CN205787907U - A kind of unmanned aerial vehicle controls work station - Google Patents
A kind of unmanned aerial vehicle controls work station Download PDFInfo
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- CN205787907U CN205787907U CN201620472547.6U CN201620472547U CN205787907U CN 205787907 U CN205787907 U CN 205787907U CN 201620472547 U CN201620472547 U CN 201620472547U CN 205787907 U CN205787907 U CN 205787907U
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Abstract
nullThe utility model discloses a kind of unmanned aerial vehicle and control work station，Wherein，Link switch board is arranged on the right side of task control cabinet，Flight switch board is arranged on the right side of link switch board，Task control cabinet、The bottom of link switch board and flight switch board is fitted with supporting leg，It is fitted with switch and distribution box in task control cabinet and flight switch board，Left liquid crystal display is arranged in task control cabinet，Left touch-screen display is arranged in task control cabinet，Task control cabinet、It is fitted with throttle lever on the table top of link switch board and flight switch board、Control bar and KVM switcher，CPCI calculates unit and is arranged in link switch board，Middle touch-screen display is arranged in link switch board，Middle liquid crystal display is arranged in link switch board，UPS device is arranged in link switch board，Right liquid crystal display is arranged in flight switch board，Right touch-screen display is arranged in flight switch board.
Description
Technical field
This utility model relates to a kind of unmanned aerial vehicle (UAV) control technical field, specifically, particularly to a kind of unmanned
Machine ground controls work station.
Background technology
In recent years, the research of unmanned plane and application have worldwide obtained cognitive widely and have paid close attention to, I
State's correlational study unit has also put into sizable energy in the research and development of unmanned plane.And unmanned plane ground
Face control station system is the command and control center of whole UAS, the unmanned aerial vehicle of a set of perfect in shape and function
Control station system can be good at ancillary terrestrial operator and unmanned plane carries out flight condition supervision with in real time
Control, and complete corresponding task system function.
The ground control station of unmanned plane is as the command centre of whole UAS, in unmanned plane during flying process
In, play absolute central role.In order to preferably improve the command system of unmanned plane, people design
Various types of earth station systems, carry out auxiliary operation person to the various flying qualities of unmanned plane and task system
Status of equipment monitors in real time, to guarantee that the safety of unmanned plane during flying is simultaneously to occur at case of emergency
Time corresponding measure can be taked in time to ensure the safety of unmanned plane.Owing to ground control station can fly
According to changes such as actual geographical environment, weather environment or other non-artificial factor, anthropic factors in journey, control
System changes predetermined task scheduling, such that it is able to be effectively improved unmanned plane to perform the ability of actual task.
Ground control station in the market is many based on handheld portable, its observing and controlling distance and wireless data chain
The passback distance on road is the shortest, it is impossible to meets the whole information transmission in remote flight course planning task and dashes forward
The demand of the hand-off dynamic flight of condition of oestrusing incision, more cannot meet the modern demand to multi-functional integration technology.
Vehicular ground control station system is owing to being placed in vehicle interior, and its relevant corollary apparatus can combine with locomotive
(such as transmitting terminal and receiving terminal), on the one hand can solve to carry the portability problem of aircraft, on the other hand
Owing to the master control system of vehicle-mounted ground control station is more advanced, its main frame can take up space bigger, and it can provide
The function that more handheld portable earth stations do not have, most important of which is a little and commanding in the rear center
Carry out real-time function of holding a conference or consultation online, the rear situation analysis to front and work so can be provided more easily
War is disposed, and checks including history video, file passback, word holds a conference or consultation.This ground control station system simultaneously
Two unmanned aerial vehicle platforms can be carried out flight course planning, it is achieved round trip flight single control function.
Utility model content
Technical problem to be solved in the utility model is, for above-mentioned deficiency of the prior art, to disclose
A kind of unmanned aerial vehicle controls work station, and it can effectively solve the problem that current various unmanned plane and the survey of payload platform
The control skimble-scamble problem of agreement.
This utility model solves its technical problem and be the technical scheme is that a kind of unmanned aerial vehicle controls work
Stand, including task control cabinet, supporting leg, link switch board, CPCI calculate unit, switch, distribution box,
Throttle lever, flight switch board, right touch-screen display, right LCDs, speech talkback equipment, UPS
Device, left liquid crystal display, left touch-screen display, control bar, middle liquid crystal display, middle touch screen display
Show device and KVM switcher；Described link switch board is arranged on the right side of task control cabinet, and described flight controls
Cabinet is arranged on the right side of link switch board, described task control cabinet, link switch board and the end of flight switch board
Portion is fitted with supporting leg, is fitted with switch and distribution box in described task control cabinet and flight switch board,
Two described left liquid crystal displays are arranged in task control cabinet, and two described left touch-screen displays are arranged on
In task control cabinet and left touch-screen display is positioned at the lower section of left liquid crystal display, described task control cabinet,
It is fitted with throttle lever on the table top of link switch board and flight switch board, controls bar and KVM switcher, institute
State in CPCI calculating unit is arranged on link switch board and CPCI calculates unit near the end of link switch board
Face, described middle touch-screen display is arranged in link switch board, and described middle liquid crystal display is arranged on link
Interior and the middle liquid crystal display of switch board is positioned at the top of middle touch-screen display, and described speech talkback equipment is installed
In link switch board and speech talkback equipment be positioned in above liquid crystal display, described UPS device is installed
In link switch board and UPS device is positioned at above speech talkback equipment, two described right liquid crystal displays
Being arranged in flight switch board, two described right touch-screen displays are arranged on the interior and right touch of flight switch board
Panel type display is positioned at the lower section of right liquid crystal display.
As a kind of preferred implementation of the present utility model, described CPCI calculates unit by the control meter that flies
Calculation machine, mission control computer, link monitoring computer, mission planning computer, record are fast regards computer
Form with information processing computer.
As a kind of preferred implementation of the present utility model, described left touch-screen display and right touch screen display
Show that device surrounding is both provided with hard button.
As a kind of preferred implementation of the present utility model, described task control cabinet, link switch board and fly
The metal keyboard of band trace ball it is fitted with on row switch board.
In this utility model: carried out modularization for flight monitoring cabinet, Mission Monitor cabinet, link monitoring cabinet
Design, connects cabinet by one group three and manipulates seat accordingly, can realize the control to a frame unmanned plane.
The software composition of ground control station includes that Flight Control Software, state of flight display software, load control
Software, loaded-up condition display software, record are fast regarding software, mission planning software, Target track displaying software, chain
Road monitoring software and protocol conversion software, altogether 9 software configuration items, as shown in Figure 3.
The major function of Flight Control Software is to realize the real-time control to aircraft platform, has track data pipe
Reason function, it is possible to realize the inquiry of way point information, change and inject.Telecommand is supported soft instruction, is firmly referred to
Order and three kinds of generating modes of car outer control.
The major function of state of flight display software is the telemetry by resolving aircraft platform state, obtains
The state of flight information of unmanned plane, then shows in the mode such as form, figure, thus realizes flight shape
The real-time function for monitoring of state information.
It is to realize the real-time control to payload platform that load controls the major function of software, support O-E Payload,
The multiple load such as digital camera and SAR.
The major function of loaded-up condition display software is the remote measurement number by receiving and parsing through payload platform state
According to, obtain the status information of payload platform, then show in the mode such as form, figure, thus realize
The real-time function for monitoring of loaded-up condition information.
The fast major function depending on software of record is to receive and record the initial data that unmanned plane passes down, including distant
Survey, remote control and view data, show in real time after view data is carried out decompression, and have
The function of data readback.
The major function of mission planning software is the requirement according to aerial mission, quickly generates executable task
Course line, makes the unmanned plane can be according to predetermined airline operation, it is ensured that unmanned plane performs effectiveness and the peace of task
Quan Xing.
The major function of Target track displaying software is to receive the telemetry parameter of unmanned plane during flying attitude and default course line
Information, carry out in two/three-dimensional visualization environment unmanned plane real-time flight simulation simulation, preset course line and
Practical flight flight path may be superimposed on and shows in numerical map background.
The major function of link monitoring software is to realize the real-time prison to data chain device and ground tracking equipment
Depending on and control.
The major function of protocol conversion software is to realize unmanned plane and the special observing and controlling agreement of load and general survey
Frame format conversion between control agreement so that the software of ground control station is no longer dependent on each model unmanned plane
Observing and controlling agreement, but use general observing and controlling agreement to be programmed and realize.
This utility model compared with prior art has the advantage that
Disclosed in this utility model, a kind of unmanned aerial vehicle controls work station, this ground control station and ground data
Terminal car, airborne data terminal coordinate, it is achieved that the command and control function to many types of unmanned plane and load；
Use General design, it is possible to effectively solve current various unmanned plane and the observing and controlling agreement disunity of payload platform
Problem.
Accompanying drawing explanation
Fig. 1 is the structural front view of a kind of detailed description of the invention of the present utility model；
Fig. 2 is the structure left view of a kind of detailed description of the invention of the present utility model；
Fig. 3 is the software composition signal that a kind of detailed description of the invention ground of the present utility model controls work station
Figure；
Fig. 4 is the software information stream signal that a kind of detailed description of the invention ground of the present utility model controls work station
Figure.
Description of reference numerals:
1: task control cabinet, 2: supporting leg, 3: link switch board, 4:CPCI calculate unit, and 5: exchange
Machine, 6: distribution box, 7: throttle lever, 8: flight switch board, 9: right touch-screen display, 10: right liquid
Crystal display screen, 11: speech talkback equipment, 12:UPS device, 13: left liquid crystal display, 14: left tactile
Touch panel type display, 15: control bar, 16: middle liquid crystal display, 17: middle touch-screen display, 18:KVM
Switch.
Detailed description of the invention
Below in conjunction with the accompanying drawings and embodiment describes this utility model detailed description of the invention:
It should be noted that the structure of signal, ratio, size etc. in this specification institute accompanying drawing, the most only in order to
Coordinate the content disclosed in description, understand for those skilled in the art and read, being not limited to
The enforceable qualifications of this utility model, the modification of any structure, the change of proportionate relationship or the tune of size
Whole, under not affecting effect that this utility model can be generated by and the purpose that can reach, all should still fall at this
In the range of technology contents disclosed in utility model obtains and can contain.
Meanwhile, in this specification cited as " on ", D score, "left", "right", " middle "
And the term of " " etc., it is merely convenient to understanding of narration, and is not used to limit this utility model and can implement
Scope, being altered or modified of its relativeness, without essence change technology contents under, when being also considered as this reality
With novel enforceable category.
As shown in Figure 1 to 4, it illustrates detailed description of the invention of the present utility model；As it can be seen, this
Disclosed in utility model, a kind of unmanned aerial vehicle controls work station, including task control cabinet 1, supporting leg 2, chain
Road switch board 3, CPCI calculate unit 4, switch 5, distribution box 6, throttle lever 7, flight switch board 8,
Right touch-screen display 9, right LCDs 10, speech talkback equipment 11, UPS device 12, left liquid crystal
Display 13, left touch-screen display 14, control bar 15, middle liquid crystal display 16, middle touch screen show
Device 17 and KVM switcher 18；Described link switch board 3 is arranged on the right side of task control cabinet 1, described
Flight switch board 8 is arranged on the right side of link switch board 3, described task control cabinet 1, link switch board 3
It is fitted with supporting leg 2, in described task control cabinet 1 and flight switch board 8 with the bottom of flight switch board 4
Being fitted with switch 5 and distribution box 6, two described left liquid crystal displays 13 are arranged on task control cabinet 1
In, two described left touch-screen displays 14 are arranged on the interior and left touch-screen display 14 of task control cabinet 1
It is positioned at the lower section of left liquid crystal display 13, described task control cabinet 1, link switch board 3 and flight switch board
It is fitted with throttle lever 7 on the table top of 8, controls bar 15 and KVM switcher 18, described CPCI computer
In group 4 is arranged on link switch board 3 and CPCI calculates unit 4 near the bottom surface of link switch board 3, institute
Stating touch-screen display 17 to be arranged in link switch board 3, described middle liquid crystal display 16 is arranged on chain
Interior and the middle liquid crystal display 16 of road switch board 3 is positioned at the top of middle touch-screen display 17, described voice pair
Say equipment 11 be arranged on link switch board 3 in and speech talkback equipment 11 be positioned at middle liquid crystal display 16
Top, in described UPS device 12 is arranged on link switch board 3 and UPS device 12 is positioned at speech talkback and sets
The top of standby 11, two described right liquid crystal displays 10 are arranged in flight switch board 8, two described right sides
Touch-screen display 9 is arranged on the interior and right touch-screen display 9 of flight switch board 8 and is positioned at right liquid crystal display
The lower section of 10.
Preferably, described CPCI calculates unit 4 by flight-control computer, mission control computer, chain
Road monitoring computer, mission planning computer, record are fast regards computer and information processing computer composition.
Preferably, described left touch-screen display 14 and right touch-screen display 9 surrounding be both provided with firmly by
Key.
In this utility model, ground control station uses ICP/IP protocol to realize the full networked of information transmission,
Remote measurement, remote control and image are all transmitted with network data frame, and wherein, telemetry and telecommand uses UDP multicast
Protocol transmission, image uses Transmission Control Protocol transmission.Fig. 4 gives the information of remote measurement, remote control and view data
Flow diagram.Wherein, Data-Link remote-control data and Data-Link telemetry are applicable to data chain device, other
Frame is all applicable to aircraft platform and payload platform, universal remote control data and general telemetry and refers to towards logical
With the Frame of observing and controlling agreement, special remote control data and special telemetry refer to towards unmanned plane and load special
Frame by observing and controlling agreement.
Above in conjunction with accompanying drawing, this utility model preferred implementation is explained in detail, but this utility model
It is not limited to above-mentioned embodiment, in the ken that those of ordinary skill in the art are possessed, it is also possible to
Make a variety of changes without departing from the premise of this utility model objective.
Many other can be made without departing from spirit and scope of the present utility model to change and remodeling.Should manage
Solving, this utility model is not limited to specific embodiment, and scope of the present utility model is limited by claims
Fixed.
Claims (4)
1. a unmanned aerial vehicle controls work station, it is characterised in that: include task control cabinet, supporting leg, chain
Road switch board, CPCI calculate unit, switch, distribution box, throttle lever, flight switch board, right touch screen
Display, right LCDs, speech talkback equipment, UPS device, left liquid crystal display, left touch screen display
Show device, control bar, middle liquid crystal display, middle touch-screen display and KVM switcher；Described link controls
Cabinet is arranged on the right side of task control cabinet, and described flight switch board is arranged on the right side of link switch board, described
The bottom of task control cabinet, link switch board and flight switch board is fitted with supporting leg, described task control cabinet
Be fitted with switch and distribution box in flight switch board, two described left liquid crystal displays are arranged on task
In switch board, in two described left touch-screen displays are arranged on task control cabinet and left touch-screen display position
In the lower section of left liquid crystal display, on the table top of described task control cabinet, link switch board and flight switch board
Being fitted with throttle lever, control bar and KVM switcher, described CPCI calculates unit and is arranged on link switch board
In and CPCI calculate unit near the bottom surface of link switch board, described middle touch-screen display is arranged on link control
In cabinet processed, described middle liquid crystal display is arranged on the interior and middle liquid crystal display of link switch board and is positioned at middle touch screen
The top of display, during described speech talkback equipment is arranged in link switch board and speech talkback equipment is positioned at
The top of liquid crystal display, described UPS device is arranged in link switch board and UPS device is positioned at voice pair
Say that the top of equipment, two described right liquid crystal displays are arranged in flight switch board, two described right touches
Panel type display is arranged on the interior and right touch-screen display of flight switch board and is positioned at the lower section of right liquid crystal display.
2. a kind of unmanned aerial vehicle as claimed in claim 1 controls work station, it is characterised in that: described CPCI
Calculate unit by flight-control computer, mission control computer, link monitoring computer, mission planning meter
Calculation machine, record are fast regards computer and information processing computer composition.
3. a kind of unmanned aerial vehicle as claimed in claim 1 controls work station, it is characterised in that: a described left side
Touch-screen display and right touch-screen display surrounding are both provided with hard button.
4. a kind of unmanned aerial vehicle as claimed in claim 1 controls work station, it is characterised in that: described
The metal keyboard of band trace ball it is fitted with on business switch board, link switch board and flight switch board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201620472547.6U CN205787907U (en) | 2016-05-23 | 2016-05-23 | A kind of unmanned aerial vehicle controls work station |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620472547.6U CN205787907U (en) | 2016-05-23 | 2016-05-23 | A kind of unmanned aerial vehicle controls work station |
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| CN205787907U true CN205787907U (en) | 2016-12-07 |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106406356A (en) * | 2016-12-13 | 2017-02-15 | 天津成周科技有限公司 | Control system for electronic-information-based unmanned aerial vehicle formation management and management method thereof |
| CN106707819A (en) * | 2017-01-20 | 2017-05-24 | 四方继保（武汉）软件有限公司 | Intelligent operation panel for unmanned ship and initialization operation method of intelligent operation panel for unmanned ship |
| CN107024937A (en) * | 2017-03-13 | 2017-08-08 | 武汉飞流智能技术有限公司 | The self-identifying of unmanned plane load and parameter Self Matching method and ground Adaptable System |
| CN107826261A (en) * | 2017-10-13 | 2018-03-23 | 南京涵曦月自动化科技有限公司 | A kind of multifunctional single rotor wing unmanned aerial vehicle control platform |
| CN109523193A (en) * | 2018-11-28 | 2019-03-26 | 中电科（德阳广汉）特种飞机系统工程有限公司 | Flight control and task management system, method, apparatus and readable storage medium storing program for executing |
| CN109841092A (en) * | 2019-01-28 | 2019-06-04 | 西安爱生技术集团公司 | A kind of unmanned aerial vehicle command and control system |
| CN110045663A (en) * | 2019-05-14 | 2019-07-23 | 山东蜂巢航空科技有限公司 | A kind of vehicle-mounted unmanned aerial vehicle ground control system |
| CN110232918A (en) * | 2019-05-22 | 2019-09-13 | 成都飞机工业（集团）有限责任公司 | A kind of UAV ground control station's speech control system and control method |
-
2016
- 2016-05-23 CN CN201620472547.6U patent/CN205787907U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106406356A (en) * | 2016-12-13 | 2017-02-15 | 天津成周科技有限公司 | Control system for electronic-information-based unmanned aerial vehicle formation management and management method thereof |
| CN106707819A (en) * | 2017-01-20 | 2017-05-24 | 四方继保（武汉）软件有限公司 | Intelligent operation panel for unmanned ship and initialization operation method of intelligent operation panel for unmanned ship |
| CN107024937A (en) * | 2017-03-13 | 2017-08-08 | 武汉飞流智能技术有限公司 | The self-identifying of unmanned plane load and parameter Self Matching method and ground Adaptable System |
| CN107826261A (en) * | 2017-10-13 | 2018-03-23 | 南京涵曦月自动化科技有限公司 | A kind of multifunctional single rotor wing unmanned aerial vehicle control platform |
| CN109523193A (en) * | 2018-11-28 | 2019-03-26 | 中电科（德阳广汉）特种飞机系统工程有限公司 | Flight control and task management system, method, apparatus and readable storage medium storing program for executing |
| CN109841092A (en) * | 2019-01-28 | 2019-06-04 | 西安爱生技术集团公司 | A kind of unmanned aerial vehicle command and control system |
| CN110045663A (en) * | 2019-05-14 | 2019-07-23 | 山东蜂巢航空科技有限公司 | A kind of vehicle-mounted unmanned aerial vehicle ground control system |
| CN110232918A (en) * | 2019-05-22 | 2019-09-13 | 成都飞机工业（集团）有限责任公司 | A kind of UAV ground control station's speech control system and control method |
| CN110232918B (en) * | 2019-05-22 | 2022-05-06 | 成都飞机工业（集团）有限责任公司 | Unmanned aerial vehicle ground control station voice control system and control method |
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