CN103076810A - Portable miniature ground mobile workstation for unmanned aerial vehicle - Google Patents
Portable miniature ground mobile workstation for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN103076810A CN103076810A CN2013100148644A CN201310014864A CN103076810A CN 103076810 A CN103076810 A CN 103076810A CN 2013100148644 A CN2013100148644 A CN 2013100148644A CN 201310014864 A CN201310014864 A CN 201310014864A CN 103076810 A CN103076810 A CN 103076810A
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- mobile workstation
- flight
- industrial computer
- 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.)
- Pending
Links
Images
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a portable miniature ground mobile workstation for an unmanned aerial vehicle and aims at accomplishing the task planning of the unmanned aerial vehicle, displaying the position and the flight path of the unmanned aerial vehicle on an electronic map in real time, performing the functions of transmitting, displaying and processing the flight state data of the unmanned aerial vehicle in real time and ensuring the flight accuracy and safety of the unmanned aerial vehicle. The workstation consists of an upper box body, a display screen, a switch, a touchpad, a lower box body, an elastic clasp, a handle, a radio modem, a rocker rod, a keypad, a butterfly hinge, a power supply module and an industrial computer. With the mobile workstation disclosed by the invention, the work of receiving, monitoring and displaying remotely measured data of the unmanned aerial vehicle in real time and sending remote control data can be accomplished by one person.
Description
Technical field
The present invention relates to a kind of workstation, particularly a kind of portable small-sized unmanned aerial vehicle mobile workstation.
Background technology
Along with the development of science and technology, unmanned plane obtains broad research and development in countries in the world, all has important using value at military, civilian and scientific research three aspects:.Militarily can be used for investigation, supervision, communication repeating, electronic countermeasure, firepower guidance, combat success assessment, harassing and wrecking, temptation, over the ground (sea) attack, target simulation and early warning etc.; On civilian, can be used for the supervision of geodetic surveying, urban environment detection, earth resources survey and forest fire protection, agriculture exploration, traffic, civil navigation, environmental protection, border patrol and control, disaster and rescue etc.; Aspect scientific research, can be used for atmospheric research, meteorological observation, to the sampling of examining biochemical contaminated area and the verification experimental verification of monitoring, new technology and equipment and new aircraft etc.The surface work station is core and the soul of SUAV (small unmanned aerial vehicle), it relates to the multiple technologies such as wireless transmission, Long-distance Control and mission planning, major function is flight course and the tasks carrying situation of monitoring unmanned plane, and it is a Real-time Collection and analyzes the comprehensive ground monitoring system that the functions such as telemetry, not timing transmission telecommand, demonstration state of flight are incorporated into one.
The surface work station of at present existing associated portable SUAV (small unmanned aerial vehicle) mainly contains following problem and shortage:
(1) adopt split type design, by the data communication unit, process computer, Display control computer and Digiplex etc. partly form, and volume is larger, and portable is relatively poor, and power consumption is large.
(2) need two bit manipulation personnel coordinated manipulations, the process computer of a bit manipulation workstation is used for receiving the telemetry that unmanned plane sends; Another one operate wireless telepilot, the transmitting portion telecommand.The fly operating personnel of Digiplex of control of unmanned plane are wanted to know that the state of flight of unmanned plane can only be by the passing on of process computer operating personnel, very inconvenient.
(3) process computer and Display control computer adopt the mechanical type hard disk, and shake-proof ability is poor, and keyboard and touch pad do not adopt water proof and dust proof to process, and adaptive capacity to environment is poor.
(4) do not adopt electronic chart to show the state of flight of unmanned plane, be unfavorable for observing the particular location of unmanned plane.
Summary of the invention
In order to address the above problem, the present invention proposes a kind of portable small-sized unmanned aerial vehicle mobile workstation, this workstation only needs operating personnel just can finish the flight control of unmanned plane, the reception of unmanned plane telemetry detects, the workstation portable is good, volume is little, lightweight, the data receiver demonstration is real-time, has improved SUAV (small unmanned aerial vehicle) flight control convenience and real-time.
