CN216596241U - Unmanned aerial vehicle airborne task system - Google Patents
Unmanned aerial vehicle airborne task system Download PDFInfo
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- CN216596241U CN216596241U CN202123351900.5U CN202123351900U CN216596241U CN 216596241 U CN216596241 U CN 216596241U CN 202123351900 U CN202123351900 U CN 202123351900U CN 216596241 U CN216596241 U CN 216596241U
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Abstract
The utility model discloses an unmanned aerial vehicle machine carries task system, unmanned aerial vehicle is connected with the power interface board electricity through expansion interface and supplies power for whole system, and power interface board is connected with TX2 support plate, wireless transceiver module and coding board electricity and is supplied power for TX2 support plate, wireless transceiver module and coding board respectively; the unmanned aerial vehicle is also electrically connected with a TX2 carrier plate through an expansion interface, the TX2 carrier plate is electrically connected with a TX2 core board, and the unmanned aerial vehicle performs data interaction with a TX2 core board through a TX2 carrier plate; the wireless transceiver module carries out data interaction with the TX2 carrier plate through a power interface board, is connected with the coding plate, converts data sent by the unmanned aerial vehicle into network flow and then transmits the network flow to the ground through the wireless transceiver module. The utility model provides an unmanned aerial vehicle machine carries task system, interference killing feature is strong, spectral efficiency is high, transmission distance is far away, anti-fading capability is strong, diffraction ability is strong, can realize real-time, high-quality wireless two-way data transmission under complicacy, non-line of sight environment.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle machine carries task system.
Background
At present, unmanned aerial vehicles are widely applied to a plurality of fields such as map surveying and mapping, electric power line patrol, security monitoring, emergency disaster relief, agricultural remote sensing and the like. The unmanned aerial vehicle is required to automatically complete set tasks under many conditions, and the unmanned aerial vehicle state needs to be monitored in real time in the process to ensure the safety and reliability of task completion. However, the existing unmanned aerial vehicle needs manual operation control during task execution and during take-off and landing, and the unmanned aerial vehicle cannot be monitored in real time or is limited by signal strength, so that the monitoring distance is insufficient, the signal transmission is delayed and the like.
SUMMERY OF THE UTILITY MODEL
Therefore, the embodiment of the utility model provides an unmanned aerial vehicle machine carries task system to the unmanned aerial vehicle who solves prior art existence needs artificial carrying on manual operation control in carrying out the task and when taking off and landing, and unable real time monitoring unmanned aerial vehicle state or receive signal strength restriction influence and lead to the monitorable distance not enough, signal transmission lag scheduling problem.
In order to achieve the above object, the embodiment of the present invention provides the following technical solutions:
an unmanned aerial vehicle airborne task system comprises a power interface board, a TX2 carrier board, a TX2 core board, a wireless transceiver module and a coding board, wherein an unmanned aerial vehicle is electrically connected with the power interface board through an expansion interface to supply power to the whole system, and the power interface board is electrically connected with the TX2 carrier board, the wireless transceiver module and the coding board to respectively supply power to the TX2 carrier board, the wireless transceiver module and the coding board; the unmanned aerial vehicle is also electrically connected with the TX2 carrier board through an expansion interface, the TX2 carrier board is electrically connected with the TX2 core board, and the unmanned aerial vehicle performs data interaction with the TX2 core board through the TX2 carrier board; the wireless transceiver module performs data interaction with the TX2 carrier plate through the power interface board, is connected with the coding plate, and converts data sent by the unmanned aerial vehicle into network flow and transmits the network flow to the ground through the wireless transceiver module.
Further, the unmanned aerial vehicle provides 24V direct current for the whole system through the expansion interface.
Furthermore, the power interface board comprises a power switching circuit, a USB to RS232 interface and a network interface, the unmanned aerial vehicle is electrically connected with the power switching circuit through an expansion interface to supply power to the whole system, and the power switching circuit is electrically connected with the TX2 carrier plate, the wireless transceiver module and the code plate to respectively supply power to the TX2 carrier plate, the wireless transceiver module and the code plate; the TX2 carrier plate is electrically connected with the USB-to-RS 232 interface and the network interface, the wireless transceiver module is electrically connected with the USB-to-RS 232 interface and the network interface, and the TX2 carrier plate transmits data sent by the unmanned aerial vehicle to the wireless transceiver module through the USB-to-RS 232 interface and the network interface.
Further, the power supply switching circuit converts 24V direct current into 1 path of 18V direct current and two paths of 12V direct current respectively to supply power to the TX2 carrier board, the wireless transceiver module and the encoding board.
Further, the power interface board and the TX2 carrier board are electrically connected to the expansion interface of the unmanned aerial vehicle through a TYPEC-to-DB 15 patch cord, respectively.
