CN106688319B - A kind of integrated UAV ground control station - Google Patents
A kind of integrated UAV ground control stationInfo
- Publication number
- CN106688319B CN106688319B CN201010047142.5A CN201010047142A CN106688319B CN 106688319 B CN106688319 B CN 106688319B CN 201010047142 A CN201010047142 A CN 201010047142A CN 106688319 B CN106688319 B CN 106688319B
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- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000004891 communication Methods 0.000 claims description 8
- 238000005259 measurement Methods 0.000 claims description 7
- 230000003028 elevating Effects 0.000 claims description 6
- 241001269238 Data Species 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000005755 formation reaction Methods 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 3
- 238000000926 separation method Methods 0.000 abstract 1
- 230000032258 transport Effects 0.000 abstract 1
- 230000001276 controlling effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000000875 corresponding Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Abstract
A kind of integrated UAV ground control station：The UAV ground control station adopts car-cabin separation design, and is fixedly mounted with overhead kick and column base, transports extremely convenient.The earth station has corrected and antenna had been placed in the exposed design concept of roof in the past, propose the dynamic antenna structure of belt lifting mechanism controlled using servo control mechanism, only in the task of execution, antenna could launch, and so effectively increase the service life of antenna, reduce the probability spied out by enemy air.The earth station employs many places Redundancy Design, employs third generation ups power redundancy technique and double telemeter channel redundancy techniques, greatly reduces operation troubles rate.
Description
Technical field
This technology is mainly used in unmanned aerial vehicle station system, is a kind of unmanned aerial vehicle of Highgrade integration
Stand design.
Background technology
Unmanned aerial vehicle station system, as " nerve center " of whole UAS, is controlled whole
The successful realization of the various functions of system, is used as an independent subsystem of most expensive in whole UAS
System, while being also most hidden in whole UAS, is most difficult exposure and a least flimsy son
System, it should more functions in whole system are integrated into earth station's subsystem to realize.Earth station
System can as whole UAS combat operations center, control aircraft flight course, fly
Row flight path, efficient completion of the payload to task, normal work of communication link etc..Unmanned aerial vehicle
The function that the system of station should be played also must be the pith of whole UAS, except that should complete
Basic flight state control and the reception of payload data, processing, while also require that can be flexible
Overcome various unknown natures, the adverse effect of human factor, adapt to various complex environments, it is ensured that
The successful realization of whole system allomeric function.
Unmanned aerial vehicle station common at present, function is less, the shorter shortcoming of command range.In system event
During barrier, it is impossible to preferably quickly put into it is secondary use, such as when dump, ups power turn-on time
Longer, input current ripple is larger, there is certain pulse shock to the equipment being currently running；If special feelings
When telemeter channel breaks down under condition, without backup link, it is impossible to know unmanned plane current flight state.
The content of the invention
Present invention solves the technical problem that：There is provided a kind of integrated UAV ground control station, Ke Yishi
The now display and the control of payload of the attitude, payload data of control aircraft, mission planning,
Map denotation, Radio Link, state of data link monitoring and the day line traffic control of unmanned plane position and flight path,
The functions such as Strike control, voice communication.
The technical solution of the present invention：The UAV ground control station is used inside the long shelters of 6m, shelter
It is divided into two parts of aerial compartment and equipment compartment.Antenna is parabolic shape antenna, and antenna pedestal is installed on lift
On structure, when earth station organizes work, elevating mechanism is controlled, antenna is completely disposed at out of my cabin.Equipment compartment is then
Two telemeter channels and a remote control channel 10 are integrated with, two telemeter channels are distant by two respectively
Computer is surveyed with Data-Link monitoring computer 9 to be connected；Data-Link monitoring computer 9 respectively with the first remote measurement
Channel 1, the first remote measurement computer 2, the second telemeter channel 6, the second remote measurement computer connected 7；Antenna
Control unit 5 monitors computer 9 by Data-Link and controls antenna driver element 4, antenna driver element 4
It is connected with antenna pedestal 3；DGPS base stations 8 are connected with Data-Link monitoring computer 9, Data-Link monitoring
Computer 9 is connected by remote control channel 10 with antenna；Mission planning unit 11, mission payload unit 12,
Fire control unit 13 is connected with Data-Link monitoring computer respectively；The ultra-short wave radio installed in earth station
Platform and supply power supply unit.
Advantage of the present invention relative to other technologies：
1st, the system integration degree is high, convenient transport；
The 2nd, parabola antenna is placed in the base of elevating mechanism, servomotor rapid deployment is utilized.
