CN101923789A - Safe airplane approach method based on multisensor information fusion - Google Patents

Safe airplane approach method based on multisensor information fusion Download PDF

Info

Publication number
CN101923789A
CN101923789A CN 201010132161 CN201010132161A CN101923789A CN 101923789 A CN101923789 A CN 101923789A CN 201010132161 CN201010132161 CN 201010132161 CN 201010132161 A CN201010132161 A CN 201010132161A CN 101923789 A CN101923789 A CN 101923789A
Authority
CN
China
Prior art keywords
information
airport
airplane
fusion
dimensional
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.)
Granted
Application number
CN 201010132161
Other languages
Chinese (zh)
Other versions
CN101923789B (en
Inventor
赵龙
李铁军
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Inner Mongolia Shengbang Beidou Satellite Information Service Co., Ltd.
Original Assignee
Beihang University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Beihang University filed Critical Beihang University
Priority to CN2010101321618A priority Critical patent/CN101923789B/en
Publication of CN101923789A publication Critical patent/CN101923789A/en
Application granted granted Critical
Publication of CN101923789B publication Critical patent/CN101923789B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention relates to a safe airplane approach method based on multisensor information fusion. In the method, space-time registration and fusion are carried out on a flight control radar, a ground surveillance radar, navigation localization information, infrared and visible light image information to obtain space and ground target (barrier, people, vehicle and airplane) information, automatically generate a safe airplane approach channel and display both the targets and safe approach channel information in the three-dimensional airport scene in a fused mode. The concrete implementation steps are as follows: firstly, employing a radar and a navigation positioning system to obtain airplane information and carrying out time-space registration and fusion to obtain three-dimensional airplane information; secondly, carrying out detection, tracking and behavior prediction on ground targets to obtain track information of ground targets by using the information obtained after registration and fusion of visible light and infrared images are performed; thirdly, reestablishing a three-dimensional airplane information scene; and finally, fusing the real time detected target information in the three-dimensional airplane information scene and establishing the safe airplane approach channel and displaying the channel in the three-dimensional airplane information scene in real time so as to provide decision-making information for flight control personnel.

