CN215219511U - Unmanned aerial vehicle data control system - Google Patents
Unmanned aerial vehicle data control system Download PDFInfo
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- CN215219511U CN215219511U CN202120941940.6U CN202120941940U CN215219511U CN 215219511 U CN215219511 U CN 215219511U CN 202120941940 U CN202120941940 U CN 202120941940U CN 215219511 U CN215219511 U CN 215219511U
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Abstract
The utility model provides an unmanned aerial vehicle data control system, include: the system comprises a flight controller, a flight control actuating mechanism, a sensor, a data analysis board and a wireless module, wherein the flight control actuating mechanism, the sensor and the data analysis board are connected with the flight controller, and the wireless module is connected with the data analysis board. The wireless module is used for receiving and sending data, and the data analysis board is used for packaging the data transmitted by the flight controller and transmitting the data to the wireless module. The data analysis board is also used for decoupling the data received by the wireless module and transmitting the decoupled data to the flight controller. Therefore, data decoupling is realized, and the influence on the response speed of the flight control mechanism due to the phenomenon of data coupling after the data are processed by the flight controller and transmitted to the flight control mechanism is prevented.
Description
[ technical field ] A method for producing a semiconductor device
The utility model relates to an unmanned aerial vehicle's technical field especially relates to an unmanned aerial vehicle data control system.
[ background of the invention ]
As is well known, drones are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, and as drones are increasingly used in industry, many industries are increasingly using drones for the performance of advertisements or programs.
At present, data transmission between an existing unmanned aerial vehicle and remote control equipment generally adopts a wireless mode to transmit data, for example, remote control data of a three-proofing ground station is sent through a ground transmitting terminal, after the data is received by a receiving terminal at the unmanned aerial vehicle end, the received data is transmitted to a flight controller after being transparently transmitted or simply processed by a data link, and different protocols are often adopted by communication modes of load and other executing mechanisms, so that the flight controller needs to analyze different protocols for the data, and then the processed data is transmitted to a task load or an executing mechanism related to flight control, so that data coupling is easily caused, and response of the flight control mechanism or the task load of the unmanned aerial vehicle is influenced.
Accordingly, the prior art is in need of improvement and development.
[ Utility model ] content
An object of the utility model is to provide an unmanned aerial vehicle data control system for solve current unmanned aerial vehicle and easily cause data coupling and influence flight control mechanism response speed's problem.
The technical scheme of the utility model as follows: an unmanned aerial vehicle data control system comprising: the system comprises a flight controller, a flight control actuating mechanism, a sensor and a data analysis board which are connected with the flight controller, and a wireless module connected with the data analysis board;
the wireless module is used for receiving and sending data, and the data analysis board is used for packaging the data transmitted by the flight controller and transmitting the data to the wireless module; the data analysis board is also used for decoupling the data received by the wireless module and transmitting the decoupled data to the flight controller, and the data analysis board is also used for packaging the data acquired by the task load and transmitting the packaged data to the wireless module.
Preferably, the unmanned aerial vehicle data control system further comprises a task load connected with the data analysis board, and the data analysis board further transmits the analyzed data to the task load.
Preferably, the wireless module is an image and number integrated wireless transmission module.
Preferably, the sensors include accelerometers, gyroscopes, magnetic compasses, barometers, ultrasonic sensors, GPS locators.
Preferably, the flight control actuator comprises a propeller.
Preferably, the task load is one or more of a camera, a laser radar and an infrared sensor.
The beneficial effects of the utility model reside in that: compared with the prior art, the utility model discloses an increase a data analysis board between wireless module and flight controller, utilize the data analysis board to carry out the decoupling zero with the data that wireless module received and transmit for flight controller after to realize data decoupling zero, prevent to transmit after flight controller handles and influence flight control mechanism's response speed for the phenomenon that flight control mechanism exists data coupling for flight control mechanism.
[ description of the drawings ]
Fig. 1 is a schematic block diagram of the present invention.
[ detailed description ] embodiments
The present invention will be further described with reference to the accompanying drawings and embodiments.
