CN108196569A - A kind of general unmanned machine earth station - Google Patents
A kind of general unmanned machine earth station Download PDFInfo
- Publication number
- CN108196569A CN108196569A CN201711384945.8A CN201711384945A CN108196569A CN 108196569 A CN108196569 A CN 108196569A CN 201711384945 A CN201711384945 A CN 201711384945A CN 108196569 A CN108196569 A CN 108196569A
- Authority
- CN
- China
- Prior art keywords
- computer
- control computer
- flight control
- mission payload
- load
- Prior art date
- 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.)
- Granted
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 78
- 230000005540 biological transmission Effects 0.000 claims abstract description 36
- 230000005611 electricity Effects 0.000 claims abstract description 35
- 239000004973 liquid crystal related substance Substances 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 5
- 238000009432 framing Methods 0.000 claims description 3
- 235000006508 Nelumbo nucifera Nutrition 0.000 claims 4
- 240000002853 Nelumbo nucifera Species 0.000 claims 4
- 235000006510 Nelumbo pentapetala Nutrition 0.000 claims 4
- 238000009434 installation Methods 0.000 claims 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000012800 visualization Methods 0.000 description 1
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
Landscapes
- 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)
- Selective Calling Equipment (AREA)
Abstract
The invention discloses a kind of general unmanned machine earth station, including ground control computer, display terminal, data chain device;The ground control computer includes flight control computer and mission payload computer, and the flying-controlled box of unmanned plane and load control software are respectively mounted on flight control computer, mission payload computer;The data chain device conducts electricity platform, data radio station including figure;Data radio station is connected by serial port switching device with flight control computer and mission payload computer;Figure conduct electricity platform include digital transmission module and figure transmission module;Digital transmission module is connected by serial port switching device with flight control computer and mission payload computer, and figure transmission module connection interchanger passes through network connection between interchanger and flight control computer and mission payload computer;Data exchange is carried out by serial ports between flight control computer and mission payload computer;Flight control computer and mission payload computer backup each other in earth station of the present invention, improve equipment dependability.
Description
Technical field
The invention belongs to unmanned planes to command control field, more particularly to a kind of Portable unmanned machine earth station.
Background technology
Ground control's control station is the important component of UAV system, mainly by computer, display terminal, data
The equipment such as chain, load beep box form.At present, there are mainly three types of forms at unmanned aerial vehicle station:That is vehicle mounted square cabin, mobile charge vehicle
With portable type ground station.The ground control that portable type ground station is suitable for small drone controls, and integrated level is high, at low cost,
Portability is strong, and transition is convenient, is widely used in unmanned plane field.
Existing Portable unmanned machine earth station is the dedicated ground station designed for specific model mostly, general to be only equipped with one
Platform computer and a display terminal, no backup functionality, data communication link is mostly using external mode, and versatility, autgmentability are not
By force, integrated level is not high.Therefore, it designs a kind of with multiple display terminals, integrated data links and with the portable of backup functionality
Formula unmanned aerial vehicle station can command control to provide more powerful platform for unmanned aerial vehicle and support
Invention content
Present invention solves the technical problem that it is:Design is a kind of with multiple display terminals, integrated data links and with standby
The general unmanned machine earth station of part function.
Present invention particularly provides a kind of portable unmanned aerial vehicle stations.
