CN106828956A - A kind of unmanned plane wind speed early warning protection system and method - Google Patents
A kind of unmanned plane wind speed early warning protection system and method Download PDFInfo
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- CN106828956A CN106828956A CN201710171148.5A CN201710171148A CN106828956A CN 106828956 A CN106828956 A CN 106828956A CN 201710171148 A CN201710171148 A CN 201710171148A CN 106828956 A CN106828956 A CN 106828956A
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- 238000000034 method Methods 0.000 title claims abstract description 12
- 238000005259 measurement Methods 0.000 claims abstract description 19
- 238000004321 preservation Methods 0.000 claims abstract description 18
- 238000004891 communication Methods 0.000 claims abstract description 14
- 230000003993 interaction Effects 0.000 claims abstract description 12
- 238000007689 inspection Methods 0.000 claims description 8
- 238000007726 management method Methods 0.000 claims description 7
- 238000013500 data storage Methods 0.000 claims description 3
- 230000004927 fusion Effects 0.000 claims description 3
- 230000002452 interceptive effect Effects 0.000 claims 1
- 239000000203 mixture Substances 0.000 claims 1
- 238000012544 monitoring process Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000025518 detection of mechanical stimulus involved in sensory perception of wind Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process 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
- 239000000575 pesticide Substances 0.000 description 1
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- 238000005507 spraying Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
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- Automation & Control Theory (AREA)
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Abstract
The invention discloses a kind of unmanned plane wind speed early warning protection system and method, it is related to unmanned air vehicle technique field, including unmanned plane and ground control station, the unmanned plane is provided with selftest module before flying, wind speed measurement module, wireless communication module, data memory module, flight Preservation tactics module, flight attitude control module and central control module, the ground control station is provided with human-computer interaction interface module, it is described to fly preceding selftest module, wind speed measurement module, wireless communication module, data memory module, flight Preservation tactics module is electrically connected with central control module, the flight attitude control module is electrically connected with flight Preservation tactics module, this invention, it is intelligent high, accuracy is high, improve flight safety stability.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of unmanned plane wind speed early warning protection system and method.
Background technology
With social development and the raising of scientific and technological progress, the demand that unmanned plane is used is continuously increased, such as forest department
Gloomy anti-harmful organism monitoring, pesticide spraying, forest fire protection dynamically monitor, the ground topography and geomorphology mapping of the state of land resources department or
The dynamically estimation prevention and control of the liaison in sudden geographical disaster region or disaster, marine monitoring etc., electric stringing, line data-logging,
Public safety traffic management, city management also have started to application.
The safety inspection of current UAS is less comprehensive, the option for especially checking wind-force size neither one,
When the excessive influence unmanned plane during flying of wind-force, some unnecessary losses are likely to result in, especially some maritime affairs operations, wind-force pair
The influence of unmanned plane is very big, if without a set of wind speed early warning protection system, can be impacted to unmanned plane.
If the unmanned plane obstruction warning system of Chinese Application No. " 201310480659.7 ", mainly for in-flight
Obstruction warning, does not detect, it is impossible to ensure the safe and stable operation of unmanned plane to the wind-force in flight course.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of unmanned plane wind speed early warning protection system and method, to solve
Caused above-mentioned multinomial defect in the prior art.
To achieve the above object, the present invention provides following technical scheme：A kind of unmanned plane wind speed early warning protection system, bag
Include unmanned plane and ground control station, the unmanned plane be provided with selftest module before flying, wind speed measurement module, wireless communication module,
Data memory module, flight Preservation tactics module, flight attitude control module and central control module, the ground control station set
Have a human-computer interaction interface module, it is described fly before selftest module, wind speed measurement module, wireless communication module, data memory module, fly
Row Preservation tactics module is electrically connected with central control module, the flight attitude control module and flight Preservation tactics module
It is electrically connected with, the central control module is connected with human-computer interaction interface module by wireless communication module.
Preferably, the wind speed measurement module is made up of 4 pitots, 4 pitots be separately positioned on many rotors nobody
On the spiral arm of the four direction of machine.
Preferably, the flight attitude control module includes the controlled motor for driving unmanned plane during flying attitude to change, described
Controlled motor is electrically connected with central control module.
A kind of unmanned plane wind speed early warning guard method, comprises the following steps：
(1) before unmanned plane takes off, selftest module before flying is started first, then by the human-computer interaction interface of ground control station
Module sets self-inspection wind speed scale before taking off；
(2) after unmanned plane starts, wind speed measurement module starts, and wind speed measurement module can obtain the data fusion of wind speed
Go out the size and Orientation of wind-force, related data is then sent to central control module, and line number is entered by data memory module
According to storage；
(3) central control module sends the data to the human-computer interaction interface mould of ground control station by wireless communication module
Block, carries out data storage, so as to tracing management, in the flight course of unmanned plane, if wind speed scale is more than self-inspection before taking off
Wind speed scale, central control module then starts flight Preservation tactics module, and flight Preservation tactics module starts flight attitude control
Module, is adjusted flight attitude or makes a return voyage or land.