3rd, the Double redundancy backup with communication link and electric power system, can avoid unmanned plane out of control.
4th, function is more powerful, and the equipment such as a variety of communications, power supply, control are integrated with shelter.
Brief description of the drawings：
Fig. 1：Earth station system data flowchart.
Embodiment：
Fig. 1 is earth station system data flowchart, including：First telemeter channel 1, the first remote measurement is calculated
Machine 2；Antenna pedestal 3；Antenna driver element 4；Antenna control unit 5；Second telemeter channel 6；Second is distant
Survey computer 7；DGPS base stations 8；Data-Link monitors computer 9；Remote control channel 10；Mission planning
Unit 11；Mission payload unit 12；Fire control unit 13.
The UAV ground control station to use and be divided into aerial compartment and equipment compartment two inside the long shelters of 6m, shelter
Individual part.Antenna is parabolic shape antenna, and floor installation is on elevating mechanism, when earth station organizes work,
Elevating mechanism is controlled, antenna is completely disposed at out of my cabin.Equipment compartment is then integrated with measuring and controlling equipment, set for distribution
Standby, antenna controling equipment, voice communication apparatus, mixed-media network modules mixed-media, communication test set, mission payload control
Device processed, DGPS differential reference stations etc..
The function that earth station realizes：
Control the attitude of aircraft.The acquisition of flight state is completed by airborne various sensors
, these sensors are obtained after corresponding state of flight information, by data link by these data with
Predetermined format transmission is to earth station.Earth station is after these data are obtained according to control rate
Control instruction is calculated, then control instruction is transferred on flight control computer by data link, is counted
Calculation machine handles these information, sends control instruction to control the attitude of aircraft.
2) display of payload data and the control of payload.Payload is holding for unmanned plane task
Row unit.The One function of ground control station seeks to realize the control to payload, so as to hold
Row is scouted and combat duty.
3) map denotation of mission planning, unmanned plane position and flight path.The main purpose of this part of functions
Exactly realize the navigation task during unmanned plane during flying.Operating personnel can be according to actual task
It is required that pre-planning is carried out to the course line of unmanned plane, while can also be in task implementation procedure to flight path
Realize monitoring in real time.
4) Radio Link.Telemeter channel and remote control channel, telemeter channel transmission nothing are integrated with earth station
The man-machine information for passing ground back, including telemetry intelligence (TELINT), control back to make, location information, reconnaissance
Deng, using PCM-FM regime transmissions downlink datas, can with general remote-measuring equipment receive unmanned plane under
Row data, reach hardware compatibility and improve the effect of utilization rate of equipment and installations.Face remote control transmission
The command control information of unmanned plane, using PCM-DS-BPSK regime transmissions.Same spatial domain is formed into columns
The multiple UAVs of flight, telemeter channel uses TDMA time-division systems, and remote control channel uses FDMA
Frequency division system.
5) state of data link monitoring and day line traffic control.Double telemeter channels and one are integrated with earth station
Remote control channel, by data link monitoring software, can watch feedback system in display data link and day at any time
Every state of system.
6) Strike is controlled.Strike control is mainly when unmanned plane carry guided missile and bomb perform work
During war task, the dispensing of air weapon is realized by ground control, so as to realize the strike to target.
7) DGPS differential reference stations.DGPS base stations are as DGPS pith, and base station will acquisition
Differential corrections or obtain raw observation, by up channel with RTCM SC-104 difference assist
View uploads to airborne DGPS, and airborne DGPS obtains more accurate positional information by resolving, so that
Precise control flight track.
8) voice communication.Ultrashort wave radio station is mounted with earth station, can be realized by it inside and outside cabin
Voice communication, especially the collaborative work of personnel is particularly important inside and outside unmanned plane section of taking off, cabin.
9) power supply unit is supplied.It is the support Unit of whole earth station system for power supply unit, it is earth station
Each equipment provides the different voltages such as 12V, 28V, 220V, 380V, it is ensured that each in earth station system
The normal work of subsystem；Simultaneously the supply input of civil power and oil machine can also be provided for power supply unit.
10) ups system.Earth station system is powered using three UPS as emergency backup, is used as system
One of composition is ensured, it can be in the case of its exterior power failure, it is ensured that each in system
Subsystem normal work is not less than ten minutes.
The function that the ground control station is realized is above described, its main effect is to realize ground control
Control and monitoring of the personnel to unmanned plane, so observing and controlling function is the core of whole ground control station system,
By TT＆C system, the upper hair of telecommand and the passback and display of telemetry are realized.Figure below is ground
The flow of each data in standing.
