CN103135554A - Unmanned helicopter ground control system applied to electric transmission line routing inspection - Google Patents
Unmanned helicopter ground control system applied to electric transmission line routing inspection Download PDFInfo
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- CN103135554A CN103135554A CN2011103816624A CN201110381662A CN103135554A CN 103135554 A CN103135554 A CN 103135554A CN 2011103816624 A CN2011103816624 A CN 2011103816624A CN 201110381662 A CN201110381662 A CN 201110381662A CN 103135554 A CN103135554 A CN 103135554A
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Abstract
The invention relates to a device for performing ground control on an unmanned aerial vehicle. The device is in a box structure, an open box comprises an upper panel and a lower panel, a liquid crystal displayer A is installed on the upper panel, a core computer, a video collector, a data acquisition unit, a power manager and a wireless data transmission device are mounted on the lower portion of the lower panel, the video collector, the data acquisition unit, the power manager and the wireless data transmission device are connected with the core computer, the wireless data transmission device is in a communicating connection with a flight control system of an unmanned helicopter, a liquid crystal displayer B, a keyboard, trackballs and communication interfaces are covered on the lower panel, remote-control levers capable of ascending and descending are matched with left and right ends of the liquid crystal displayer B and connected with the core computer through the data acquisition unit, and the liquid crystal displayer A, the liquid crystal displayer B, the keyboard and the trackballs are respectively connected with the core computer. According to the device, the device is in the box structure, and a box cover can be closed when the device is idle, so that a rain-proof function is achieved; a free wave wireless transmission module is configured, and the maximum transmission distance can reach to 20km; and two liquid crystal displayers are mounted, so that the display area is increased, and a user can conveniently observe various unmanned aerial vehicle downlink information.
Description
Technical field
The present invention relates to a kind of transmission line-oriented and patrol and examine the depopulated helicopter ground control system of application, specifically a kind of unmanned plane is carried out ground control device.
Background technology
This product belongs to the hardware platform that the Flight Control Software of the polling transmission line depopulated helicopter that Chinese Academy of Sciences's Shenyang automation research developed moves, and this control box can connect depopulated helicopter by the wireless transmission radio station.Various attributes to depopulated helicopter are configured, and control unmanned plane and airborne equipment carries out various operations.Control box is controlled software in conjunction with depopulated helicopter ground can make depopulated helicopter carry out accurate flying and to control unmanned plane and airborne equipment carries out Semi-automatic flight by rocking bar according to the coordinate points on map.
At present, domestic there is no perfect, the polling transmission line unmanned plane of highly integrating and the controller of airborne equipment.For filling up this domestic blank, this unmanned aerial vehicle (UAV) control case is intended to the control with unmanned plane and load, power management, and the unmanned plane common functions such as video demonstration are entirely integrated in a system, accomplish that the height of system is integrated, and the control of unmanned plane is oversimplified, and are integrated.
The depopulated helicopter ground control box is connected with the flight control system of depopulated helicopter by the data transmission radio station, can send instruction to unmanned aerial vehicle control system, has rich in natural resources and system interface, can adapt to the exploitation of various unmanned plane softwares.
Summary of the invention
At present, domestic there is no perfect, the polling transmission line unmanned plane of highly integrating and the opertaing device of airborne equipment.For filling up this domestic blank, for the Development characteristics of modern unmanned aerial vehicle control system, can be with the control of unmanned plane, map location is browsed, and airborne airborne equipment is controlled, and video tour is entirely integrated in a system, accomplish the height integration of system, the control of unmanned plane is oversimplified, integrated.
The technical scheme that the present invention adopts for achieving the above object is: transmission line-oriented is patrolled and examined the depopulated helicopter ground control system of application, and described ground control system is body structure, and the casing of opening is divided into top panel and lower panel;
Top panel is equipped with liquid crystal display 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 described radio data-transmission equipment is connected with the flight control system communication of depopulated helicopter;
Be coated with liquid crystal display B, keyboard, trace ball and each communication interface on lower panel, two ends, liquid crystal display B left and right also are furnished with liftable remote-control lever, are connected with the core computer by data acquisition unit;
Described liquid crystal display A, liquid crystal display B, keyboard and trace ball are connected with the core computer and are connected.
Described remote-control lever is technical grade four axle triple bond remote-control levers.
Described video collector and data acquisition unit are two PCI integrated circuit boards that are integrated in the core computer.
Described data acquisition unit is the collector of an analog to digital signal, gathers the simulating signals of 32 tunnel inputs with single ended mode, and is translated into the digital signal confession core computer identification of 16.
Described radio data-transmission equipment adopts the 900MHz wireless data transfer module, and maximum bandwidth is 115200bps, the 12V power voltage supply.
Described keyboard is connected USB interface and is connected with the core computer with trace ball.
It is whole device power supply that described power supervisor is converted to the 12V direct current with the 220V alternating current, also has the 9AH lead accumulator as standby power supply.
The present invention has the following advantages:
1. the present invention is 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 at most 20 kilometers;
3. two liquid crystal display are housed, increase display area, facilitate the user to observe various unmanned plane back informations;
4. be furnished with two the technical grade four axle triple bond remote-control levers in left and right, facilitate the user to control aircraft and various airborne equipment;
5. built-in reserve battery, have in use breakpoint of outage and overload protection, do not affect user's operation;
6. abundant interface and pilot lamp are arranged on lower panel, be user-friendly to, and can observe at any time the body power status.
Description of drawings
Fig. 1 is the block diagram of system of the present invention.
Embodiment
The present invention is described in further detail below in conjunction with drawings and Examples.
As shown in Figure 1, the present invention is body structure, and the casing of opening is divided into top panel and lower panel; Top panel is equipped with liquid crystal display 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 described radio data-transmission equipment is connected with the flight control system communication of depopulated helicopter; Be coated with liquid crystal display B, keyboard, trace ball and each communication interface on lower panel, two ends, liquid crystal display B left and right also are furnished with liftable remote-control lever, are connected with the core computer by data acquisition unit; Described liquid crystal display A, liquid crystal display B, keyboard and trace ball are connected with the core computer and are connected.
The core computer is connected by the patchcord of a Dvi one-to-two with two liquid crystal display, wherein a liquid crystal display directly is connected with computer with the VGA interface after telling, a liquid crystal display in addition is owing to lacking the HDMI interface, so after need to converting its signal to the VGA signal by the HDMI signal with converter, then the VGA signal is sent in liquid crystal display.
Video collector can provide the video acquisition passage of two high speeds, and this device only uses one of them passage.Collection jack on panel directly is connected on video collector by a video acquisition line.
Data acquisition unit is the collector of an analog to digital signal, and it can gather with single ended mode the simulating signals of 32 tunnel inputs, and is translated into the digital signal of 16 and identifies for computer.Used altogether 14 tunnel collection of simulant signal passage to identify the current state of remote-control lever in this device.
Two remote-control levers in left and right are responded to 4 positions that axle is present by 4 swept resistances respectively, and 5V and the ground of distribution power supply board received respectively at the two ends of these swept resistances.Output terminal in the middle of remote-control lever is integrated into the winding displacement port of 37 pins on the distribution power supply board, receive by winding displacement on the analog signal collector of computer.By this collector, the digital signal that the analog signal conversion of remote control rod output is computer-readable is processed.
Power supervisor also has another reserve battery input except the 220V input.If the power supply of 220V is outage suddenly in use, this moment, power supply can continue to adopt electric continual supply whole system from reserve battery.Reserve battery can be by the charging jack on panel, and the charger of specially joining with equipment charges, and after charger inserts on panel, the power supply knob of white is forwarded on the position of charging, after the pilot lamp on charger becomes redness, begins the charging for system.After battery was full of, indication etc. became green.
The man-machine interaction of this device is partly that a keyboard is arranged, and trace ball forms.Keyboard and trace ball are all USB interface.The operation of the operation of this keyboard and common computer keyboard is without any difference.Trace ball on panel has substituted the function of computer mouse, the trace ball on rotary panel, and mouse pointer moves to respective direction at once.
In this unmanned aerial vehicle (UAV) control case, software is controlled in the war of prepackage unmanned aerial vehicle, can control unmanned plane during flying track and various airborne equipment.
Claims (7)
1. a transmission line-oriented is patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, described ground control system is body structure, and the casing of opening is divided into top panel and lower panel;
Top panel is equipped with liquid crystal display 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 described radio data-transmission equipment is connected with the flight control system communication of depopulated helicopter;
Be coated with liquid crystal display B, keyboard, trace ball and each communication interface on lower panel, two ends, liquid crystal display B left and right also are furnished with liftable remote-control lever, are connected with the core computer by data acquisition unit;
Described liquid crystal display A, liquid crystal display B, keyboard and trace ball are connected with the core computer and are connected.
2. transmission line-oriented according to claim 1 is patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, described remote-control lever is technical grade four axle triple bond remote-control levers.
3. transmission line-oriented according to claim 1 is patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, described 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 3 described transmission line-orienteds are patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, described data acquisition unit is the collector of an analog to digital signal, gather the simulating signals of 32 tunnel inputs with single ended mode, and be translated into the digital signal confession core computer identification of 16.
5. transmission line-oriented according to claim 1 is patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, described radio data-transmission equipment adopts the 900MHz wireless data transfer module, and maximum bandwidth is 115200bps, the 12V power voltage supply.
6. transmission line-oriented according to claim 1 is patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, described keyboard is connected USB interface and is connected with the core computer with trace ball.
7. transmission line-oriented according to claim 1 is patrolled and examined the depopulated helicopter ground control system of application, it is characterized in that, it is whole device power supply that described power supervisor is converted to the 12V direct current with the 220V alternating current, also has the 9AH lead accumulator as standby power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011103816624A CN103135554A (en) | 2011-11-25 | 2011-11-25 | Unmanned helicopter ground control system applied to electric transmission line routing inspection |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011103816624A CN103135554A (en) | 2011-11-25 | 2011-11-25 | Unmanned helicopter ground control system applied to electric transmission line routing inspection |
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| CN103135554A true CN103135554A (en) | 2013-06-05 |
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| CN2011103816624A Pending CN103135554A (en) | 2011-11-25 | 2011-11-25 | Unmanned helicopter ground control system applied to electric transmission line routing inspection |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104179584A (en) * | 2014-08-25 | 2014-12-03 | 北京航空航天大学 | Dual-redundancy emergency shutdown device for piston-type unmanned helicopter ground test |
| CN104199460A (en) * | 2014-08-29 | 2014-12-10 | 河南科技大学 | Intelligent four-rotor aircraft reconnoitering system based on image recognition and tracking |
| CN105468021A (en) * | 2015-12-31 | 2016-04-06 | 天津御遨航空科技发展有限公司 | Portable unmanned aerial vehicle ground station |
| CN105527966A (en) * | 2016-01-29 | 2016-04-27 | 重庆德新机器人检测中心有限公司 | Automated vehicle remote control operation platform |
| CN105549615A (en) * | 2015-12-31 | 2016-05-04 | 天津御遨航空科技发展有限公司 | Portable ground station of unmanned aerial vehicle |
| 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 |
| CN109240328A (en) * | 2018-09-11 | 2019-01-18 | 国网电力科学研究院武汉南瑞有限责任公司 | A kind of autonomous method for inspecting of shaft tower based on unmanned plane |
| CN114280995A (en) * | 2021-12-27 | 2022-04-05 | 广州信邦智能装备股份有限公司 | Monitoring system for ground combined test bed of unmanned aerial vehicle environment control system |
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| CN200976108Y (en) * | 2006-11-24 | 2007-11-14 | 中国科学院沈阳自动化研究所 | Small-size unmanned helicopter is flight control system independently |
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| CN102255259A (en) * | 2011-03-29 | 2011-11-23 | 山东鲁能智能技术有限公司 | Transmission line tour inspection device suitable for unmanned aerial vehicle |
| CN202331208U (en) * | 2011-11-25 | 2012-07-11 | 中国科学院沈阳自动化研究所 | Ground unmanned helicopter control system applied to power transmission line inspection |
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2011
- 2011-11-25 CN CN2011103816624A patent/CN103135554A/en active Pending
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| CN200976108Y (en) * | 2006-11-24 | 2007-11-14 | 中国科学院沈阳自动化研究所 | Small-size unmanned helicopter is flight control system independently |
| CN201397468Y (en) * | 2009-03-04 | 2010-02-03 | 北京航空航天大学 | Ground control station system for aerial detection unmanned plane |
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| CN102064493A (en) * | 2010-11-02 | 2011-05-18 | 北京交通大学 | Method for paying off overhead transmission line by unmanned helicopter |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104179584A (en) * | 2014-08-25 | 2014-12-03 | 北京航空航天大学 | Dual-redundancy emergency shutdown device for piston-type unmanned helicopter ground test |
| CN104179584B (en) * | 2014-08-25 | 2016-12-07 | 北京航空航天大学 | A kind of urgent stopping arrangement of double remainings for piston type depopulated helicopter ground experiment |
| CN104199460A (en) * | 2014-08-29 | 2014-12-10 | 河南科技大学 | Intelligent four-rotor aircraft reconnoitering system based on image recognition and tracking |
| CN105468021A (en) * | 2015-12-31 | 2016-04-06 | 天津御遨航空科技发展有限公司 | Portable unmanned aerial vehicle ground station |
| CN105549615A (en) * | 2015-12-31 | 2016-05-04 | 天津御遨航空科技发展有限公司 | Portable ground station of unmanned aerial vehicle |
| CN105527966A (en) * | 2016-01-29 | 2016-04-27 | 重庆德新机器人检测中心有限公司 | Automated vehicle remote control operation platform |
| 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 |
| CN109240328A (en) * | 2018-09-11 | 2019-01-18 | 国网电力科学研究院武汉南瑞有限责任公司 | A kind of autonomous method for inspecting of shaft tower based on unmanned plane |
| CN114280995A (en) * | 2021-12-27 | 2022-04-05 | 广州信邦智能装备股份有限公司 | Monitoring system for ground combined test bed of unmanned aerial vehicle environment control system |
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Application publication date: 20130605 |