CN112631330A - Unmanned aerial vehicle flight control system - Google Patents
Unmanned aerial vehicle flight control system Download PDFInfo
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- CN112631330A CN112631330A CN202011501947.2A CN202011501947A CN112631330A CN 112631330 A CN112631330 A CN 112631330A CN 202011501947 A CN202011501947 A CN 202011501947A CN 112631330 A CN112631330 A CN 112631330A
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title claims abstract description 21
- 238000004891 communication Methods 0.000 claims abstract description 19
- 238000012545 processing Methods 0.000 claims abstract description 19
- 238000007405 data analysis Methods 0.000 claims abstract description 15
- 230000005540 biological transmission Effects 0.000 claims abstract description 12
- 238000000034 method Methods 0.000 claims abstract description 9
- 238000004458 analytical method Methods 0.000 claims abstract description 5
- 238000012544 monitoring process Methods 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
Abstract
The invention discloses an unmanned aerial vehicle flight control system which comprises a single chip microcomputer, a data acquisition module, a data analysis module, a transmission module, a wireless communication module, a central processing module and a power supply module, wherein the single chip microcomputer is used for acquiring data; the single-chip microcomputer with data acquisition module, wireless communication module and power module connect, data acquisition module gathers unmanned aerial vehicle flight in-process data, and data acquisition back is with data feedback to data analysis module, utilizes data analysis module to handle and the analysis to the data of gathering, obtains unmanned aerial vehicle flight in-process actual conditions, data transmission to central processing module after wireless communication module will handling, central processing module control unmanned aerial vehicle's flight action, power module includes battery pack and solar cell. The invention realizes the flight control of the unmanned aerial vehicle, has simple structure and better stability, and can realize the rapid and accurate control of the unmanned aerial vehicle.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a flight control system of an unmanned aerial vehicle.
Background
With the improvement of social development and technological progress, the demand for the use of unmanned aerial vehicles is increasing, for example, forest industry departments such as forest pest monitoring, pesticide spraying, forest fire prevention dynamic monitoring, national and local topographic and geomorphic mapping of national and local resources, communication in sudden geographic disaster areas, disaster dynamic estimation, prevention and control, ocean monitoring and the like, and electric power wiring, line inspection, public security traffic management, city management and video shooting have also started to be widely applied.
In all kinds of unmanned aerial vehicles, flight control system is its core component, and flight control system reliability, stability still remain further to improve at present, especially unmanned aerial vehicle's flight control system still needs to be smart simple and practical, and among the prior art, most unmanned aerial vehicle's flight control system adopts stability relatively poor, and the structure is complicated, and operating procedure is numerous and diverse, is difficult to realize quick, accurate control to unmanned aerial vehicle.
Disclosure of Invention
The invention overcomes the defects of the prior art and provides an unmanned aerial vehicle flight control system to solve the problems in the prior art.
In order to achieve the purpose, the invention adopts the technical scheme that: an unmanned aerial vehicle flight control system comprises a single chip microcomputer, a data acquisition module, a data analysis module, a transmission module, a wireless communication module, a central processing module and a power supply module; the single-chip microcomputer with data acquisition module, wireless communication module and power module connect, data acquisition module gathers unmanned aerial vehicle flight in-process data, and data acquisition back is with data feedback to data analysis module, utilizes data analysis module to handle and the analysis to the data of gathering, obtains unmanned aerial vehicle flight in-process actual conditions, data transmission to central processing module after wireless communication module will handling, central processing module control unmanned aerial vehicle's flight action, power module includes battery pack and solar cell.
In a preferred embodiment of the present invention, the wireless communication module is 4G, 5G or WiFi.
In a preferred embodiment of the present invention, the data acquisition module includes a sensor unit and an image unit, the sensor unit acquires sensing data outside the unmanned aerial vehicle, and the image unit acquires image data outside the unmanned aerial vehicle.
In a preferred embodiment of the present invention, the sensor unit includes a speed sensor, a temperature sensor, a humidity sensor, and an altitude sensor.
In a preferred embodiment of the present invention, the image unit includes a video camera and a camera, and is used for acquiring images of the unmanned aerial vehicle during flight.
In a preferred embodiment of the present invention, the central processing module includes a decision unit and an instruction unit.
The invention solves the defects in the background technology, and has the following beneficial effects:
the unmanned aerial vehicle flight control system realizes flight control of the unmanned aerial vehicle under the matching action of the single chip microcomputer, the data acquisition module, the data analysis module, the transmission module, the wireless communication module, the central processing module and the power supply module, has a simple structure and good stability, and can realize quick and accurate control of the unmanned aerial vehicle.
Drawings
The invention is further explained below with reference to the figures and examples;
FIG. 1 is a schematic overall structure of a preferred embodiment of the present invention;
Detailed Description
The invention will now be described in further detail with reference to the accompanying drawings and examples, which are simplified schematic drawings and illustrate only the basic structure of the invention in a schematic manner, and thus show only the constituents relevant to the invention.
As shown in fig. 1, an unmanned aerial vehicle flight control system includes a single chip microcomputer, a data acquisition module, a data analysis module, a transmission module, a wireless communication module, a central processing module and a power supply module; the single-chip microcomputer with data acquisition module, wireless communication module and power module connect, data acquisition module gathers unmanned aerial vehicle flight in-process data, and data acquisition back is with data feedback to data analysis module, utilizes data analysis module to handle and the analysis to the data of gathering, obtains unmanned aerial vehicle flight in-process actual conditions, data transmission to central processing module after wireless communication module will handling, central processing module control unmanned aerial vehicle's flight action, power module includes battery pack and solar cell.
