CN106976567A - A kind of aircraft autonomous parking direction guides dynamic display system - Google Patents
A kind of aircraft autonomous parking direction guides dynamic display system Download PDFInfo
- Publication number
- CN106976567A CN106976567A CN201710019905.7A CN201710019905A CN106976567A CN 106976567 A CN106976567 A CN 106976567A CN 201710019905 A CN201710019905 A CN 201710019905A CN 106976567 A CN106976567 A CN 106976567A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- led display
- full
- control system
- dynamic
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
Abstract
The invention belongs to aircraft berth technical field, specifically related to a kind of aircraft autonomous parking direction guiding dynamic display system, including LED display controller and full-color LED display screen, the LED display controller is connected with aircraft docking guidance control system, for receiving the aircraft offset direction of aircraft docking guidance control system offer and the data of deviation angle；The full-color LED display screen is connected with LED display controller, for showing dynamic arrow directional signal.The present invention provides a kind of dynamic direction and indicates form, and the instruction of intuitively adjustment amount is also provided while indicating that this is adjusted to that direction to pilot, so that pilot's energy exact operations, more accurately stop aircraft.
Description
Technical field
The invention belongs to aircraft berth technical field, especially a kind of aircraft autonomous parking direction guiding Dynamic Announce system
System.
Background technology
At present, visual navaid guiding equipment typically only indicates this to the left still using arrow in vector aircraft to pilot
Slide to the right.But pilot only knows that aircraft is inclined to that direction after seeing instruction content, but can not know that aircraft deviate from
How much, pilot does not know adjustment amount is how many when adjustment yet.
The content of the invention
The problem to be solved in the present invention is to provide a kind of operation degree of accuracy height, the achievable aircraft autonomous parking precisely stopped
Direction guides dynamic display system.
In order to solve the above technical problems, the technical solution adopted by the present invention is：A kind of aircraft autonomous parking direction guiding is dynamic
State shows system, including LED display controller and full-color LED display screen, and the LED display controller draws with aircraft berth
Lead control system to be connected, for receiving the aircraft offset direction of aircraft docking guidance control system offer and the number of deviation angle
According to；The full-color LED display screen is connected with LED display controller, for showing dynamic arrow directional signal.
Due to using above-mentioned technical proposal, when carrying out the guiding of aircraft direction, LED display controllers receive aircraft berth
Guide after the aircraft offset direction of control system offer and the data of deviation angle, full-color LED display screen can be inclined in aircraft
One side shows the arrow of opposite direction, to indicate aircraft institute's folk prescription to this is adjusted to other direction with prompting pilot；While LED
Displaying screen controller control arrow rolls what is advanced, if full-color LED display screen is received from aircraft docking guidance control system
Aircraft-position information in aircraft deviation distance it is bigger, pilot, which needs to adjust bigger amount, can just return to berth center line, LED
Screen controller control full-color LED display screen makes arrow rolling speed faster；Aircraft bias is smaller in the information received, flight
Member needs the amount adjusted smaller, then LED screen controller control full-color LED display screen makes arrow rolling speed slower.Opposite direction
It is also such.Aircraft without departing from when both sides arrows do not show, the aircraft adjustment direction and adjustment amount are indicated with this.
The present invention provides a kind of dynamic direction and indicates form, while indicating that this is adjusted to that direction to pilot
Also the instruction of intuitively adjustment amount is provided, so that pilot's energy exact operations, more accurately stop aircraft.
The beneficial effects of the invention are as follows：Have the advantages that the operation degree of accuracy is high, can be achieved precisely to stop.
Brief description of the drawings
The present invention is specifically described below with reference to accompanying drawing and with reference to example, advantages of the present invention and implementation will
More obvious, wherein content is only used for explanation of the present invention shown in accompanying drawing, without constituting to the present invention in all senses
On limitation, in the accompanying drawings：
Fig. 1 is the structured flowchart of the present invention
In figure：
1st, LED display controller 2, full-color LED display screen
3rd, aircraft docking guidance control system
Embodiment
As shown in figure 1, a kind of aircraft autonomous parking direction guiding dynamic display system of the invention, including LED display control
Device 1 and full-color LED display screen 2 processed, the LED display controller 1 is connected with aircraft docking guidance control system 3, for connecing
The aircraft offset direction of the offer of aircraft docking guidance control system 3 and the data of deviation angle are provided；The full-color LED display screen 2
It is connected with LED display controller 1, for showing dynamic arrow directional signal.
When carrying out the guiding of aircraft direction, LED display controllers 1 receive the offer of aircraft docking guidance control system 3
After the data of aircraft offset direction and deviation angle, the side that full-color LED display screen 2 can be inclined in aircraft shows opposite direction
Arrow, to indicate aircraft institute's folk prescription to this is adjusted to other direction with prompting pilot；LED display controller 1 is controlled simultaneously
Arrow rolls what is advanced, if the aircraft-position information that full-color LED display screen 2 is received from aircraft docking guidance control system 3
Middle aircraft deviation distance is bigger, and the amount that pilot needs adjustment bigger can just return to berth center line, and LED screen controller 1 is controlled
Full-color LED display screen 2 makes arrow rolling speed faster；Aircraft bias is smaller in the information received, and pilot needs adjustment
Amount it is smaller, then LED screen controller 1 control full-color LED display screen 2 make arrow rolling speed slower.Opposite direction is also such.
