CN202331208U - Ground unmanned helicopter control system applied to power transmission line inspection - Google Patents
Ground unmanned helicopter control system applied to power transmission line inspection Download PDFInfo
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- CN202331208U CN202331208U CN 201120479301 CN201120479301U CN202331208U CN 202331208 U CN202331208 U CN 202331208U CN 201120479301 CN201120479301 CN 201120479301 CN 201120479301 U CN201120479301 U CN 201120479301U CN 202331208 U CN202331208 U CN 202331208U
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- control system
- unmanned helicopter
- core computer
- transmission line
- acquisition unit
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Abstract
The utility model relates to a ground unmanned helicopter control system applied to power transmission line inspection. The ground unmanned helicopter control system is of a box structure, and the opened box is divided into an upper panel and a lower panel; a liquid crystal display A is mounted on the upper panel; a core computer, a video acquisition unit, a data acquisition unit, a power management unit and a wireless data transmission unit are mounted on the lower part of the lower panel, the core computer is connected with the video acquisition unit, the data acquisition unit, the power management unit and the wireless data transmission unit, and the wireless data transmission unit communicates with and is connected with a flight control system of an unmanned helicopter; the lower panel is provided with a liquid crystal display B, a keyboard, a track ball and communication interfaces, and liftable remote control sticks are arranged to the left and right of the liquid crystal display B as well, and are connected with the core computer through the data acquisition unit; and the core computer is respectively connected with the liquid crystal display A, the liquid crystal display B, the keyboard and the track ball. Since the ground unmanned helicopter control system is of the box structure, when the ground unmanned helicopter control system is not used, the box cover can be closed, and therefore the ground unmanned helicopter control system has a rain-proofing function; because the ground unmanned helicopter control system is provided with a FreeWave wireless transmission module, the transmission distance can reach 20 kilometers at most; since the two liquid crystal displays are mounted on the ground unmanned helicopter control system, the display area is enlarged, and thereby a user can conveniently view various information sent back by the unmanned helicopter.
Description
Technical field
The utility model relates to a kind of depopulated helicopter ground control system of using towards polling transmission line, specifically a kind of unmanned plane is carried out ground control device.
Background technology
This product belongs to the hardware platform that Flight Control Software moved of the polling transmission line depopulated helicopter that Shenyang robotization research institute of the Chinese Academy of Sciences developed, and this control box can connect depopulated helicopter through the wireless transmission radio station.Various attributes to depopulated helicopter are configured, and control unmanned plane and airborne equipment carry out various operations.Control box combines depopulated helicopter Ground Control software can make depopulated helicopter carry out accurate flying and to carry out semi-automatic flight through rocking bar control unmanned plane and airborne equipment according to the coordinate points on the map.
At present, domestic still do not have perfect, the polling transmission line unmanned plane of highly integrating and the controller of airborne equipment.For filling up this domestic blank, this UAV control case is intended to the control with unmanned plane and load, power management, and unmanned plane common functions such as video demonstration are entirely integrated in the system, accomplish that the height of system is integrated, and the control of unmanned plane is oversimplified, and are integrated.
Depopulated helicopter Ground Control case is connected with the flight control system of depopulated helicopter through the data transmission radio station, can send instruction and give the UAV control system, has rich in natural resources and system interface, can adapt to various unmanned plane Development of Software.
The utility model content
At present, domestic still do not have perfect, the polling transmission line unmanned plane of highly integrating and the opertaing device of airborne equipment.For filling up this domestic blank, to the Development characteristics of modern UAV control system, can be with the control of unmanned plane; Map location is browsed, airborne airborne equipment control, and video tour is entirely integrated in the system; Accomplish the height integration of system, the control of unmanned plane is oversimplified, integrated.
The utility model for realizing the technical scheme that above-mentioned purpose adopted is: towards the depopulated helicopter ground control system that polling transmission line is used, said ground control system is a body structure, and the casing of opening is divided into top panel and lower panel;
Top panel is equipped with LCD A;
Core computer and the video collector, data acquisition unit, power supervisor, the radio data-transmission equipment that are connected with the core computer are equipped with in the lower panel bottom, and said radio data-transmission equipment is connected with the flight control system communication of depopulated helicopter;
Be coated with LCD B, keyboard, trace ball and each communication interface on the lower panel, LCD B right ends also is furnished with liftable remote-control lever, links to each other with the core computer through data acquisition unit;
Said LCD A, LCD B, keyboard and trace ball are connected with the core computer respectively.
Said remote-control lever is four triple bond remote-control levers of technical grade.
Said video collector and data acquisition unit are two PCI integrated circuit boards that are integrated in the core computer.
Said data acquisition unit is the collector of an analog to digital signal, gathers the simulating signal of 32 tunnel inputs with single ended mode, and is translated into 16 digital signal confession core computer identification.
Said radio data-transmission equipment adopts the 900MHz wireless data transfer module, and maximum bandwidth is 115200bps, the 12V power voltage supply.
Said keyboard is connected with the core computer through USB interface with trace ball.
It is whole device power supply that said power supervisor converts the 220V alternating current into the 12V direct current, also has the 9AH lead accumulator as standby power supply.
The utlity model has following advantage:
1. the utility model is a body structure, and when not using, the case lid that closes has rainproof function;
2. be equipped with the FreeWave wireless transport module, transmission range can reach 20 kilometers at most;
3. two LCDs are housed, increase display area, make things convenient for the user to observe various unmanned plane back informations;
4. four triple bond remote-control levers of two technical grades make things convenient for the user to control aircraft and various airborne equipment about being furnished with;
5. built-in reserve battery has outage and overload protection breakpoint in use, does not influence user's operation;
6. abundant interface and pilot lamp are arranged on the lower panel, be user-friendly to, and can observe the body power status at any time.
Description of drawings
Fig. 1 is the utility model block diagram of system.
Embodiment
Below in conjunction with accompanying drawing and embodiment the utility model is done further detailed description.
As shown in Figure 1, the utility model is a body structure, and the casing of opening is divided into top panel and lower panel; Top panel is equipped with LCD A; Core computer and the video collector, data acquisition unit, power supervisor, the radio data-transmission equipment that are connected with the core computer are equipped with in the lower panel bottom, and said radio data-transmission equipment is connected with the flight control system communication of depopulated helicopter; Be coated with LCD B, keyboard, trace ball and each communication interface on the lower panel, LCD B right ends also is furnished with liftable remote-control lever, links to each other with the core computer through data acquisition unit; Said LCD A, LCD B, keyboard and trace ball are connected with the core computer respectively.
The core computer is connected through the patchcord of a Dvi one-to-two with two LCDs; Wherein a LCD directly is connected with computer with the VGA interface after telling; A LCD in addition is owing to lack the HDMI interface; So after need its signal being become the VGA signal by the HDMI conversion of signals with converter, again the VGA signal is sent in the LCD.
Video collector can provide the video acquisition passage of two high speeds, and this device only uses one of them passage.Collection jack on the panel directly is connected on the video collector through a video acquisition line.
Data acquisition unit is the collector of an analog to digital signal, and it can gather the simulating signal of 32 tunnel inputs with single ended mode, and is translated into 16 digital signal and discerns for computer.Used 14 tunnel collection of simulant signal passage to discern the remote-control lever current states in this device altogether.
About two remote-control levers respond to 4 positions that axle is present through 4 swept resistances respectively, the 5V of distribution power supply board and is on the ground received at the two ends of these swept resistances respectively.Output terminal in the middle of the remote-control lever is integrated into the winding displacement port of one 37 pin on the distribution power supply board, receive through winding displacement on the analog signal collector of computer.Through this collector, be that the digital signal of computer-readable is handled with the analog signal conversion of remote control rod output.
Power supervisor also has another reserve battery input except the 220V input.If the power supply of 220V is sudden power in use, then this moment, power supply can continue from reserve battery, to adopt electric continual supply total system.Reserve battery can be through the charging jack on the panel, and the charger of specially joining with equipment charges, and after charger inserts on the panel, the power supply knob of white is forwarded on the position of charging, after the pilot lamp on the charger becomes redness, begins the charging for system.After battery was full of, indication etc. became green.
The man-machine interaction of this device partly is that a keyboard is arranged, and trace ball is formed.Keyboard and trace ball all are USB interface.The operation of operation of this keyboard and common computer keyboard has no difference.Trace ball on the panel has substituted the function of computer mouse, the trace ball on the rotary panel, and mouse pointer moves to respective direction at once.
Prepackage unmanned aerial vehicle war Control Software, may command unmanned plane during flying track and various airborne equipment in this UAV control case.
Claims (7)
1. a depopulated helicopter ground control system of using towards polling transmission line is characterized in that said ground control system is a body structure, and the casing of opening is divided into top panel and lower panel;
Top panel is equipped with LCD A;
Core computer and the video collector, data acquisition unit, power supervisor, the radio data-transmission equipment that are connected with the core computer are equipped with in the lower panel bottom, and said radio data-transmission equipment is connected with the flight control system communication of depopulated helicopter;
Be coated with LCD B, keyboard, trace ball and each communication interface on the lower panel, LCD B right ends also is furnished with liftable remote-control lever, links to each other with the core computer through data acquisition unit;
Said LCD A, LCD B, keyboard and trace ball are connected with the core computer respectively.
2. the depopulated helicopter ground control system of using towards polling transmission line according to claim 1 is characterized in that said remote-control lever is four triple bond remote-control levers of technical grade.
3. the depopulated helicopter ground control system of using towards polling transmission line according to claim 1 is characterized in that said video collector and data acquisition unit are two PCI integrated circuit boards that are integrated in the core computer.
4. according to claim 1 or the 3 described depopulated helicopter ground control systems of using towards polling transmission line; It is characterized in that; Said data acquisition unit is the collector of an analog to digital signal; Gather the simulating signal of 32 tunnel inputs with single ended mode, and be translated into 16 digital signal confession core computer identification.
5. the depopulated helicopter ground control system of using towards polling transmission line according to claim 1 is characterized in that said radio data-transmission equipment adopts the 900MHz wireless data transfer module, and maximum bandwidth is 115200bps, the 12V power voltage supply.
6. the depopulated helicopter ground control system of using towards polling transmission line according to claim 1 is characterized in that said keyboard is connected with the core computer through USB interface with trace ball.
7. the depopulated helicopter ground control system of using towards polling transmission line according to claim 1; It is characterized in that; It is whole device power supply that said power supervisor converts the 220V alternating current into the 12V direct current, also has the 9AH lead accumulator as standby power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120479301 CN202331208U (en) | 2011-11-25 | 2011-11-25 | Ground unmanned helicopter control system applied to power transmission line inspection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120479301 CN202331208U (en) | 2011-11-25 | 2011-11-25 | Ground unmanned helicopter control system applied to power transmission line inspection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202331208U true CN202331208U (en) | 2012-07-11 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120479301 Expired - Lifetime CN202331208U (en) | 2011-11-25 | 2011-11-25 | Ground unmanned helicopter control system applied to power transmission line inspection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202331208U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103135554A (en) * | 2011-11-25 | 2013-06-05 | 中国科学院沈阳自动化研究所 | Unmanned helicopter ground control system applied to electric transmission line routing inspection |
| 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 |
| CN104573703A (en) * | 2013-10-29 | 2015-04-29 | 中国科学院沈阳自动化研究所 | Method for quickly identifying power transmission line based on partial derivative distribution and boundary strategy |
| CN106768008A (en) * | 2015-11-25 | 2017-05-31 | 中国科学院沈阳自动化研究所 | A kind of flight data acquisition system towards light helicopter |
-
2011
- 2011-11-25 CN CN 201120479301 patent/CN202331208U/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103135554A (en) * | 2011-11-25 | 2013-06-05 | 中国科学院沈阳自动化研究所 | Unmanned helicopter ground control system applied to electric transmission line routing inspection |
| 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 |
| CN104573703A (en) * | 2013-10-29 | 2015-04-29 | 中国科学院沈阳自动化研究所 | Method for quickly identifying power transmission line based on partial derivative distribution and boundary strategy |
| CN104573703B (en) * | 2013-10-29 | 2017-09-29 | 中国科学院沈阳自动化研究所 | Power transmission line method for quickly identifying with border strategy is distributed based on local derviation |
| CN106768008A (en) * | 2015-11-25 | 2017-05-31 | 中国科学院沈阳自动化研究所 | A kind of flight data acquisition system towards light helicopter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20120711 |
|
| CX01 | Expiry of patent term |