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CN106774321A - Accessory system and householder method are taken off and landed to one kind - Google Patents

Accessory system and householder method are taken off and landed to one kind Download PDF

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Publication number
CN106774321A
CN106774321A CN201611177277.7A CN201611177277A CN106774321A CN 106774321 A CN106774321 A CN 106774321A CN 201611177277 A CN201611177277 A CN 201611177277A CN 106774321 A CN106774321 A CN 106774321A
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CN
China
Prior art keywords
information
ground
aircraft
landing
current
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Pending
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CN201611177277.7A
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Chinese (zh)
Inventor
杨鑫
韩梅
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Chengdu Four Wei Electronics Co Ltd Chengdu Star Stone Science And Technology Branch
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Chengdu Four Wei Electronics Co Ltd Chengdu Star Stone Science And Technology Branch
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Priority to CN201611177277.7A priority Critical patent/CN106774321A/en
Publication of CN106774321A publication Critical patent/CN106774321A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/02Control of position or course in two dimensions
    • G05D1/0202Control of position or course in two dimensions specially adapted to aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)

Abstract

Taken off the invention provides one kind and landed accessory system and householder method, obtain current location information, ground geography information and the route planning information of current aircraft, formed current aircraft travel path navigation information and simultaneously shown;The ground geography information includes airport ground navigation channel information, airport routing information and break point information;The route planning information refers to the travel path that takes off plan the route planning information of formation, or to landing travel path plan the route planning information of formation.Compared with prior art, when taking off and land, in the traveling process of ground, expeditiously ensure that the security in aircraft traveling process;The data message be given using ground control centre, the safety auxiliary that realization is taken off and landed, resource utilization is higher, and method is simple, and cost is lower, and more effective accurate.