Description

A kind of safe airplane approach method based on multi-sensor information fusion
Technical field
The present invention relates to a kind of safe airplane approach method, can be used for the aviation safety management domain, realize that the blank pipe personnel provide decision-making assistant information for the airport, reduction accident/sign rate to the real-time monitoring of aerial and terrain object based on multi-sensor information fusion.
Background technology
In existing air traffic control system, utilize the flight path of surveillance radar surveillance aircraft and predict, but for ground runway intrusion event majority is to rely on the people to finish to monitor and dredge, particularly under complicated weather condition, rely on ground controlling officer's guiding to finish aircraft especially and advance nearly landing.
Aircraft is in high density traffic zone around the airport during advancing nearly landing, the required running program complexity of finishing of unit, particularly under the changeable condition of weather, the problem that is run into is generally all comparatively thorny and require to deal carefully with in the short time, therefore the unit work load is heavy, pressure is big, is accident and the accident proneness stage occurred frequently in the whole flight course.How reducing the accident rate that aircraft advances the nearly stage, is global military-civil field question of common concern.
At present advance accident/sign when near, take usually putting prevention first, and strengthening the unit operation training at ordinary times and improving the program executive capability for reducing aircraft.In the last few years, along with the development of information science technology, aeronautical technology had obtained fast development, at threat object and crashproof, on machine successful Application the height and flight collision warning system, airborne collision avoidance system and Automatic dependent surveillance broadcast system etc.And adopt the safety of multi-sensor information fusion technology to advance the attention that nearly technology is subjected to more and more countries and civil aviation organization.Safe airplane approach method based on multi-sensor information fusion is on the basis that makes up the airport three-dimensional scenic, will from multi-angle, various dimensions to various sensor acquisition to information carry out registration, fusion and analysis, realization is to the wisdom perception of environment, and will be aerial and terrain object information be added in real time in the three-dimensional scenic of airport, and then plan that aircraft safety advances nearly passage and also is presented in real time in the three-dimensional scenic of airport, guarantee that aircraft advances nearly landing safely under complex environment.
Summary of the invention
The technical problem to be solved in the present invention is: advance nearly landing period because the limitation of driver's vision is to cause aircraft to advance the principal element of nearly accident with the foreign body intrusion that advances in the nearly passage at aircraft.Under complicated weather condition, existing airport monitoring system can not guarantee aerial and terrain object are effectively surveyed.For improving, provide a kind of safe airplane approach method based on multi-sensor information fusion to aerial and terrain object real-time detection ability.
The technical solution used in the present invention is: a kind of safe airplane approach method based on multi-sensor information fusion, infrared image and visible light image information that this method utilizes information that airport air traffic control radar, ground surveillance radar, navigation positioning system obtain and photoelectric sensor to obtain carry out space-time registration and fusion, obtain aerial and ground target (barrier, people, car and aircraft) information, and generate aircraft safety automatically according to target information and advance nearly channel information, target information and safety are advanced nearly channel information merge and be presented in the three-dimensional virtual scene of airport.The specific implementation step is:
(1) utilize airport air traffic control radar, ground surveillance radar and navigation positioning system to obtain airplane information, and information is carried out synchronous registration of space-time and fusion, the step of calculating the three dimensional local information of aircraft is:
1. the airplane information that ground surveillance radar, air traffic control radar and navigation positioning system are obtained carries out registration and fusion;
2. the airplane information after merging is carried out coordinate transform, airplane information is downconverted under the rectangular coordinate system in space from polar coordinates, obtain the three dimensional local information of aircraft under world coordinate system.
(2) visible images and the infrared image information of photoelectric sensor collection are carried out registration and fusion, and detect on a surface target, tracking and behavior prediction, the step that obtains the positional information of terrain object is:
1. utilize photoelectric sensor to obtain visible images and infrared image, realize visible images and infrared image registration and fusion;
2. utilize fused images to the airport ground target detect, tracking and behavior prediction, obtain the information of terrain object in real time;
3. according to the perspective imaging principle, calculate the three dimensional local information of terrain object under world coordinate system.
(3) utilizing 3S is GPS---Global Positioning System (GPS), and RS---remote sensing system, the concrete steps that GIS---geographic information system technology is set up the airport three-dimensional scenic are:
1. utilizing the 3S technology to obtain the airport digital elevation model is that dem data, digital surface model are that DSM data and orthophotoquad are the DOM data;
2. utilize 3D MAX and AUTO cad tools software and dem data, DSM data and DOM data to set up the airport three-dimensional scene models, and the coordinate of definite airport in world coordinate system.
The positional information of the aerial and terrain object that (4) will real-time detect merges in the three-dimensional scenic of described airport, and set up aircraft safety according to the positional information of aerial and terrain object and advance nearly channel information, and described safety is advanced the concrete steps that nearly channel information is presented in the three-dimensional scenic of described airport in real time be:
1. according to the three-dimensional space position information of the aerial and terrain object that real-time detects, will be aerial and terrain object merge in the three-dimensional scenic of airport, make in the air and terrain object demonstration in real time in the three dimensions of airport;
2. generate aircraft safety in real time according to the positional information of the aerial and terrain object that real-time detects and advance nearly channel information, and described safety is advanced nearly channel information be presented in real time in the three-dimensional scenic of described airport.
Principle of the present invention is: at first, utilize airport air traffic control radar, ground surveillance radar and navigation positioning system to obtain airplane information, and information is carried out synchronous registration of space-time and fusion, obtain the three dimensional local information of aircraft; Secondly, the visible images and the infrared image information of photoelectric sensor collection are carried out registration and fusion, and detect on a surface target, tracking and behavior prediction, obtain the positional information of terrain object; Once more, utilizing 3S is GPS---Global Positioning System (GPS), and RS---remote sensing system, GIS---geographic information system technology is set up the airport three-dimensional scenic; At last, with the aerial and terrain object information fusion that real-time detects in the three-dimensional scenic of airport, and set up aircraft safety according to aerial and terrain object information and advance nearly passage, and escape way information is presented in the three-dimensional scenic of airport in real time, personnel provide decision information for blank pipe.
The present invention's advantage compared with prior art is: the present invention has remedied the deficiency of existing air traffic control system, can not effectively survey and threaten the people in the airport ground target, car and barrier and carry out early warning, can't guarantee that under complicated weather condition aircraft safety advances nearly landing; And the blank pipe personnel can only rely on artificial and the radar surveillance picture carries out safe approach guidance, can't form visual three-dimensional environment.Safe airplane approach method based on multi-sensor information fusion is to utilize Multi-sensor Fusion information to guarantee aerial and terrain object are effectively surveyed and intellectual analysis, aerial and terrain object information real time fusion are presented in the three-dimensional scenic of airport, and form aircraft safety and advance nearly passage, make full use of the real space sense of three-dimensional scenic.Can be blank pipe and flight based on the safe airplane approach method of multi-sensor information fusion and drive safe decision-making assistant information is provided, improve China's aviation safety management level.
Description of drawings
Fig. 1 is a kind of safe airplane approach method theory diagram based on multi-sensor information fusion of the present invention.
Embodiment
As shown in Figure 1, specific implementation method of the present invention is as follows:
(1) utilize airport air traffic control radar, ground surveillance radar and navigation positioning system to obtain airplane information, and information is carried out synchronous registration of space-time and fusion, the step of calculating the three dimensional local information of aircraft is:
1. the airplane information that ground surveillance radar, air traffic control radar and navigation positioning system are obtained carries out registration and fusion;
2. the airplane information after merging is carried out coordinate transform, airplane information is downconverted under the rectangular coordinate system in space from polar coordinates, obtain the three dimensional local information of aircraft under world coordinate system.
(2) visible images and the infrared image information of photoelectric sensor collection are carried out registration and fusion, and detect on a surface target, tracking and behavior prediction, the step that obtains the positional information of terrain object is:
1. utilize photoelectric sensor to obtain visible images and infrared image, realize visible images and infrared image registration and fusion;
2. utilize fused images to the airport ground target detect, tracking and behavior prediction, obtain the information of terrain object in real time;
3. according to the perspective imaging principle, calculate the three dimensional local information of terrain object under world coordinate system.
(3) utilizing 3S is GPS---Global Positioning System (GPS), and RS---remote sensing system, the concrete steps that GIS---geographic information system technology is set up the airport three-dimensional scenic are:
1. utilizing the 3S technology to obtain the airport digital elevation model is that dem data, digital surface model are that DSM data and orthophotoquad are the DOM data;
2. utilize 3D MAX and AUTO cad tools software and dem data, DSM data and DOM data to set up the airport three-dimensional scene models, and the coordinate of definite airport in world coordinate system.
The positional information of the aerial and terrain object that (4) will real-time detect merges in the three-dimensional scenic of described airport, and set up aircraft safety according to the positional information of aerial and terrain object and advance nearly channel information, and described safety is advanced the concrete steps that nearly channel information is presented in the three-dimensional scenic of described airport in real time be:
1. according to the three-dimensional space position information of the aerial and terrain object that real-time detects, will be aerial and terrain object merge in the three-dimensional scenic of airport, make in the air and terrain object demonstration in real time in the three dimensions of airport;
2. generate aircraft safety in real time according to the positional information of the aerial and terrain object that real-time detects and advance nearly channel information, and described safety is advanced nearly channel information be presented in real time in the three-dimensional scenic of described airport.