Further, an unmanned aerial vehicle extension interface is electrically connected with a USB interface and a TTL serial port interface of the TX2 carrier plate.
Furthermore, the wireless transceiver module comprises a sky end and a ground end, and the sky end is connected with the ground end through a wireless network.
The ground terminal is electrically connected with the ground terminal, the other end of the ground terminal is electrically connected with the display, and the decoder decodes the data received by the ground terminal and displays the decoded data on the display screen.
Further, the wireless transceiver module is connected with the coding board through a network interface.
The utility model discloses following beneficial effect has at least: the utility model provides an unmanned aerial vehicle machine carries task system, including power interface board, TX2 support plate, TX2 nuclear core plate, wireless transceiver module and coding board, unmanned aerial vehicle passes through expansion interface and is connected to the power interface board electricity and supplies power for entire system, and power interface board is connected with TX2 support plate, wireless transceiver module and coding board electricity and is supplied power for TX2 support plate, wireless transceiver module and coding board respectively; the unmanned aerial vehicle is also electrically connected with a TX2 carrier plate through an expansion interface, a TX2 carrier plate is electrically connected with a TX2 core board, and the unmanned aerial vehicle performs data interaction with a TX2 core board through a TX2 carrier plate; the wireless transceiver module carries out data interaction with the TX2 carrier plate through a power interface board, is connected with the coding plate, converts data sent by the unmanned aerial vehicle into network flow and then transmits the network flow to the ground through the wireless transceiver module. The utility model provides an unmanned aerial vehicle machine carries task system, interference killing feature is strong, spectral efficiency is high, transmission distance is far away, anti-fading capability is strong, diffraction ability is strong, can realize real-time, high-quality wireless two-way data transmission under complicacy, non-line of sight environment.
Drawings
In order to clearly illustrate the prior art and the present invention, the drawings needed to be used in the description of the prior art and the embodiments of the present invention will be briefly described. It should be apparent that the drawings in the following description are merely exemplary, and that other drawings may be derived from the provided drawings by those of ordinary skill in the art without inventive effort.
The structure, ratio, size and the like shown in the present specification are only used for matching with the content disclosed in the specification, so as to be known and read by people familiar with the technology, and are not used for limiting the limit conditions that the present invention can be implemented, and any modification of the structure, change of the ratio relation or adjustment of the size should still fall within the scope that the technical content disclosed in the present invention can cover without affecting the efficacy that the present invention can produce and the purpose that can be achieved.
Fig. 1 is a block diagram of an airborne task system module of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a flow chart of the operation of the embodiment of the present invention;
fig. 3 is a schematic view of a software configuration interface according to an embodiment of the present invention;
fig. 4 is a schematic diagram of a software configuration interface provided in the embodiment of the present invention;
fig. 5 is a third schematic view of a software configuration interface provided in an embodiment of the present invention.
Description of reference numerals:
1-a power interface board; 11-power switching circuit; 12-a network interface; 13-USB to 232 interface;
2-TX2 carrier board; 3-TX2 core board; 4-a wireless transceiver module sky end; 5-a coding plate; 6-wireless transceiver module ground end; 7-a decoder; 8-unmanned plane.
Detailed Description
In order to make the objects, technical solutions and advantages of the present application more apparent, the present application is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.
In the description of the present invention, "a plurality" means two or more unless otherwise specified. The terms "first," "second," "third," "fourth," and the like in the description and claims of the present invention and in the above-described drawings (if any) are intended to distinguish between the referenced items. For a scheme with a time sequence flow, the term expression does not need to be understood as describing a specific sequence or a sequence order, and for a scheme of a device structure, the term expression does not have distinction of importance degree, position relation and the like.
Furthermore, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements specifically listed, but may include other steps or elements not expressly listed that are inherent to such process, method, article, or apparatus or that are added to such process, method, article, or apparatus based on the concepts of the present invention.
Referring to fig. 1, an embodiment of the present invention provides an airborne mission system for an unmanned aerial vehicle, including a power interface board 1, a TX2 carrier board 2, a TX2 core board 3, a wireless transceiver module and a code board 5, where an unmanned aerial vehicle 8 is directly electrically connected to the power interface board 1 through an expansion interface to provide 24V dc for the whole system, and the power interface board 1 is electrically connected to the TX2 carrier board 2, the wireless transceiver module and the code board 5 to respectively supply power to the TX2 carrier board 2, the wireless transceiver module and the code board 5; the unmanned aerial vehicle 8 is also electrically connected with a USB interface and a TTL serial port interface of the TX2 carrier plate 2 through an expansion interface, the TX2 carrier plate 2 is electrically connected with the TX2 core board 3, and the unmanned aerial vehicle 8 performs data interaction with the TX2 core board 3 through the TX2 carrier plate 2, namely transmits images and data to the TX2 core board 3 and receives commands from the TX2 core board 3; the wireless transceiver module performs data interaction with the TX2 carrier plate 2 through the power interface board 1, the wireless transceiver module is connected with the encoding plate 5 through a network interface, and the encoding plate 5 converts data sent by the unmanned aerial vehicle 8 into network flow and transmits the network flow to the ground through the wireless transceiver module.
