CN107356940A - Low-altitude surveillance system based on Beidou satellite communication - Google Patents
Low-altitude surveillance system based on Beidou satellite communication Download PDFInfo
- Publication number
- CN107356940A CN107356940A CN201710683355.9A CN201710683355A CN107356940A CN 107356940 A CN107356940 A CN 107356940A CN 201710683355 A CN201710683355 A CN 201710683355A CN 107356940 A CN107356940 A CN 107356940A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- big dipper
- equipment
- ground
- flight
- 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
- 238000004891 communication Methods 0.000 title claims abstract description 30
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 claims abstract description 96
- 238000012545 processing Methods 0.000 claims abstract description 43
- 238000000034 method Methods 0.000 claims abstract description 12
- 231100001261 hazardous Toxicity 0.000 claims description 12
- 238000009434 installation Methods 0.000 claims description 2
- 230000007547 defect Effects 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 16
- 230000005540 biological transmission Effects 0.000 description 5
- 230000001133 acceleration Effects 0.000 description 2
- 241001269238 Data Species 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000007405 data analysis Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/18502—Airborne stations
- H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/18502—Airborne stations
- H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
- H04B7/18508—Communications with or from aircraft, i.e. aeronautical mobile service with satellite system used as relay, i.e. aeronautical mobile satellite service
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
- H04W4/12—Messaging; Mailboxes; Announcements
- H04W4/14—Short messaging services, e.g. short message services [SMS] or unstructured supplementary service data [USSD]
Abstract
The invention discloses a kind of low-altitude surveillance system based on Beidou satellite communication, short message communication function based on big-dipper satellite, by installing airborne Big Dipper equipment aboard, ground Big Dipper equipment is installed on ground, ground Big Dipper equipment is connected with data processing platform (DPP), the flight parameter of aircraft is detected by airborne Big Dipper equipment and it is sent to ground Big Dipper equipment by big-dipper satellite, flight parameter is sent to by data processing platform (DPP) by ground Big Dipper equipment again, data processing platform (DPP) calculates the position of aircraft further according to flight parameter, aircraft is traced and monitored so as to realize.The present invention uses the signal sending and receiving equipment based on Beidou satellite communication, it is weak and the defects of be easily blocked preferably to solve existing aircraft tracking technique tracking signal, simultaneously as the decoding chip small volume of its core of Big Dipper chip, so that whole signal sending and receiving equipment miniaturization, is easy to carry.
Description
Technical field
The present invention relates to Big Dipper location technology, more particularly to a kind of low-altitude surveillance system based on Beidou satellite communication.
Background technology
Aircraft tracking technique generally comprises the tracking technique based on mobile network, the tracking technique based on radio, is based on
The technology of satellite communication and the technology based on radar, various technologies are all defective：
Tracking technique based on mobile network is limited to the cover height of mobile network, and general more than 1000 meters unless set up
Special base station enhancing equipment, otherwise without mobile network signals.And aircraft flight is highly generally more than 1000 meters, ship etc. is more
It is not possess versatility away from continent, this technology, can only be used in the case where ground signal is relatively strong.
Tracking technique based on radio need to dispose it is substantial amounts of receive base station, while radio in city easily by
The stop of high building causes received signal quality to be deteriorated.In addition, wireless device, especially aircraft and ship with wireless device all
It is costly.
Technology based on satellite communication is more ripe, but ground launch equipment volume is larger, while user's entry threshold is high,
Set for transmission power and antenna and all have higher requirements, and most of satellite equipment needs access external power supply to work.
Technology based on radar is divided into primary radar technology and secondary radar technology.Primary radar technology can only track, but
The details of tracking object can not be grasped；It is larger, relatively high that secondary radar technology needs all dispose volume on ground and aircraft
Expensive transmitting and receiving apparatus, be not suitable for low cost operation, be also not suitable for installing on a large scale.In addition, radar and radio have altogether
The shortcomings that same, easily blocked by high building.
