CN106774017A - A kind of Unmanned Aerial Vehicle Data acquisition system - Google Patents
A kind of Unmanned Aerial Vehicle Data acquisition system Download PDFInfo
- Publication number
- CN106774017A CN106774017A CN201710079592.4A CN201710079592A CN106774017A CN 106774017 A CN106774017 A CN 106774017A CN 201710079592 A CN201710079592 A CN 201710079592A CN 106774017 A CN106774017 A CN 106774017A
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- aerial vehicle
- unmanned aerial
- data acquisition
- acquisition system
- vehicle data
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- 230000003993 interaction Effects 0.000 claims abstract description 14
- 238000000034 method Methods 0.000 abstract description 2
- 230000005611 electricity Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 238000007405 data analysis Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/24—Pc safety
- G05B2219/24215—Scada supervisory control and data acquisition
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a kind of Unmanned Aerial Vehicle Data acquisition system, including airborne equipment, airborne collector, adapter, main control computer and human-computer interaction module, the output end of airborne equipment is connected with the input of adapter, airborne collector is connected with adapter, adapter is connected with main control computer, and main control computer is connected with human-computer interaction module.The present invention may act as the black box of system, in the case that system goes wrong, is analyzed according to note flying quality；It is analyzed by flying quality, is conducive to showing and early warning the flying quality of system in real time；Forecast failure in advance in the process of running, reduce the probability that failure occurs.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, more particularly to a kind of Unmanned Aerial Vehicle Data acquisition system.
Background technology
At present, civilian Unmanned Aerial Vehicle Data acquisition system, is primarily present following shortcoming：
1st, the data of collection are more single, it is impossible to comprehensively analyze UAS；
2nd, do not possess the ability of data analysis and disposal；
3rd, traditional unmanned aerial vehicle detection scene needs to configure various test and sensing devices, for the various of unmanned plane
Signal is measured and analyzed, and so using inconvenience, efficiency is also low.
4th, the automation unmanned plane during flying data acquisition system for integrating various tests and measurement function is lacked above market
System.
Accordingly, it would be desirable to a kind of new Unmanned Aerial Vehicle Data acquisition system is designed, to solve above-mentioned technical problem.
The content of the invention
It is an object of the invention to provide a kind of Unmanned Aerial Vehicle Data acquisition system, by the Unmanned Aerial Vehicle Data acquisition system
Using solving existing problem.
In order to solve the above technical problems, the present invention is achieved by the following technical solutions：
The present invention is a kind of Unmanned Aerial Vehicle Data acquisition system, including airborne equipment, airborne collector, adapter, main control computer
And human-computer interaction module, the output end of the airborne equipment is connected with the input of adapter, the airborne collector be adapted to
Device is connected, and the adapter is connected with main control computer, and the main control computer is connected with human-computer interaction module.
Further, the airborne equipment includes flight controller, Power Component and Posture acquisition module, wherein power packages
Part includes electric mechanical, electrical mediation engine, and the flight attitude that the Posture acquisition module is used in real time to unmanned plane is acquired.
Further, the airborne collector obtains winged control parameter, engine parameter, the electricity of airborne equipment by adapter
Gas parameter, radio command and GPS parameters, wherein flying control parameter includes height, course, attitude, speed and steering wheel position, start
Machine parameter includes throttle parameter, and the electric parameter includes power supply state, real time power consumption, and radio command is sent out by RC receivers
Go out.
Further, FLASH memory is provided with inside the airborne collector, for storing flying quality, and is led to
Adapter is crossed to send to main control computer.
Further, the main control computer sends to human-computer interaction module after processing the flying quality for receiving.
Further, the human-computer interaction module includes display, keyboard and printer, and wherein display is used to show winged
Row data, the printer is used to print flying quality, and the keyboard is used for manually operated inquiry or control.
Further, the flying quality includes flying control parameter, engine parameter, electric parameter, radio command and GPS
Parameter.
The invention has the advantages that：
The present invention may act as the black box of system, in the case that system goes wrong, be divided according to note flying quality
Analysis；It is analyzed by flying quality, is conducive to showing and early warning the flying quality of system in real time；In running
In forecast failure in advance, reduce the probability that failure occurs.
Certainly, implement any product of the invention to it is not absolutely required to while reaching all the above advantage.
Brief description of the drawings
Technical scheme in order to illustrate more clearly the embodiments of the present invention, uses required for being described to embodiment below
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present invention, for ability
For the those of ordinary skill of domain, on the premise of not paying creative work, can also obtain other attached according to these accompanying drawings
Figure.
Fig. 1 is a kind of work block diagram of Unmanned Aerial Vehicle Data acquisition system of the invention state in the air；
Fig. 2 is a kind of work block diagram of the Unmanned Aerial Vehicle Data acquisition system of the invention in the state of ground.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is all other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Refer to shown in Fig. 1 and Fig. 2, the present invention is a kind of Unmanned Aerial Vehicle Data acquisition system, including airborne equipment, airborne adopt
Storage, adapter, main control computer, human-computer interaction module, the output end of airborne equipment are connected with the input of adapter, airborne collection
Device is connected with adapter, and adapter is connected with main control computer, and main control computer is connected with human-computer interaction module.
Wherein, airborne equipment includes flight controller, Power Component and Posture acquisition module, and wherein Power Component includes electricity
Mechanical, electrical mediation engine, the flight attitude that Posture acquisition module is used in real time to unmanned plane is acquired.
Wherein, airborne collector by adapter obtain the winged control parameter of airborne equipment, engine parameter, electric parameter,
Radio command and GPS parameters, wherein flying control parameter includes height, course, attitude, speed and steering wheel position, engine parameter
Including throttle parameter, electric parameter includes power supply state, real time power consumption, and radio command is sent by RC receivers.
Wherein, FLASH memory is provided with inside airborne collector, for storing flying quality, and is passed through adapter
Send to main control computer；Main control computer sends to human-computer interaction module after processing the flying quality for receiving；Human-computer interaction module
Including display, keyboard and printer, wherein display is used to show flying quality that printer to be used to print flying quality
Come, keyboard is used for manually operated inquiry or control；Above-mentioned flying quality includes flying control parameter, engine parameter, electric parameter, nothing
The instruction of line electricity and GPS parameters.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
Specific features, structure, material or the feature described with reference to the embodiment or example are contained at least one implementation of the invention
In example or example.In this manual, the schematic representation to above-mentioned term is not necessarily referring to identical embodiment or example.
And, the specific features of description, structure, material or feature can be in one or more any embodiments or example closing
Suitable mode is combined.
Finally it should be noted that present invention disclosed above preferred embodiment is only intended to help illustrates the present invention.It is excellent
The embodiment not all of details of detailed descriptionthe is selected, it is only described specific embodiment that the invention is not limited yet.Obviously, root
According to the content of this specification, can make many modifications and variations.This specification is chosen and specifically describes these embodiments, be in order to
Principle of the invention and practical application are preferably explained, so that skilled artisan can be best understood by and utilize
The present invention.The invention is limited only by the claims and the full scope thereof and equivalents thereof.
Claims (7)
1. a kind of Unmanned Aerial Vehicle Data acquisition system, it is characterised in that：Including airborne equipment, airborne collector, adapter, main control computer
And human-computer interaction module, the output end of the airborne equipment is connected with the input of adapter, the airborne collector be adapted to
Device is connected, and the adapter is connected with main control computer, and the main control computer is connected with human-computer interaction module.
2. a kind of Unmanned Aerial Vehicle Data acquisition system according to claim 1, it is characterised in that：The airborne equipment includes flying
Line control unit, Power Component and Posture acquisition module, wherein Power Component include electric mechanical, electrical mediation engine, and the attitude is adopted
The flight attitude that collection module is used in real time to unmanned plane is acquired.
3. a kind of Unmanned Aerial Vehicle Data acquisition system according to claim 1, it is characterised in that：The airborne collector passes through
Adapter obtains winged control parameter, engine parameter, electric parameter, radio command and the GPS parameters of airborne equipment, wherein flying control
Parameter includes height, course, attitude, speed and steering wheel position, and engine parameter includes throttle parameter, and the electric parameter includes
Power supply state, real time power consumption, radio command are sent by RC receivers.
