any place on the earth surface or in the near-earth space. Consequently, can accurately obtain the positional information of the unmanned aerial vehicle of the accident through this GNSS positioning system's signal, sending this positional information to ground end receiving equipment through a radio station, the concrete position of the unmanned aerial vehicle of the accident can be learnt fast to the ground end, can arrange the search and rescue ship fast like this and go to the position of unmanned aerial vehicle of the accident, utilize the ship anchor 3 to salvage the unmanned aerial vehicle of the accident ashore, as shown in fig. 2, in order to avoid losing of the information that unmanned aerial vehicle detected.
In practical application, if the buoyancy generated by water to the beacon 1 is set to be larger than the difference value between the gravity of the unmanned aerial vehicle and the buoyancy of the unmanned aerial vehicle in water. Beacon 1 can pull unmanned aerial vehicle by its buoyancy effect after the unmanned aerial vehicle accident falls into water, and beacon 1 can float in the surface of water like this, avoids the interference that the surface of water produced the signal below, and the recognition beacon position that can be more accurate. Of course, under the condition that the precision requirement is moderate, the size of the beacon 1 is also considered, the buoyancy generated by water to the beacon 1 can be set to be slightly smaller than the difference value between the gravity of the unmanned aerial vehicle and the buoyancy of the unmanned aerial vehicle in water, so that the beacon can float in water, and the position of the beacon can also be detected, as shown in fig. 2.
In specific implementation, as an optional implementation mode, the searching device may further include a mounting plate 4, as shown in fig. 3 and 4, the mounting plate 4 may be connected to the top of the unmanned aerial vehicle rotor head 9; the beacon 1 may be mounted on a mounting plate 4. Specifically, the mounting plate 4 may be connected to the top of the drone rotor head 9 by a screw 5. Beacon 1 can be more convenient float like this and break away from unmanned aerial vehicle, avoids the rope to be sheltered from by the screw.
On the basis of the above-described embodiment of the mounting plate 4, the searching apparatus further comprises a beacon chamber 7, as shown in fig. 5 and 7, the beacon chamber 7 can be fixedly connected to the mounting plate 4 by bolts 6, and then in this embodiment, the beacon 1 can be mounted in the beacon chamber 7. Therefore, the unmanned aerial vehicle is provided with a beacon 1 placing space, namely a beacon cabin 7, so that the installation and protection of the beacon 1, the rope 2 and other structures can be facilitated.
On the basis of the above-described embodiment of the beacon chamber 7, the searching device further comprises a roller 8 for winding the rope 2, as shown in fig. 6, and the roller 8 is installed in the beacon chamber 7 and is located at the bottom of the beacon 1. The setting of gyro wheel 8 can improve the speed and the smooth and easy nature that beacon 1 floats and breaks away from unmanned aerial vehicle.
Example 2
Unlike the various embodiments of example 1 described above, as shown in fig. 8, the roller 8 for winding the rope is fixedly attached directly to the mounting plate 4; of course, the wheels may be mounted directly on the drone, for example, the wheels 8 are fixed to the top of the drone rotor head 9. The mounting plate 4 and the beacon chamber 7 are not essential components and can be increased, decreased, and deformed as appropriate according to the actual situation.
In addition, the beacon cabin 7 can also be directly and fixedly connected to the top of the rotor head 9 of the unmanned aerial vehicle; the beacon 1 is mounted in a beacon chamber 7.
It should be noted that in the above embodiments, in order to make it easier to float and reduce the installation volume, the beacon 1 may be formed in a hemispherical shape, and the round bottom surface of the beacon 1 is provided with a recess for accommodating the roller 8. Thus, the installation space can be saved, and the floating speed can be improved due to the action of the recess.
In the above-mentioned embodiment, all place beacon 1 in unmanned aerial vehicle rotor head 9 tops, but not only be limited to in practical application and place in unmanned aerial vehicle rotor head 9 tops, can also install beacon 1 on positions such as unmanned aerial vehicle fuselage, fin. The specific setting position of the beacon 1 is not limited as long as the normal operation of the drone is not hindered.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.
The principles and embodiments of the present invention have been described herein using specific examples, which are provided only to help understand the method and the core concept of the present invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, the specific embodiments and the application range may be changed. In view of the above, the present disclosure should not be construed as limiting the invention.