Aircraft without departing from when both sides arrows do not show, the aircraft adjustment direction and adjustment amount are indicated with this.
The present invention provides a kind of dynamic direction and indicates form, while indicating that this is adjusted to that direction to pilot
Also the instruction of intuitively adjustment amount is provided, so that pilot's energy exact operations, more accurately stop aircraft.
Embodiments of the invention are described in detail above, but the content is only presently preferred embodiments of the present invention,
It is not to be regarded as the practical range for limiting the present invention.All equivalent changes made according to the scope of the invention and improvement etc., all should
Still belong within this patent covering scope.
Claims (1)
1. a kind of aircraft autonomous parking direction guides dynamic display system, it is characterised in that：Including LED display controller and entirely
Color LED display, the LED display controller is connected with aircraft docking guidance control system, draws for receiving aircraft berth
The aircraft offset direction of control system offer and the data of deviation angle are provided；The full-color LED display screen is controlled with LED display
Device is connected, for showing dynamic arrow directional signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710019905.7A CN106976567A (en) | 2017-01-11 | 2017-01-11 | A kind of aircraft autonomous parking direction guides dynamic display system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710019905.7A CN106976567A (en) | 2017-01-11 | 2017-01-11 | A kind of aircraft autonomous parking direction guides dynamic display system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106976567A true CN106976567A (en) | 2017-07-25 |
Family
ID=59340114
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710019905.7A Pending CN106976567A (en) | 2017-01-11 | 2017-01-11 | A kind of aircraft autonomous parking direction guides dynamic display system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106976567A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1787946A (en) * | 2003-04-09 | 2006-06-14 | 机场标志有限公司 | Docking guidance |
| CN101366064A (en) * | 2006-01-11 | 2009-02-11 | 法国空中巴士公司 | Method and device for assisting the flying of an aircraft during an autonomous approach |
| CN101639991A (en) * | 2009-08-28 | 2010-02-03 | 张积洪 | Visual deviation rectifying guide system of airplane berthing |
| CN103786893A (en) * | 2014-01-24 | 2014-05-14 | 中国民用航空总局第二研究所 | Aircraft berthing automatic guide method and device based on laser ranging technology |
| CN104443423A (en) * | 2013-09-18 | 2015-03-25 | 爱乐基股份有限公司 | Correction positioning method of aircraft entering guide system |
| CN105302151A (en) * | 2014-08-01 | 2016-02-03 | 深圳中集天达空港设备有限公司 | Aircraft docking guidance and type recognition system and method |
| CN105336221A (en) * | 2014-08-01 | 2016-02-17 | 深圳中集天达空港设备有限公司 | Real-time docking airplane capturing method and system |
| CN105427677A (en) * | 2015-12-21 | 2016-03-23 | 天津华德宝航翼光电科技有限公司 | Distance display system of airplane berth guiding device |
| CN106251711A (en) * | 2016-08-24 | 2016-12-21 | 桂林信通科技有限公司 | A kind of aircraft docking guidance and distance display and information system |
-
2017
- 2017-01-11 CN CN201710019905.7A patent/CN106976567A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1787946A (en) * | 2003-04-09 | 2006-06-14 | 机场标志有限公司 | Docking guidance |
| CN101366064A (en) * | 2006-01-11 | 2009-02-11 | 法国空中巴士公司 | Method and device for assisting the flying of an aircraft during an autonomous approach |
| CN101639991A (en) * | 2009-08-28 | 2010-02-03 | 张积洪 | Visual deviation rectifying guide system of airplane berthing |
| CN104443423A (en) * | 2013-09-18 | 2015-03-25 | 爱乐基股份有限公司 | Correction positioning method of aircraft entering guide system |
| CN103786893A (en) * | 2014-01-24 | 2014-05-14 | 中国民用航空总局第二研究所 | Aircraft berthing automatic guide method and device based on laser ranging technology |
| CN105302151A (en) * | 2014-08-01 | 2016-02-03 | 深圳中集天达空港设备有限公司 | Aircraft docking guidance and type recognition system and method |
| CN105336221A (en) * | 2014-08-01 | 2016-02-17 | 深圳中集天达空港设备有限公司 | Real-time docking airplane capturing method and system |
| CN105427677A (en) * | 2015-12-21 | 2016-03-23 | 天津华德宝航翼光电科技有限公司 | Distance display system of airplane berth guiding device |
| CN106251711A (en) * | 2016-08-24 | 2016-12-21 | 桂林信通科技有限公司 | A kind of aircraft docking guidance and distance display and information system |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170725 |
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| WD01 | Invention patent application deemed withdrawn after publication |