Technical scheme of the present invention one is:A kind of portable general unmanned aerial vehicle station including ground control computer, is shown
Show terminal, data chain device;
The ground control computer includes flight control computer and mission payload computer, flight control computer, mission payload
The flying-controlled box of unmanned plane and load control software are respectively mounted on computer;The data chain device conducts electricity platform, number including figure
Conduct electricity platform;Data radio station is connected by serial port switching device with flight control computer and mission payload computer;Figure conducts electricity platform including counting
Transmission module and figure transmission module;Digital transmission module is connected by serial port switching device with flight control computer and mission payload computer, and figure passes
Module connects interchanger, passes through network connection between interchanger and flight control computer and mission payload computer;Flight control computer
Data exchange is carried out by serial ports between mission payload computer;
The display terminal includes three display interfaces, and display interface 1 is connected with flight control computer, and display interface 3 is with appointing
Business LOAD FOR machine is connected;
Unmanned plane is performed in task process, and flight control computer, mission payload computer are separately operable mounted on respectively calculating
Uplink load remote-control data is sent to winged by flying-controlled box and load control software on machine, mission payload computer by serial ports
Computer is controlled, flight control computer will be sent after uplink flight remote-control data and uplink load remote-control data framing by data radio station
To unmanned plane;Downlink state of flight information and downlink loaded-up condition information are sent to flight control computer by data radio station, by
The downlink information of reception is sent to mission payload computer by flight control computer by serial ports;The load image information of downlink passes through
Figure conducts electricity platform access switch;Flight control computer, mission payload computer obtain downlink load image by network from interchanger
Information;State of flight and loaded-up condition are shown by display interface 1, display interface 3;
When a certain radio station is broken down in a computer failure in ground control computer or data chain device
When, fault-free computer with fault-free radio station is connected by serial port switching device, it is soft to run winged control simultaneously by fault-free computer
Part and load control software.
Technical scheme of the present invention second is that:A kind of portable general unmanned aerial vehicle station including ground control computer, is shown
Show terminal, data chain device;
The ground control computer includes flight control computer and mission payload computer, flight control computer, mission payload
The flying-controlled box of unmanned plane and load control software are respectively mounted on computer;The data chain device conducts electricity platform, number including figure
Conduct electricity platform;Data radio station is connected by serial port switching device with flight control computer and mission payload computer;Figure conducts electricity platform including counting
Transmission module and figure transmission module;Digital transmission module is connected by serial port switching device with flight control computer and mission payload computer, and figure passes
Module connects interchanger, passes through network connection between interchanger and flight control computer and mission payload computer;Flight control computer
Data exchange is carried out by serial ports between mission payload computer;
The display terminal includes three display interfaces, and display interface 1 is connected with flight control computer, and display interface 3 is with appointing
Business LOAD FOR machine is connected;
Unmanned plane is performed in task process, and flight control computer, mission payload computer are separately operable mounted on respectively calculating
Flying-controlled box and load control software on machine, flight control computer send uplink flight remote-control data by data radio station and receive
Downlink state of flight information, mission payload computer send uplink load remote-control data by digital transmission module and receive downlink load
Status information receives downlink load image information and access switch by figure transmission module;Flight control computer, mission payload calculate
Respective uplink is sent information by machine by serial ports, downlink reception information swaps, and downlink load is obtained from interchanger
Image information;State of flight and loaded-up condition are shown by display interface 1, display interface 3;
When a certain radio station is broken down in a computer failure in ground control computer or data chain device
When, fault-free computer with fault-free radio station is connected by serial port switching device, it is soft to run winged control simultaneously by fault-free computer
Part and load control software.
Further, load console is further included, digital transmission module passes through serial port switching device and flight control computer, mission payload
Computer, load console are connected;When selection sends uplink load by load console controls information, switched by serial ports
Load console is connected by device with digital transmission module, by the button or rocking bar on operation load console, realizes on unmanned plane
The control of mission payload.
Further, the display terminal further includes display interface 2, and display interface 2 passes through USB switch and HDMI
Switch is connected with flight control computer and mission payload computer.
Further, display interface 2 is connected by HDMI switcher with external HDMI interface, externally input to earth station
Image information is shown.
Further, it supplies electricity to earth station by city to power, charge the battery simultaneously, after alternating current power-off, be immediately switched to electricity
Pond powers, it is ensured that earth station does not shut down.
Further, figure conducts electricity platform and data radio station is equipped with antenna, when unmanned plane during flying radius is when within 10km, adopts
Use omnidirectional antenna;When more than 10km, using directional aerial.