The power interface board 1 comprises a power switching circuit 11, a USB-to-RS 232 interface 13 and a network interface 12, the unmanned aerial vehicle 8 is electrically connected with the power switching circuit 11 through an expansion interface to provide 24V direct current for the whole system, the power switching circuit 11 is electrically connected with the TX2 carrier board 2, the wireless transceiver module and the coding board 5, and respectively converts the 24V direct current into 1 path of 18V direct current and two paths of 12V direct currents to respectively supply power for the TX2 carrier board 2, the wireless transceiver module and the coding board 5, and three power supplies are isolated from each other to avoid interference between the three power supplies; the TX2 carrier plate 2 is electrically connected to the USB to RS232 interface 13 and the network interface 12, the wireless transceiver module is electrically connected to the USB to RS232 interface 13 and the network interface 12, and the TX2 carrier plate 2 transmits data sent by the drone 8 to the wireless transceiver module through the USB to RS232 interface 13 and the network interface 12.
The wireless transceiver module comprises a wireless transceiver module sky end 4 and a wireless transceiver module ground end 6, and the wireless transceiver module sky end 4 is connected with the wireless transceiver module ground end 6 through a wireless network.
The embodiment of the utility model provides an unmanned aerial vehicle machine carries task system still includes decoder 7 and display, and 7 one end of decoder are connected with wireless transceiver module ground end 6 electricity, and the other end is connected with the display electricity, and decoder 7 decodes the back with wireless transceiver module ground end 6 received data and shows on the display screen and watch. Each item data in the flight of the unmanned aerial vehicle 8 is also sent to the ground end through the wireless receiving and sending module, and the real-time data of the unmanned aerial vehicle can be monitored through software installed on a ground end computer. Meanwhile, the ground end can also send the unmanned aerial vehicle control command to the sky end, and the unmanned aerial vehicle 8 is remotely controlled through the TX2 core board 3.
The embodiment of the utility model provides an unmanned aerial vehicle machine carries task system does not rely on current network infrastructure, supports arbitrary network topology, and is different with traditional wireless network, and it is a wireless broadband system that does not have center, distributing type, multihop relay, dynamic routing, survivability are strong and the expansibility is good, and inside uses own routing protocol, forwards through wireless multihop and accomplishes the wireless communication between each node. The self-organizing distributed broadband wireless network transmission system with an efficient MAC layer transmission protocol and a two-layer routing protocol. All nodes are completely equivalent, a special self-organizing network among mobile nodes can be quickly constructed without any infrastructure, instant self-adaptive communication is provided, excellent broadband performance is achieved, and real-time transmission of multimedia information such as additional video coding and audio coding is supported. The system technology has the advantages of strong anti-interference capability, high spectrum efficiency, long transmission distance, fading resistance, strong diffraction capability and the like. The wireless bidirectional data transmission function with real time and high quality can be realized in a complex and non-line-of-sight environment. The unmanned aerial vehicle information communication transmission in the complex environment is oriented, the remote measurement, remote control and high-speed real-time transmission of load data of the unmanned terminals by the ground control station and the information cooperative interaction function between the unmanned terminals are realized according to the design principles of generalization, modularization and standardization. The whole system can work continuously, stably and reliably for a long time after being tested for many times.
Please refer to fig. 2 to 5, install on unmanned aerial vehicle the utility model provides an unmanned aerial vehicle machine carries task system time, use the support to fix entire system on unmanned aerial vehicle after assembling each module of sky end earlier, use TYPEC to change DB15 patch cord and connect sky end and unmanned aerial vehicle, then be connected ground end and decoder and display, open control software and carry out the configuration of IP and other parameters, be connected sky end and ground end, it starts unmanned aerial vehicle to fly to confirm to connect after succeeding in, operating personnel just can observe unmanned aerial vehicle's real-time picture and data on the display screen.
The utility model discloses in can be according to PCB territory preparation power interface board and TX2 support plate, use the TYPEC patch cord to be connected between unmanned aerial vehicle and the system, use silica gel wire and XH1.25 connector, FPC winding displacement and HDMI adapter to press the interface on the circuit board to correspond between the inside each module of system and connect, external antenna need be connected to wireless transceiver module.
