CN105739372A - Unmanned plane GCU system - Google Patents
Unmanned plane GCU system Download PDFInfo
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- CN105739372A CN105739372A CN201410766293.4A CN201410766293A CN105739372A CN 105739372 A CN105739372 A CN 105739372A CN 201410766293 A CN201410766293 A CN 201410766293A CN 105739372 A CN105739372 A CN 105739372A
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Abstract
The invention relates to an unmanned plane GCU system. The unmanned plane GCU system comprises equipment hardware and WINDOWS-based platform software which are integrated in an equipment box. By utilizing the computer technology, unmanned plane task systems are integrated to form a professional mobile unmanned plane task station system, touch screen holder control software capable of improving user experience is developed, reception, recording and output of images are carried out, a health state of a power source is monitored, Google/Baidu maps are added, so users are made to conveniently master flight lines and flight tracks, a user function module is added, such as an equipment power source (12V) opening/closing/switching system switch. Integrated unmanned plane task system problems are solved.
Description
Technical field
The present invention is applicable to the control of task system of depopulated helicopter, relate to a kind of novel synthesization with computer technology be core unmanned plane complex control system, solve the difficult problem of unmanned plane task system synthesization.As unmanned plane image/video gathers, records a video and output, the health status monitoring of unmanned plane electrical source of power, the switch of load power source, add Google/Baidu's map, it is easy to user and grasps aircraft flight route and flight path, increase user function module, such as device power supply (DPS) (12V) open and close, delivery system switch.
Background technology
According to current unmanned air vehicle technique state, except flight control system (FCU) is increased income except APM, all the other all do not carry out increasing income or announcing communications protocol, thus cause unmanned plane task end to merge with flight control system and produce technology barriers, current task system is all scatteredization, disordering, most tasks system can only rely on a data radio station or utilize receiver idle channel mutual with ground staff, unmanned plane is installed multiple task system simultaneously and means several data radio stations practical, will result in interstation interfering and weight, power consumption, the increase of cost, many radio station coexist and are difficult to hoisting power increase transmission range simultaneously, it is difficult to be promoted to over the horizon mission payload further control.
Therefore current unmanned plane is difficulty with the common carry of multitask and performs mission payload, and the strategy taked in industry is only to install 1-2 sub-task system every time, need to mounted subtask system be removed when its sub-systems is installed.
Along with unmanned plane is in the extensive use in each field, its aircraft body is quite ripe, task load part constantly develops along with sector application, and its task system develops into the trend of variation, complication, how unmanned plane task system integrated management is had urgent demand.Along with the development of computer technology, computer is miniaturization progressively, at high speed, up-to-date Haswell platform technology processing procedure has reached 22nm, carrying core video card capabilities constantly to strengthen, WIN8 system achieves touch screen, considerably increases experience and industrial picture, the data-handling capacity of user.
Summary of the invention
To be solved by this invention it has a problem in that, utilize computer technology, by unmanned plane task system synthesization, form the movable unmanned helicopter task station system of a set of specialty, develop the touch screen cradle head control software strengthening Consumer's Experience, image is received, records a video and exports, the health status monitoring of power supply, adds Google/Baidu's map, it is simple to user grasps aircraft flight route and flight path, increase user function module, such as device power supply (DPS) (12V) open and close, delivery system switch.
This invention address that it technical problem is that to realize by the following technical solutions:
1, based on Haswell computer platform and WIN8 operating system, utilize the standardization board resources such as PCI/PCIE bus extension video frequency collection card, serial port board, unmanned plane image is sent to computer video capture card by scheming biography receiving terminal, carry out recording a video and output display through certainly grinding the software processing based on VC++, user's user interface according to image end, touch screen realizes the control instruction of The Cloud Terrace is inputted, user instruction is sent to unmanned plane The Cloud Terrace by data radio station by computer, it is achieved double-direction control.
2, exploitation unmanned plane task system integrated communication agreement, all loads adopt RS232/RS422 bus response communication mode, it is simple to task system is formed control standard.
3, the user side software ground it is developed from, it is achieved Full Featured touch screen, the real-time display of image, control virtual key and video superimpose, form task gesture and control the user side software of The Cloud Terrace operation.Increase Baidu/Google Maps, utilize the positional information of the GPS/ Beidou navigation module of unmanned plane to carry out the display monitoring of aircraft trace, increase and flight control system software, hardware interface, it is achieved destination planning flight.
The present invention compared with prior art has significant advantage and beneficial effect.
By task system computerization, utilize speed and the process advantage of computer, it may be achieved cradle head control, numerically controlled standardization, experienced to the unmanned plane task system manipulation that user is brand-new by WIN8 system touchscreen user end.
Owing to computer hardware cost constantly reduces, the task system of synthesization can be substantially reduced earth station's cost, and subsequent calculations machine HardwareUpgring does not result in the phenomenon that software is incompatible, need secondary development.
Present invention achieves the fusion of computer technology and embedded technology, the embedded board utilizing PCI/PCIE bus design user side own carries out communication with computer, can break the dependence to flight control system to avoid risk simultaneously.
Accompanying drawing explanation
Fig. 1 is depopulated helicopter GCU systematic schematic diagram；
Fig. 2 is depopulated helicopter GCU system architecture diagram；
The specific embodiment of the present invention is shown in detail in by following example and accompanying drawing thereof.
Detailed description of the invention
Below in conjunction with accompanying drawing and preferred embodiment, to according to detailed description of the invention provided by the invention, structure, feature and effect thereof, describe in detail as after.
Referring to Fig. 1-2, image transmitting receives the picture signal that plate receives, computer is passed to by video frequency collection card, user side software is utilized to show in real time, user side interface is provided with task gesture and button, software may identify which the contact action instruction of user, realize video record, it is sent to RS232 serial port expanding module by PCI/PCIE bus, unmanned plane The Cloud Terrace, power-supply management system, the subtask systems such as system of propagandaing directed to communicate is controlled to data radio station, thus realizing the synthesization of task by the output of RS232 bus；GCU ground surface end data radio station receives the information such as GPS/ Beidou navigation locating module, acceleration sensor module, Height sensor module, extends 2 road R232 serial ports and controls ground surface end equipment, such as subtask systems such as beam antennas.
Claims (1)
1. a unmanned plane GCU system, including equipment GCU hardware with based on WINDOWS platform GCU system, it is characterised in that: described GCU hardware includes based on Intel's Haswell platform, PCI/PCIE Interface Video capture card, serial port expanding module, touch-screen display, number passes, figure conducts electricity platform；GCU system is for the real-time display of image, gather HD video, control virtual key and video superimpose, use touch screen to realize the control of The Cloud Terrace/optics gondola by task gesture and switch, increase Baidu/Google Maps, utilize the positional information of the GPS/ Beidou navigation module of unmanned plane to carry out the display monitoring of aircraft trace, increase and flight control system, hardware interface, realize destination planning flight, increase user function module, such as device power supply (DPS) (12V) open and close, delivery system switch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410766293.4A CN105739372A (en) | 2014-12-11 | 2014-12-11 | Unmanned plane GCU system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410766293.4A CN105739372A (en) | 2014-12-11 | 2014-12-11 | Unmanned plane GCU system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105739372A true CN105739372A (en) | 2016-07-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410766293.4A Pending CN105739372A (en) | 2014-12-11 | 2014-12-11 | Unmanned plane GCU system |
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| CN (1) | CN105739372A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106125747A (en) * | 2016-07-13 | 2016-11-16 | 国网福建省电力有限公司 | Based on the servo-actuated Towed bird system in unmanned aerial vehicle onboard the first visual angle mutual for VR |
-
2014
- 2014-12-11 CN CN201410766293.4A patent/CN105739372A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106125747A (en) * | 2016-07-13 | 2016-11-16 | 国网福建省电力有限公司 | Based on the servo-actuated Towed bird system in unmanned aerial vehicle onboard the first visual angle mutual for VR |
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| C06 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160706 |