Claims (5)

1. safe airplane approach method based on multi-sensor information fusion is characterized in that may further comprise the steps:
(1) utilizes airport air traffic control radar, ground surveillance radar and navigation positioning system to obtain airplane information, and information is carried out the synchronous registration of space-time, calculate the three dimensional local information of aircraft;
(2) visible images and the infrared image information of photoelectric sensor collection are carried out registration and fusion, and detect on a surface target, tracking and behavior prediction, obtain the positional information of terrain object;
(3) utilizing 3S is GPS---Global Positioning System (GPS), and RS---remote sensing system, GIS---geographic information system technology is set up the airport three-dimensional scenic;
The positional information of the aerial and terrain object that (4) will real-time detect merges in the three-dimensional scenic of described airport, and set up aircraft safety according to the positional information of aerial and terrain object and advance nearly channel information, and described safety is advanced nearly channel information be presented in real time in the three-dimensional scenic of described airport.
2. a kind of safe airplane approach method according to claim 1 based on multi-sensor information fusion, it is characterized in that: utilize airport air traffic control radar, ground surveillance radar and navigation positioning system to obtain airplane information in the described step (1), and information carried out synchronous registration of space-time and fusion, the step of calculating the three dimensional local information of aircraft is:
1. the airplane information that ground surveillance radar, air traffic control radar and navigation positioning system are obtained carries out registration and fusion;
2. the airplane information after merging is carried out coordinate transform, airplane information is downconverted under the rectangular coordinate system in space from polar coordinates, obtain the three dimensional local information of aircraft under world coordinate system.
3. a kind of safe airplane approach method according to claim 1 based on multi-sensor information fusion, it is characterized in that: in the described step (2) visible images and the infrared image information of photoelectric sensor collection are carried out registration and fusion, and detect on a surface target, tracking and behavior prediction, the step that obtains the positional information of terrain object is:
1. utilize photoelectric sensor to obtain visible images and infrared image, realize visible images and infrared image registration and fusion;
2. utilize fused images to the airport ground target detect, tracking and behavior prediction, obtain the information of terrain object in real time;
3. according to the perspective imaging principle, calculate the three dimensional local information of terrain object under world coordinate system.
4. a kind of safe airplane approach method according to claim 1 based on multi-sensor information fusion, it is characterized in that: utilizing 3S in the described step (3) is GPS---Global Positioning System (GPS), the concrete steps that RS---remote sensing system, GIS---geographic information system technology are set up the airport three-dimensional scenic are:
1. utilizing the 3S technology to obtain the airport digital elevation model is that dem data, digital surface model are that DSM data and orthophotoquad are the DOM data;
2. utilize 3D MAX and AUTO cad tools software and dem data, DSM data and DOM data to set up the airport three-dimensional scene models, and the coordinate of definite airport in world coordinate system.
5. a kind of safe airplane approach method according to claim 1 based on multi-sensor information fusion, it is characterized in that: the positional information of the aerial and terrain object that will real-time detect in the described step (4) merges in the three-dimensional scenic of described airport, and set up aircraft safety according to the positional information of aerial and terrain object and advance nearly channel information, and described safety is advanced the concrete steps that nearly channel information is presented in the three-dimensional scenic of described airport in real time be:
1. according to the three-dimensional space position information of the aerial and terrain object that real-time detects, will be aerial and terrain object merge in the three-dimensional scenic of airport, make in the air and terrain object demonstration in real time in the three dimensions of airport;
2. generate aircraft safety in real time according to the positional information of the aerial and terrain object that real-time detects and advance nearly channel information, and described safety is advanced nearly channel information be presented in real time in the three-dimensional scenic of described airport.
CN2010101321618A 2010-03-24 2010-03-24 Safe airplane approach method based on multisensor information fusion Active CN101923789B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010101321618A CN101923789B (en) 2010-03-24 2010-03-24 Safe airplane approach method based on multisensor information fusion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010101321618A CN101923789B (en) 2010-03-24 2010-03-24 Safe airplane approach method based on multisensor information fusion

Publications (2)

Publication Number Publication Date
CN101923789A true CN101923789A (en) 2010-12-22
CN101923789B CN101923789B (en) 2011-11-16

Family

ID=43338690

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010101321618A Active CN101923789B (en) 2010-03-24 2010-03-24 Safe airplane approach method based on multisensor information fusion

Country Status (1)

Country Link
CN (1) CN101923789B (en)

Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101833104A (en) * 2010-04-27 2010-09-15 北京航空航天大学 Three-dimensional visual navigation method based on multi-sensor information fusion
CN102103803A (en) * 2011-01-19 2011-06-22 南京莱斯信息技术股份有限公司 Method for monitoring aircraft in airport terminal area
CN102253381A (en) * 2011-04-20 2011-11-23 上海交通大学 System and method for automatically detecting foreign object debris (FOD) on airfield runways
CN102279602A (en) * 2011-04-26 2011-12-14 江西省机场集团公司 Civil aviation airport navigation signal acquisition and processing method based on fully digital optical transmission
CN102332214A (en) * 2011-08-04 2012-01-25 南京航空航天大学 Enhanced airport scene monitoring system
CN103714719A (en) * 2014-01-16 2014-04-09 天津天航创力科技有限公司 Navigation flight navigating system based on BeiDou satellite navigation
CN103857035A (en) * 2012-12-06 2014-06-11 中国电信股份有限公司 Three-point stereo base station positioning method and device
CN104064057A (en) * 2014-06-13 2014-09-24 沈阳飞机工业(集团)有限公司 Method for implementing complementation and fusion of image tracking measurement data and radar measurement data
CN104200689A (en) * 2014-08-28 2014-12-10 长城汽车股份有限公司 Road early warning method and device
CN104240542A (en) * 2014-09-03 2014-12-24 南京航空航天大学 Airport surface maneuvering target identifying method based on geomagnetic sensor network
CN104267738A (en) * 2014-09-25 2015-01-07 安徽科耀智能科技有限公司 Anti-collision system for unmanned aerial vehicle
CN104406589A (en) * 2014-11-13 2015-03-11 中国测绘科学研究院 Flight method of aircraft passing through radar area
CN104601953A (en) * 2015-01-08 2015-05-06 中国航空无线电电子研究所 Video image fusion-processing system
CN104616124A (en) * 2015-03-06 2015-05-13 重庆大学 Real-time issuing method and system of safe and economic operation state of thermal power plant
CN104807456A (en) * 2015-04-29 2015-07-29 深圳市保千里电子有限公司 Method for automatic return flight without GPS (global positioning system) signal
CN105139606A (en) * 2015-07-29 2015-12-09 重庆赛乐威航空科技有限公司 Low-altitude aircraft information interaction system
CN105550502A (en) * 2015-12-08 2016-05-04 南京邮电大学 Data processing method based on health monitoring
CN105549110A (en) * 2015-12-08 2016-05-04 北京无线电计量测试研究所 Airport runway foreign object debris detection device and airport runway foreign object debris detection method
CN105653726A (en) * 2016-01-22 2016-06-08 中国电子科技集团公司第二十九研究所 Multi-dimensional target information acquisition method applied to multi-source sensing system
CN105812733A (en) * 2016-03-15 2016-07-27 中国民用航空总局第二研究所 Civil aviation air traffic control scene monitoring and guiding system
CN105810023A (en) * 2016-05-16 2016-07-27 福建福光股份有限公司 Automatic airport undercarriage retraction and extension monitoring system and method
CN106204629A (en) * 2016-08-17 2016-12-07 西安电子科技大学 Space based radar and infrared data merge moving target detection method in-orbit
CN106597498A (en) * 2017-01-18 2017-04-26 哈尔滨工业大学 Multi-sensor fusion system time and space deviation combined calibration method
CN107146475A (en) * 2017-06-06 2017-09-08 中国民用航空总局第二研究所 Ground service system, airborne guiding system and aircraft enter nearly Landing Guidance System
CN107272731A (en) * 2017-06-05 2017-10-20 陈金良 The automatic anti-collision system of unmanned plane
CN107424440A (en) * 2017-06-06 2017-12-01 中国民用航空总局第二研究所 Aircraft enters nearly landing monitoring system
CN107608003A (en) * 2017-09-06 2018-01-19 广州辰创科技发展有限公司 A kind of FOD detection device for foreign matter and method based on virtual reality technology
CN108195384A (en) * 2016-12-08 2018-06-22 中国航空无线电电子研究所 A kind of way point indicating means based on outdoor scene towards low flyer
CN108428370A (en) * 2018-02-28 2018-08-21 内蒙古司拓民航科技有限责任公司 A kind of machine level ground comprehensive control method and system
CN108521808A (en) * 2017-10-31 2018-09-11 深圳市大疆创新科技有限公司 A kind of complaint message display methods, display device, unmanned plane and system
CN108762286A (en) * 2018-05-31 2018-11-06 智飞智能装备科技东台有限公司 A kind of ground control system for the control that can fly to multiple UAVs
CN109191924A (en) * 2018-09-26 2019-01-11 中国船舶重工集团公司第七0九研究所 A kind of air traffic anti-collision system and method
CN109714567A (en) * 2018-11-08 2019-05-03 中国船舶重工集团公司七五0试验场 A kind of real-time construction method of three-dimensional virtual scene based on infrared viewing device and device
CN111524396A (en) * 2020-04-30 2020-08-11 成都民航空管科技发展有限公司 Low altitude warning method, system, data processing terminal and medium for terminal area
CN112329592A (en) * 2020-10-30 2021-02-05 北京百度网讯科技有限公司 Airport collaborative decision-making method, device, equipment and storage medium
CN114078325A (en) * 2020-08-19 2022-02-22 北京万集科技股份有限公司 Multi-perception system registration method and device, computer equipment and storage medium
CN114967756A (en) * 2022-07-07 2022-08-30 华能盐城大丰新能源发电有限责任公司 Auxiliary landing method, system and device for offshore wind turbine inspection unmanned aerial vehicle and storage medium
CN116309569A (en) * 2023-05-18 2023-06-23 中国民用航空飞行学院 Airport environment anomaly identification system based on infrared and visible light image registration
CN116609124A (en) * 2023-07-19 2023-08-18 北京建工环境修复股份有限公司 Device and method for taking columnar mud sample underwater