Description

Accessory system and householder method are taken off and landed to one kind
Technical field
Taken off the present invention relates to one kind and landed accessory system and householder method, more particularly to a kind of being applied to flies During machine takeoff and landing, taking off in the traveling process of ground and land accessory system and householder method.
Background technology
Taking off for aircraft is most important with the security of landing.Take off and the landing of existing aircraft rely primarily on ground and refer to Waving personnel's voice at center carries out the artificial judgment of commander and pilot, not only inefficiency, and security cannot also be obtained Ensure.
Aircraft when taking off with landing, it is necessary to the moment keeps in touch with ground control centre, and receive ground control centre Control with scheduling.But, because ground control centre needs the business for the treatment of simultaneously too many, the limited amount of commanding, Can occur obstacle during being exchanged with pilot unavoidably.For this problem, if any Patent No. The Chinese patent of CN201010500078.1《Aircraft landing accessory system and method based on virtual reality technology》Disclose one Aircraft stable landing accessory system and method based on virtual reality technology are planted, current Airport Road can be simulated in control terminal From the real-time pictures of the relative position between aircraft landing wheel, assisting in flying person realizes the stable landing of aircraft.
But, virtual reality technology is too high to the hardware requirement of control terminal, and real-time pictures are easily subject to ambient light Influence, limitation is larger.In addition, not setting up unified high-performance treatments platform, it has not been convenient to which control centre is concentrated Management.
The content of the invention
The technical problem to be solved in the present invention is to provide one kind when taking off and landing, high in the traveling process of ground Efficiency ensures taking off and land accessory system and householder method for security.
The technical solution adopted by the present invention is as follows:Accessory system is taken off and landed to one kind, including,
Geographical position acquisition module, obtains the current location information of current aircraft;
Path planning module, when taking off, current location information, airport routing information and planning ground navigation channel according to current aircraft Information, carries out planning and forms route planning information to the travel path that takes off;During landing, the present bit confidence according to current aircraft Breath, planning ground navigation channel information and destination information, carry out planning and form route planning information to landing travel path;
Map datum module, the ground geography information for storing airport, including ground navigation channel information, airport routing information and stop Machine point information;
Maps processing module, for loading the ground geography information, route planning information and the present bit confidence of current aircraft Breath, forms travel path navigation information;
Display module, for showing the travel path navigation information.
The maps processing module is arranged in ground control centre or individually airborne or mobile accessory system;Work as map Processing module is arranged on when in airborne or mobile accessory system, and the ground geography information can be stored separately in the control of ground The heart is called for maps processing module, it is also possible to be directly stored in airborne or mobile accessory system;Maps processing module is another Aspect obtains the route planning information and current location information of current aircraft, comprehensive ground geography information, shape by communication module Into travel path navigation information.The latest edition of maps processing module real-time monitoring ground geography information is simultaneously updated.
Also include,
Detection of obstacles module, enters to the barrier or conflict objective in the range of the current location setting geographical threshold of current aircraft Row detection;
Barrier warning module, when the barrier or conflict objective is detected, carries out alarm early warning.In to drawing the line Barrier or conflict objective(Such as aircraft)Detected, when barrier or conflict thing has been detected, carried out timely early warning.Institute Stating detection of obstacles can detect for backstage radar system, testing result sent to display module by communication module carry out it is pre- It is alert.
The geographical position acquisition module is radar system or gps system, or other geographical position obtain system.
The display module is secondary module, and the work of airborne Primary Display System is not influenceed.
The secondary module is mobile display module, such as Pad, convenient auxiliary display, without influence Primary Display System Display work.
Householder method is taken off and landed to one kind, and specific method is:Obtain current location information, the ground of current aircraft Geography information and route planning information, form current aircraft travel path navigation information and are shown;The geographical letter in the ground Breath includes airport ground navigation channel information, airport routing information and break point information;The route planning information refers to, to playing flight Inbound path plan the route planning information of formation, or to landing travel path plan the route planning information of formation.
According to existing airport aircraft current location information acquisition methods, the current location information of current aircraft is obtained;And Route planning information and newest ground geography information according to backstage, with reference to the current location information of the current aircraft for obtaining, Current aircraft conduct path navigation information is formed, is shown in display terminal;Display content includes, current aircraft is described Current location in reason terrestrial information, and the path planning wire figure in information inside geography.Conventionally, as Ground control centre will inherently be detected to the positional information of each aircraft, and each flight is taken off and landed Ground navigation channel planned, therefore, the data message be given using ground control centre, the safety that realization is taken off and landed Auxiliary, resource utilization is higher, and cost is lower, and more effective accurate, realizes safer takeoff and landing auxiliary.
Methods described also includes that detection of obstacles early warning, the current location to current aircraft is set in the range of geographical threshold Barrier or conflict objective detected, when the barrier or conflict objective is detected, carry out alarm early warning.By barrier Hinder analyte detection and early warning, effectively prevent the potential safety hazard that conflict collision etc. is caused.
The specific method of detection of obstacles is:With current aircraft geographical position as the center of circle, predeterminable range R is radius, setting Horizontal area justifies scope;If other aircrafts or barrier are appeared in current area circle, then it is considered as conflict thing or barrier Hinder thing;Wherein, R=v*t, v are the travel rate of current aircraft, and t is Preset Time;When detected conflict thing or barrier go out Now, then sound and light alarm is carried out, and the positional information of barrier or conflict thing is shown on display module.According to current aircraft Travel rate and Preset Time set predeterminable range, and more effectively reasonably dynamic sets safe range.
Methods described also includes, before current aircraft travel path navigation information is formed, each aircraft in airport is determined Position, and positional information is sent to detection of obstacles module;Aircraft travel path is carried out with reference to each aircraft-position information in airport Planning, eventually form current aircraft travel path navigation information so that higher efficiency avoid having aircraft in aircraft traveling process Conflict objective occurs.
The specific method of current location information for obtaining current aircraft is:Obtained using ground radar system or gps system The current location information of current aircraft, or other geographical position acquisition methods.
Compared with prior art, the beneficial effects of the invention are as follows:When taking off and landing, in the traveling process of ground, Expeditiously ensure that the security in aircraft traveling process;The data message be given using ground control centre, realizes aircraft The safety auxiliary of takeoff and landing, resource utilization is higher, and method is simple, and cost is lower, and more effective accurate.
Brief description of the drawings
Fig. 1 is the collision detection flow chart of a wherein embodiment of the invention.