Referring to fig. 1, an embodiment of the present invention provides an unmanned aerial vehicle data control system
This unmanned aerial vehicle data control system includes: the flight controller 2, a flight control actuator 6, a sensor 1, and a data analysis board 3 connected to the flight controller 2, and a wireless module 4 connected to the data analysis board 3. The wireless module 4 is used for receiving and transmitting data, and the data analysis board 3 is used for packaging the data transmitted by the flight controller 2 and transmitting the data to the wireless module 4. The data analysis board 3 is further configured to decouple the data received by the wireless module 4, and transmit the decoupled data to the flight controller 2.
The utility model discloses an increase a data analysis board 3 between wireless module 4 and flight controller 2, utilize data analysis board 3 to carry out the decoupling zero with the data that wireless module 4 received and transmit for flight controller 2 after, thereby realize the data decoupling zero, prevent to handle the back through flight controller 2 and transmit the phenomenon that has the data coupling for flight control mechanism 6 and influence the response speed of flight control actuating mechanism 6, improve the response speed of flight control actuating mechanism 6, thereby solve prior art's problem.
In an embodiment, the data control system of the unmanned aerial vehicle further includes a task load 5 connected to the data analysis board 3, and the data analysis board 3 further transmits the analyzed data to the task load 5. The data analysis board 3 is directly connected with the task load 5, so that the data received by the wireless module 4 are decoupled and then transmitted to the task load 5, the task load 5 executes a task, and the coupling phenomenon is prevented from influencing the response speed of the task load 5. And when the data collected by the task load 5 needs to be fed back to the ground station, the collected data is packaged by the data analysis board 3 and then transmitted to the wireless module 4, and the wireless module 4 transmits the data to the ground station.
Specifically, in the above embodiment, in order to optimize the performance of the present invention, the wireless module 4 is an integral wireless transmission module of figures. The figure and number integrated wireless transmission module 4 has a transmitting end and a receiving end, and can realize the receiving and sending of data.
Specifically, the sensors 1 comprise an accelerometer, a gyroscope, a magnetic compass, a barometer, an ultrasonic sensor, a GPS (global positioning system) positioner and the like, the sensors 1 are used for acquiring data of the unmanned aerial vehicle such as flight and the like, transmitting the data to the data analysis board 3 through the flight controller 2, packaging the data, and then sending the data to control systems such as a ground station through a wireless module, so that monitoring and the like are realized. The flight control actuator 6 includes a propeller and the like, thereby realizing flight control of the unmanned aerial vehicle. The task load 5 is one or more of a camera, a laser radar and an infrared sensor, and can be configured by a manufacturer according to requirements.
The above embodiments of the present invention are only described, and it should be noted that, for those skilled in the art, modifications can be made without departing from the inventive concept, but these all fall into the protection scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle data control system, comprising: the system comprises a flight controller, a flight control actuating mechanism, a sensor and a data analysis board which are connected with the flight controller, and a wireless module connected with the data analysis board;
the wireless module is used for receiving and sending data, and the data analysis board is used for packaging the data transmitted by the flight controller and transmitting the data to the wireless module; the data analysis board is also used for decoupling the data received by the wireless module and transmitting the decoupled data to the flight controller.
2. The unmanned aerial vehicle data control system of claim 1, further comprising a task load connected to the data parser board, wherein the data parser board further transmits parsed data to the task load, and the data parser board further packages data collected by the task load and transmits the packaged data to the wireless module.
3. The unmanned aerial vehicle data control system of claim 2, wherein the wireless module is a graphical and numerical integrated wireless transmission module.
4. The drone data control system of claim 3, wherein the sensors include accelerometers, gyroscopes, magnetic compasses, barometers, ultrasonic sensors, GPS locators.
5. The drone data control system of claim 4, wherein the flight control actuators include propellers.
6. The drone data control system of claim 5, wherein the mission load is one or more of a camera, a lidar, an infrared sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120941940.6U CN215219511U (en) | 2021-04-30 | 2021-04-30 | Unmanned aerial vehicle data control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120941940.6U CN215219511U (en) | 2021-04-30 | 2021-04-30 | Unmanned aerial vehicle data control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215219511U true CN215219511U (en) | 2021-12-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120941940.6U Expired - Fee Related CN215219511U (en) | 2021-04-30 | 2021-04-30 | Unmanned aerial vehicle data control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215219511U (en) |
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2021
- 2021-04-30 CN CN202120941940.6U patent/CN215219511U/en not_active Expired - Fee Related
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211217 |
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| CF01 | Termination of patent right due to non-payment of annual fee |