Further, directional aerial wants external and gain >=12dBi.
Further, display terminal preferentially selects the liquid crystal display with touch function;Liquid crystal display is using highlighted liquid crystal display, screen
Curtain brightness >=800nits.
Further, entire earth station is designed to a briefcase, which includes upper box and lower box;
Display interface 1 and display interface 2 are arranged on upper box, other equipment is integrated on lower box, upper box and lower box
Junction sets telescope, and display interface 1, display interface 2 and the line of other equipment are placed in casing.
The present invention is with the advantages of prior art:
1st, the present invention provides a kind of general Portable unmanned machine earth stations, wherein flight control computer and mission payload meter
Calculation machine backups each other, and improves equipment dependability;
2nd, earth station integrates data radio station and figure conducts electricity platform, can be achieved at the same time data transmission and image transmitting, wherein, figure
The platform that conducts electricity carries digital transmission module, backups each other with data radio station, improves the reliability of data transmission;
3rd, earth station sets three display and control terminals, can more fully show unmanned plane status information, load image, three
Tie up situation information etc., the visualization for improving earth station is horizontal, enhances the situation of battlefield consciousness of operating personnel, improve work and
The efficiency of decision-making;
4th, earth station's installed load control software, while load console is set, can either load control be realized by software
System, and can realize that load controls by the button on load console and rocking bar;
5th, earth station sets a variety of man-machine interaction modes, including:Keyboard, mouse, touch control, button, rocking bar, enhance
Human-computer interaction is horizontal, mitigates operator's live load.
6th, earth station can set abundant external interface, can carry out data exchange with external equipment, be convenient for carrying, general
Property it is strong, integrated level is high, reliability is high, can meet unmanned plane commander demand for control.
Description of the drawings
Fig. 1 is portable type ground station theory of constitution figure;
Fig. 2 is a kind of appearance schematic diagram of the specific embodiment in portable type ground station.
Specific embodiment
The present invention is described in detail below with reference to the accompanying drawings and embodiments.
As shown in Figure 1, a kind of portable general unmanned aerial vehicle station provided by the invention, mainly by flight control computer, appoint
Conduct electricity platform, data radio station, interchanger, switch, load console, key mouse and outside of business LOAD FOR machine, touch screen, figure connects
Mouth composition.
The flying-controlled box of unmanned plane and load control software are respectively mounted on flight control computer and mission payload computer;Number
The platform that conducts electricity is connected by serial port switching device with flight control computer and mission payload computer;Figure conduct electricity platform include digital transmission module and figure
Transmission module;Digital transmission module is connected by serial port switching device with flight control computer and mission payload computer, and the connection of figure transmission module is handed over
It changes planes, passes through network connection between interchanger and flight control computer and mission payload computer;Flight control computer and mission payload
Data exchange is carried out by serial ports between computer.
Display interface 1 (touch screen 1 is used in this example) is connected by USB interface and USB interface with flight control computer, is shown
Interface 3 (touch screen 3) is connected by USB interface and USB interface with mission payload computer.Display interface 2 (touch screen 2) passes through
USB switch is connected respectively at flight control computer with mission payload computer, by HDMI switcher respectively at flight control computer,
HDMI IN in mission payload computer and external interface 1 are connected.
Unmanned plane is performed in task process, and flight control computer, mission payload computer are separately operable mounted on respectively calculating
Flying-controlled box and load control software on machine, show state of flight and loaded-up condition by touch screen 1, touch screen 3.Meter
Remote-control romote-sensing between calculation machine and unmanned plane can be realized by two ways.
First way:Uplink load remote-control data is sent to flight control computer by mission payload computer by serial ports,
Flight control computer will be sent to unmanned plane after uplink flight remote-control data and uplink load remote-control data framing by data radio station;
Downlink state of flight information and downlink loaded-up condition information are sent to flight control computer by data radio station, by flight control computer
The downlink information of reception is sent to by mission payload computer by serial ports;The load image information of downlink is connect by the figure platform that conducts electricity
Enter interchanger;Flight control computer, mission payload computer obtain downlink load image information by network from interchanger.