Fig. 2 is that the ground geographical map of a wherein embodiment of the invention looks into new technological process figure.
Specific embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples The present invention is further elaborated.It should be appreciated that specific embodiment described herein is only used to explain the present invention, not For limiting the present invention.
This specification(Including summary and accompanying drawing)Disclosed in any feature, unless specifically stated otherwise, can be equivalent by other Or the alternative features with similar purpose are replaced.I.e., unless specifically stated otherwise, each feature is a series of equivalent or class An example in like feature.
Specific embodiment 1
Accessory system is taken off and landed to one kind, including,
Geographical position acquisition module, obtains the current location information of current aircraft;
Path planning module, when taking off, current location information, airport routing information and planning ground navigation channel according to current aircraft Information, carries out planning and forms route planning information to the travel path that takes off;During landing, the present bit confidence according to current aircraft Breath, planning ground navigation channel information and destination information, carry out planning and form route planning information to landing travel path;
Map datum module, the ground geography information for storing airport, including ground navigation channel information, airport routing information and stop Machine point information;
Maps processing module, for loading the ground geography information, route planning information and the present bit confidence of current aircraft Breath, forms travel path navigation information;
Display module, for showing the travel path navigation information.
The maps processing module is arranged in ground control centre or individually airborne or mobile accessory system;Work as map Processing module is arranged on when in airborne or mobile accessory system, and the ground geography information can be stored separately in the control of ground The heart is called for maps processing module, it is also possible to be directly stored in airborne or mobile accessory system;Maps processing module is another Aspect obtains the route planning information and current location information of current aircraft, comprehensive ground geography information, shape by communication module Into travel path navigation information.The latest edition of maps processing module real-time monitoring ground geography information is simultaneously updated.
In this specific embodiment, update method is as shown in Fig. 2 pilot opens the accessory system, accessory system Connection maps processing device carries out map datum and engine map is looked into newly.The accessory system communicates with maps processing device, if auxiliary The map datum or engine map of the display module in system than map datum module in it is old, then be updated.
Specific embodiment 2
On the basis of specific embodiment 1, also include,
Detection of obstacles module, enters to the barrier or conflict objective in the range of the current location setting geographical threshold of current aircraft Row detection;
Barrier warning module, when the barrier or conflict objective is detected, carries out alarm early warning.In to drawing the line Barrier or conflict objective(Such as aircraft)Detected, when barrier or conflict thing has been detected, carried out timely early warning.Institute Stating detection of obstacles can detect for backstage radar system, testing result sent to display module by communication module carry out it is pre- It is alert.
Specific embodiment 3
On the basis of specific embodiment 1 or 2, the geographical position acquisition module is radar system or gps system, or Other geographical position obtain system.
Specific embodiment 4
On the basis of one of specific embodiment 1 to 3, the display module is secondary module, and airborne main display is not influenceed The work of system.
Specific embodiment 5
On the basis of specific embodiment 4, the secondary module is mobile display module, and such as Pad, convenient auxiliary shows, Display work without influenceing Primary Display System.
Specific embodiment 6
Householder method is taken off and landed to one kind, and specific method is:Current location information, the ground for obtaining current aircraft are geographical Information and route planning information, form current aircraft travel path navigation information and are shown;The ground geography information bag Include airport ground navigation channel information, airport routing information and break point information;The route planning information refers to, to traveling road of taking off Footpath plan the route planning information of formation, or to landing travel path plan the route planning information of formation.
Specific embodiment 7
On the basis of one of specific embodiment 1 to 5, householder method is taken off and landed to one kind, and specific method is:Obtain and work as The current location information of preceding aircraft, ground geography information and route planning information, form current aircraft travel path navigation information And shown;The ground geography information includes airport ground navigation channel information, airport routing information and break point information;It is described Route planning information refers to the travel path that takes off plan the route planning information of formation, or landing travel path is entered Professional etiquette draws the route planning information for being formed.
Specific embodiment 8
On the basis of one of specific embodiment 1 to 7, methods described also includes, detection of obstacles early warning, and current aircraft is worked as Front position setting geographical threshold in the range of barrier or conflict objective detected, when detect the barrier or conflict mesh Timestamp, carries out alarm early warning.Break the barriers detection and early warning, effectively prevent the potential safety hazard that conflict collision etc. is caused.
Specific embodiment 9
On the basis of one of specific embodiment 1 to 8, the specific method of detection of obstacles is:It is with current aircraft geographical position The center of circle, predeterminable range R is radius, setting horizontal area circle scope;If other aircrafts or barrier appear in it is current In area circle, then it is considered as conflict thing or barrier;Wherein, R=v*t, v are the travel rate of current aircraft, and t is Preset Time;When Conflict thing or barrier are detected when occurring, has then carried out sound and light alarm, and show barrier on display module or the thing that conflicts Positional information.
Specific embodiment 10
On the basis of one of specific embodiment 1 to 9, methods described also includes, is forming current aircraft travel path navigation letter Before breath, each aircraft in airport is positioned, and positional information is sent to detection of obstacles module;With reference to each aircraft position in airport Confidence ceases to be planned aircraft travel path, eventually forms current aircraft travel path navigation information, so that higher efficiency ground Avoid thering is aircraft conflict objective to occur in aircraft traveling process.
Specific embodiment 11
On the basis of one of specific embodiment 1 to 10, the specific method for obtaining the current location information of current aircraft is:Using Ground radar system or gps system obtain the current location information of current aircraft, or other geographical position acquisition methods.
Specific embodiment 12
First, pilot opens the accessory system, and accessory system connection maps processing device carries out map datum and map draws Hold up and look into new.The accessory system communicates with maps processing device, if the map datum or map of the display module in accessory system Engine than map datum module in it is old, then be updated, its flow chart is as shown in Figure 2.
Then, airport ground-control centre is positioned to each aircraft in airport, and positional information is sent into obstacle quality testing Survey module;
Detection of obstacles module carries out barrier or conflict objective detection, if having other aircrafts or barrier with the position of the aircraft It is set to the center of circle, predeterminable range R(The speed v * preset time ts of R=current aircraft)Within for the area circle of radius, then it is considered as barrier Hinder thing or conflict objective, as shown in Figure 1.
Then, the result of detection of obstacles is sent to path planning module.
Then, path planning module carries out path planning calculating with reference to the information such as positional information and flights arrangement of each aircraft Detected with conflict navigation channel.The navigation channel that will have been planned(Such as S1->S2->S3->…->SN), the position that is currently located of aircraft, fly with this Machine may have the target of conflict(Position)Position send to each mobile terminal.