The utility model provides an unmanned aerial vehicle machine carries task system can let unmanned aerial vehicle accomplish the task of setting for automatically, reduces and controls the demand of unmanned aerial vehicle to the manpower. And can carry out real time monitoring to the unmanned aerial vehicle state at unmanned aerial vehicle operation in-process, ensure to accomplish the security and the reliability of task. The occupied space is small, the weight is light, and the normal flight of the unmanned aerial vehicle cannot be influenced. The protective performance is good, and the device can work normally in a large temperature range and in rainy and snowy weather. The receiving and transmitting frequency is adjustable, the signal transmission distance is long, the signal delay is low, the anti-interference capability is strong, the frequency spectrum efficiency is high, and the anti-fading capability and the diffraction capability are strong.
The above specific embodiments may be combined with each other, and details of the same or similar concepts or processes may not be repeated in some embodiments.
All the technical features of the above embodiments can be arbitrarily combined (as long as there is no contradiction between the combinations of the technical features), and for brevity of description, all the possible combinations of the technical features in the above embodiments are not described; these examples, which are not explicitly described, should be considered to be within the scope of the present description.
The present invention has been described in considerable detail by the general description and the specific examples given above. It should be noted that, without departing from the inventive concept, it is obvious that several variations and modifications can be made to the specific embodiments, which fall within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (9)
1. An airborne task system of an unmanned aerial vehicle is characterized by comprising a power interface board, a TX2 carrier board, a TX2 core board, a wireless transceiver module and a coding board, wherein the unmanned aerial vehicle is electrically connected with the power interface board through an expansion interface to supply power to the whole system, and the power interface board is electrically connected with the TX2 carrier board, the wireless transceiver module and the coding board to respectively supply power to the TX2 carrier board, the wireless transceiver module and the coding board; the unmanned aerial vehicle is also electrically connected with the TX2 carrier board through an expansion interface, the TX2 carrier board is electrically connected with the TX2 core board, and the unmanned aerial vehicle performs data interaction with the TX2 core board through the TX2 carrier board; the wireless transceiver module performs data interaction with the TX2 carrier plate through the power interface board, is connected with the coding plate, and converts data sent by the unmanned aerial vehicle into network flow and transmits the network flow to the ground through the wireless transceiver module.
2. The unmanned aerial vehicle airborne mission system of claim 1, wherein the unmanned aerial vehicle provides 24V dc power to the entire system via the extended interface.
3. The unmanned aerial vehicle airborne task system of claim 2, wherein the power interface board comprises a power adapter circuit, a USB to RS232 interface and a network interface, the unmanned aerial vehicle is electrically connected with the power adapter circuit through an expansion interface to supply power to the whole system, and the power adapter circuit is electrically connected with the TX2 carrier board, the wireless transceiver module and the encoder board to respectively supply power to the TX2 carrier board, the wireless transceiver module and the encoder board; the TX2 carrier plate is electrically connected with the USB-to-RS 232 interface and the network interface, the wireless transceiver module is electrically connected with the USB-to-RS 232 interface and the network interface, and the TX2 carrier plate transmits data sent by the unmanned aerial vehicle to the wireless transceiver module through the USB-to-RS 232 interface and the network interface.
4. The unmanned aerial vehicle airborne task system of claim 3, wherein the power supply switching circuit converts 24V direct current into 1 path of 18V direct current and two paths of 12V direct current respectively for supplying power to the TX2 carrier board, the wireless transceiver module and the encoder board.
5. The unmanned aerial vehicle on-board task system of claim 1, wherein the power interface board and the TX2 carrier board are electrically connected to the unmanned aerial vehicle expansion interface via a TYPEC-to-DB 15 patch cord, respectively.
6. The unmanned aerial vehicle airborne task system of claim 1, wherein unmanned aerial vehicle extension interface is electrically connected to the USB interface and TTL serial interface of the TX2 carrier board.
7. The unmanned aerial vehicle airborne task system of claim 1, wherein the wireless transceiver module comprises a sky end and a ground end, and the sky end and the ground end are connected through a wireless network.
8. The unmanned aerial vehicle airborne task system of claim 7, further comprising a decoder and a display, wherein one end of the decoder is electrically connected with the ground end, the other end of the decoder is electrically connected with the display, and the decoder decodes data received by the ground end and displays the decoded data on the display.
9. The unmanned aerial vehicle airborne task system of claim 1, wherein the wireless transceiver module is connected to the encoder board via a network interface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123351900.5U CN216596241U (en) | 2021-12-28 | 2021-12-28 | Unmanned aerial vehicle airborne task system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123351900.5U CN216596241U (en) | 2021-12-28 | 2021-12-28 | Unmanned aerial vehicle airborne task system |
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| Publication Number | Publication Date |
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| CN216596241U true CN216596241U (en) | 2022-05-24 |
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| CN202123351900.5U Active CN216596241U (en) | 2021-12-28 | 2021-12-28 | Unmanned aerial vehicle airborne task system |
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- 2021-12-28 CN CN202123351900.5U patent/CN216596241U/en active Active
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