Beneficial effect using above technical scheme is：The unmanned plane wind speed early warning protection system that the present invention is provided, passes through
Unmanned plane wind speed early warning protection system carries out safety monitoring according to flight requirement, it is to avoid wind speed is excessive and causes the unmanned plane can not to pacify
Full operation, and tracing management can be easy to, and can be adjusted flight appearance according to wind conditions in real time with record data
State, when the wind speed scale of wind speed measurement module detection is more than setting value, it is understood that there may be when dangerous, then make a return voyage or land, the nothing
Man-machine wind speed early warning guard method, intelligent high, accuracy is high, improves flight safety stability.
Brief description of the drawings
Fig. 1 is theory diagram of the invention.
Specific embodiment
The preferred embodiment that the invention will now be described in detail with reference to the accompanying drawings.
Fig. 1 shows specific embodiment of the invention：A kind of unmanned plane wind speed early warning protection system, including unmanned plane and ground
Face control station, the unmanned plane be provided with fly before selftest module, wind speed measurement module, wireless communication module, data memory module,
Flight Preservation tactics module, flight attitude control module and central control module, the ground control station are provided with man-machine interaction circle
Face mould block, it is described to fly preceding selftest module, wind speed measurement module, wireless communication module, data memory module, flight Preservation tactics mould
Block is electrically connected with central control module, and the flight attitude control module is electrically connected with flight Preservation tactics module, institute
Central control module is stated to be connected by wireless communication module with human-computer interaction interface module.
In the present embodiment, the wind speed measurement module is made up of 4 pitots, and 4 pitots are separately positioned on many rotors
On the spiral arm of the four direction of unmanned plane.
In the present embodiment, the flight attitude control module includes the controlled motor for driving unmanned plane during flying attitude to change,
The controlled motor is electrically connected with central control module.
A kind of unmanned plane wind speed early warning guard method, comprises the following steps：
(1) before unmanned plane takes off, selftest module before flying is started first, then by the human-computer interaction interface of ground control station
Module sets self-inspection wind speed scale before taking off；
(2) after unmanned plane starts, wind speed measurement module starts, and wind speed measurement module can obtain the data fusion of wind speed
Go out the size and Orientation of wind-force, related data is then sent to central control module, and line number is entered by data memory module
According to storage；
(3) central control module sends the data to the human-computer interaction interface mould of ground control station by wireless communication module
Block, carries out data storage, so as to tracing management, in the flight course of unmanned plane, if wind speed scale is more than self-inspection before taking off
Wind speed scale, central control module then starts flight Preservation tactics module, and flight Preservation tactics module starts flight attitude control
Module, is adjusted flight attitude or makes a return voyage or land.
Based on above-mentioned, the unmanned plane wind speed early warning protection system that the present invention is provided, system is protected by the early warning of unmanned plane wind speed
System carries out safety monitoring according to flight requirement, it is to avoid wind speed it is excessive and cause unmanned plane can not safety operation, and can remember
Record data, are easy to tracing management, and can be adjusted flight attitude according to wind conditions in real time, when the detection of wind speed measurement module
Wind speed scale be more than setting value when, it is understood that there may be when dangerous, then make a return voyage or land, the unmanned plane wind speed early warning guard method,
Intelligent high, accuracy is high, improves flight safety stability.
Above-described is only the preferred embodiment of the present invention, it is noted that for one of ordinary skill in the art
For, without departing from the concept of the premise of the invention, various modifications and improvements can be made, these belong to the present invention
Protection domain.
Claims (4)
1. a kind of unmanned plane wind speed early warning protection system, including unmanned plane and ground control station, it is characterised in that：The unmanned plane
Be provided with fly before selftest module, wind speed measurement module, wireless communication module, data memory module, flight Preservation tactics module, fly
Row gesture stability module and central control module, the ground control station are provided with human-computer interaction interface module, described to fly preceding self-inspection
Module, wind speed measurement module, wireless communication module, data memory module, flight Preservation tactics module are and central control module
Electric connection, the flight attitude control module and the electric connection of flight Preservation tactics module, the central control module and people
Machine interactive interface module is connected by wireless communication module.
2. unmanned plane wind speed early warning protection system according to claim 1, it is characterised in that：The wind speed measurement module by
4 pitot compositions, 4 pitots are separately positioned on the spiral arm of the four direction of multi-rotor unmanned aerial vehicle.
3. unmanned plane wind speed early warning protection system according to claim 1, it is characterised in that：The flight attitude controls mould
Block includes the controlled motor for driving unmanned plane during flying attitude to change, and the controlled motor is electrically connected with central control module.
4. a kind of unmanned plane wind speed early warning guard method as claimed in claim 1, it is characterised in that：Comprise the following steps：
(1) before unmanned plane takes off, selftest module before flying is started first, then by the human-computer interaction interface module of ground control station
Setting take off before self-inspection wind speed scale；
(2) after unmanned plane starts, wind speed measurement module starts, and the data fusion of wind speed can be obtained air-out by wind speed measurement module
The size and Orientation of power, is then sent to related data central control module, and carries out data by data memory module and deposit
Storage；
(3) central control module sends the data to the human-computer interaction interface module of ground control station by wireless communication module,
Data storage is carried out, so as to tracing management, in the flight course of unmanned plane, if wind speed scale is more than self-inspection wind speed before taking off
Grade, central control module then starts flight Preservation tactics module, and flight Preservation tactics module starts flight attitude control module,
It is adjusted flight attitude or makes a return voyage or land.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201710171148.5A CN106828956A (en) | 2017-03-21 | 2017-03-21 | A kind of unmanned plane wind speed early warning protection system and method |
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| CN201710171148.5A CN106828956A (en) | 2017-03-21 | 2017-03-21 | A kind of unmanned plane wind speed early warning protection system and method |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107153424A (en) * | 2017-07-06 | 2017-09-12 | 上海复亚通信科技有限公司 | A kind of full-automatic unmanned machine of energy anti-strong wind patrols winged system |
| CN109164827A (en) * | 2018-08-23 | 2019-01-08 | 杭州华耕土地规划设计咨询有限公司 | A kind of data collection system based on unmanned plane |
| WO2020062166A1 (en) * | 2018-09-29 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Control method of unmanned aerial vehicles and unmanned aerial vehicles |
| CN111352438A (en) * | 2020-03-11 | 2020-06-30 | 深圳市多翼创新科技有限公司 | Full-automatic control method, device and system for unmanned aerial vehicle |
| CN111976981A (en) * | 2020-08-14 | 2020-11-24 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method and device and storage medium |
| CN113433964A (en) * | 2021-07-23 | 2021-09-24 | 武汉华武合胜网络科技有限公司 | Unmanned aerial vehicle operation flight attitude intelligent regulation and control method, system and computer storage medium |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105059558A (en) * | 2015-07-16 | 2015-11-18 | 珠海云洲智能科技有限公司 | Take-off and landing system for unmanned ship-borne unmanned aerial vehicle |
| CN106101511A (en) * | 2016-08-10 | 2016-11-09 | 南京奇蛙智能科技有限公司 | A kind of full-automatic unmanned machine system |
| CN106292683A (en) * | 2016-11-10 | 2017-01-04 | 广东容祺智能科技有限公司 | A kind of unmanned plane wind resistance stability augmentation system and autocontrol method thereof |
| CN106325300A (en) * | 2016-10-21 | 2017-01-11 | 广东容祺智能科技有限公司 | Remote condition monitoring and controlling system of unmanned aerial vehicle based on GSM-4G communication |
-
2017
- 2017-03-21 CN CN201710171148.5A patent/CN106828956A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105059558A (en) * | 2015-07-16 | 2015-11-18 | 珠海云洲智能科技有限公司 | Take-off and landing system for unmanned ship-borne unmanned aerial vehicle |
| CN106101511A (en) * | 2016-08-10 | 2016-11-09 | 南京奇蛙智能科技有限公司 | A kind of full-automatic unmanned machine system |
| CN106325300A (en) * | 2016-10-21 | 2017-01-11 | 广东容祺智能科技有限公司 | Remote condition monitoring and controlling system of unmanned aerial vehicle based on GSM-4G communication |
| CN106292683A (en) * | 2016-11-10 | 2017-01-04 | 广东容祺智能科技有限公司 | A kind of unmanned plane wind resistance stability augmentation system and autocontrol method thereof |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107153424A (en) * | 2017-07-06 | 2017-09-12 | 上海复亚通信科技有限公司 | A kind of full-automatic unmanned machine of energy anti-strong wind patrols winged system |
| CN109164827A (en) * | 2018-08-23 | 2019-01-08 | 杭州华耕土地规划设计咨询有限公司 | A kind of data collection system based on unmanned plane |
| CN109164827B (en) * | 2018-08-23 | 2021-08-03 | 杭州华耕土地规划设计咨询有限公司 | Data acquisition system based on unmanned aerial vehicle |
| WO2020062166A1 (en) * | 2018-09-29 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Control method of unmanned aerial vehicles and unmanned aerial vehicles |
| CN111352438A (en) * | 2020-03-11 | 2020-06-30 | 深圳市多翼创新科技有限公司 | Full-automatic control method, device and system for unmanned aerial vehicle |
| CN111976981A (en) * | 2020-08-14 | 2020-11-24 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method and device and storage medium |
| CN113433964A (en) * | 2021-07-23 | 2021-09-24 | 武汉华武合胜网络科技有限公司 | Unmanned aerial vehicle operation flight attitude intelligent regulation and control method, system and computer storage medium |
| CN113433964B (en) * | 2021-07-23 | 2022-12-23 | 西安天茂数码科技有限公司 | Unmanned aerial vehicle operation flight attitude intelligent regulation and control method, system and computer storage medium |
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Application publication date: 20170613 |