CN202694151U - Control terminal device for unmanned aircraft - Google Patents
Control terminal device for unmanned aircraft Download PDFInfo
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- CN202694151U CN202694151U CN 201120528133 CN201120528133U CN202694151U CN 202694151 U CN202694151 U CN 202694151U CN 201120528133 CN201120528133 CN 201120528133 CN 201120528133 U CN201120528133 U CN 201120528133U CN 202694151 U CN202694151 U CN 202694151U
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- unmanned vehicle
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Abstract
The utility model discloses a control terminal device for an unmanned aircraft. The control terminal device comprises a manual control panel, a tablet computer and a wireless data link transmission radio station. The manual control panel provides the function of controlling the flight of the aircraft in real time for an operator. The tablet computer is mainly responsible for displaying the comprehensive information and planning the flight mission. After a system starts to run, the flight state and the flight trajectory of the controlled aircraft and the main visual-angle flying vision are displayed in real time via a GPS positioning system and the wireless data link transmission radio station, for the convenience of the operator to contrast and observe in the remote control process. The utility model has the beneficial effects that display and manual control of the flight state and the flight trajectory of the aircraft are integrated, for the convenience of the operator to contrast and operate, so that a flight stabilizing and controlling system with relatively low cost is adopted to replace a relatively expensive self flight control system which is commonly used by unmanned aircraft systems; and meanwhile, a function of convenient and visual control assistance is provided to the maximum extent, simplifying the control difficulty.
Description
Technical field
The utility model designs a kind of operation control terminal device of unmanned vehicle, and the low side among the people that especially needs to control cost requires the operation unmanned vehicle.
Background technology
The mode of carrying out at present unmanned vehicle operation control in the unmanned vehicle field is mainly as follows:
GPS navigation device and self-driving are installed on the unmanned vehicle fly to control instrument, surface work staffing unmanned vehicle ground control station (generally being the portable outdoor computer), in the task planning stage, first define the course line of this aerial mission and corresponding operation behaviour in each section course line at the software terminal of controlling the station, form a complete flow of task, then by radio transmitting device the self-driving that flow of task is transferred to unmanned vehicle is flown to control on the instrument, self-driving flies to control instrument and then will control unmanned vehicle according to this part flow of task and execute the task.The shortcoming of this mode is mainly: it is high that self-driving flies to control the instrument cost, almost accounts for about 60% of whole system cost, greatly increased the cost of whole system, for equipment and the buying of applying unit increased certain difficulty.And it is not fairly obvious to compare manual control mode advantage in the advantage of carrying out general common low coverage among the people and use during task in short-term self-driving flight, on the contrary owing to the rising that has increased High Value Unit in tasks carrying front end unit and cause the windfall loss cost.
Summary of the invention
In order to solve existing unmanned vehicle control system high cost, inconvenience is used for the problem of low side operation among the people application scenario, the utility model provides a kind of operation control terminal system of unmanned vehicle, do not using expensive self-driving to fly to control under the prerequisite of instrument, control personnel for unmanned vehicle the to greatest extent convenient subsidiary function of controlling intuitively is provided, simplify and control difficulty, increase work efficiency, alleviate homework burden.
This utility model comprises a kind of for unmanned vehicle operation control terminal device, has operating rod with the flight of control unmanned vehicle, has display to show the unmanned vehicle state feedback information, communication between operation control terminal system and the unmanned vehicle realizes with the wireless data link transmission radio station, by introducing a flat computer control handle and display and wireless communication apparatus are integrated into a hand-held operation control terminal system, control and send to unmanned vehicle after instruction is processed by flat computer, the unmanned vehicle transmission of feedback information is processed by showing output by display to computer motherboard.This utility model is comprised of manual control panel, flat computer, wireless data link transmission radio station.Wherein, manual control panel provides the function of real time remote control aircraft flight for the control staff, and its button rocking bar design is similar with common model airplane remote controller, by general control staff is familiar with, is convenient to grasp and use.
The synthesis display flat computer is mainly undertaken the function that integrated information shows and aerial mission is planned, the control staff can use the aerial mission planning software to make this aerial mission plan thereon before aerial mission begins, and comprises the triggering setting of the setting of track chart, various operation behaviors, the mark of points for attention etc.After bringing into operation, system will rely on GPS positioning system and wireless data link transmission radio station to demonstrate in real time state of flight and track and the main perspective driving vision of controlled aircraft, make things convenient for the control staff when remotely piloted vehicle, to contrast and watch, aircraft is moved according to schedule.
The beneficial effects of the utility model are: because state of flight and the track display function of aircraft is integrated with manual control function, conveniently control personnel's control operations, therefore can fall the expensive self-driving flight control system that the unmanned vehicle system generally adopts by the lower flight augmentation control System Replacement of use cost, can provide convenience to greatest extent simultaneously and control intuitively subsidiary function, simplify and control difficulty, increase work efficiency, alleviate homework burden.
Description of drawings
The utility model is described in further detail below in conjunction with drawings and Examples.
Fig. 1 is principle schematic of the present utility model
Wherein:
1. left operating rod is used for carrying out the unmanned vehicle level and turns to control with forward-reverse;
2. right operating rod is used for carrying out unmanned vehicle and climbs and descend and the control of left and right sides translation;
3. wireless data link transmission radio station (data) receiving antenna is used for the reception of unmanned vehicle feedback states information;
4. touch display screen is used for demonstration and the feature operation of operation information and auxiliary monitor message and navigation map;
5. wireless data link transmission radio station (data) transmitting antenna is used for the output to the unmanned vehicle steering order;
6. Aerial Images receives the radio station, is used for receiving the Aerial Images of unmanned vehicle feedback, and auxiliary direction is controlled operation;
7. computer motherboard is the maincenter of control system, for the treatment of controlling instruction, processes and shows various supplementarys;
8. battery, the power supply when being used for outwork.
9. operating rod instruction acquisition conversion interface circuit is digital signal for the analog signal conversion that operating rod 1,2 pivot offset are produced, and is transferred to computer motherboard;
Fig. 2 is the structural drawing of first embodiment of the utility model
Wherein:
1. left operating rod, 2. right operating rod, 3. wireless data link transmission radio station (data) receiving antenna, 4. touch display screen, 5. wireless data link transmission radio station (data) emitting antenna, 6. wireless data link transmission radio station (image) receiving antenna, 8. battery compartment.
Fig. 3 is the use-pattern synoptic diagram of the embodiment among Fig. 2
Wherein:
10. unmanned vehicle operation control terminal device, 12. unmanned vehicle, 13. wireless data link transmission radio station (data), 14. flight augmentation control system, 15. wireless data link transmission radio station (image), 16. aerial cameras, the planning enroute chart that 17. touch display screens show, 18. the icon in representative the machine orientation that touch display screen shows, the 19.GPS positioning system.
Fig. 4 is the structural drawing of second embodiment of the present utility model
Wherein:
1.2. operating rod, 3. wireless data link transmission radio station receiving antenna (data), 4. touch display screen, 5. Aerial Images receiving antenna, 6. wireless data link transmission radio station transmitting antenna (image), 8. battery compartment.
Embodiment
In Fig. 1, left and right sides operating rod 1,2 is connected to operating rod instruction acquisition change-over circuit 9.The pot voltage signal that this circuit 9 is exported two operating rods carries out AD and converts digital signal to, and the angle of expression operating rod skew is passed through the data transmission port transmission again to computer motherboard 7.The steering order of operating rod output is transferred to wireless data link transmission radio station (data) transmitting antenna 5 again through Data Format Transform after being transferred to computer motherboard 7, by this antenna 5 steering order is wirelessly sent to aerial unmanned vehicle, the flight of control unmanned vehicle.Simultaneously aerial unmanned vehicle will be passed to ground under the flight of the machine and the running status, by wireless data link transmission radio station (data) receiving antenna 3 receiving data informations, receive image information by wireless data link transmission radio station (image) 6.The data message of passing back in the air and the image information that receive in real time all are transferred to computer motherboard 7, process through the data of computing machine, show by touch display screen 4 again.Show planning track chart, the machine state of flight at touch display screen 4, body each several part ruuning situation, aircraft aerial map are as information, with auxiliary operation hand control and assurance situation.Because the operation of unmanned vehicle is external field environment, therefore is furnished with battery 8 and carries out the outfield power supply.
In the embodiment shown in Figure 2, touch display screen 4 links to each other with hand-held housing part by rotating shaft, can flip an angle, and has made things convenient for the user to watch screen.Operating rod 1,2 design are similar to the rocking bar of model airplane remote controller, have made things convenient for the manipulator who accepted the model plane training to grasp rapidly operating handle.The wireless data link transmission radio station receives and transmitting antenna is connected on the casing by rotating shaft, can adjust angle according to operating position.
In embodiment use-pattern synoptic diagram shown in Figure 3, unmanned vehicle 12 is equiped with lower-cost flight augmentation control device 14, wireless data link transmission radio station (data) 13, aerial camera 16 and wireless data link transmission radio station (image) 15, gps antenna 19.Unmanned vehicle receives the steering order of ground operation control terminal example 11 by wireless data link transmission radio station 13, simultaneously the local state data message is sent to operation control terminal example 11 by radio station 13, the machine Aerial Images is sent to operation control terminal example 11 by radio station 15.Operation control terminal example 11 demonstrates planning track chart and the machine orientation at touch display screen, makes things convenient for the manipulator to control aircraft and draws close to default course line.
In the second embodiment shown in Figure 4, display screen 4 and operating rod 1,2 are incorporated on the compact housing, to obtain the small and exquisite advantage of being convenient to portable of profile.Operating rod 1,2 is controlled comfortable feel.
Embodiment recited above only is described preferred implementation of the present utility model; be not that design of the present utility model and scope are limited; do not breaking away under the utility model design concept prerequisite; various modification and improvement that those skilled in the art makes the technical solution of the utility model; all should fall into protection domain of the present utility model; the technology contents that the utility model is asked for protection all is documented in claims.
Claims (3)
1. one kind is used for unmanned vehicle operation control terminal device, has operating rod with the flight of control unmanned vehicle, has display to show the unmanned vehicle state feedback information, communication between operation control terminal system and the unmanned vehicle realizes with the wireless data link transmission radio station, it is characterized in that: by introducing a flat computer control handle and display and wireless communication apparatus are integrated into a hand-held operation control terminal system, control and send to unmanned vehicle after instruction is processed by flat computer, the unmanned vehicle transmission of feedback information is processed by showing output by display to computer motherboard.
2. according to claim 1 for unmanned vehicle operation control terminal device, it is characterized in that: planning track chart, flight state monitoring information, Aerial Images show all to be incorporated on the display that hand-held operation control terminal has and show output.
3. according to claim 1 for unmanned vehicle operation control terminal device, it is characterized in that: described control handle comprises two manual control lever, the output signal of manual control lever enters the flat computer mainboard and carries out the instruction dissection process, sends to unmanned vehicle by wireless communication apparatus again.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120528133 CN202694151U (en) | 2011-12-16 | 2011-12-16 | Control terminal device for unmanned aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120528133 CN202694151U (en) | 2011-12-16 | 2011-12-16 | Control terminal device for unmanned aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202694151U true CN202694151U (en) | 2013-01-23 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN 201120528133 Expired - Fee Related CN202694151U (en) | 2011-12-16 | 2011-12-16 | Control terminal device for unmanned aircraft |
Country Status (1)
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| CN (1) | CN202694151U (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102520730A (en) * | 2011-12-16 | 2012-06-27 | 新时代集团国防科技研究中心 | Realization method applied to unmanned vehicle control terminal |
| CN103345826A (en) * | 2013-07-05 | 2013-10-09 | 深圳市大疆创新科技有限公司 | Remote control terminal of unmanned flight vehicle, as well as flight auxiliary system and method of unmanned flight vehicle |
| CN103344250A (en) * | 2013-07-05 | 2013-10-09 | 深圳市大疆创新科技有限公司 | Flight assisting method and device of unmanned aerial vehicle |
| CN103365298A (en) * | 2013-07-05 | 2013-10-23 | 深圳市大疆创新科技有限公司 | Flight assisting system and method for unmanned aerial vehicle |
| WO2014198189A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Smart display remote control and flight control system |
| CN105388906A (en) * | 2015-11-30 | 2016-03-09 | 无锡觅睿恪科技有限公司 | Height detection remote control for unmanned aerial vehicle (UAV) |
| CN105425814A (en) * | 2015-11-24 | 2016-03-23 | 木牛（青岛）科技有限公司 | Control system and control method for unmanned plane |
| CN105446353A (en) * | 2015-11-30 | 2016-03-30 | 无锡觅睿恪科技有限公司 | Unmanned plane remote controller with built-in gyroscope |
| WO2016045018A1 (en) * | 2014-09-24 | 2016-03-31 | 深圳市大疆创新科技有限公司 | Remote controller, handle structure thereof, and control method for uav |
| CN105518371A (en) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Retaining device and remote controller using same |
| CN105518558A (en) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Method, device and system for processing flight mission |
| CN103942940B (en) * | 2014-04-02 | 2016-09-07 | 重庆翼动科技有限公司 | A kind of flight control |
| US9665345B2 (en) | 2014-07-29 | 2017-05-30 | Honeywell International Inc. | Flight deck multifunction control display unit with voice commands |
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2011
- 2011-12-16 CN CN 201120528133 patent/CN202694151U/en not_active Expired - Fee Related
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102520730A (en) * | 2011-12-16 | 2012-06-27 | 新时代集团国防科技研究中心 | Realization method applied to unmanned vehicle control terminal |
| WO2014198189A1 (en) * | 2013-06-13 | 2014-12-18 | Tian Yu | Smart display remote control and flight control system |
| CN103345826A (en) * | 2013-07-05 | 2013-10-09 | 深圳市大疆创新科技有限公司 | Remote control terminal of unmanned flight vehicle, as well as flight auxiliary system and method of unmanned flight vehicle |
| CN103344250A (en) * | 2013-07-05 | 2013-10-09 | 深圳市大疆创新科技有限公司 | Flight assisting method and device of unmanned aerial vehicle |
| CN103365298A (en) * | 2013-07-05 | 2013-10-23 | 深圳市大疆创新科技有限公司 | Flight assisting system and method for unmanned aerial vehicle |
| CN107256030A (en) * | 2013-07-05 | 2017-10-17 | 深圳市大疆创新科技有限公司 | Remote terminal, flight assisting system and the method for unmanned vehicle |
| CN107203219A (en) * | 2013-07-05 | 2017-09-26 | 深圳市大疆创新科技有限公司 | The flight assisting system and method for unmanned vehicle |
| CN107203219B (en) * | 2013-07-05 | 2020-10-23 | 深圳市大疆创新科技有限公司 | Flight assistance system and method for unmanned aerial vehicle |
| CN107065914A (en) * | 2013-07-05 | 2017-08-18 | 深圳市大疆创新科技有限公司 | The flight householder method and device of unmanned vehicle |
| CN103365298B (en) * | 2013-07-05 | 2017-06-20 | 深圳市大疆创新科技有限公司 | The flight assisting system and method for unmanned vehicle |
| CN107065914B (en) * | 2013-07-05 | 2020-04-28 | 深圳市大疆创新科技有限公司 | Flight assistance method and device for unmanned aerial vehicle |
| CN103942940B (en) * | 2014-04-02 | 2016-09-07 | 重庆翼动科技有限公司 | A kind of flight control |
| US9665345B2 (en) | 2014-07-29 | 2017-05-30 | Honeywell International Inc. | Flight deck multifunction control display unit with voice commands |
| USRE49067E1 (en) | 2014-07-29 | 2022-05-10 | Honeywell International Inc. | Flight deck multifunction control display unit |
| CN105612468A (en) * | 2014-09-24 | 2016-05-25 | 深圳市大疆创新科技有限公司 | Remote controller, handle structure thereof, and control method for uav |
| US10675551B2 (en) | 2014-09-24 | 2020-06-09 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
| WO2016045018A1 (en) * | 2014-09-24 | 2016-03-31 | 深圳市大疆创新科技有限公司 | Remote controller, handle structure thereof, and control method for uav |
| US11179650B2 (en) | 2014-09-24 | 2021-11-23 | SZ DJI Technology Co., Ltd. | Remote controller and handle structure thereof, and method for controlling a UAV |
| CN105518558B (en) * | 2014-09-30 | 2018-02-02 | 深圳市大疆创新科技有限公司 | A kind of aerial mission processing method, apparatus and system |
| US10222794B2 (en) | 2014-09-30 | 2019-03-05 | SZ DJI Technology Co., Ltd. | Remote controller using retaining device |
| CN105518558A (en) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Method, device and system for processing flight mission |
| CN105518371A (en) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Retaining device and remote controller using same |
| US11041737B2 (en) | 2014-09-30 | 2021-06-22 | SZ DJI Technology Co., Ltd. | Method, device and system for processing a flight task |
| US11566915B2 (en) | 2014-09-30 | 2023-01-31 | SZ DJI Technology Co., Ltd. | Method, device and system for processing a flight task |
| CN105425814A (en) * | 2015-11-24 | 2016-03-23 | 木牛（青岛）科技有限公司 | Control system and control method for unmanned plane |
| CN105446353A (en) * | 2015-11-30 | 2016-03-30 | 无锡觅睿恪科技有限公司 | Unmanned plane remote controller with built-in gyroscope |
| CN105388906A (en) * | 2015-11-30 | 2016-03-09 | 无锡觅睿恪科技有限公司 | Height detection remote control for unmanned aerial vehicle (UAV) |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
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Address after: 100088 the 6 floor, seat B of the conference center, No. 6, Huayuan Road, Haidian District, Beijing Patentee after: Poly national defence science and Technology Research Center Co Ltd Address before: 100088 the 6 floor, seat B of the conference center, No. 6, Huayuan Road, Haidian District, Beijing Patentee before: Defense Technology Research Center of China New Era Group Cororation |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130123 Termination date: 20191216 |