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2302318A (en) * 1995-06-14 1997-01-15 Bodenseewerk Geraetetech Aircraft landing procedure
JP2002260200A (en) * 2001-02-27 2002-09-13 Joho Kagaku Kenkyusho:Kk Stereoscopically displayed flight navigation system
US7136012B2 (en) * 2003-04-01 2006-11-14 Lockheed Martin Corporation Approach radar with array antenna having rows and columns skewed relative to the horizontal
JP2008070262A (en) * 2006-09-14 2008-03-27 Toshiba Corp Target position confirmation system and radar signal processor
CN101295021A (en) * 2007-04-24 2008-10-29 上海民航华东激光科技有限公司 Laser guiding aircraft landing system and use method
CN101551457A (en) * 2009-04-29 2009-10-07 电子科技大学 A construction method of forward looking linear array three-dimensional synthetic aperture radar system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2302318A (en) * 1995-06-14 1997-01-15 Bodenseewerk Geraetetech Aircraft landing procedure
JP2002260200A (en) * 2001-02-27 2002-09-13 Joho Kagaku Kenkyusho:Kk Stereoscopically displayed flight navigation system
US7136012B2 (en) * 2003-04-01 2006-11-14 Lockheed Martin Corporation Approach radar with array antenna having rows and columns skewed relative to the horizontal
JP2008070262A (en) * 2006-09-14 2008-03-27 Toshiba Corp Target position confirmation system and radar signal processor
CN101295021A (en) * 2007-04-24 2008-10-29 上海民航华东激光科技有限公司 Laser guiding aircraft landing system and use method
CN101551457A (en) * 2009-04-29 2009-10-07 电子科技大学 A construction method of forward looking linear array three-dimensional synthetic aperture radar system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
《中国雷达》 20081231 谭丽伟,盛蔚 雷达/惯导组合导航在MUAV进近着陆中的应用 , 第3期 2 *

Cited By (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101833104B (en) * 2010-04-27 2012-09-05 北京航空航天大学 Three-dimensional visual navigation method based on multi-sensor information fusion
CN101833104A (en) * 2010-04-27 2010-09-15 北京航空航天大学 Three-dimensional visual navigation method based on multi-sensor information fusion
CN102103803A (en) * 2011-01-19 2011-06-22 南京莱斯信息技术股份有限公司 Method for monitoring aircraft in airport terminal area
CN102253381A (en) * 2011-04-20 2011-11-23 上海交通大学 System and method for automatically detecting foreign object debris (FOD) on airfield runways
CN102279602A (en) * 2011-04-26 2011-12-14 江西省机场集团公司 Civil aviation airport navigation signal acquisition and processing method based on fully digital optical transmission
CN102279602B (en) * 2011-04-26 2013-03-27 江西省机场集团公司 Civil aviation airport navigation signal acquisition and processing method based on fully digital optical transmission
CN102332214A (en) * 2011-08-04 2012-01-25 南京航空航天大学 Enhanced airport scene monitoring system
CN103857035A (en) * 2012-12-06 2014-06-11 中国电信股份有限公司 Three-point stereo base station positioning method and device
CN103714719B (en) * 2014-01-16 2016-02-10 天津天航创力科技有限公司 Based on the Flight navigational system of Beidou satellite navigation
CN103714719A (en) * 2014-01-16 2014-04-09 天津天航创力科技有限公司 Navigation flight navigating system based on BeiDou satellite navigation
CN104064057A (en) * 2014-06-13 2014-09-24 沈阳飞机工业(集团)有限公司 Method for implementing complementation and fusion of image tracking measurement data and radar measurement data
CN104064057B (en) * 2014-06-13 2016-08-17 沈阳飞机工业(集团)有限公司 Image trace measurement data and the implementation method of radar measured data Mutually fusion
CN104200689A (en) * 2014-08-28 2014-12-10 长城汽车股份有限公司 Road early warning method and device
CN104240542A (en) * 2014-09-03 2014-12-24 南京航空航天大学 Airport surface maneuvering target identifying method based on geomagnetic sensor network
CN104267738A (en) * 2014-09-25 2015-01-07 安徽科耀智能科技有限公司 Anti-collision system for unmanned aerial vehicle
CN104406589A (en) * 2014-11-13 2015-03-11 中国测绘科学研究院 Flight method of aircraft passing through radar area
CN104406589B (en) * 2014-11-13 2017-05-24 中国测绘科学研究院 Flight method of aircraft passing through radar area
CN104601953A (en) * 2015-01-08 2015-05-06 中国航空无线电电子研究所 Video image fusion-processing system
CN104601953B (en) * 2015-01-08 2017-12-15 中国航空无线电电子研究所 A kind of video image fusion processing system
CN104616124A (en) * 2015-03-06 2015-05-13 重庆大学 Real-time issuing method and system of safe and economic operation state of thermal power plant
CN104616124B (en) * 2015-03-06 2018-08-17 重庆大学 A kind of real-time release method and system of thermal power plant safety and economic operation state
CN104807456A (en) * 2015-04-29 2015-07-29 深圳市保千里电子有限公司 Method for automatic return flight without GPS (global positioning system) signal
CN104807456B (en) * 2015-04-29 2018-04-17 深圳市保千里电子有限公司 A kind of method maked a return voyage automatically during GPS no signals
CN105139606A (en) * 2015-07-29 2015-12-09 重庆赛乐威航空科技有限公司 Low-altitude aircraft information interaction system
CN105550502A (en) * 2015-12-08 2016-05-04 南京邮电大学 Data processing method based on health monitoring
CN105550502B (en) * 2015-12-08 2018-04-03 南京邮电大学 A kind of data processing method based on health monitoring
CN105549110A (en) * 2015-12-08 2016-05-04 北京无线电计量测试研究所 Airport runway foreign object debris detection device and airport runway foreign object debris detection method
CN105653726A (en) * 2016-01-22 2016-06-08 中国电子科技集团公司第二十九研究所 Multi-dimensional target information acquisition method applied to multi-source sensing system
CN105653726B (en) * 2016-01-22 2018-10-23 中国电子科技集团公司第二十九研究所 A kind of Multidimensional object information collecting method for multi-source sensor-based system
CN105812733A (en) * 2016-03-15 2016-07-27 中国民用航空总局第二研究所 Civil aviation air traffic control scene monitoring and guiding system
CN105812733B (en) * 2016-03-15 2017-12-15 中国民用航空总局第二研究所 A kind of scene monitoring guiding system of air traffic control
CN105810023A (en) * 2016-05-16 2016-07-27 福建福光股份有限公司 Automatic airport undercarriage retraction and extension monitoring system and method
CN106204629A (en) * 2016-08-17 2016-12-07 西安电子科技大学 Space based radar and infrared data merge moving target detection method in-orbit
CN108195384B (en) * 2016-12-08 2021-12-17 中国航空无线电电子研究所 Low-altitude aircraft-oriented route point indication method based on real scene
CN108195384A (en) * 2016-12-08 2018-06-22 中国航空无线电电子研究所 A kind of way point indicating means based on outdoor scene towards low flyer
CN106597498B (en) * 2017-01-18 2020-04-24 哈尔滨工业大学 Space-time deviation joint calibration method for multi-sensor fusion system
CN106597498A (en) * 2017-01-18 2017-04-26 哈尔滨工业大学 Multi-sensor fusion system time and space deviation combined calibration method
CN107272731A (en) * 2017-06-05 2017-10-20 陈金良 The automatic anti-collision system of unmanned plane
CN107272731B (en) * 2017-06-05 2020-10-02 陈金良 Automatic collision avoidance system of unmanned aerial vehicle
CN107146475A (en) * 2017-06-06 2017-09-08 中国民用航空总局第二研究所 Ground service system, airborne guiding system and aircraft enter nearly Landing Guidance System
CN107424440A (en) * 2017-06-06 2017-12-01 中国民用航空总局第二研究所 Aircraft enters nearly landing monitoring system
CN107608003A (en) * 2017-09-06 2018-01-19 广州辰创科技发展有限公司 A kind of FOD detection device for foreign matter and method based on virtual reality technology
CN108521808A (en) * 2017-10-31 2018-09-11 深圳市大疆创新科技有限公司 A kind of complaint message display methods, display device, unmanned plane and system
CN108428370A (en) * 2018-02-28 2018-08-21 内蒙古司拓民航科技有限责任公司 A kind of machine level ground comprehensive control method and system
CN108762286A (en) * 2018-05-31 2018-11-06 智飞智能装备科技东台有限公司 A kind of ground control system for the control that can fly to multiple UAVs
CN109191924A (en) * 2018-09-26 2019-01-11 中国船舶重工集团公司第七0九研究所 A kind of air traffic anti-collision system and method
CN109714567B (en) * 2018-11-08 2021-05-18 中国船舶重工集团公司七五0试验场 Real-time three-dimensional virtual scene construction method and device based on infrared night vision device
CN109714567A (en) * 2018-11-08 2019-05-03 中国船舶重工集团公司七五0试验场 A kind of real-time construction method of three-dimensional virtual scene based on infrared viewing device and device
CN111524396A (en) * 2020-04-30 2020-08-11 成都民航空管科技发展有限公司 Low altitude warning method, system, data processing terminal and medium for terminal area
CN114078325A (en) * 2020-08-19 2022-02-22 北京万集科技股份有限公司 Multi-perception system registration method and device, computer equipment and storage medium
CN114078325B (en) * 2020-08-19 2023-09-05 北京万集科技股份有限公司 Multi-perception system registration method, device, computer equipment and storage medium
CN112329592A (en) * 2020-10-30 2021-02-05 北京百度网讯科技有限公司 Airport collaborative decision-making method, device, equipment and storage medium
CN114967756A (en) * 2022-07-07 2022-08-30 华能盐城大丰新能源发电有限责任公司 Auxiliary landing method, system and device for offshore wind turbine inspection unmanned aerial vehicle and storage medium
CN116309569A (en) * 2023-05-18 2023-06-23 中国民用航空飞行学院 Airport environment anomaly identification system based on infrared and visible light image registration
CN116309569B (en) * 2023-05-18 2023-08-22 中国民用航空飞行学院 Airport environment anomaly identification system based on infrared and visible light image registration
CN116609124A (en) * 2023-07-19 2023-08-18 北京建工环境修复股份有限公司 Device and method for taking columnar mud sample underwater
CN116609124B (en) * 2023-07-19 2023-09-29 北京建工环境修复股份有限公司 Device and method for taking columnar mud sample underwater

Also Published As

Publication number Publication date
CN101923789B (en) 2011-11-16

Similar Documents

Publication Publication Date Title
CN101923789B (en) Safe airplane approach method based on multisensor information fusion
CN101833104B (en) Three-dimensional visual navigation method based on multi-sensor information fusion
CN105812733B (en) A kind of scene monitoring guiding system of air traffic control
CN107161141B (en) Unmanned automobile system and automobile
CN206691107U (en) Pilotless automobile system and automobile
CN108313088B (en) Non-contact rail vehicle barrier detection system
US9575174B2 (en) Systems and methods for filtering wingtip sensor information
US20200346662A1 (en) Information processing apparatus, vehicle, mobile object, information processing method, and program
CN107272683A (en) Parallel intelligent vehicle control based on ACP methods
CN107167139A (en) A kind of Intelligent Mobile Robot vision positioning air navigation aid and system
KR20160129010A (en) Systems and methods for ground collision avoidance
CN106527480A (en) Multi-sensor fusion obstacle avoiding system of unmanned aerial vehicle and method
JP4174559B2 (en) Advanced visibility information providing system and method using satellite image and flight obstacle recognition system and method
CN103794088A (en) Systems and methods for providing runway-entry awareness and alerting
CN110989642B (en) Intelligent aircraft ground traction auxiliary method and system based on three-dimensional path tracking
CN107783547A (en) Post disaster relief rotor wing unmanned aerial vehicle obstacle avoidance system and method
CN107521678A (en) The UAS and its method for positioning and capturing for nuclear radiation radioactive source
CN109375629A (en) A kind of cruiser and its barrier-avoiding method that navigates
EP3431397A1 (en) Method and system for rendering and displaying a perspective view of aircraft taxi operation
CN115236673A (en) Multi-radar fusion sensing system and method for large vehicle
AU2022220403A1 (en) Systems and methods for monitoring activities in an aviation environment
CN206282147U (en) A kind of general unmanned plane Multi-sensor Fusion obstruction-avoiding control system
Vanek et al. Performance analysis of a vision only sense and avoid system for small UAVs
CN108154715A (en) A kind of side collision monitoring method
WO2023284461A1 (en) Method and system for aircraft ground movement collision avoidance

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20190515

Address after: 010000 Section B, Wangdi Jiahua Commercial Building, North of Alatan Street, Jinqiao Development Zone, Hohhot City, Inner Mongolia Autonomous Region

Patentee after: Inner Mongolia Shengbang Beidou Satellite Information Service Co., Ltd.

Address before: 100191 No. 37 Xueyuan Road, Haidian District, Beijing

Patentee before: Beihang University

TR01 Transfer of patent right