CN214929257U - Automatic follow and tie unmanned aerial vehicle system - Google Patents
Automatic follow and tie unmanned aerial vehicle system Download PDFInfo
- Publication number
- CN214929257U CN214929257U CN202120837695.4U CN202120837695U CN214929257U CN 214929257 U CN214929257 U CN 214929257U CN 202120837695 U CN202120837695 U CN 202120837695U CN 214929257 U CN214929257 U CN 214929257U
- Authority
- CN
- China
- Prior art keywords
- vehicle
- aircraft
- unmanned aerial
- aerial vehicle
- ground
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Radio Relay Systems (AREA)
Abstract
The utility model discloses an automatic follow mooring unmanned aerial vehicle system, including ground vehicle, aircraft, take off and land platform, on-vehicle basic station, ground main control system, mooring stranded conductor equipment, mooring line. The ground vehicle is provided with a vehicle-mounted base station and a control host, the control host is connected with the aircraft through a mooring line to supply power to the aircraft, and the control host is in communication connection with the aircraft through the mooring line or a wireless communication module. Automatic follow and remove on-vehicle mooring unmanned aerial vehicle system in, aerial unmanned aerial vehicle can follow ground vehicle synchronous motion automatically to need not personnel control alright with realizing independently following, independently take off and land etc. action, and ground vehicle need not park and retrieve unmanned aerial vehicle, ground vehicle can accomplish unmanned aerial vehicle release and retrieve in driving.
Description
Technical Field
The utility model relates to an aviation technical field, in particular to automatic follow mooring unmanned aerial vehicle system.
Background
Tethered drones are a successful direction of application for drone systems, some need to work continuously and do not require environmental conditions for long range navigation, tethered drones have gained good application, for example: overhead lighting, aerial base stations, and the like. However, as an aircraft, the characteristic that a tethered unmanned aerial vehicle is inconvenient to move limits the application field of the tethered unmanned aerial vehicle, and existing tethered unmanned aerial vehicle systems are all unmovable unmanned aerial vehicles and have single functions; and some on-vehicle unmanned aerial vehicle also are simple vehicle and the simple combination of mooring unmanned aerial vehicle, do not break through essence.
SUMMERY OF THE UTILITY MODEL
The utility model aims at overcoming above-mentioned problem, provide an automatic follow and tie unmanned aerial vehicle system.
In order to achieve the purpose, the utility model discloses a method is: the utility model provides an automatic follow mooring unmanned aerial vehicle system, includes ground vehicle and aircraft ground vehicle on be provided with on-vehicle basic station and main control system, main control system through mooring line with the aircraft connect, for the aircraft power supply, main control system through mooring line or wireless communication module with aircraft communication connection.
Preferably, the ground vehicle is further provided with a mooring stranded wire device, and the mooring line is further connected with the mooring stranded wire device.
As the utility model discloses a preferred, ground control host computer inside have the electric power storage power, ground control host computer link to each other with ground vehicle, ground vehicle is the ground control host computer power supply after the start.
Preferably, the ground vehicle is further provided with a lifting platform, and the lifting platform is fixedly connected with the ground vehicle; the lifting platform is provided with an electromagnet capable of controlling the disappearance of magnetism; the aircraft lands on the take-off and landing platform, and the electromagnet adsorbs and fixes the aircraft on the take-off and landing platform; when the aircraft takes off, the electromagnet is demagnetized, and the aircraft is separated from the take-off and landing platform.
As the utility model discloses a preferred, on-vehicle basic station fix on the ground vehicle roof.
As the utility model discloses a preferred, the aircraft be unmanned helicopter, many rotor unmanned aerial vehicle, the fixed wing unmanned aerial vehicle that verts, unmanned dirigible, fixed wing unmanned aerial vehicle, one of flapping wing unmanned aerial vehicle.
Has the advantages that:
the utility model breaks through the limitation that the tethered unmanned aerial vehicle is inconvenient to move fundamentally, and enlarges the application field of the tethered unmanned aerial vehicle; the utility model discloses an automatic function is followed, has realized taking off and landing in the removal, and work in the removal does not need personnel's control operation, compares ordinary mooring unmanned aerial vehicle, can remove at will. Compare ordinary unmanned aerial vehicle and compare, more unlimited duration.
Drawings
Fig. 1 is a schematic diagram of a system standby state of the present invention;
FIG. 2 is a schematic view of the overall working state of the present invention;
fig. 3 is a schematic diagram of the internal structure of the system part of the present invention.
Detailed Description
The present invention will be further clarified by the following embodiments with reference to the attached drawings, which are implemented on the premise of the technical solution of the present invention, and it should be understood that these embodiments are only used for illustrating the present invention and are not used for limiting the scope of the present invention.
Example 1:
as shown in fig. 1 to 3, the embodiment discloses an automatic following mooring unmanned aerial vehicle system, which comprises a ground vehicle 1, an aircraft 2, a take-off and landing platform 3, an on-vehicle base station 4, a ground control host 5, mooring stranded wire equipment 6 and a mooring line 7.
The mooring stranded wire equipment 6 is also connected with a mooring line 7, and the aircraft 2 is reeled and paid out by reeling and paying out the mooring line 7; the vehicle-mounted base station 4 is fixed on the ground vehicle 1.
The vehicle-mounted base station 4 observes and acquires the speed, direction and position of the vehicle and the ground vehicle 1 in real time through sensors and antennas such as an IMU (inertial measurement Unit), a magnetic compass and a GPS (global positioning system); the vehicle-mounted base station 4 and the aircraft 2 establish a radio data link for mutual communication, and certainly, the vehicle-mounted base station 4 and the aircraft 2 can also adopt a mooring line 7 for communication; and the vehicle-mounted base station 4 sends the information of the ground vehicle 1 to the aircraft 2.
The aircraft 2 is provided with real-time observation equipment which can adopt one technology of UWB (ultra wide band) technology, RTK (real time kinematic) differential positioning technology, laser positioning technology, visual positioning technology and radar positioning technology to observe the speed, direction and position of the aircraft in real time, and the aircraft 2 keeps the relative position of the aircraft and the ground vehicle 1 in the horizontal direction overlapped all the time through the acquired real-time position information of the aircraft 2 and the ground vehicle 1; the aircraft 2 is automatically driven to move along with the ground vehicle 1. Of course, the aircraft 2 may also observe the aircraft 2 by loading optical equipment on the ground vehicle 1, and obtain the relative position between the aircraft 2 and the ground vehicle 1; the vehicle-mounted base station 4 sends information to the aircraft 2; the aircraft 2 automatically drives the following vehicle after comparing the position information.
The lifting platform 3 is fixedly connected with the ground vehicle 1; the lifting platform 3 is provided with an electromagnet capable of controlling the disappearance of magnetism; the aircraft 2 lands on the take-off and landing platform 3, and the electromagnet adsorbs and fixes the aircraft 2 on the take-off and landing platform 3; when the aircraft 2 takes off, the electromagnet is controlled to be demagnetized, and the aircraft 2 takes off after taking off.
The ground control host 5 is internally provided with an electric storage power supply, the ground control host 5 is connected with the ground vehicle 1, and the ground vehicle 1 continuously supplies power to the ground control host 5 after being started.
Example 2:
the rest of this embodiment is the same as embodiment 1, except that in this embodiment, the ground vehicle 1 may also be any one of mobile platforms such as an automobile, a ship, a large-scale low-speed fixed wing aircraft, and the like, so that the application scenario of the automatic following and mooring unmanned aerial vehicle system can be improved.
The technical means disclosed by the scheme of the utility model is not limited to the technical means disclosed by the technical means, but also comprises the technical scheme formed by the arbitrary combination of the technical characteristics. The foregoing is a detailed description of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations are also considered as the protection scope of the present invention.
Claims (6)
1. The utility model provides an automatic follow and tie unmanned aerial vehicle system which characterized in that: including ground vehicle and aircraft ground vehicle on be provided with on-vehicle basic station and main control system, main control system through the mooring line with the aircraft connect, for the aircraft power supply, main control system through mooring line or wireless communication module with the aircraft communication connection.
2. An automatic following tethered drone system as claimed in claim 1, wherein: and the ground vehicle is also provided with a mooring stranded wire device, and the mooring line is also connected with the mooring stranded wire device.
3. An automatic following tethered drone system as claimed in claim 1, wherein: the control host is internally provided with an electric storage power supply and is connected with a ground vehicle, and the ground vehicle supplies power to the control host after being started.
4. An automatic following tethered drone system as claimed in claim 1, wherein: the ground vehicle is also provided with a lifting platform which is fixedly connected with the ground vehicle; the lifting platform is provided with an electromagnet capable of controlling the disappearance of magnetism; the aircraft lands on the take-off and landing platform, and the electromagnet adsorbs and fixes the aircraft on the take-off and landing platform; when the aircraft takes off, the electromagnet is demagnetized, and the aircraft is separated from the take-off and landing platform.
5. An automatic following tethered drone system as claimed in claim 1, wherein: the vehicle-mounted base station is fixed on the roof of the ground vehicle.
6. An automatic follow-up tethered drone system according to any of claims 1 to 5, wherein: the aircraft is one of an unmanned helicopter, a multi-rotor unmanned aerial vehicle, a tilting fixed-wing unmanned aerial vehicle, an unmanned airship, a fixed-wing unmanned aerial vehicle and a flapping-wing unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120837695.4U CN214929257U (en) | 2021-04-22 | 2021-04-22 | Automatic follow and tie unmanned aerial vehicle system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120837695.4U CN214929257U (en) | 2021-04-22 | 2021-04-22 | Automatic follow and tie unmanned aerial vehicle system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214929257U true CN214929257U (en) | 2021-11-30 |
Family
ID=79044028
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120837695.4U Active CN214929257U (en) | 2021-04-22 | 2021-04-22 | Automatic follow and tie unmanned aerial vehicle system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214929257U (en) |
-
2021
- 2021-04-22 CN CN202120837695.4U patent/CN214929257U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11858631B2 (en) | Aerial launch and/or recovery for unmanned aircraft with submersible devices, and associated systems and methods | |
| US12017797B2 (en) | Systems and methods for UAV docking | |
| US20200039373A1 (en) | Systems and methods for charging an unmanned aerial vehicle with a host vehicle | |
| US20190100331A1 (en) | Unmanned aerial vehicle (uav) recharging/refuelling station | |
| CN106809402B (en) | Automatic auxiliary landing system of rotor unmanned aerial vehicle and control method thereof | |
| IL176200A (en) | Unmanned air vehicle system | |
| CN110471453A (en) | The autonomous landing plateform system of vehicle-mounted unmanned aerial vehicle | |
| JP6997067B2 (en) | How to display information and vehicles | |
| WO2022110116A1 (en) | Flight charging method and system and charging unmanned aerial vehicle | |
| CN106325300A (en) | Remote condition monitoring and controlling system of unmanned aerial vehicle based on GSM-4G communication | |
| KR102149858B1 (en) | Transport drOne system equipped with wired relay drone and its operatiOn method | |
| KR20190067601A (en) | Apparatus for monitoring and observing offshore with flight vehicle and underwater vehicle | |
| CN214929257U (en) | Automatic follow and tie unmanned aerial vehicle system | |
| CN116710360A (en) | Flight body, processor, flight control method, program, and flight assistance device | |
| CN111474959A (en) | Large-scale freight unmanned aerial vehicle remote navigation implementation method | |
| CN110588986A (en) | Airborne unmanned aerial vehicle group aerial collecting and releasing method and system | |
| CN220672061U (en) | Unmanned aerial vehicle remote control system for construction site orbit determination inspection | |
| CN217718084U (en) | Radar quick erecting and collecting system suitable for complex mountain environment | |
| CN207917163U (en) | A kind of unmanned plane based on wireless communication technique | |
| CN112572782A (en) | Wired electric helicopter | |
| CN114252846A (en) | Radar quick erecting and collecting system suitable for complex mountain environment | |
| CN117950414A (en) | Fixed wing unmanned aerial vehicle data link failure emergency recovery navigation method and device thereof | |
| CN115167516A (en) | System for placing unmanned aerial vehicle warning tripod by remote control unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |