CN105487518B - Four axis UAV Flight Control Systems - Google Patents
Four axis UAV Flight Control Systems Download PDFInfo
- Publication number
- CN105487518B CN105487518B CN201511027547.1A CN201511027547A CN105487518B CN 105487518 B CN105487518 B CN 105487518B CN 201511027547 A CN201511027547 A CN 201511027547A CN 105487518 B CN105487518 B CN 105487518B
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- China
- Prior art keywords
- information processing
- processing system
- control system
- unmanned plane
- flight control
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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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 36
- 230000010365 information processing Effects 0.000 claims abstract description 24
- 230000003993 interaction Effects 0.000 claims abstract description 16
- 230000005540 biological transmission Effects 0.000 claims abstract description 4
- 238000004891 communication Methods 0.000 claims description 8
- 230000005611 electricity Effects 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 230000002452 interceptive effect Effects 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000012549 training Methods 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
- G05B19/418—Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS] or computer integrated manufacturing [CIM]
- G05B19/4188—Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS] or computer integrated manufacturing [CIM] characterised by CIM planning or realisation
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/02—Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Quality & Reliability (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Selective Calling Equipment (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of four axis UAV Flight Control Systems.It includes human-computer interaction interface, operation control system and the information processing system of earth station, information processing system connect with human-computer interaction interface and being capable of mutual data transmission information, information processing system is connect by input equipment interface with operation control system, information processing system is connect with data radio station, information processing system receive after operational order will treated that data information is sent to human-computer interaction interface is shown and controlled, while unmanned plane and airborne equipment are sent to by data radio station.After above-mentioned structure, operation interface multiplicity reduces the use cost of UAV system；Airborne equipment on unmanned plane can be controlled, further reduced the cost of system；The real-time flight data received from flight control system is made full use of, On-line Fault anticipation is carried out, the reliability of UAV system is substantially improved, reduces air crash risk.
Description
Technical field
The present invention relates to a kind of control system of unmanned plane, specifically a kind of four axis UAV Flight Control Systems.
Background technique
Ground control station is the important component of UAV system, not only to undertake the real-time prison of unmanned plane during flying state
Control task, while to be also responsible for the planning management of unmanned plane during flying task；Currently, all unmanned plane enterprises are directed to respective unmanned plane
Set earth station's navigation control system of system can complete the basic training such as drone status monitoring and aerial mission planning
Energy.The generally existing following deficiency of these ground station control systems:
(1) operation interface is single, in synchronization, is merely able to control a frame unmanned plane；When an only airplane
Any problem is not had when independently working, but if there is multiple UAVs operation simultaneously, is just necessary for each airplane configuration one
Independent earth station system is covered, this undoubtedly increases the use cost of UAV system.
(2) these unmanned aerial vehicle stations only consider monitoring and controlling for unmanned plane itself, are not involved with other and airborne set
Standby control causes other than earth station system, also to configure corresponding airborne equipment controlling terminal, equally increase system
Cost.
It (3), also can basis although these unmanned aerial vehicle station systems have reception and save unmanned plane real-time flight parameter
These parameters do some simple failure anticipations, and most of accident analysis will be completed by offline manual analysis, and not had
Analysis result is directly used in the flight protection control of unmanned plane, earth station's computer hardware platforms could not be made full use of to be promoted
The performance of UAV system.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of reasonable in design, manipulation convenience, high reliablity, using at
This four low axis UAV Flight Control System.
In order to solve the above-mentioned technical problem, four axis UAV Flight Control Systems of the invention, including the man-machine of earth station
Interactive interface, operation control system and information processing system, human-computer interaction interface include parameter display panel, flight control surface
Plate, airborne equipment control panel and mission planning panel, operation control system include airborne equipment control button, flight control
And unmanned plane switching push button, information processing system have data radio station interface, input equipment interface, information processing system with it is man-machine
Interactive interface connection and can mutual data transmission information, information processing system pass through input equipment interface and operation control system
It connects and can also pass through data radio station interface and number biography from the operational order of input operation control system, information processing system
Radio station connects and can carry out between unmanned plane and airborne equipment real-time communication, and information processing system is received from input behaviour
Data information handle after the operational order of action control system and data information is sent to human-computer interaction interface by treated
It is shown and is controlled, while unmanned plane and airborne equipment are sent to by data radio station.
