CN111007868A - Unmanned aerial vehicle autonomous control method - Google Patents
Unmanned aerial vehicle autonomous control method Download PDFInfo
- Publication number
- CN111007868A CN111007868A CN201811169510.6A CN201811169510A CN111007868A CN 111007868 A CN111007868 A CN 111007868A CN 201811169510 A CN201811169510 A CN 201811169510A CN 111007868 A CN111007868 A CN 111007868A
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- unmanned aerial
- aerial vehicle
- height
- integrated controller
- power
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- 238000000034 method Methods 0.000 title claims abstract description 12
- 238000006073 displacement reaction Methods 0.000 claims abstract description 10
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 7
- 238000012544 monitoring process Methods 0.000 claims description 3
- 238000001514 detection method Methods 0.000 abstract description 4
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 230000010152 pollination Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
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Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention provides an unmanned aerial vehicle autonomous control method, which comprises a touch display screen, an integrated controller, an empennage direction adjusting device, a power lithium battery and a displacement correction device, wherein the touch display screen is connected with the integrated controller; the touch display screen is used for inputting the zero point, the flight path and the height of the flight path through finger touch and controlling the opening and closing of the power device and the flight speed; the integrated controller is used for detecting and correcting the direction and the height of the airplane in the flying process by adopting the airplane route adjusting device and controlling the empennage direction adjusting device and the power device to adjust the direction and the power by utilizing the integrated controller according to the detection result, so that the accuracy of the flying route of the unmanned aerial vehicle can be ensured, and the flying detection data can be obtained in time.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle autonomous control method.
Background
The unmanned aerial vehicle is a general name of the unmanned aerial vehicle, is provided with equipment such as a flight controller and a GPS device, and can operate, track and position flight equipment through a ground station or a flight hand. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, etc. Can take off perpendicularly under radio remote control, during the recovery, can land automatically, can use repeatedly, wherein plant protection unmanned aerial vehicle extensively is used for agriculture relevant tasks such as pesticide spraying, pollination, seeding.
The unmanned aerial vehicle needs to set the air route, the flying height and the flying route in advance in the using process, but when the air route of the unmanned aerial vehicle deviates from the set air route, the air route is difficult to find in time and cannot be adjusted in time.
Therefore, it is very necessary to invent an unmanned aerial vehicle autonomous control method.
Disclosure of Invention
Aiming at the defects existing in the prior art of strip steel polishing, the invention mainly aims to provide an unmanned aerial vehicle autonomous control method.
In order to solve the technical problems, the invention provides an unmanned aerial vehicle autonomous control method, which comprises a touch display screen, an integrated controller, a tail fin direction adjusting device, a power lithium battery and a displacement correction device, wherein the touch display screen is connected with the integrated controller;
the touch display screen is used for inputting the zero point, the flight path and the height of the flight path through finger touch and controlling the opening and closing of the power device and the flight speed;
the integrated controller is used for transmitting a control signal to the empennage direction adjusting device and the power device according to the zero point, the flight route and the height of the input flight route and the zero point, the flight route and the height of the input flight route;
the tail wing direction adjusting device adjusts the unmanned aerial vehicle to adjust the direction according to the direction signal input by the integrated controller, so that the aircraft flies according to the input route;
the power device is used for providing power for the unmanned aerial vehicle and adjusting the rotating speed and the flying height of the power device according to the input signal of the integrated controller;
the power lithium battery is used for providing electric energy for the touch display screen, the integrated controller, the tail fin direction adjusting device and the power device;
the displacement correction device is used for monitoring whether the position and the height of the unmanned aerial vehicle meet the air route in real time, and if the position and the height of the unmanned aerial vehicle do not meet the air route, the displacement correction device timely inputs and controls the tail fin direction adjusting device and the power device to adjust the air route of the height and the direction of the unmanned aerial vehicle if the position and the height of the unmanned aerial.
The invention adopts the airplane flight line adjusting device to detect and correct the direction and the height of the airplane in the flying process, and utilizes the integrated controller to control the tail wing direction adjusting device and the power device to adjust the direction and the power according to the detection result, thereby ensuring the accuracy of the flight line of the unmanned aerial vehicle and obtaining the flight detection data in time.
Drawings
The invention is further illustrated with reference to the following figures and examples.
Fig. 1 is a schematic framework of the present invention.
Detailed Description
The present invention is further illustrated by the following figures and examples, which include, but are not limited to, the following examples.