The second way:Flight control computer sends uplink flight remote-control data by data radio station and receives downlink flight shape
State information, mission payload computer send uplink load remote-control data and receive downlink load by the conduct electricity digital transmission module of platform of figure
Status information, the figure transmission module reception downlink load image information and access switch of the platform that conducted electricity by figure;Flight control computer is appointed
Respective uplink is sent information by business LOAD FOR machine by serial ports, downlink reception information is swapped, and obtained from interchanger
Remove row load image information.
When thering is one to break down in flight control computer and mission payload computer or data radio station and the figure platform that conducts electricity have
During one failure, fault-free computer is connected with fault-free radio station by serial port switching device, it is same by fault-free computer
Shi Yunhang flying-controlled box and load control software.
For three touch screens using screen is highlighted, screen intensity is not less than 800nits, meets the use under outdoor strong light
It is required that.Wherein the display of touch screen 1 flies control state, and touch screen 3 shows loaded-up condition.Earth station under normal usage, touches
Screen 2 is connected with mission payload computer, shows load image information;When mission payload computer breaks down, touch screen 2 can
It is connected by USB switch and HDMI switcher with flight control computer, so as to show flight control computer picture.In external interface 1
HDMI IN can connect external input image, be connected by HDMI switcher with touch screen 2, so as to by external input image
It is shown on touch screen 2.
Load console includes button, Hall remote pole and analog input card;The conduct electricity digital transmission module of platform of figure is switched by serial ports
Device is connected with flight control computer, mission payload computer, load console;When selection sends uplink load by load console
When controlling information, load console with digital transmission module is connected by serial port switching device, button and Hall remote pole can be used to realize
The control of mission payload on unmanned plane.
The power-supply system at portable general unmanned aerial vehicle station includes DC power supply and lithium battery, when alternating current inputs, by straight
Galvanic electricity source power supply to the device, while DC power supply can charge the battery;When city is electrically disconnected, battery powered is automatically switched to, it is real
Existing earth station uninterrupted power supply.
Figure conducts electricity platform and data radio station is equipped with antenna, when unmanned plane during flying radius is when within 10km, using omnidirectional antennas
Line;When more than 10km, using directional aerial, directional aerial wants external and gain >=12dBi.
Earth station is equipped with external interface 1 and external interface 2, data exchange can be carried out with external equipment, versatility is good, extension
Property it is strong, can meet more multiple no-manned plane accuse demand.
One specific embodiment at portable general unmanned aerial vehicle station integrates as shown in Fig. 2, illustrating earth station in figure
External layout schematic diagram afterwards.
Earth station is mainly made of upper box 1 and lower box 7.Two touch display terminals are set on upper box panel, it is left
Touch screen 1 (touch screen 1 in Fig. 1) is connected with flight control computer, and main display flies control state;Right (the touching in Fig. 1 of touch screen 2
Touch screen 2) generally it is connected with mission payload computer, it is main to show load image information.Electricity is additionally provided on upper box panel
Display 14, for showing the electricity of earth station's lithium battery, electric-quantity display device 14 sets two antennal interfaces, wherein antenna above
Interface 15 conducts electricity platform antennal interface for figure, and antennal interface 16 is data radio station antennal interface.
Interface panel 4 and 12 is set on lower box panel, and keyboard 6 and 11 touches the (touch screen in Fig. 1 of display terminal 5
3), load console 8, radiator fan panel 9, attachment cover plate 10.
