CN218578034U - Unmanned aerial vehicle group flight track control device - Google Patents
Unmanned aerial vehicle group flight track control device Download PDFInfo
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- CN218578034U CN218578034U CN202222804859.0U CN202222804859U CN218578034U CN 218578034 U CN218578034 U CN 218578034U CN 202222804859 U CN202222804859 U CN 202222804859U CN 218578034 U CN218578034 U CN 218578034U
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Abstract
The utility model discloses an unmanned aerial vehicle crowd flight track controlling means relates to unmanned aerial vehicle controlling means technical field, its technical essential: the ground control device comprises a large-scale carrier, a ground control device and an unmanned aerial vehicle unit, and comprises a base, wherein mounting holes are formed in mounting folded plates, the mounting holes are in threaded connection with the top of the large-scale carrier through bolts, four corners of the bottom of the base are provided with idler wheels through telescopic rods, the telescopic rods are sleeved with buffer springs, the ground control device comprises a signal input module and a first communication module, each unmanned aerial vehicle is internally provided with a second communication module in wireless communication connection with the first communication module, the second communication module is connected with a control module of the unmanned aerial vehicle, each unmanned aerial vehicle is internally provided with a distance sensor which mutually senses, and the distance sensors are connected with the control module of the unmanned aerial vehicle; the utility model discloses a ground controlling means is convenient for install on the carrier, and guarantee unmanned aerial vehicle crowd is in reasonable scope, guarantee control accuracy and sensitivity with ground controlling means's distance.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle controlling means technique and specifically relates to an unmanned aerial vehicle crowd flight track controlling means is related to.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. Because it need not personnel and drives, so can carry out more dangerous task, the extensive application in investigation search field of unmanned aerial vehicle technique.
The traditional unmanned aerial vehicle flight control system comprises a wireless remote controller, a control device and a driving device. The operating personnel sends control parameter to the controlling means who installs on unmanned aerial vehicle through wireless remote controller according to unmanned aerial vehicle's current position, and controlling means adjusts unmanned aerial vehicle's flight parameter according to control parameter control drive arrangement to realize unmanned aerial vehicle wireless control. The existing application number is CN201420687441.9 unmanned aerial vehicle flight control system, and receiver input device receives the given track command and transmits to flight control device, and positioner acquires unmanned aerial vehicle's geographical position information and sends to flight control device, and sensor device gathers unmanned aerial vehicle's flight parameter and sends to flight control device. The flight control device outputs a motor control signal to the electric motor adjusting device, controls the electric motor adjusting device to adjust the flight parameters of the unmanned aerial vehicle, and realizes the control of the position and the posture of the unmanned aerial vehicle. An operator only needs to send a fixed track command to the receiver input device, the current position of the unmanned aerial vehicle does not need to be observed in real time, and the flight control device controls the electric control motor device to adjust the flight parameters of the unmanned aerial vehicle according to the acquired information.
The unmanned aerial vehicle has the advantages of multiple purposes, strong flexibility, convenience in assembly, lower expenditure and the like, and is widely concerned and developed in the military and civil fields. Compared with a single unmanned aerial vehicle system, the cooperative application of the multi-unmanned aerial vehicle system has the advantages of stronger survivability, higher expandability, faster task completion and the like. In the existing method and device for controlling communication between cluster unmanned aerial vehicles with application number CN202010106094.6, a point-to-point communication technology applied in a computer is adopted, so that one-to-one communication can be realized in the cluster unmanned aerial vehicles, collisions in a network are avoided, and the data transfer rate of the network is improved. The base station transmits signals to the main unmanned aerial vehicle group, the main unmanned aerial vehicle serves as a signal relay, and the signals of the base station are transmitted to the slave unmanned aerial vehicle one to one, so that the reliability of signal transmission is improved, the control burden of the base station is reduced, and the cluster unmanned aerial vehicle communication system has good communication control performance.
However, the ground control devices required by the conventional unmanned aerial vehicle cluster flight trajectory control device are inconvenient to move, and when the unmanned aerial vehicle cluster is far away from the ground control devices, the control accuracy and sensitivity are influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle crowd flies track controlling means, on ground controlling means was convenient for install the carrier, guarantee unmanned aerial vehicle crowd was in reasonable within range, guarantee control accuracy and sensitivity with ground controlling means's distance.
In order to achieve the above purpose, the utility model provides a following technical scheme:
the utility model provides an unmanned aerial vehicle crowd flight orbit controlling means, includes large-scale carrier, ground controlling means and contains a plurality of unmanned aerial vehicle's unmanned aerial vehicle group, ground controlling means and unmanned aerial vehicle group wireless communication connection still include the base, ground controlling means establishes in the base top, base week side is equipped with the installation folded plate, it has the mounting hole to open on the installation folded plate, the mounting hole passes through bolt and large-scale carrier top threaded connection, base bottom four corners is equipped with the gyro wheel through the telescopic link, the telescopic link overcoat is equipped with buffer spring, ground controlling means includes signal input module and first communication module, each be equipped with the second communication module with first communication module wireless communication connection in the unmanned aerial vehicle, second communication module is connected with unmanned aerial vehicle's control module, each be equipped with the distance sensor of mutual-induction in the unmanned aerial vehicle, distance sensor is connected with unmanned aerial vehicle's control module.