4. a kind of Unmanned Aerial Vehicle Data acquisition system according to claim 1, it is characterised in that：Inside the airborne collector
FLASH memory is provided with, is sent to main control computer for storing flying quality, and being passed through adapter.
5. a kind of Unmanned Aerial Vehicle Data acquisition system according to claim 1, it is characterised in that：The main control computer is to receiving
Flying quality sends to human-computer interaction module after being processed.
6. a kind of Unmanned Aerial Vehicle Data acquisition system according to claim 1, it is characterised in that：The human-computer interaction module bag
Display, keyboard and printer are included, wherein display is used to show flying quality that the printer to be used to print flying quality
Out, the keyboard is used for manually operated inquiry or control.
7. a kind of Unmanned Aerial Vehicle Data acquisition system according to claim 4 to 6 any one, it is characterised in that：It is described to fly
Row data include flying control parameter, engine parameter, electric parameter, radio command and GPS parameters.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710079592.4A CN106774017A (en) | 2017-02-15 | 2017-02-15 | A kind of Unmanned Aerial Vehicle Data acquisition system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710079592.4A CN106774017A (en) | 2017-02-15 | 2017-02-15 | A kind of Unmanned Aerial Vehicle Data acquisition system |
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| Publication Number | Publication Date |
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| CN106774017A true CN106774017A (en) | 2017-05-31 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710079592.4A Pending CN106774017A (en) | 2017-02-15 | 2017-02-15 | A kind of Unmanned Aerial Vehicle Data acquisition system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108196578A (en) * | 2018-01-24 | 2018-06-22 | 广东容祺智能科技有限公司 | A kind of digitlization unmanned plane during flying Performance Test System |
| WO2019227282A1 (en) * | 2018-05-28 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Method and device for processing flight log of unmanned aerial vehicle |
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| CN103279082A (en) * | 2013-05-02 | 2013-09-04 | 广州航新航空科技股份有限公司 | Aeronautic integrated data acquisition and control system |
| CN105322998A (en) * | 2014-06-30 | 2016-02-10 | 空中客车运营有限公司 | Data collection apparatus, data collection system and method for data collection in vehicles |
| CN205582036U (en) * | 2016-02-17 | 2016-09-14 | 中国人民解放军92728部队 | Unmanned helicopter dual antenna surveys appearance direction -finding and flight data acquisition and recording system |
| CN205862559U (en) * | 2016-04-29 | 2017-01-04 | 北京军懋国兴科技股份有限公司 | On-board data synthetical collection system |
| CN206440981U (en) * | 2017-02-15 | 2017-08-25 | 合肥市融宇电子有限公司 | A kind of Unmanned Aerial Vehicle Data acquisition system |
-
2017
- 2017-02-15 CN CN201710079592.4A patent/CN106774017A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103279082A (en) * | 2013-05-02 | 2013-09-04 | 广州航新航空科技股份有限公司 | Aeronautic integrated data acquisition and control system |
| CN105322998A (en) * | 2014-06-30 | 2016-02-10 | 空中客车运营有限公司 | Data collection apparatus, data collection system and method for data collection in vehicles |
| CN205582036U (en) * | 2016-02-17 | 2016-09-14 | 中国人民解放军92728部队 | Unmanned helicopter dual antenna surveys appearance direction -finding and flight data acquisition and recording system |
| CN205862559U (en) * | 2016-04-29 | 2017-01-04 | 北京军懋国兴科技股份有限公司 | On-board data synthetical collection system |
| CN206440981U (en) * | 2017-02-15 | 2017-08-25 | 合肥市融宇电子有限公司 | A kind of Unmanned Aerial Vehicle Data acquisition system |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108196578A (en) * | 2018-01-24 | 2018-06-22 | 广东容祺智能科技有限公司 | A kind of digitlization unmanned plane during flying Performance Test System |
| WO2019227282A1 (en) * | 2018-05-28 | 2019-12-05 | 深圳市大疆创新科技有限公司 | Method and device for processing flight log of unmanned aerial vehicle |
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