External interface (external interface 1 in Fig. 1), the power supply of mission payload computer is set to open wherein on interface panel 4
Pass, facility switching, heat emission hole;External interface (external interface 2 in Fig. 1), the string of flight control computer are set on interface panel 12
Mouth switch button, USB switch button, HDMI switcher button, heat emission hole;The external interface of computer mainly includes net
Mouth, USB interface, earphone microphone interface, serial ports, HDMI interface.Keyboard 6 is mission payload computer keyboard, and keyboard 11 is calculated to fly control
Switch disk.It touches display terminal 5 to connect with mission payload computer, shows loaded-up condition.Load console 8 can be by pressing
Mission payload on key, Hall remote pole control unmanned plane.Equipped with radiator fan on radiator fan panel 9, meet inside lower box
Equipment cooling demand.Open the attachment cover plate 10, and mouse, flight remote controller, cable etc. can be stored in accessory case.
In addition wiring sleeve 3 is also provided between earth station's upper and lower box, the connecting line between upper and lower box can be protected
Cable makes equipment more beautiful from damage.Wiring sleeve 3 is for the either on or off rotation being applicable between upper and lower box, peace
On the relative rotation axis of upper and lower box, and using the form of telescopic sleeve pipe.
Unspecified part of the present invention belongs to the common knowledge of those skilled in the art.
Claims (10)
1. a kind of general unmanned machine earth station, it is characterised in that:Including ground control computer, display terminal, data chain device;
The ground control computer includes flight control computer and mission payload computer, and flight control computer, mission payload calculate
The flying-controlled box of unmanned plane and load control software are respectively mounted on machine;The data chain device including figure conduct electricity platform, number conduct electricity
Platform;Data radio station is connected by serial port switching device with flight control computer and mission payload computer;Figure conducts electricity platform including counting biography mould
Block and figure transmission module;Digital transmission module is connected by serial port switching device with flight control computer and mission payload computer, figure transmission module
Interchanger is connected, passes through network connection between interchanger and flight control computer and mission payload computer;Flight control computer and appoint
Data exchange is carried out by serial ports between business LOAD FOR machine;
The display terminal includes three display interfaces, and display interface I is connected with flight control computer, and display interface III is carried with task
Lotus computer is connected;
Unmanned plane is performed in task process, and flight control computer, mission payload computer are separately operable installation on the respective computers
Flying-controlled box and load control software, mission payload computer by serial ports by uplink load remote-control data be sent to fly control meter
Calculation machine, flight control computer will be sent to nothing after uplink flight remote-control data and uplink load remote-control data framing by data radio station
It is man-machine;Downlink state of flight information and downlink loaded-up condition information are sent to flight control computer by data radio station, by flying control
The downlink information of reception is sent to mission payload computer by computer by serial ports;The load image information of downlink is passed by scheming
Radio station access switch;Flight control computer, mission payload computer obtain downlink load image information by network from interchanger;
State of flight and loaded-up condition are shown by display interface I, display interface III;
When a certain radio station is broken down in a computer failure in ground control computer or data chain device, lead to
It crosses serial port switching device fault-free computer is connected with fault-free radio station, flying-controlled box and load is run by fault-free computer simultaneously
Lotus control software.
2. a kind of general unmanned machine earth station, it is characterised in that:Including ground control computer, display terminal, data chain device;
The ground control computer includes flight control computer and mission payload computer, and flight control computer, mission payload calculate
The flying-controlled box of unmanned plane and load control software are respectively mounted on machine;The data chain device including figure conduct electricity platform, number conduct electricity
Platform;Data radio station is connected by serial port switching device with flight control computer and mission payload computer;Figure conducts electricity platform including counting biography mould
Block and figure transmission module;Digital transmission module is connected by serial port switching device with flight control computer and mission payload computer, figure transmission module
Interchanger is connected, passes through network connection between interchanger and flight control computer and mission payload computer;Flight control computer and appoint
Data exchange is carried out by serial ports between business LOAD FOR machine;
The display terminal includes three display interfaces, and display interface I is connected with flight control computer, and display interface III is carried with task
Lotus computer is connected;
Unmanned plane is performed in task process, and flight control computer, mission payload computer are separately operable installation on the respective computers
Flying-controlled box and load control software, flight control computer uplink flight remote-control data is sent by data radio station and receives downlink
State of flight information, mission payload computer send uplink load remote-control data by digital transmission module and receive downlink loaded-up condition
Information receives downlink load image information and access switch by figure transmission module;Flight control computer, mission payload computer lead to
Serial ports is crossed to swap, and obtain downlink load image from interchanger respective uplink transmission information, downlink reception information
Information;State of flight and loaded-up condition are shown by display interface I, display interface III;
When a certain radio station is broken down in a computer failure in ground control computer or data chain device, lead to
It crosses serial port switching device fault-free computer is connected with fault-free radio station, flying-controlled box and load is run by fault-free computer simultaneously
Lotus control software.