For achieving the above object, the present invention adopts following technical scheme:
A kind of portable small-sized unmanned aerial vehicle mobile workstation is comprised of upper box, display screen, switch, touch pad, lower box, Spring Card, handle, data radio station, rocking bar, keyboard, butterfly hinge, power module and industrial computer; Described upper box and lower box trailing edge are by described butterfly hinge link, and leading edge links to each other by described Spring Card; Described handle connects firmly on described lower box.
Described data radio station connects described industrial computer, swap data by the RS232 data line.
Described rocking bar connects industrial computer by USB interface.
Described display screen adopts four split screens to show: the upper left quarter zone is SUAV (small unmanned aerial vehicle) flight map area; The upper right quarter zone is SUAV (small unmanned aerial vehicle) state of flight district; The right lower quadrant zone is SUAV (small unmanned aerial vehicle) flight state of a control district; The lower left quarter zone is the system setting area.
Described industrial computer uses solid state hard disc.
Described touch pad, keyboard and industrial computer all adopt the water proof and dust proof design.
The software agent framework comprises data communication module based on the Labview programmed environment, monitoring module, and flight control module and data are preserved four modules such as module.
Adopt electronic chart to show in real time position and the flight path of unmanned plane.
Compared with prior art, the present invention has advantages of following outstanding:
(1) adopt integrated design philosophy, greatly reduced the volume and weight of workstation, portable performance is good.
(2) only need bit manipulation personnel just can operate whole mobile workstation, saved human resources, simplified simultaneously operation.
(3) adopt keyboard, the touch pad of solid state hard disc and water proof and dust proof, can better adapt to the demand of field work.
(4) adopt electronic chart, can not only intuitively obtain the positional information of unmanned plane region, can also obtain unmanned plane surrounding enviroment situation, improved the reliability of unmanned plane during flying.
Description of drawings
Fig. 1 is outside drawing of the present invention.
Fig. 2 is rear view of the present invention.
Fig. 3 is system framework figure of the present invention.
Fig. 4 is workflow diagram of the present invention.
Embodiment
Understand and enforcement the present invention for the ease of those skilled in the art, the present invention is described in further detail below in conjunction with the drawings and the specific embodiments.
Such as Fig. 1, Fig. 2 and shown in Figure 3, a kind of portable small-sized unmanned aerial vehicle mobile workstation is comprised of upper box 1, display screen 2, switch 3, touch pad 4, lower box 5, Spring Card 6, handle 7, data radio station 8, rocking bar 9, keyboard 10, butterfly hinge 11, power module 12 and industrial computer 13; Described upper box 1 and lower box 5 trailing edges are by described butterfly hinge 11 links, and leading edge links to each other by described Spring Card 6; Described handle 7 connects firmly on described lower box 5.
Described data radio station 8 is selected the 9XStream(900MHz of U.S. XStream company) the type data radio station, connect described industrial computer 13, swap data by the RS232 data line.
Described rocking bar 9 connects industrial computer 13 by USB interface.
Display screen selects 10.1 inches IPS LCD LG firmly to shield, and adopts four split screens to show: the upper left quarter zone is SUAV (small unmanned aerial vehicle) flight map area; The upper right quarter zone is SUAV (small unmanned aerial vehicle) state of flight district; The right lower quadrant zone is SUAV (small unmanned aerial vehicle) flight state of a control district; The lower left quarter zone is the system setting area.
The flight map area adopts the Google Earth electronic chart integrate network technology, the communication technology, GIS technology, utilizes longitude, latitude and elevation information to determine the particular location of SUAV (small unmanned aerial vehicle), shows flight path that it is predetermined and current flight path.Can the predetermined flight path of online modification by clicking the flight map, amended flight path information exchange is crossed data communication module and is sent the airborne flight control system of SUAV (small unmanned aerial vehicle) to.
The state of flight district adopts special-purpose instrument interface control design virtual instrument, the state of flight information that shows SUAV (small unmanned aerial vehicle), comprise flight attitude (crab angle, the angle of pitch and roll angle), velocity information (air speed, GPS ground velocity), engine speed, the steering wheel position, airborne flight control system supply voltage, flight time and distance objective point distance etc.