The flight control system that can control unmanned plane and airborne equipment is provided on the unmanned plane, the number conducts electricity
Platform and flight control system connection between unmanned plane and airborne equipment so that carry out real-time communication.
After above-mentioned structure, since operation control system has airborne equipment control button and flight control and cuts
Button is changed, human-computer interaction interface has multiple panels, therefore on the one hand makes operation interface various, if there is multiple UAVs are same
Shi Zuoye can control more unmanned planes, without configuring a set of independent earth station system for each airplane, reduce
The use cost of UAV system；Still further aspect, airborne equipment control button are integrated in operation control system, can be with
Airborne equipment on unmanned plane is controlled, does not need to be reconfigured corresponding airborne equipment controlling terminal, further reduced
The cost of system；In another aspect, the connection of the flight control system of data radio station and unmanned plane is real to carry out between unmanned plane
When communicate, thus make full use of the real-time flight data received from flight control system, carry out On-line Fault anticipation, and according to
The result of failure anticipation issues necessary protection control instruction to system for flight control computer, and UAV system can be substantially improved
Reliability reduces air crash risk.
Detailed description of the invention
Fig. 1 is the functional block diagram of four axis UAV Flight Control Systems of the invention.
Specific embodiment
With reference to the accompanying drawings and detailed description, four axis UAV Flight Control Systems of the invention are made further detailed
It describes in detail bright.
As shown, four axis UAV Flight Control Systems of the invention, human-computer interaction interface, operation including earth station
Control system and information processing system, human-computer interaction interface include parameter display panel, flight control surface plate, airborne equipment control
Panel processed and mission planning panel, operation control system include airborne equipment control button and flight control button and nobody
Machine switching push button, flight control button can control the flight control of unmanned plane, and flight switching push button unmanned plane switching push button can
Realize the control switching of different number unmanned plane, information processing system has data radio station interface, input equipment interface, at information
Reason system connect with human-computer interaction interface and can mutual data transmission information, information processing system by input equipment interface with
Operation control system connection simultaneously can also pass through several conduct electricity from the operational order of input operation control system, information processing system
Platform interface and data radio station connect and can carry out between unmanned plane and airborne equipment real-time communication, and information processing system receives
Data information handle after to the operational order from input operation control system and data information is sent to by treated
Human-computer interaction interface is shown and is controlled, while being sent to unmanned plane and airborne equipment by data radio station, in the present embodiment, nothing
Man-machine switching push button has two stations of single machine control model and two-shipper control model, has two frame unmanned planes to devote oneself to work when simultaneously
When, state of flight monitoring can be carried out simultaneously to two frame unmanned planes using two-shipper control model and aerial mission controls；System is every
Airplane is assigned with an independent communication, each communicates a corresponding unique ID number；The ID that system passes through identification communication
Message is sent to specified human-computer interaction interface, to realize the association of unmanned plane with corresponding interface.
Wherein, airborne equipment includes the equipment such as the gondola, throwing mechanism and retractable landing gear installed on unmanned plane, nothing
The flight control system that can control unmanned plane and airborne equipment is provided on man-machine, data radio station and flight control system connect
It connects to carry out real-time communication between unmanned plane and airborne equipment.
When work, pass through human-computer interaction interface (flight control surface plate, airborne equipment control panel and mission planning face
Plate) and operation control system on input equipment (airborne equipment control button and flight control button and unmanned plane switching
Button) operational order of acquisition user is sent to information processing system, and is received by data radio station and fly control calculating from unmanned plane
The real-time flight data of machine (flight control system)；Logic unit in information processing system completes data processing and control logic
After operation, flying quality is sent to parameter display panel and shows state of flight, control instruction is sent to nobody by data radio station
Machine flight control computer.
Claims (2)
1. a kind of four axis UAV Flight Control Systems, it is characterised in that: human-computer interaction interface, operation control including earth station
System and information processing system, the human-computer interaction interface include parameter display panel, flight control surface plate, airborne equipment control
Panel processed and mission planning panel, the operation control system include airborne equipment control button, flight control button and nothing
Man-machine switching push button, the information processing system have data radio station interface, input equipment interface, the information processing system with
Human-computer interaction interface connection and can mutual data transmission information, the information processing system by input equipment interface with operate
Control system connection simultaneously can also pass through several conduct electricity from the operational order of input operation control system, the information processing system
Platform interface and data radio station connect and can carry out real-time communication, the information processing system between unmanned plane and airborne equipment
It receives and data information handle after the operational order from input operation control system and will treated data information
It is sent to human-computer interaction interface to be shown and controlled, while unmanned plane and airborne equipment is sent to by data radio station, make full use of
The real-time flight data received from flight control system carries out On-line Fault anticipation, and according to the result of failure anticipation to nothing
Man-machine flight control system issues necessary protection control instruction.
2. four axis UAV Flight Control System described in accordance with the claim 1, it is characterised in that: be provided on the unmanned plane
Can control the flight control system of unmanned plane and airborne equipment, the data radio station connect with flight control system to
Real-time communication is carried out between unmanned plane and airborne equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511027547.1A CN105487518B (en) | 2015-12-31 | 2015-12-31 | Four axis UAV Flight Control Systems |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511027547.1A CN105487518B (en) | 2015-12-31 | 2015-12-31 | Four axis UAV Flight Control Systems |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105487518A CN105487518A (en) | 2016-04-13 |
| CN105487518B true CN105487518B (en) | 2019-01-15 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201511027547.1A Expired - Fee Related CN105487518B (en) | 2015-12-31 | 2015-12-31 | Four axis UAV Flight Control Systems |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106200630A (en) * | 2016-07-12 | 2016-12-07 | 上海集成电路研发中心有限公司 | A kind of ability of posture control remote manipulator system and remote control thereof |
| CN106094858A (en) * | 2016-08-26 | 2016-11-09 | 广东容祺智能科技有限公司 | A kind of full link control system of unmanned plane and control method thereof |
| CN106374941A (en) * | 2016-09-20 | 2017-02-01 | 北京韦加无人机科技股份有限公司 | Data transfer radio used for real-time connection between unmanned aerial vehicle and ground control device |
| CN106719546B (en) * | 2016-12-13 | 2022-08-30 | 上海埃威航空电子有限公司 | Aviation pesticide spraying monitoring system and method |
| CN107544529A (en) * | 2017-09-07 | 2018-01-05 | 重庆微眼航空科技有限公司 | Flight control parameter on-line tuning method and system |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103314395B (en) * | 2010-11-01 | 2016-09-28 | 寇博租赁有限公司 | The method create, connected and show three-dimensional object |
| CN104076820A (en) * | 2014-07-19 | 2014-10-01 | 国家电网公司 | Unmanned aerial vehicle electric power line polling control system and method based on three-dimensional GIS |
| CN204297111U (en) * | 2014-12-05 | 2015-04-29 | 江苏苏科畅联科技有限公司 | The comprehensive information acquisition system of unmanned vehicle |
| CN104750111B (en) * | 2015-03-09 | 2019-02-22 | 王琪杰 | A kind of unmanned plane during flying monitoring system |
| CN205388699U (en) * | 2015-12-31 | 2016-07-20 | 江苏首控制造技术有限公司 | Four -axis unmanned aerial vehicle flight control |
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| CN105487518A (en) | 2016-04-13 |
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Granted publication date: 20190115 |