Claims (5)
1. a kind of integrated UAV ground control station, it is characterised in that：The UAV ground control station uses
It is divided into two parts of aerial compartment and equipment compartment inside the long shelters of 6m, shelter, antenna is parabolic shape antenna,
Antenna pedestal (3) is installed on elevating mechanism, when earth station organizes work, and is controlled elevating mechanism, is made day
Line is completely disposed at out of my cabin；Equipment compartment is then integrated with two telemeter channels and a remote control channel (10),
Two telemeter channels monitor computer (9) by two remote measurement computers and Data-Link respectively and are connected；Number
According to chain monitoring computer (9) respectively with the first telemeter channel (1), the first remote measurement computer (2),
Second telemeter channel (6), the second remote measurement computer are connected (7)；Antenna control unit (5) passes through
Data-Link monitoring computer (9) control antenna driver element (4), antenna driver element (4) and day
Line seat (3) is connected；DGPS base stations (8) are connected with Data-Link monitoring computer (9), Data-Link
Monitoring computer (9) is connected with remote control channel (10)；Mission planning unit (11), mission payload
Unit (12), fire control unit (13) are connected with Data-Link monitoring computer respectively；Installed in earth station
Ultrashort wave radio station and supply power supply unit；Attitude, the payload of control aircraft can be realized
The display of data and the control of payload, mission planning, the map denotation of unmanned plane position and flight path,
Radio Link, state of data link monitoring and day line traffic control, Strike control, function of voice communication.
2. a kind of integrated UAV ground control station according to claim 1, it is characterised in that：Ground
Telemeter channel and remote control channel are integrated with the station of face, telemeter channel transmission unmanned plane passes the letter on ground back
Breath, using PCM-FM regime transmissions downlink datas；The commander for facing unmanned plane is controlled remote control transmission
Information processed, using PCM-DS-BPSK regime transmissions；To the multiple UAVs of same spatial domain formation flight,
Telemeter channel uses TDMA time-division systems, and remote control channel uses FDMA frequency division systems.
3. a kind of integrated UAV ground control station according to claim 1, it is characterised in that：Institute
The DGPS base stations stated are by the differential corrections of acquisition or obtain raw observation, by up channel with
RTCM SC-104 DIFFERENTIAL PROTOCOLs upload to airborne DGPS, and airborne DGPS obtains more accurate by resolving
Positional information so that precise control flight track.
4. a kind of integrated UAV ground control station according to claim 1, it is characterised in that：Institute
The confession power supply unit stated can provide 12V, 28V, 220V, 380V voltage for each equipment of earth station；Together
When the supply input of civil power and oil machine can also be provided for power supply unit.
5. a kind of integrated UAV ground control station according to claim 1, it is characterised in that：Ground
Face station system is powered using three UPS as emergency backup, it can its exterior power failure feelings
Under condition, it is ensured that subsystems normal work is not less than ten minutes in system.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106688319B true CN106688319B (en) | 2013-10-23 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107264792A (en) * | 2017-07-04 | 2017-10-20 | 张洋 | A kind of modular unmanned plane of dynamical system |
| CN107426016A (en) * | 2017-06-06 | 2017-12-01 | 上海卫星工程研究所 | The highly reliable ground TTC channel design method of satellite launch area electrical testing |
| CN107831783A (en) * | 2017-11-10 | 2018-03-23 | 南昌航空大学 | A kind of ground station control system for supporting multiple no-manned plane autonomous flight |
| CN110562482A (en) * | 2019-09-11 | 2019-12-13 | 中国航空工业集团公司沈阳飞机设计研究所 | Integrated guarantee shelter for test flight |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107426016A (en) * | 2017-06-06 | 2017-12-01 | 上海卫星工程研究所 | The highly reliable ground TTC channel design method of satellite launch area electrical testing |
| CN107426016B (en) * | 2017-06-06 | 2020-07-14 | 上海卫星工程研究所 | Design method of high-reliability ground measurement and control link for satellite emission area electrical test |
| CN107264792A (en) * | 2017-07-04 | 2017-10-20 | 张洋 | A kind of modular unmanned plane of dynamical system |
| CN107831783A (en) * | 2017-11-10 | 2018-03-23 | 南昌航空大学 | A kind of ground station control system for supporting multiple no-manned plane autonomous flight |
| CN110562482A (en) * | 2019-09-11 | 2019-12-13 | 中国航空工业集团公司沈阳飞机设计研究所 | Integrated guarantee shelter for test flight |
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