3. earth station according to claim 1 or 2, it is characterised in that:Load console is further included, digital transmission module passes through string
Mouth switch is connected with flight control computer, mission payload computer, load console;When selection is sent by load console
When row load controls information, load console with digital transmission module is connected by serial port switching device, passes through operation load console
On button or rocking bar, realize unmanned plane on mission payload control.
4. earth station according to claim 1 or 2, it is characterised in that:The display terminal further includes display interface II,
Display interface II is connected by USB switch and HDMI switcher with flight control computer and mission payload computer.
5. earth station according to claim 4, it is characterised in that:Display interface 2 passes through HDMI switcher and outside HDMI
Interface is connected, and to earth station, externally input image information is shown.
6. earth station according to claim 1 or 2, it is characterised in that:Earth station is supplied electricity to by city to power, while to battery
Charging after alternating current power-off, is immediately switched to battery powered, it is ensured that earth station does not shut down.
7. earth station according to claim 1 or 2, it is characterised in that:Figure conducts electricity platform and data radio station is equipped with antenna, when
Unmanned plane during flying radius is when within 10km, using omnidirectional antenna;When more than 10km, using directional aerial.
8. earth station according to claim 1 or 2, it is characterised in that:Directional aerial wants external and gain >=12dBi.
9. earth station according to claim 1 or 2, it is characterised in that:Display terminal is preferentially selected with touch function
Liquid crystal display;Liquid crystal display is using highlighted liquid crystal display, screen intensity >=800ni ts.
10. earth station according to claim 1 or 2, it is characterised in that:Entire earth station is designed to a portable instrument
Case, the instrument container include upper box and lower box;Display interface 1 and display interface 2 are arranged on upper box, other equipment collection
Into on lower box, the junction setting telescope of upper box and lower box, display interface 1, display interface 2 and other
The line of equipment is placed in casing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711384945.8A CN108196569B (en) | 2017-12-20 | 2017-12-20 | General unmanned aerial vehicle ground satellite station |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711384945.8A CN108196569B (en) | 2017-12-20 | 2017-12-20 | General unmanned aerial vehicle ground satellite station |
Publications (2)
Publication Number | Publication Date |
---|---|
CN108196569A true CN108196569A (en) | 2018-06-22 |
CN108196569B CN108196569B (en) | 2021-02-09 |
Family
ID=62577364
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201711384945.8A Active CN108196569B (en) | 2017-12-20 | 2017-12-20 | General unmanned aerial vehicle ground satellite station |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108196569B (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108964749A (en) * | 2018-08-24 | 2018-12-07 | 彭彦平 | A kind of unmanned plane double screen earth station that suitable field uses |
CN109634139A (en) * | 2018-12-10 | 2019-04-16 | 中国航天空气动力技术研究院 | Hypersonic aircraft navigation and control system semi-matter simulating system and method |