The content of the invention
The present invention provides a kind of low-altitude surveillance system based on Beidou satellite communication, with solve existing aircraft means of tracking with
Track signal is weak and is easily blocked, the bulky defect of synchronous signal transceiver.The present invention is to be achieved through the following technical solutions
's：
A kind of low-altitude surveillance system based on Beidou satellite communication, including airborne Big Dipper equipment, ground Big Dipper equipment sum
According to processing platform；
The airborne Big Dipper equipment installation aboard, for detecting the flight parameter of the aircraft in real time, and passes through north
The flight parameter is sent to the ground Big Dipper equipment by bucket satellite；The flight parameter includes moment, and the aircraft
Longitude, latitude, flying height, flying speed and heading at the moment；
The ground Big Dipper equipment is used to the flight parameter received being sent to the data processing platform (DPP) in real time；
The data processing platform (DPP) is used to calculate the position of the aircraft at the moment according to the flight parameter.
Further, the flight parameter is encoded into after binary data again by the north by the airborne Big Dipper equipment
Bucket satellite is sent to the ground Big Dipper equipment.
Further, the data processing platform (DPP) is based on the institute being calculated according to the flight parameter received every time
The position of aircraft is stated, and the flight path curve of the aircraft is generated using Lagrange's interpolation algorithm.
Further, the data platform is according to the flight path curve of different aircrafts, the possibility that prediction interplane bumps against
Property, and prediction may bump against in the case of, by the ground Big Dipper equipment to may bump against aircraft on the airborne Big Dipper
Equipment sends warning message.
Further, the data processing platform (DPP) herein in connection with the aircraft history flight path data, to the aircraft
Current location carry out big data prediction, and according to the current location of the aircraft predicted judge the aircraft currently whether
In hazardous flight state.
Further, judge currently whether the method in hazardous flight state is the aircraft：
When the present bit is equipped with high building altitude information, flown according to the high building altitude information of the current location with described
The current flight height of machine, judge the aircraft whether in hazardous flight height；
When the current location does not have high building altitude information, according to the terrain data of the current location and the aircraft
Current flight height, judge the aircraft whether in hazardous flight height.
Further, the data processing platform (DPP) is additionally operable to the current course line according to the aircraft, by the current course line
The Weather information in front is sent to the ground Big Dipper equipment, and the ground Big Dipper equipment is used to pass through the big-dipper satellite by institute
State Weather information and be sent to the airborne Big Dipper equipment.
Further, built-in voice coding can be two by the airborne Big Dipper equipment and/or the ground Big Dipper equipment
Sent again by the big-dipper satellite after binary data.
Further, the airborne Big Dipper equipment is additionally operable to the ADS-B signals by the big-dipper satellite by the aircraft
The ground Big Dipper equipment is sent to, the ADS-B signals are sent to the data processing platform (DPP) by the ground Big Dipper equipment,
The ADS-B signals of each aircraft are broadcasted by the data processing platform (DPP).
Further, the data processing platform (DPP) is additionally operable to the true course line according to the aircraft, and real-time reception arrives
The flight parameter of the aircraft, the time that the aircraft reaches next way point is calculated in real time.
The present invention compared with prior art, has the following advantages that and beneficial effect：
Low-altitude surveillance system provided by the invention based on Beidou satellite communication, the short message communication work(based on big-dipper satellite
Can, by installing airborne Big Dipper equipment aboard, ground Big Dipper equipment is installed on ground, at ground Big Dipper equipment and data
Platform connects, and detects the flight parameter of aircraft by airborne Big Dipper equipment and it is sent into the ground Big Dipper by big-dipper satellite
Equipment, then flight parameter is sent to by data processing platform (DPP) by ground Big Dipper equipment, data processing platform (DPP) is joined further according to flight
Number calculates the position of aircraft, and aircraft is traced and monitored so as to realize.The present invention is received using the signal based on Beidou satellite communication
Equipment is sent out, it is weak and the defects of be easily blocked preferably to solve existing aircraft tracking technique tracking signal, simultaneously as Big Dipper core
The decoding chip small volume of its core of piece so that whole signal sending and receiving equipment miniaturization, be easy to carry.
Brief description of the drawings
Fig. 1 is the system structure diagram of the low-altitude surveillance system based on Beidou satellite communication.
Embodiment
For the object, technical solutions and advantages of the present invention are more clearly understood, with reference to embodiment and accompanying drawing, to this
Invention is described in further detail.
As shown in figure 1, the low-altitude surveillance system provided by the invention based on Beidou satellite communication, including airborne Big Dipper equipment
1st, ground Big Dipper equipment 2 and data processing platform (DPP) 3.
Airborne Big Dipper equipment 1 is installed aboard, for detecting the flight parameter of aircraft in real time, and passes through big-dipper satellite 4
Flight parameter is sent to ground Big Dipper equipment 2.Flight parameter includes the moment, and longitude of the aircraft at the moment, latitude,
Flying height, flying speed and heading.
Ground Big Dipper equipment 2 is used to the flight parameter received being sent to data processing platform (DPP) 3 in real time.Data processing is put down
Platform 3 is used to calculate position of the aircraft at the moment according to flight parameter.Fly at the time of in each flight parameter to detect this
At the time of during row parameter, therefore all it is different at the time of in the flight parameter obtained every time.Data processing platform (DPP) 3 obtains to continuous
To flight parameter calculated in real time, so as to be continuously available aircraft in the position at each moment.Data processing platform (DPP) 3 can use
Computer system, comprising the longitude and latitude aircraft when at different moments in different flight parameters, determined according to longitude and latitude
The position of aircraft belongs to known technology, will not be repeated here.
Short message communication function of the invention based on big-dipper satellite, flight is sent by big-dipper satellite in the form of short message
The various data such as parameter, it is weak and the defects of be easily blocked to solve existing aircraft tracking technique tracking signal.In order to aboard
There is preferable communication efficiency, and adapt to the demand that aircraft carries out different maneuvers, airborne Big Dipper equipment 1 is connected with 4 days
Line, 4 antennas are separately positioned on the head, tail and both sides of aircraft, and without dead angle the position of aircraft is entered so as to 360 degree
Row monitoring, while lift the communication efficiency of Big Dipper short message.Meanwhile it is additionally provided with airborne Big Dipper equipment 1 for detecting aircraft
The gyroscope of flight attitude, the acceleration transducer for detecting aircraft acceleration and for detecting interior of aircraft atmospheric pressure
Barometric pressure sensor, these data can be sent to ground Big Dipper equipment 2 by airborne Big Dipper equipment 1 by big-dipper satellite 4, then be passed through
Ground Big Dipper equipment 2 is sent remotely to data processing centre, and data processing centre, can by gathering the above-mentioned data of different aircrafts
To carry out big data analysis to related flight parameter of the different aircrafts under even in everyday situations, so as to be carried out when occurring abnormal
Alarm, may be in the case of generation accident, look-ahead.
Ground Big Dipper equipment 2 can enter row data communication by internet and data processing platform (DPP) 3.The low-altitude surveillance system is also
May include the mobile phone 6, tablet personal computer 5 and notebook computer 7 for entering row data communication with data processing platform (DPP) 3, can by mobile phone 6,
Tablet personal computer 5 or the grade of notebook computer 7 access data processing platform (DPP) 3 and aircraft related data are inquired about.
Flight parameter is encoded into after binary data and is sent to ground north by big-dipper satellite 4 again by airborne Big Dipper equipment 1
Struggle against equipment 2.Short message information is sent by big-dipper satellite 4, Big Dipper minute card can only transmit 73 byte datas every time, if using
Textual form carries out the transmission of flight parameter, can only once transmit 1 flight parameter, flight parameter can be carried out into binary system pressure
Contracting, is transmitted after being compressed into binary data, can thus 24 byte transmission, one flight parameter be used, so as to realize once
3 flight parameters are transmitted, improve efficiency of transmission.
Position of the data processing platform (DPP) 3 based on the aircraft being calculated according to the flight parameter received every time, and utilize
Lagrange's interpolation algorithm generates the flight path curve of aircraft.The cycle of the system renewal aircraft-position information is 20 millisecond one
It is secondary.And system is per minute can only obtain 3 three flight parameters, during whole one minute, can be calculated by Lagrange's interpolation
Method carries out interpolation calculation to the positional information of aircraft so that the flight path of aircraft seems smooth true.Specifically, data
Processing platform 3 can carry out a Lagrange's interpolation every 20 milliseconds and calculate, and make two neighboring aircraft position on flight path curve
Time difference between putting is 20 milliseconds, so as to reduce the complexity of calculating.
Data platform is according to the flight path curve of different aircrafts, the possibility that prediction interplane bumps against, and can in prediction
In the case of bumping against, alarm signal is sent to the airborne Big Dipper equipment 1 on the aircraft that may bump against by ground Big Dipper equipment 2
Breath.Longitude, latitude, flying height, flight speed in the current flight parameter of the flight path curve and aircraft of aircraft
The follow-up flight path and flying speed of aircraft can be predicted in the parameter such as degree and heading, so as to predict phase between two airplanes
Hit the height of possibility.
Data processing platform (DPP) 3 carries out big data herein in connection with the history flight path data of aircraft to the current location of aircraft
Prediction, and judge whether aircraft is currently in hazardous flight state according to the current location of the aircraft predicted.Specifically, sentence
Currently whether the method in hazardous flight state can be disconnected aircraft：When present bit is equipped with high building altitude information, according to work as
The high building altitude information of front position and the current flight height of aircraft, judge aircraft whether in hazardous flight height；When current
When position does not have high building altitude information, according to the current flight of the terrain data of current location and aircraft height, judge that aircraft is
It is no to be in hazardous flight height.
Data processing platform (DPP) 3 is led to by WebSocket agreements with being connected to the browser progress data of data processing platform (DPP) 3
Letter.If using browser access data processing platform (DPP) 3, to be monitored to aircraft, generally conventional way is webpage brush
New technology, the positional information of aircraft is obtained in real time by constantly refreshing webpage, such Consumer's Experience extreme difference, by using
HTML5 WebSocket technologies, can accomplish not refresh browser and real-time exhibition aircraft position, improve Consumer's Experience.
Data processing platform (DPP) 3 is additionally operable to the current course line according to aircraft, and the Weather information in front of current course line is sent to
Ground Big Dipper equipment 2, ground Big Dipper equipment 2 are used to Weather information is sent into airborne Big Dipper equipment 1 by big-dipper satellite 4.Knot
High-precision weather information is closed, the Weather information in front of the current course line in course line can be arrived by Big Dipper short message technology real time propelling movement
Airborne Big Dipper equipment 1, so as to be provided safeguard for flight safety.
The transmission content length limitation of Big Dipper short message is limited to, speech data can not possibly be sent substantially.It is if however, logical
Cross airborne Big Dipper equipment 1 and/or ground Big Dipper equipment 2 by built-in voice coding be binary data after again by big-dipper satellite 4
Send, it is possible to the voice recorded in advance is sent when needing, is communicated so as to realize by conventional voice.
Airborne Big Dipper equipment 1 is additionally operable to that the ADS-B signals of aircraft are sent into ground Big Dipper equipment 2 by big-dipper satellite 4,
ADS-B signals are sent to data processing platform (DPP) 3 by ground Big Dipper equipment 2, and data processing platform (DPP) 3 is by the ADS-B signals of each aircraft
It is broadcasted, so as to realize low flyer and civil aviaton's aircraft anti-collision early warning, avoids installing ADS-B equipment additional aboard and produced
Raw cost, greatly facilitate low-latitude flying user.
Data processing platform (DPP) 3 is additionally operable to the true course line according to aircraft, and the flight parameter of aircraft that real-time reception arrives, real
When calculate the time that aircraft reaches next way point.During specific calculating, real-time wind speed, heading and flight speed should be taken into account
The factors such as degree, this is not available for other data processing platform (DPP)s 3.
Above-described embodiment is only preferred embodiment, the protection domain being not intended to limit the invention, every the present invention's
All any modification, equivalent and improvement made within spirit and principle etc., should be included in the scope of the protection.
Claims (10)
1. a kind of low-altitude surveillance system based on Beidou satellite communication, it is characterised in that including airborne Big Dipper equipment, the ground Big Dipper
Equipment and data processing platform (DPP)；
The airborne Big Dipper equipment installation aboard, is defended for detecting the flight parameter of the aircraft in real time, and by the Big Dipper
The flight parameter is sent to the ground Big Dipper equipment by star；The flight parameter includes moment, and the aircraft in institute
State longitude, latitude, flying height, flying speed and the heading during moment；
The ground Big Dipper equipment is used to the flight parameter received being sent to the data processing platform (DPP) in real time；
The data processing platform (DPP) is used to calculate the position of the aircraft at the moment according to the flight parameter.
2. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that the airborne Big Dipper
The flight parameter is encoded into after binary data and is sent to the ground Big Dipper equipment by the big-dipper satellite again by equipment.
3. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that the data processing
Position of the platform based on the aircraft being calculated according to the flight parameter received every time, and inserted using Lagrange
Value-based algorithm generates the flight path curve of the aircraft.
4. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 3, it is characterised in that the data platform
According to the flight path curve of different aircrafts, the possibility of prediction interplane collision, and in the case where prediction may bump against, lead to
Cross the ground Big Dipper equipment and send warning message to the airborne Big Dipper equipment on the aircraft that may bump against.
5. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that the data processing
Platform carries out big data prediction, and root herein in connection with the history flight path data of the aircraft to the current location of the aircraft
It is predicted that the current location of the aircraft arrived judges whether the aircraft is currently in hazardous flight state.
6. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 5, it is characterised in that judge the aircraft
It is current that whether the method in hazardous flight state is：
When the present bit is equipped with high building altitude information, according to the high building altitude information of the current location and the aircraft
Current flight height, judge the aircraft whether in hazardous flight height；
When the current location does not have high building altitude information, according to working as the terrain data of the current location and the aircraft
Preceding flying height, judge the aircraft whether in hazardous flight height.
7. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that the data processing
Platform is additionally operable to the current course line according to the aircraft, and the Weather information in front of the current course line is sent into the ground north
Struggled against equipment, and the ground Big Dipper equipment is set for the Weather information to be sent into the airborne Big Dipper by the big-dipper satellite
It is standby.
8. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that the airborne Big Dipper
Equipment and/or the ground Big Dipper equipment can be sent out built-in voice coding by the big-dipper satellite again after binary data
Send.
9. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that the airborne Big Dipper
Equipment is additionally operable to that the ADS-B signals of the aircraft are sent into the ground Big Dipper equipment by the big-dipper satellite, describedly
The ADS-B signals are sent to the data processing platform (DPP) by face Big Dipper equipment, and the data processing platform (DPP) is by each aircraft
ADS-B signals are broadcasted.
10. the low-altitude surveillance system based on Beidou satellite communication as claimed in claim 1, it is characterised in that at the data
Platform is additionally operable to the true course line according to the aircraft, and the flight parameter of the aircraft that real-time reception arrives, and calculates in real time
The aircraft reaches the time of next way point.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710683355.9A CN107356940A (en) | 2017-08-11 | 2017-08-11 | Low-altitude surveillance system based on Beidou satellite communication |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710683355.9A CN107356940A (en) | 2017-08-11 | 2017-08-11 | Low-altitude surveillance system based on Beidou satellite communication |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107356940A true CN107356940A (en) | 2017-11-17 |
Family
ID=60288230
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710683355.9A Pending CN107356940A (en) | 2017-08-11 | 2017-08-11 | Low-altitude surveillance system based on Beidou satellite communication |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107356940A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108196578A (en) * | 2018-01-24 | 2018-06-22 | 广东容祺智能科技有限公司 | A kind of digitlization unmanned plane during flying Performance Test System |
| CN108768492A (en) * | 2018-03-29 | 2018-11-06 | 中国人民解放军国防科技大学 | Aerial target tracking method based on satellite-borne ADS-B special telegraph text |
| CN109116348A (en) * | 2018-07-23 | 2019-01-01 | 北京理工大学 | A kind of remote trace simulation method taken off towards insect communities with cruise |
| CN113362655A (en) * | 2021-05-24 | 2021-09-07 | 东方红卫星移动通信有限公司 | Remote information aggregation method based on ADS-B |
| CN113382364A (en) * | 2021-04-30 | 2021-09-10 | 航天恒星科技有限公司 | Return type aircraft track measuring and communication device based on Beidou short message |