Flight state of a control district shows PWM value and the current control surface deflection information of SUAV (small unmanned aerial vehicle) of driftage, pitching, three control channels of lift-over.The demonstration of PWM value comprises automatic control PWM and manual PWM, if PWM value overrun gives alarm and shows.
The setting of system's setting area completion system function.
The SSD solid state hard disc that described industrial computer 13 adopts is selected 2.5 inches SSD solid state hard discs of Samsung 64G SATA3.
Described touch pad 4, keyboard 10 and industrial computer 13 all adopt the water proof and dust proof design.
The software agent framework comprises data communication module based on the Labview programmed environment, monitoring module, and flight control module and data are preserved four modules such as module.
As shown in Figure 4, the transmission of the reception of telemetry and remote-control data is mainly realized by following step:
Step 1: start, open monitoring software, system is carried out initialization, finish program initialization and serial ports initialization.
Step 2: by data radio station, utilize data communication module to receive the telemetry that SUAV (small unmanned aerial vehicle) passes down, according to predetermined data layout it is decoded.
Step 3: the timer counting, in data memory module, every telemetry of 20ms storage, preserve with the form of Microsoft Excel.
Step 4: every 100ms, the telemetry that data communication module is received gives the split screen demonstration by monitoring module.The upper left quarter zone is SUAV (small unmanned aerial vehicle) flight map area; The upper right quarter zone is SUAV (small unmanned aerial vehicle) state of flight district; The right lower quadrant zone is SUAV (small unmanned aerial vehicle) flight state of a control district; The lower left quarter zone is the system setting area.
Step 5: when telemetry needed playback, the telemetry in the calling data memory module gave split screen by monitoring module and shows.
Step 6: utilize rocking bar and instruction dish, send continuous control command, discrete control command to the flight control module, utilize data communication module by data radio station telecommand to be sent to the airborne flight control system of SUAV (small unmanned aerial vehicle).
Step 7: finish shutdown.
Claims (6)
1. portable small-sized unmanned aerial vehicle mobile workstation, it is characterized in that, formed by upper box (1), display screen (2), switch (3), touch pad (4), lower box (5), Spring Card (6), handle (7), data radio station (8), rocking bar (9), keyboard (10), butterfly hinge (11), power module (12) and industrial computer (13); Described upper box (1) and lower box (5) trailing edge are by described butterfly hinge (11) link, and leading edge links to each other by described Spring Card (6); Described handle (7) connects firmly on described lower box (5).
2. portable small-sized unmanned aerial vehicle mobile workstation according to claim 1 is characterized in that, described data radio station (8) connects described industrial computer (13), swap data by the RS232 data line.
3. portable small-sized unmanned aerial vehicle mobile workstation according to claim 1 is characterized in that, described rocking bar (9) connects industrial computer (13), swap data by USB interface.
4. portable small-sized unmanned aerial vehicle mobile workstation according to claim 1 is characterized in that, described display screen (2) adopts four split screens to show: the upper left quarter zone is SUAV (small unmanned aerial vehicle) flight map area; The upper right quarter zone is SUAV (small unmanned aerial vehicle) state of flight district; The right lower quadrant zone is SUAV (small unmanned aerial vehicle) flight state of a control district; The lower left quarter zone is the system setting area.
5. portable small-sized unmanned aerial vehicle mobile workstation according to claim 1 is characterized in that, described industrial computer (13) uses solid state hard disc.
6. portable small-sized unmanned aerial vehicle mobile workstation according to claim 1 is characterized in that, described touch pad (4), keyboard (10) and industrial computer (13) all adopt the water proof and dust proof design.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2013100148644A CN103076810A (en) | 2013-01-16 | 2013-01-16 | Portable miniature ground mobile workstation for unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2013100148644A CN103076810A (en) | 2013-01-16 | 2013-01-16 | Portable miniature ground mobile workstation for unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
CN103076810A true CN103076810A (en) | 2013-05-01 |
Family
ID=48153377
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2013100148644A Pending CN103076810A (en) | 2013-01-16 | 2013-01-16 | Portable miniature ground mobile workstation for unmanned aerial vehicle |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103076810A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103529718A (en) * | 2013-09-24 | 2014-01-22 | 安徽泽众安全科技有限公司 | Ground monitoring control system for unmanned aerial vehicle |
CN104977939A (en) * | 2015-07-10 | 2015-10-14 | 江苏首控制造技术有限公司 | Multifunctional portable earth station controller for unmanned plane |
CN105513433A (en) * | 2016-01-19 | 2016-04-20 | 清华大学合肥公共安全研究院 | Ground control station based on airborne system of unmanned aerial vehicle |
CN105704462A (en) * | 2016-04-15 | 2016-06-22 | 中广华芯科技有限公司 | Device for supervising flying of unmanned plane |
CN106197380A (en) * | 2016-09-04 | 2016-12-07 | 南京理工大学 | Aquatic vegetation monitoring method based on unmanned plane and system |
CN106879083A (en) * | 2017-02-28 | 2017-06-20 | 四方继保(武汉)软件有限公司 | Unmanned boat portable base station |
CN107544545A (en) * | 2017-10-13 | 2018-01-05 | 南京涵曦月自动化科技有限公司 | A kind of control platform of detectable unmanned plane state |
CN109644233A (en) * | 2017-02-24 | 2019-04-16 | 深圳市大疆创新科技有限公司 | More head assemblies |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080215192A1 (en) * | 2004-12-16 | 2008-09-04 | Hardman Brian T | Interactive device for legacy cockpit environments |
EP1842030B1 (en) * | 2005-01-07 | 2009-11-11 | Raytheon Company | Programmable cockpit upgrade system |
CN101738608A (en) * | 2009-12-11 | 2010-06-16 | 北京航空航天大学 | Telemetry information comprehensive treatment system of unmanned plane and compressive treatment display method thereof |
CN201622703U (en) * | 2009-10-30 | 2010-11-03 | 北京航空航天大学 | Earth station layout of unmanned aerial vehicle |
CN102081159A (en) * | 2009-11-30 | 2011-06-01 | 北京天宇数字城市科技有限公司 | Special work station for receiving and processing aerial remote sensing underground data of portable unmanned aerial vehicle |
CN102193559A (en) * | 2011-04-06 | 2011-09-21 | 嘉兴电力局 | Ground station remote control device of unmanned vehicle |
CN102591346A (en) * | 2011-12-05 | 2012-07-18 | 大连理工大学 | Small-size handheld ground monitoring system for unmanned aerial vehicle |
CN102774505A (en) * | 2012-07-16 | 2012-11-14 | 北京航空航天大学 | Ground station of universalized configurable unmanned aerial vehicle |
-
2013
- 2013-01-16 CN CN2013100148644A patent/CN103076810A/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080215192A1 (en) * | 2004-12-16 | 2008-09-04 | Hardman Brian T | Interactive device for legacy cockpit environments |
EP1842030B1 (en) * | 2005-01-07 | 2009-11-11 | Raytheon Company | Programmable cockpit upgrade system |
CN201622703U (en) * | 2009-10-30 | 2010-11-03 | 北京航空航天大学 | Earth station layout of unmanned aerial vehicle |
CN102081159A (en) * | 2009-11-30 | 2011-06-01 | 北京天宇数字城市科技有限公司 | Special work station for receiving and processing aerial remote sensing underground data of portable unmanned aerial vehicle |
CN101738608A (en) * | 2009-12-11 | 2010-06-16 | 北京航空航天大学 | Telemetry information comprehensive treatment system of unmanned plane and compressive treatment display method thereof |
CN102193559A (en) * | 2011-04-06 | 2011-09-21 | 嘉兴电力局 | Ground station remote control device of unmanned vehicle |
CN102591346A (en) * | 2011-12-05 | 2012-07-18 | 大连理工大学 | Small-size handheld ground monitoring system for unmanned aerial vehicle |
CN102774505A (en) * | 2012-07-16 | 2012-11-14 | 北京航空航天大学 | Ground station of universalized configurable unmanned aerial vehicle |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103529718A (en) * | 2013-09-24 | 2014-01-22 | 安徽泽众安全科技有限公司 | Ground monitoring control system for unmanned aerial vehicle |
CN104977939A (en) * | 2015-07-10 | 2015-10-14 | 江苏首控制造技术有限公司 | Multifunctional portable earth station controller for unmanned plane |
CN105513433A (en) * | 2016-01-19 | 2016-04-20 | 清华大学合肥公共安全研究院 | Ground control station based on airborne system of unmanned aerial vehicle |
CN105704462A (en) * | 2016-04-15 | 2016-06-22 | 中广华芯科技有限公司 | Device for supervising flying of unmanned plane |
CN106197380A (en) * | 2016-09-04 | 2016-12-07 | 南京理工大学 | Aquatic vegetation monitoring method based on unmanned plane and system |
CN109644233A (en) * | 2017-02-24 | 2019-04-16 | 深圳市大疆创新科技有限公司 | More head assemblies |
US11233943B2 (en) | 2017-02-24 | 2022-01-25 | SZ DJI Technology Co., Ltd. | Multi-gimbal assembly |
CN106879083A (en) * | 2017-02-28 | 2017-06-20 | 四方继保(武汉)软件有限公司 | Unmanned boat portable base station |
CN107544545A (en) * | 2017-10-13 | 2018-01-05 | 南京涵曦月自动化科技有限公司 | A kind of control platform of detectable unmanned plane state |
CN107544545B (en) * | 2017-10-13 | 2019-01-11 | 南京利剑无人机科技有限公司 | A kind of control platform of detectable drone status |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103076810A (en) | Portable miniature ground mobile workstation for unmanned aerial vehicle | |
CN104808675B (en) | Body-sensing flight control system and terminal device based on intelligent terminal | |
CN104808682B (en) | Small-sized rotor wing unmanned aerial vehicle automatic obstacle avoiding flight control method | |
CN203773355U (en) | Three-dimensional multi-image layer type unmanned aerial vehicle real-time positioning monitoring device | |
CN100568143C (en) | A kind of middle-size and small-size no-manned machine reclaiming positioning apparatus | |
CN103823028B (en) | Stationary pollution source flue gas emission mobile monitoring system and method based on unmanned aerial vehicle | |
Liu et al. | HAWK: An unmanned mini-helicopter-based aerial wireless kit for localization | |
CN207133659U (en) | A kind of unmanned vehicle tele-control system | |
CN102591346A (en) | Small-size handheld ground monitoring system for unmanned aerial vehicle | |
CN203405206U (en) | Panoramic image unmanned aerial vehicle acquisition system | |
CN203376646U (en) | Low-altitude remote sensing monitoring system based on combination of 3S technology and unmanned aerial vehicle | |
CN204948365U (en) | A kind of LTE base station three-dimensional planning of remote control, reconnaissance and survey system | |
CN105334861A (en) | Unmanned plane flight control module, unmanned plane flight control system and unmanned plane | |
CN105807779A (en) | Flight control system and method for unmanned aerial vehicle | |
CN105973230B (en) | A kind of double unmanned plane collaborative perceptions and planing method | |
CN102654940A (en) | Traffic information acquisition system based on unmanned aerial vehicle and processing method of traffic information acquisition system | |
CN105892476A (en) | Control method and control terminal of aircraft | |
CN205050404U (en) | Flight simulation training system based on model airplane | |
CN201876969U (en) | Early warning device for forest fire prevention unmanned aerial vehicle | |
CN104316900B (en) | Aerial radio monitoring intelligent robot | |
CN108965124A (en) | A kind of unmanned aerial vehicle control system | |
CN104316901B (en) | For the aerial intelligent robot of radio monitoring | |
CN104316899B (en) | A kind of on-air radio pyroelectric monitor intelligent robot | |
CN107544533A (en) | Multifunctional portable micro unmanned aerial vehicle system | |
CN106184781B (en) | Trainer aircraft redundance man-machine interactive system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130501 |