By adopting the scheme, when the control device is used, the ground control device is pushed, the ground control device is moved to a large carrier (a small pickup truck or a truck) under the assistance of the roller, then the mounting folded plate is mounted above the large carrier (a threaded hole is reserved at the top of the large carrier) by using the bolt to complete fixation, the carrier can be moved to drive the ground control device to move, the distance between the unmanned aerial vehicle group and the ground control device is ensured to be within a reasonable range, and the control precision and the sensitivity are ensured; a user can input a control parameter signal through the signal input module, the control signal is transmitted to the control module of the unmanned aerial vehicle through the first communication module and the second communication module, so that the flight track of the unmanned aerial vehicle is controlled, the flight parameter of the unmanned aerial vehicle is transmitted into the ground control device through the second communication module and the first communication module, and the user can conveniently check the flight parameter of the unmanned aerial vehicle; the distance sensors in the unmanned aerial vehicles mutually sense the distance between the unmanned aerial vehicles, and when the distance is detected to be too close or too far, the flight tracks of the related unmanned aerial vehicles are adjusted through the control module, so that the normal flight of the unmanned aerial vehicle cluster is ensured.
Preferably, the ground control device comprises a shell, a display screen and an input device are arranged on the shell, the input device is connected with the signal input module, and the display screen is connected with the first communication module.
Preferably, a seat is rotatably arranged on one side of the shell through a lifting cylinder.
Preferably, casing one side is equipped with the cabinet of placing that is used for placing unmanned aerial vehicle.
Preferably, the control module of the unmanned aerial vehicle is a 51-single-chip microcomputer which can be programmed by Keil 5.
The utility model discloses following beneficial effect has:
when the control device is used, the ground control device is pushed, the ground control device is moved to a large-scale carrier (a small pickup truck or a truck) under the assistance of the roller, then the mounting folded plate is mounted above the large-scale carrier (a threaded hole is reserved at the top of the large-scale carrier) by using a bolt, the fixing is completed, the carrier can be moved to drive the ground control device to move, the distance between the unmanned aerial vehicle group and the ground control device is ensured to be within a reasonable range, and the control precision and the sensitivity are ensured; a user can input a control parameter signal through the signal input module, the control signal is transmitted to the control module of the unmanned aerial vehicle through the first communication module and the second communication module, so that the flight track of the unmanned aerial vehicle is controlled, the flight parameter of the unmanned aerial vehicle is transmitted into the ground control device through the second communication module and the first communication module, and the user can conveniently check the flight parameter of the unmanned aerial vehicle; the distance sensors in the unmanned aerial vehicles mutually sense the distance between the unmanned aerial vehicles, and when the distance is detected to be too close or too far, the flight tracks of the related unmanned aerial vehicles are adjusted through the control module, so that the normal flight of the unmanned aerial vehicle cluster is ensured.
Drawings
Fig. 1 is a schematic structural diagram of an embodiment of the present invention.
Fig. 2 is a diagram of the connection relationship of the components according to the embodiment of the present invention.
In the figure: 1. a large carrier; 2. a ground control device; 201. a housing; 202. a display screen; 203. an input device; 3. an unmanned aerial vehicle set; 301. an unmanned aerial vehicle; 4. a base; 5. mounting a folded plate; 6. a telescopic rod; 7. a roller; 8. a buffer spring; 9. a lifting cylinder; 10. a seat; 11. a placing cabinet.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments.
A track control device for group flight of Unmanned Aerial Vehicles (UAVs), as shown in figures 1-2, comprises a large-scale carrier 1, a ground control device 2 and an unmanned aerial vehicle set 3 containing a plurality of UAVs 301, wherein the ground control device 2 is in wireless communication connection with the unmanned aerial vehicle set 3, the device further comprises a base 4, the ground control device 2 is arranged above the base 4, mounting folded plates 5 are arranged on the periphery of the base 4, mounting holes are formed in the mounting folded plates 5, the mounting holes are in threaded connection with the top of the large-scale carrier 1 through bolts, rollers 7 are arranged at four corners of the bottom of the base 4 through telescopic rods 6, buffer springs 8 are sleeved outside the telescopic rods 6, the ground control device 2 comprises a signal input module and a first communication module, a second communication module in wireless communication connection with the first communication module is arranged in each UAV 301, the second communication module is connected with a control module of the UAVs 301, distance sensors which are mutually inducted are arranged in each UAV 301, and are connected with the control module of the UAVs 301;
as shown in fig. 1-2, when the control device is used, the ground control device 2 is pushed, the ground control device 2 is moved to the large-sized carrier 1 (a small pickup or a truck) with the aid of the rollers 7, then the mounting folded plate 5 is mounted above the large-sized carrier 1 (a threaded hole is reserved at the top of the large-sized carrier 1) by using bolts, and the fixation is completed, so that the ground control device 2 can be driven to move by the movement of the carrier, the distance between the unmanned aerial vehicle 301 group and the ground control device 2 is ensured to be within a reasonable range, and the control precision and sensitivity are ensured; the telescopic rod 6 and the buffer spring 8 can play a role in buffering in the ground control device 2, and when the base 4 is fixed through the bolt, tension is provided for bolt fixing, so that the bolt is less prone to falling off, and the mounting stability of the bolt is improved; a user can input a control parameter signal through the signal input module, the control signal is transmitted to the control module of the unmanned aerial vehicle 301 through the first communication module and the second communication module, so that the flight trajectory of the unmanned aerial vehicle 301 is controlled, the flight parameters of the unmanned aerial vehicle 301 are transmitted into the ground control device 2 through the second communication module and the first communication module, and the user can conveniently check the flight parameters of the unmanned aerial vehicle 301; the distance sensors in each unmanned aerial vehicle 301 mutually sense the distance between them, and when the detected distance is too close or too far, the flight trajectory of the relevant unmanned aerial vehicle 301 is adjusted through the control module, so that the normal flight of the unmanned aerial vehicle 301 group is ensured.
As shown in fig. 1-2, the ground control device 2 includes a housing 201, a display 202 and an input device 203 are disposed on the housing 201, the input device 203 is connected to a signal input module, and the display 202 is connected to a first communication module; the parameters of each unmanned aerial vehicle 301 and the output parameter signals are displayed through the display screen 202; the input device 203 is one or more of a mouse, a keyboard, or control buttons, which facilitate signal input.
As shown in fig. 1, a seat 10 is rotatably provided on one side of a housing 201 by a lifting cylinder 9; the user of being convenient for sits down, operates, improves the comfort level.
As shown in fig. 1, a cabinet 11 for placing an unmanned aerial vehicle 301 is arranged on one side of a shell 201; be convenient for place unmanned aerial vehicle 301, it is more convenient to take unmanned aerial vehicle 301.
The control module of unmanned aerial vehicle 301 is set to 51 singlechips that can use Keil5 to programme, and 51 singlechips are convenient for programme, convenient adjustment, and the degree of freedom is high.
The above are only specific embodiments of the present invention, but the technical features of the present invention are not limited thereto. Any simple changes, equivalent replacements or modifications made based on the present invention to solve the same technical problems and achieve the same technical effects are all covered in the protection scope of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle crowd flight orbit controlling means, includes large-scale carrier (1), ground controlling means (2) and contains unmanned aerial vehicle group (3) of a plurality of unmanned aerial vehicle (301), ground controlling means (2) and unmanned aerial vehicle group (3) wireless communication connection, its characterized in that: still include base (4), ground controlling means (2) are established in base (4) top, base (4) week side is equipped with installation folded plate (5), it has the mounting hole to open on installation folded plate (5), the mounting hole passes through bolt and large-scale carrier (1) top threaded connection, base (4) bottom four corners is equipped with gyro wheel (7) through telescopic link (6), telescopic link (6) overcoat is equipped with buffer spring (8), ground controlling means (2) are including signal input module and first communication module, each be equipped with the second communication module with first communication module wireless communication connection in unmanned aerial vehicle (301), the second communication module is connected with the control module of unmanned aerial vehicle (301), each be equipped with the distance sensor of mutual-induction in unmanned aerial vehicle (301), the distance sensor is connected with the control module of unmanned aerial vehicle (301).
2. The unmanned aerial vehicle group flight trajectory control device of claim 1, characterized in that: the ground control device (2) comprises a shell (201), a display screen (202) and an input device (203) are arranged on the shell (201), the input device (203) is connected with a signal input module, and the display screen (202) is connected with a first communication module.
3. The unmanned aerial vehicle group flight trajectory control device of claim 2, characterized in that: one side of the shell (201) is rotatably provided with a seat (10) through a lifting cylinder (9).
4. The apparatus of claim 3, wherein: casing (201) one side is equipped with places cabinet (11) that are used for placing unmanned aerial vehicle (301).
5. The apparatus for controlling group flight trajectories of unmanned aerial vehicles according to claim 1, wherein: the control module of the unmanned aerial vehicle (301) is set to be a 51 single chip microcomputer which can be programmed by Keil 5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222804859.0U CN218578034U (en) | 2022-10-24 | 2022-10-24 | Unmanned aerial vehicle group flight track control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222804859.0U CN218578034U (en) | 2022-10-24 | 2022-10-24 | Unmanned aerial vehicle group flight track control device |
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| Publication Number | Publication Date |
|---|---|
| CN218578034U true CN218578034U (en) | 2023-03-07 |
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| CN202222804859.0U Active CN218578034U (en) | 2022-10-24 | 2022-10-24 | Unmanned aerial vehicle group flight track control device |
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| CN (1) | CN218578034U (en) |
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- 2022-10-24 CN CN202222804859.0U patent/CN218578034U/en active Active
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