Claims (10)

1. accessory system is taken off and landed to one kind, it is characterised in that:Including,
Geographical position acquisition module, obtains the current location information of current aircraft;
Path planning module, when taking off, current location information, airport routing information and planning ground navigation channel according to current aircraft Information, carries out planning and forms route planning information to the travel path that takes off;During landing, the present bit confidence according to current aircraft Breath, planning ground navigation channel information and destination information, carry out planning and form route planning information to landing travel path;
Map datum module, the ground geography information for storing airport, including ground navigation channel information, airport routing information and stop Machine point information;
Maps processing module, for loading the ground geography information, route planning information and the present bit confidence of current aircraft Breath, forms travel path navigation information;
Display module, for showing the travel path navigation information.
It is 2. according to claim 1 to take off and accessory system of landing, it is characterised in that:Also include,
Detection of obstacles module, enters to the barrier or conflict objective in the range of the current location setting geographical threshold of current aircraft Row detection;
Barrier warning module, when the barrier or conflict objective is detected, carries out alarm early warning.
It is 3. according to claim 1 to take off and accessory system of landing, it is characterised in that:The geographical position obtains mould Block is radar system or gps system.
It is 4. according to claim 1 to take off and accessory system of landing, it is characterised in that:The display module is auxiliary Display module.
It is 5. according to claim 4 to take off and accessory system of landing, it is characterised in that:The secondary module is Mobile display module.
6. householder method is taken off and landed to one kind, and specific method is:Obtain current location information, the ground ground of current aircraft Reason information and route planning information, form current aircraft travel path navigation information and are shown;The ground geography information Including airport ground navigation channel information, airport routing information and break point information;The route planning information refers to, to traveling of taking off Path plan the route planning information of formation, or to landing travel path plan the route planning information of formation.
7. according to claim 6 to take off and householder method of landing, methods described also includes that detection of obstacles is pre- It is alert, the barrier or conflict objective in the range of the current location setting geographical threshold of current aircraft are detected, when detecting When the barrier or conflict objective, alarm early warning is carried out.
8. according to claim 7 to take off and householder method of landing, the specific method of detection of obstacles is:With current Aircraft geographical position is the center of circle, and predeterminable range R is radius, setting horizontal area circle scope;If other aircrafts or obstacle Thing is appeared in current area circle, then be considered as conflict thing or barrier;Wherein, R=v*t, v are the travel rate of current aircraft, T is Preset Time;When conflict thing has been detected or barrier occurs, then sound and light alarm is carried out, and shown on display module The positional information of barrier or conflict thing.
9. take off and householder method of landing according to one of claim 6 to 8 is described, methods described also includes, formed Before current aircraft travel path navigation information, each aircraft in airport is positioned, and positional information is sent to obstacle quality testing Survey module;Aircraft travel path is planned with reference to each aircraft-position information in airport, eventually forms current aircraft travel path Navigation information.
10. it is according to claim 6 to take off and householder method of landing, obtain the current location information of current aircraft Specific method is:The current location information of current aircraft is obtained using ground radar system or gps system.
CN201611177277.7A 2016-12-19 2016-12-19 Accessory system and householder method are taken off and landed to one kind Pending CN106774321A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112783198A (en) * 2020-12-23 2021-05-11 武汉量宇智能科技有限公司 Method for judging aircraft control starting point
US12307913B2 (en) 2020-05-12 2025-05-20 Beijing Sankuai Online Technology Co., Ltd. Method and system for guiding landing of unmanned aerial vehicle, auxiliary positioning system, and unmanned aerial vehicle