In this embodiment, after data information was gathered with the image element to the sensor unit of data acquisition module, by transmission module and wireless communication module cooperation, with data information transmission to data analysis module, carry out analysis and judgment to data information, transmit data information to central processing module again, be handled data information by central processing module, control unmanned aerial vehicle's flight action then.
Specifically, in this embodiment, the wireless communication module is 4G, 5G or WiFi.
In this embodiment, the data acquisition module includes sensor unit and image unit, the sensor unit acquires the outside sensing data of unmanned aerial vehicle, the image unit acquires the image data outside the unmanned aerial vehicle.
Further, the sensor unit includes a speed sensor, a temperature sensor, a humidity sensor, and an altitude sensor.
Specifically, the image unit comprises a video camera and a camera, and is used for acquiring images of the unmanned aerial vehicle in the flying process.
In this embodiment, the central processing module includes a decision unit and an instruction unit.
In summary, under the cooperation of the single chip microcomputer, the data acquisition module, the data analysis module, the transmission module, the wireless communication module, the central processing module and the power supply module, the flight control of the unmanned aerial vehicle is realized, the structure is simple, the stability is good, and the unmanned aerial vehicle can be controlled quickly and accurately.
In light of the foregoing description of the preferred embodiment of the present invention, it is to be understood that various changes and modifications may be made by one skilled in the art without departing from the spirit and scope of the invention. The technical scope of the present invention is not limited to the content of the specification, and must be determined according to the scope of the claims.
Claims (6)
1. An unmanned aerial vehicle flight control system is characterized by comprising a single chip microcomputer, a data acquisition module, a data analysis module, a transmission module, a wireless communication module, a central processing module and a power supply module; the single-chip microcomputer with data acquisition module, wireless communication module and power module connect, data acquisition module gathers unmanned aerial vehicle flight in-process data, and data acquisition back is with data feedback to data analysis module, utilizes data analysis module to handle and the analysis to the data of gathering, obtains unmanned aerial vehicle flight in-process actual conditions, data transmission to central processing module after wireless communication module will handling, central processing module control unmanned aerial vehicle's flight action, power module includes battery pack and solar cell.
2. The unmanned aerial vehicle flight control system of claim 1, wherein the wireless communication module is 4G, 5G or WiFi.
3. The unmanned aerial vehicle flight control system of claim 1, wherein the data acquisition module comprises a sensor unit and an image unit, the sensor unit acquires sensing data outside the unmanned aerial vehicle, and the image unit acquires image data outside the unmanned aerial vehicle.
4. The unmanned aerial vehicle flight control system of claim 3, wherein the sensor unit comprises a speed sensor, a temperature sensor, a humidity sensor and an altitude sensor.
5. The unmanned aerial vehicle flight control system of claim 3, wherein the image unit comprises a video camera and a camera for capturing images of the unmanned aerial vehicle during flight.
6. The unmanned aerial vehicle flight control system of claim 1, wherein the central processing module comprises a decision unit and an instruction unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011501947.2A CN112631330A (en) | 2020-12-18 | 2020-12-18 | Unmanned aerial vehicle flight control system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011501947.2A CN112631330A (en) | 2020-12-18 | 2020-12-18 | Unmanned aerial vehicle flight control system |
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| CN112631330A true CN112631330A (en) | 2021-04-09 |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204515535U (en) * | 2015-03-30 | 2015-07-29 | 西京学院 | A kind of SUAV (small unmanned aerial vehicle) flight control system |
| CN105929839A (en) * | 2016-05-23 | 2016-09-07 | 深圳市金鹰悦飞科技有限公司 | Unmanned aerial vehicle flight control method and control system |
| CN109656260A (en) * | 2018-12-03 | 2019-04-19 | 北京采立播科技有限公司 | A kind of unmanned plane geographic information data acquisition system |
| CN111198004A (en) * | 2020-01-06 | 2020-05-26 | 华北电力大学（保定） | Electric power inspection information acquisition system based on unmanned aerial vehicle |
| CN111427377A (en) * | 2020-04-08 | 2020-07-17 | 海南耐威科技系统技术研究院有限公司 | Special flight control system for plant protection unmanned aerial vehicle |
-
2020
- 2020-12-18 CN CN202011501947.2A patent/CN112631330A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204515535U (en) * | 2015-03-30 | 2015-07-29 | 西京学院 | A kind of SUAV (small unmanned aerial vehicle) flight control system |
| CN105929839A (en) * | 2016-05-23 | 2016-09-07 | 深圳市金鹰悦飞科技有限公司 | Unmanned aerial vehicle flight control method and control system |
| CN109656260A (en) * | 2018-12-03 | 2019-04-19 | 北京采立播科技有限公司 | A kind of unmanned plane geographic information data acquisition system |
| CN111198004A (en) * | 2020-01-06 | 2020-05-26 | 华北电力大学（保定） | Electric power inspection information acquisition system based on unmanned aerial vehicle |
| CN111427377A (en) * | 2020-04-08 | 2020-07-17 | 海南耐威科技系统技术研究院有限公司 | Special flight control system for plant protection unmanned aerial vehicle |
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Application publication date: 20210409 |
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