CN110517539A (en) * | 2019-09-12 | 2019-11-29 | 中国航空工业集团公司西安飞行自动控制研究所 | A kind of unmanned aerial vehicle station |
CN110661547A (en) * | 2019-10-30 | 2020-01-07 | 中国航天空气动力技术研究院 | Method for establishing communication connection between individual soldier guided unmanned aerial vehicle and ground station |
CN111137453A (en) * | 2019-11-05 | 2020-05-12 | 西安羚控电子科技有限公司 | Measurement and control tracking system and method for carrier-based vertical take-off and landing detection unmanned aerial vehicle |
CN112885153A (en) * | 2021-01-22 | 2021-06-01 | 北京北航天宇长鹰无人机科技有限公司 | General aviation safety monitoring system based on multi-network integration |
CN113014289A (en) * | 2021-03-15 | 2021-06-22 | 西安忠林世纪电子科技有限公司 | Unmanned aerial vehicle data chain backup method |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2827210A1 (en) * | 2013-07-15 | 2015-01-21 | BAE Systems PLC | Route planning |
CN104503460A (en) * | 2014-12-05 | 2015-04-08 | 电子科技大学 | Ground station control system for universal unmanned aerial vehicle |
CN204515875U (en) * | 2015-04-16 | 2015-07-29 | 沈阳飞羽航空科技有限公司 | Unmanned aerial vehicle station EFIS |
US9405005B1 (en) * | 2012-04-24 | 2016-08-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Automatic dependent surveillance broadcast (ADS-B) system for ownership and traffic situational awareness |
CN106526388A (en) * | 2016-12-20 | 2017-03-22 | 中国航天空气动力技术研究院 | Test system and test method for airborne avionics device of unmanned aerial vehicle |
CN206115267U (en) * | 2016-10-31 | 2017-04-19 | 成都紫瑞青云航空宇航技术有限公司 | Portable ground satellite station |
CN106933094A (en) * | 2017-03-01 | 2017-07-07 | 北京天恒长鹰科技股份有限公司 | A kind of pair of airborne flight control computer of remaining |
CN106998095A (en) * | 2017-04-20 | 2017-08-01 | 河南亿诺航空科技有限公司 | A kind of unmanned plane management platform |
CN206472226U (en) * | 2016-06-20 | 2017-09-05 | 徐州神州通达建筑智能化有限责任公司 | Digitized map passes earth station |
-
2017
- 2017-12-20 CN CN201711384945.8A patent/CN108196569B/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9405005B1 (en) * | 2012-04-24 | 2016-08-02 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Automatic dependent surveillance broadcast (ADS-B) system for ownership and traffic situational awareness |
EP2827210A1 (en) * | 2013-07-15 | 2015-01-21 | BAE Systems PLC | Route planning |
CN104503460A (en) * | 2014-12-05 | 2015-04-08 | 电子科技大学 | Ground station control system for universal unmanned aerial vehicle |
CN204515875U (en) * | 2015-04-16 | 2015-07-29 | 沈阳飞羽航空科技有限公司 | Unmanned aerial vehicle station EFIS |
CN206472226U (en) * | 2016-06-20 | 2017-09-05 | 徐州神州通达建筑智能化有限责任公司 | Digitized map passes earth station |
CN206115267U (en) * | 2016-10-31 | 2017-04-19 | 成都紫瑞青云航空宇航技术有限公司 | Portable ground satellite station |
CN106526388A (en) * | 2016-12-20 | 2017-03-22 | 中国航天空气动力技术研究院 | Test system and test method for airborne avionics device of unmanned aerial vehicle |
CN106933094A (en) * | 2017-03-01 | 2017-07-07 | 北京天恒长鹰科技股份有限公司 | A kind of pair of airborne flight control computer of remaining |
CN106998095A (en) * | 2017-04-20 | 2017-08-01 | 河南亿诺航空科技有限公司 | A kind of unmanned plane management platform |
Non-Patent Citations (2)
Title |
---|
BARIS KAYAYURT: "GROUND CONTROL STATION AVIONICS SOFTWARE DEVELOPMENT IN ANKA UAV", 《IEEE》 * |
王鑫,等: "WPF 技术在无人机地面控制站中的应用", 《无线电工程》 * |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108964749A (en) * | 2018-08-24 | 2018-12-07 | 彭彦平 | A kind of unmanned plane double screen earth station that suitable field uses |
CN109634139A (en) * | 2018-12-10 | 2019-04-16 | 中国航天空气动力技术研究院 | Hypersonic aircraft navigation and control system semi-matter simulating system and method |