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070078592A1 (en) * 2005-09-30 2007-04-05 Hugues Meunier Method and device for evaluating the licitness of the situation of a craft on the surface of an airport
CN101156189A (en) * 2005-04-04 2008-04-02 法国空中巴士公司 Method and apparatus for assisting ground navigation of an aircraft in an airport
CN102254454A (en) * 2001-12-04 2011-11-23 通用电气航空系统有限责任公司 Airport feature display system and data interchange method for conformal display
CN102298389A (en) * 2011-06-10 2011-12-28 清华大学 System fully controlled and taken over by ground station during takeoff and landing stages of unmanned plane
CN102568250A (en) * 2010-11-30 2012-07-11 空中客车运营简化股份公司 Method and system for aiding the taxiing of an aircraft on an airport domain
CN103413466A (en) * 2013-07-08 2013-11-27 中国航空无线电电子研究所 Airborne visible ground guide and warning device and guide and warning method thereof
CN105531748A (en) * 2013-09-12 2016-04-27 国立研究开发法人宇宙航空研究开发机构 Landing judgment assistance system, landing judgment assistance method, and landing judgment assistance program
CN105551312A (en) * 2016-01-29 2016-05-04 蒋维安 Airport scene traffic auxiliary assistance system and method
CN105575021A (en) * 2016-03-01 2016-05-11 杨兴文 Airport runway safety early warning system and airport runway safety early warning method
CN106020189A (en) * 2016-05-24 2016-10-12 武汉科技大学 Air-to-ground heterogeneous robot system path planning method based on neighborhood constraint

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102254454A (en) * 2001-12-04 2011-11-23 通用电气航空系统有限责任公司 Airport feature display system and data interchange method for conformal display
CN101156189A (en) * 2005-04-04 2008-04-02 法国空中巴士公司 Method and apparatus for assisting ground navigation of an aircraft in an airport
US20070078592A1 (en) * 2005-09-30 2007-04-05 Hugues Meunier Method and device for evaluating the licitness of the situation of a craft on the surface of an airport
CN102568250A (en) * 2010-11-30 2012-07-11 空中客车运营简化股份公司 Method and system for aiding the taxiing of an aircraft on an airport domain
CN102298389A (en) * 2011-06-10 2011-12-28 清华大学 System fully controlled and taken over by ground station during takeoff and landing stages of unmanned plane
CN103413466A (en) * 2013-07-08 2013-11-27 中国航空无线电电子研究所 Airborne visible ground guide and warning device and guide and warning method thereof
CN105531748A (en) * 2013-09-12 2016-04-27 国立研究开发法人宇宙航空研究开发机构 Landing judgment assistance system, landing judgment assistance method, and landing judgment assistance program
CN105551312A (en) * 2016-01-29 2016-05-04 蒋维安 Airport scene traffic auxiliary assistance system and method
CN105575021A (en) * 2016-03-01 2016-05-11 杨兴文 Airport runway safety early warning system and airport runway safety early warning method
CN106020189A (en) * 2016-05-24 2016-10-12 武汉科技大学 Air-to-ground heterogeneous robot system path planning method based on neighborhood constraint

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
汤新民 等: "《PETRI网原理及其在民航交通运输工程中的应用》", 31 January 2014, 中国民航出版社 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12307913B2 (en) 2020-05-12 2025-05-20 Beijing Sankuai Online Technology Co., Ltd. Method and system for guiding landing of unmanned aerial vehicle, auxiliary positioning system, and unmanned aerial vehicle
CN112783198A (en) * 2020-12-23 2021-05-11 武汉量宇智能科技有限公司 Method for judging aircraft control starting point
CN112783198B (en) * 2020-12-23 2022-07-29 武汉量宇智能科技有限公司 Method for judging aircraft control starting point

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