In order to achieve the purpose, the technical scheme adopted by the invention is as follows:
as shown in fig. 1, the autonomous control method for the unmanned aerial vehicle comprises a touch display screen, an integrated controller, a tail fin direction adjusting device, a power lithium battery and a displacement correction device;
the touch display screen is used for inputting the zero point, the flight path and the height of the flight path through finger touch and controlling the opening and closing of the power device and the flight speed;
the integrated controller is used for transmitting a control signal to the empennage direction adjusting device and the power device according to the zero point, the flight route and the height of the input flight route and the zero point, the flight route and the height of the input flight route;
the tail wing direction adjusting device adjusts the unmanned aerial vehicle to adjust the direction according to the direction signal input by the integrated controller, so that the aircraft flies according to the input route;
the power device is used for providing power for the unmanned aerial vehicle and adjusting the rotating speed and the flying height of the power device according to the input signal of the integrated controller;
the power lithium battery is used for providing electric energy for the touch display screen, the integrated controller, the tail fin direction adjusting device and the power device;
the displacement correction device is used for monitoring whether the position and the height of the unmanned aerial vehicle meet the air route in real time, and if the position and the height of the unmanned aerial vehicle do not meet the air route, the displacement correction device timely inputs and controls the tail fin direction adjusting device and the power device to adjust the air route of the height and the direction of the unmanned aerial vehicle if the position and the height of the unmanned aerial.
The technical solutions of the present invention or similar technical solutions designed by those skilled in the art based on the teachings of the technical solutions of the present invention are all within the scope of the present invention.
Claims (1)
1. An unmanned aerial vehicle autonomous control method is characterized by comprising a touch display screen, an integrated controller, an empennage direction adjusting device, a power lithium battery and a displacement correction device;
the touch display screen is used for inputting the zero point, the flight path and the height of the flight path through finger touch and controlling the opening and closing of the power device and the flight speed;
the integrated controller is used for transmitting a control signal to the empennage direction adjusting device and the power device according to the zero point, the flight route and the height of the input flight route and the zero point, the flight route and the height of the input flight route;
the tail wing direction adjusting device adjusts the unmanned aerial vehicle to adjust the direction according to the direction signal input by the integrated controller, so that the aircraft flies according to the input route;
the power device is used for providing power for the unmanned aerial vehicle and adjusting the rotating speed and the flying height of the power device according to the input signal of the integrated controller;
the power lithium battery is used for providing electric energy for the touch display screen, the integrated controller, the tail fin direction adjusting device and the power device;
the displacement correction device is used for monitoring whether the position and the height of the unmanned aerial vehicle meet the air route in real time, and if the position and the height of the unmanned aerial vehicle do not meet the air route, the displacement correction device timely inputs and controls the tail fin direction adjusting device and the power device to adjust the air route of the height and the direction of the unmanned aerial vehicle if the position and the height of the unmanned aerial.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811169510.6A CN111007868A (en) | 2018-10-08 | 2018-10-08 | Unmanned aerial vehicle autonomous control method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811169510.6A CN111007868A (en) | 2018-10-08 | 2018-10-08 | Unmanned aerial vehicle autonomous control method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111007868A true CN111007868A (en) | 2020-04-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811169510.6A Pending CN111007868A (en) | 2018-10-08 | 2018-10-08 | Unmanned aerial vehicle autonomous control method |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104750114A (en) * | 2015-04-08 | 2015-07-01 | 王宏博 | Portable unmanned aerial vehicle control box |
| CN205210692U (en) * | 2015-12-04 | 2016-05-04 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle air route planning system |
| CN105867407A (en) * | 2016-06-12 | 2016-08-17 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle as well as control device and control method thereof |
| CN106444848A (en) * | 2016-11-28 | 2017-02-22 | 广州极飞科技有限公司 | Method and device for controlling flying of unmanned aerial vehicle |
| US20170357255A1 (en) * | 2016-06-11 | 2017-12-14 | Shenzhen Hubsan Technology Co., Ltd. | Method for controlling unmanned aerial vehicle using smart device |
| CN107636552A (en) * | 2016-09-27 | 2018-01-26 | 深圳市大疆创新科技有限公司 | A kind of flight control method and device, control device |
-
2018
- 2018-10-08 CN CN201811169510.6A patent/CN111007868A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104750114A (en) * | 2015-04-08 | 2015-07-01 | 王宏博 | Portable unmanned aerial vehicle control box |
| CN205210692U (en) * | 2015-12-04 | 2016-05-04 | 中国航空工业集团公司沈阳飞机设计研究所 | Unmanned aerial vehicle air route planning system |
| US20170357255A1 (en) * | 2016-06-11 | 2017-12-14 | Shenzhen Hubsan Technology Co., Ltd. | Method for controlling unmanned aerial vehicle using smart device |
| CN105867407A (en) * | 2016-06-12 | 2016-08-17 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle as well as control device and control method thereof |
| CN107636552A (en) * | 2016-09-27 | 2018-01-26 | 深圳市大疆创新科技有限公司 | A kind of flight control method and device, control device |
| CN106444848A (en) * | 2016-11-28 | 2017-02-22 | 广州极飞科技有限公司 | Method and device for controlling flying of unmanned aerial vehicle |
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Application publication date: 20200414 |