Claims (10)
1. The utility model provides a search device of wrecking unmanned aerial vehicle which characterized in that, search device includes:
the beacon is fixedly connected with the unmanned aerial vehicle through a rope, and the unmanned aerial vehicle can float on the water surface when falling into the water;
the satellite positioning system receiver is hermetically arranged in the beacon and is used for receiving signals of the satellite positioning system;
and the radio station is hermetically arranged in the beacon and is used for sending the radio station signal to the ground end receiving equipment.
2. The apparatus of claim 1, wherein the buoyancy of the beacon by water is greater than the difference between the weight of the drone and the buoyancy of the drone in water.
3. The crash drone search device of claim 1, further comprising a mounting plate attached to the top of the drone rotor head; the beacon is mounted on the mounting plate.
4. The apparatus of claim 3, further comprising a beacon chamber fixedly attached to the mounting plate, wherein the beacon is mounted in the beacon chamber.
5. The searching device of claim 4, further comprising a roller for winding the rope, wherein the roller is installed in the beacon cabin and located at the bottom of the beacon.
6. The crash drone search device of claim 1, further comprising a beacon bin fixedly attached to the top of the drone rotor head; the beacon is mounted within the beacon bin.
7. The crash drone search device of claim 1, further comprising a roller for winding the rope, the roller being fixedly attached to the drone.
8. The crash drone search device of claim 7, wherein the rollers are fixed to the drone rotor head top.
9. The device as claimed in claim 4, 7 or 8, wherein the beacon is of a hemispherical shape, and the round bottom surface of the beacon is provided with a recess for accommodating the roller.
10. The apparatus of claim 1, wherein the beacon is mounted on the drone body.
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CN202011329088.3A CN112666577A (en) | 2020-11-24 | 2020-11-24 | Searching device of accident-losing unmanned aerial vehicle |
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CN202011329088.3A CN112666577A (en) | 2020-11-24 | 2020-11-24 | Searching device of accident-losing unmanned aerial vehicle |
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US20120098699A1 (en) * | 2010-10-22 | 2012-04-26 | Thales | Method and System for the Geolocation of a Radio Beacon in a Search and Rescue System |
US20120138741A1 (en) * | 2010-12-06 | 2012-06-07 | Airbus Operations (S.A.S.) | Method And Device For Aiding The Localization Of An Aircraft Wreck Submerged In A Sea |
CN102944883A (en) * | 2012-10-23 | 2013-02-27 | 吴杰 | Seaborne rescue localizer based on Beidou RDSS (Radio Determination Satellite Service) navigation system and system |
CN103065372A (en) * | 2012-12-07 | 2013-04-24 | 陕西千山航空电子有限责任公司 | Aviation recorder and automatic positioning method |
CN203930072U (en) * | 2014-06-30 | 2014-11-05 | 浙江省测绘科学技术研究院 | A kind of device for searching for the unmanned plane that falls |
CN105261082A (en) * | 2014-07-18 | 2016-01-20 | 帅晓华 | Black box intelligent land and sea amphibious positioning call-for-help device |
CN206327535U (en) * | 2016-07-15 | 2017-07-14 | 黄丽娜 | A kind of positioning buoy |
US20190287377A1 (en) * | 2018-03-19 | 2019-09-19 | Eliot Gillum | Water-borne beacon detection system for missing persons |
RU2018121199A3 (en) * | 2018-06-07 | 2019-12-09 |
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2020
- 2020-11-24 CN CN202011329088.3A patent/CN112666577A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120098699A1 (en) * | 2010-10-22 | 2012-04-26 | Thales | Method and System for the Geolocation of a Radio Beacon in a Search and Rescue System |
US20120138741A1 (en) * | 2010-12-06 | 2012-06-07 | Airbus Operations (S.A.S.) | Method And Device For Aiding The Localization Of An Aircraft Wreck Submerged In A Sea |
CN102944883A (en) * | 2012-10-23 | 2013-02-27 | 吴杰 | Seaborne rescue localizer based on Beidou RDSS (Radio Determination Satellite Service) navigation system and system |
CN103065372A (en) * | 2012-12-07 | 2013-04-24 | 陕西千山航空电子有限责任公司 | Aviation recorder and automatic positioning method |
CN203930072U (en) * | 2014-06-30 | 2014-11-05 | 浙江省测绘科学技术研究院 | A kind of device for searching for the unmanned plane that falls |
CN105261082A (en) * | 2014-07-18 | 2016-01-20 | 帅晓华 | Black box intelligent land and sea amphibious positioning call-for-help device |
CN206327535U (en) * | 2016-07-15 | 2017-07-14 | 黄丽娜 | A kind of positioning buoy |
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Application publication date: 20210416 |