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 PDFInfo
- 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
- Authority
- CN
- China
- Prior art keywords
- information
- ground
- aircraft
- landing
- current
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 47
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 9
- 230000004888 barrier function Effects 0.000 claims description 35
- 238000001514 detection method Methods 0.000 claims description 22
- 238000012545 processing Methods 0.000 claims description 17
- 238000012372 quality testing Methods 0.000 claims description 2
- 238000004891 communication Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000012544 monitoring process Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000011282 treatment Methods 0.000 description 2
- 239000012491 analyte Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/02—Control of position or course in two dimensions
- G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
Landscapes
- 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
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611177277.7A CN106774321A (en) | 2016-12-19 | 2016-12-19 | Accessory system and householder method are taken off and landed to one kind |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611177277.7A CN106774321A (en) | 2016-12-19 | 2016-12-19 | Accessory system and householder method are taken off and landed to one kind |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106774321A true CN106774321A (en) | 2017-05-31 |
Family
ID=58890373
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611177277.7A Pending CN106774321A (en) | 2016-12-19 | 2016-12-19 | Accessory system and householder method are taken off and landed to one kind |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106774321A (en) |
Cited By (2)
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)
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 |
-
2016
- 2016-12-19 CN CN201611177277.7A patent/CN106774321A/en active Pending
Patent Citations (10)
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)
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)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11645920B2 (en) | Secure unmanned aerial vehicle flight planning | |
CN105549619B (en) | Multi-take-off and landing point route planning method for cruising ability of unmanned aerial vehicle | |
EP3901728B1 (en) | Methods and system for autonomous landing | |
CN108803656B (en) | A flight control method and system based on complex low altitude | |
US11094210B2 (en) | Airport surface navigation aid | |
KR102281069B1 (en) | airport control system | |
US20190385463A1 (en) | System and method for managing traffic flow of unmanned vehicles | |
CN104932525A (en) | Drone control method and device, ground control system and drone | |
CN116931602A (en) | High-safety substation inspection unmanned aerial vehicle system and method | |
CN107291100B (en) | Monitoring method based on unmanned aerial vehicle | |
CN109084794A (en) | A kind of paths planning method | |
US20190268720A1 (en) | System and method for indicating drones flying overhead | |
US10611475B1 (en) | Updating virtual aerial map using sensors associated with aerial vehicles | |
EP4330943A1 (en) | Updating airspace awareness for unmanned aerial vehicles | |
CN115145302A (en) | A flight control method and device, cloud platform, and storage medium | |
US11535376B2 (en) | Traffic information processing equipment, system and method | |
CN108681333A (en) | A kind of radar under Navigation of Pilotless Aircraft failure of apparatus makes a return voyage system | |
KR102467524B1 (en) | Estimating method for flight plan using ADS-B data | |
CN105468022A (en) | Navigation unmanned aerial vehicle, unmanned flight navigation system and navigation method | |
CN106774321A (en) | Accessory system and householder method are taken off and landed to one kind | |
CN105528915A (en) | Helicopter fore-sight prediction false alarm inhibition method based on condition triggering | |
CN119200669A (en) | UAV flight trajectory detection method and equipment | |
CN105957405A (en) | Automatic broadcast monitoring system and method for flight state of general aircraft | |
KR20200062866A (en) | A method, apparatus and computer program for managing a route of an unmanned aerial vehicle in an selected area | |
US20240248477A1 (en) | Multi-drone beyond visual line of sight (bvlos) operation |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170531 |
|
RJ01 | Rejection of invention patent application after publication |