CN109634139B (en) * | 2018-12-10 | 2021-12-07 | 中国航天空气动力技术研究院 | Semi-physical simulation system and method for navigation and control system of hypersonic aircraft |
CN110517539A (en) * | 2019-09-12 | 2019-11-29 | 中国航空工业集团公司西安飞行自动控制研究所 | A kind of unmanned aerial vehicle station |
CN110661547A (en) * | 2019-10-30 | 2020-01-07 | 中国航天空气动力技术研究院 | Method for establishing communication connection between individual soldier guided unmanned aerial vehicle and ground station |
CN110661547B (en) * | 2019-10-30 | 2021-12-07 | 中国航天空气动力技术研究院 | Method for establishing communication connection between individual soldier guided unmanned aerial vehicle and ground station |
CN111137453A (en) * | 2019-11-05 | 2020-05-12 | 西安羚控电子科技有限公司 | Measurement and control tracking system and method for carrier-based vertical take-off and landing detection unmanned aerial vehicle |
CN112885153A (en) * | 2021-01-22 | 2021-06-01 | 北京北航天宇长鹰无人机科技有限公司 | General aviation safety monitoring system based on multi-network integration |
CN113014289A (en) * | 2021-03-15 | 2021-06-22 | 西安忠林世纪电子科技有限公司 | Unmanned aerial vehicle data chain backup method |
CN113014289B (en) * | 2021-03-15 | 2022-08-19 | 西安忠林世纪电子科技有限公司 | Unmanned aerial vehicle data chain backup method |
Also Published As
Publication number | Publication date |
---|---|
CN108196569B (en) | 2021-02-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108196569A (en) | A kind of general unmanned machine earth station | |
CN203773717U (en) | Remote visual touch screen control system for unmanned plane | |
CN104950771B (en) | A kind of unmanned plane holds ground station control system | |
CN202068445U (en) | Mobile monitoring system | |
CN202838027U (en) | Integrated ground station device for unmanned aerial vehicle | |
CN103543795A (en) | Portable remote control device | |
CN104347051A (en) | Method and system for adjusting screen brightness | |
CN105678989A (en) | Remote controller | |
CN204790354U (en) | Multi -functional unmanned aerial vehicle hand -held remote controller of distributing type LCD screen | |
CN206624007U (en) | A kind of unmanned plane is tethered at, non-is tethered at pattern quick switching structure and unmanned plane | |
CN104852836A (en) | Comprehensive data acquisition substation for underground coal mine | |
CN205644102U (en) | Portable ground satellite station | |
CN204790422U (en) | Unmanned aerial vehicle hands control system of ground satellite station | |
CN205450677U (en) | Unmanned aerial vehicle ground satellite station universal command panel able to programme | |
CN102255767A (en) | Multifunctional handheld communication tester | |
CN209149566U (en) | Unmanned controller based on android system | |
CN207382330U (en) | A kind of movable unmanned helicopter jamming equipment | |
CN205375194U (en) | Portable unmanned aerial vehicle ground satellite station | |
CN103019113A (en) | On-off control device for onboard 3G communication module and onboard wireless communication system | |
CN207164593U (en) | Unmanned controller and no-manned machine distant control system | |
CN109933082A (en) | A kind of Unmanned Aircraft Control Stations Control System | |
CN205450782U (en) | Drone's portable ground satellite station | |
CN108768502A (en) | A kind of intelligent remote controller being connect with unmanned plane big data platform | |
CN202435434U (en) | Wirelessly-controlled matrix switching device | |
CN202171780U (en) | Multifunction keyboard for portable tablet computer |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |