CN105487518A - Four-axis unmanned-aerial-vehicle flight control system - Google Patents
Four-axis unmanned-aerial-vehicle flight control system Download PDFInfo
- Publication number
- CN105487518A CN105487518A CN201511027547.1A CN201511027547A CN105487518A CN 105487518 A CN105487518 A CN 105487518A CN 201511027547 A CN201511027547 A CN 201511027547A CN 105487518 A CN105487518 A CN 105487518A
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- control system
- unmanned plane
- interface
- flight control
- airborne equipment
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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 30
- 230000003993 interaction Effects 0.000 claims abstract description 18
- 238000004891 communication Methods 0.000 claims description 10
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 3
- 230000010365 information processing Effects 0.000 abstract 4
- 238000004458 analytical method Methods 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000012545 processing 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)
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Abstract
The invention discloses a four-axis unmanned-aerial-vehicle flight control system, comprising a man-machine interaction interface of a ground station, an operation control system and an information processing system. The information processing system and the man-machine interaction interface are connected and can transmit data information to each other. The information processing system is connected with the operation control system via an input device interface and is connected with a data transfer radio. After receiving an operation command, the information processing system sends processed data information to the man-machine interaction interface for the purpose of display and control and meanwhile to a unmanned aerial vehicle and a piece of airborne equipment via the data transfer radio. By adopting the above structure, the operation interface is varied and the use cost of the unmanned aerial vehicle system is reduced. The airborne equipment on the unmanned aerial vehicle is under control, further reducing the system cost. The real-time fight data which is received from the flight control system is made full use of to conduct on-line fault prediction, thereby greatly improving the reliability of the unmanned aerial vehicle system and reducing the risk of air crash.
Description
Technical field
The present invention relates to a kind of control system of unmanned plane, specifically a kind of four axle UAV Flight Control System.
Background technology
Ground control station is the important component part of UAS, not only will bear the real-time monitor task of unmanned plane during flying state, also will be responsible for the planning management of unmanned plane during flying task simultaneously; At present, all unmanned plane enterprises can complete the basic function such as unmanned plane condition monitoring and aerial mission planning for the land station's navigation control system set by respective UAS.These ground station control system ubiquities are not enough as follows:
(1) operation interface is single, at synchronization, is merely able to control a frame unmanned plane; Any problem is not had when only having an airplane independently working, if but have multiple UAVs operation simultaneously, be just necessary for a set of independently earth station system of each airplane configuration, this adds the use cost of UAS undoubtedly.
(2) monitoring and the control of unmanned plane itself is only considered at these unmanned aerial vehicle stations, does not relate to the control of other airborne equipments, causes except earth station system, also will configure corresponding airborne equipment control terminal, add the cost of system equally.
(3) although these unmanned aerial vehicle station systems have receive and preserve unmanned plane real-time flight parameter; also some simple fault anticipations can be done according to these parameters; major part fault analysis all will be completed by the manual analysis of off-line; and analysis result is not directly used in the flight protecting control of unmanned plane, land station's computer hardware platforms could not be made full use of to promote the performance of UAS.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of reasonable in design, manipulates the four axle UAV Flight Control System convenient, reliability is high, use cost is low.
In order to solve the problems of the technologies described above, four axle UAV Flight Control System of the present invention, comprise the human-computer interaction interface of land station, operation control system and information handling system, human-computer interaction interface comprises parameter display panel, flight control surface plate, airborne equipment control panel and mission planning panel, operation control system comprises airborne equipment control knob, flight controls and unmanned plane switching push button, information handling system has data radio station interface, input equipment interface, information handling system is connected with human-computer interaction interface and can mutual data transmission information, information handling system is connected with operation control system by input equipment interface and can from the operational order of input operation control system, information handling system to be also connected with data radio station by data radio station interface and and can to carry out real-time communication between unmanned plane and airborne equipment, after information handling system receives the operational order from input operation control system, data message is processed and the data message after process is mail to human-computer interaction interface and show and control, mail to unmanned plane and airborne equipment by data radio station simultaneously.
Described unmanned plane is provided with the flight control system that can control unmanned plane and airborne equipment, described data radio station is connected with flight control system thus and carries out real-time communication between unmanned plane and airborne equipment.
After adopting above-mentioned structure, control and switching push button because operation control system has airborne equipment control knob and flies, human-computer interaction interface has multiple panel, therefore make operation interface various on the one hand, if there is multiple UAVs operation simultaneously, can controlling multiple stage unmanned plane, without the need to being a set of independently earth station system of each airplane configuration, reducing the use cost of UAS; In addition on the one hand, airborne equipment control knob is integrated in operation control system, can also control the airborne equipment on unmanned plane, does not need to configure corresponding airborne equipment control terminal again, reduce further the cost of system; Again on the one hand; data radio station be connected with the flight control system of unmanned plane thus and carry out real-time communication between unmanned plane; make full use of the real-time flight data received from flight control system thus; carry out On-line Fault anticipation; and send necessary protecting control instruction according to the result of fault anticipation to system for flight control computer; significantly can promote the reliability of UAS, reduce air crash risk.
Accompanying drawing explanation
Fig. 1 is the theory diagram of the present invention four axle UAV Flight Control System.
Embodiment
Below in conjunction with the drawings and specific embodiments, four axle UAV Flight Control System of the present invention are described in further detail.
As shown in the figure, four axle UAV Flight Control System of the present invention, comprise the human-computer interaction interface of land station, operation control system and information handling system, human-computer interaction interface comprises parameter display panel, flight control surface plate, airborne equipment control panel and mission planning panel, operation control system comprises airborne equipment control knob and fly control knob and unmanned plane switching push button, the flight that flight control knob can control unmanned plane controls, the control that flight switching push button unmanned plane switching push button can realize varying number unmanned plane switches, information handling system has data radio station interface, input equipment interface, information handling system is connected with human-computer interaction interface and can mutual data transmission information, information handling system is connected with operation control system by input equipment interface and can from the operational order of input operation control system, information handling system to be also connected with data radio station by data radio station interface and and can to carry out real-time communication between unmanned plane and airborne equipment, after information handling system receives the operational order from input operation control system, data message is processed and the data message after process is mail to human-computer interaction interface and show and control, mail to unmanned plane and airborne equipment by data radio station simultaneously, in the present embodiment, unmanned plane switching push button has unit control model and two-shipper control model two stations, when having two frame unmanned planes to devote oneself to work simultaneously, adopt two-shipper control model can carry out state of flight monitoring and aerial mission control to two frame unmanned planes simultaneously, system is that every airplane is assigned with an independently communication, each communication corresponding unique No. ID, system by identifying that the ID of communication sends message to the human-computer interaction interface of specifying, thus realizes associating of unmanned plane and corresponding interface.
Wherein, airborne equipment comprises the equipment such as gondola, throwing mechanism and the retractable landing gear that unmanned plane is installed, unmanned plane is provided with the flight control system that can control unmanned plane and airborne equipment, data radio station is connected with flight control system thus and carries out real-time communication between unmanned plane and airborne equipment.
During work, the operational order being gathered user by the input equipment (airborne equipment control knob and fly control knob and unmanned plane switching push button) in human-computer interaction interface (flight control surface plate, airborne equipment control panel and mission planning panel) and operation control system is sent to information handling system, and receives the real-time flight data from UAV flight control (flight control system) by data radio station; After logical block in information handling system completes data processing and steering logic computing, flying quality is mail to parameter display Display panel state of flight, steering order is mail to UAV flight control by data radio station.
Claims (2)
1. an axle UAV Flight Control System, it is characterized in that: the human-computer interaction interface comprising land station, operation control system and information handling system, described human-computer interaction interface comprises parameter display panel, flight control surface plate, airborne equipment control panel and mission planning panel, described operation control system comprises airborne equipment control knob, flight control knob and unmanned plane switching push button, described information handling system has data radio station interface, input equipment interface, described information handling system is connected with human-computer interaction interface and can mutual data transmission information, described information handling system is connected with operation control system by input equipment interface and can from the operational order of input operation control system, described information handling system to be also connected with data radio station by data radio station interface and and can to carry out real-time communication between unmanned plane and airborne equipment, after described information handling system receives the operational order from input operation control system, data message is processed and the data message after process is mail to human-computer interaction interface and show and control, mail to unmanned plane and airborne equipment by data radio station simultaneously.
2. according to four axle UAV Flight Control System according to claim 1, it is characterized in that: described unmanned plane is provided with the flight control system that can control unmanned plane and airborne equipment, described data radio station is connected with flight control system thus and carries out real-time communication 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 |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511027547.1A CN105487518B (en) | 2015-12-31 | 2015-12-31 | Four axis UAV Flight Control Systems |
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| Publication Number | Publication Date |
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| CN105487518A true CN105487518A (en) | 2016-04-13 |
| CN105487518B CN105487518B (en) | 2019-01-15 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| 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 |
| CN106719546A (en) * | 2016-12-13 | 2017-05-31 | 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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| US20130238290A1 (en) * | 2010-11-01 | 2013-09-12 | Greg Angevine | Creating and linking 3d spatial objects with dynamic data, and visualizing said objects in geographic information systems |
| 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 |
| CN104750111A (en) * | 2015-03-09 | 2015-07-01 | 王琪杰 | Flying monitoring system of unmanned aerial vehicle |
| 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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2015
- 2015-12-31 CN CN201511027547.1A patent/CN105487518B/en active Active
Patent Citations (5)
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| US20130238290A1 (en) * | 2010-11-01 | 2013-09-12 | Greg Angevine | Creating and linking 3d spatial objects with dynamic data, and visualizing said objects in geographic information systems |
| 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 |
| CN104750111A (en) * | 2015-03-09 | 2015-07-01 | 王琪杰 | Flying monitoring system of unmanned aerial vehicle |
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Cited By (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 |
| CN106719546A (en) * | 2016-12-13 | 2017-05-31 | 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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| CN105487518B (en) | 2019-01-15 |
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