| CN113537344A (en) * | 2021-07-15 | 2021-10-22 | 北京东进航空科技股份有限公司 | Processing method, equipment and medium for multi-source flight monitoring data fusion |
| CN113532471A (en) * | 2021-07-15 | 2021-10-22 | 浙江东进航科信息技术有限公司 | Processing method, equipment and medium for multi-source flight trajectory data fusion |
| CN114360298A (en) * | 2021-12-21 | 2022-04-15 | 芜湖通航产业技术研究院有限公司 | Low-altitude airspace ground supervision service system |
| CN115226051A (en) * | 2022-08-19 | 2022-10-21 | 王震 | Simple flight test real-time monitoring system based on short message of Beidou navigation system |
Citations (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5381140A (en) * | 1992-02-18 | 1995-01-10 | Kabushiki Kaisha Toshiba | Aircraft position monitoring system |
| EP1369665A2 (en) * | 2002-06-07 | 2003-12-10 | EADS Deutschland GmbH | Method for avoiding aircraft terrain collisions |
| US20060074559A1 (en) * | 2002-12-17 | 2006-04-06 | Thales | Onboard terrain anticollision display device |
| CN102509475A (en) * | 2011-10-26 | 2012-06-20 | 南京航空航天大学 | Air traffic control system and method for four-dimensional (4D)-trajectory-based operation |
| CN102540219A (en) * | 2010-12-31 | 2012-07-04 | 和芯星通科技(北京)有限公司 | Receiving method and receiver for signal of global navigation satellite system |
| CN202549080U (en) * | 2012-03-16 | 2012-11-21 | 中国民用航空总局第二研究所 | Fusion system of radar data, flight plan data and ADS-B data |
| CN103149937A (en) * | 2013-02-26 | 2013-06-12 | 北京航空航天大学 | Transverse lateral curve flight-path tracking method based on curvature compensation |
| CN103646569A (en) * | 2013-12-03 | 2014-03-19 | 海丰通航科技有限公司 | General aviation low-altitude monitor and service system |
| CN103853156A (en) * | 2014-02-07 | 2014-06-11 | 中山大学 | Small four-rotor aircraft control system and method based on airborne sensor |
| CN103873133A (en) * | 2014-03-13 | 2014-06-18 | 中国民用航空总局第二研究所 | Communication navigation monitoring system based on multi-mode data link |
| CN103927906A (en) * | 2014-04-29 | 2014-07-16 | 北京威胜通达科技有限公司 | Big Dipper autonomous navigation method based on Big Dipper short message and 4G communication mode |
| CN104267417A (en) * | 2014-07-29 | 2015-01-07 | 西安科远测控技术有限公司 | Beidou-based flight safety real-time monitoring system and method |
| CN104406580A (en) * | 2014-11-21 | 2015-03-11 | 北京科航军威科技有限公司 | Navigation method, device and system for general aviation aircraft |
| CN104501816A (en) * | 2015-01-08 | 2015-04-08 | 中国航空无线电电子研究所 | Multi-unmanned aerial vehicle coordination and collision avoidance guide planning method |
| CN104598747A (en) * | 2015-01-29 | 2015-05-06 | 中国航空无线电电子研究所 | Method for evaluating flight performance of aviator |
| CN204442701U (en) * | 2015-01-28 | 2015-07-01 | 张万松 | A kind of system utilizing big-dipper satellite short message to realize voice information communication |
| CN104851322A (en) * | 2015-05-28 | 2015-08-19 | 西安尚安隆软件科技有限公司 | Low-altitude flight target warning system and low-altitude flight target warning method based on Beidou satellite navigation system |
| CN204595221U (en) * | 2015-04-21 | 2015-08-26 | 中国民用航空总局第二研究所 | A kind of common aero vehicle airborne communication navigational system |
| CN104865939A (en) * | 2015-04-22 | 2015-08-26 | 中国民用航空总局第二研究所 | Ground monitoring device, method and system |
| CN105004321A (en) * | 2015-07-17 | 2015-10-28 | 湖北省电力勘测设计院 | Unmanned plane GPS-supported bundle djustment method in consideration of non-synchronous exposal |
| CN105100247A (en) * | 2015-07-29 | 2015-11-25 | 重庆赛乐威航空科技有限公司 | Low-altitude aircraft meteorological information interaction system |
| CN105676249A (en) * | 2016-04-20 | 2016-06-15 | 中国民航大学 | Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS |
| CN105894862A (en) * | 2016-05-05 | 2016-08-24 | 中国民用航空华东地区空中交通管理局 | Intelligent command system for air traffic control |
| CN105931497A (en) * | 2016-05-20 | 2016-09-07 | 中国民用航空总局第二研究所 | General aviation air collision detection method, device and general aircraft |
| CN106033646A (en) * | 2015-03-11 | 2016-10-19 | 沈阳空管技术开发有限公司 | Air traffic control system based on Beidou short message function |
| CN106155079A (en) * | 2015-04-13 | 2016-11-23 | 张谦 | A kind of unmanned aerial vehicle station system |
| CN106302055A (en) * | 2016-09-26 | 2017-01-04 | Tcl集团股份有限公司 | The synchronous updating method of a kind of smart machine state and system |
| CN205910527U (en) * | 2016-06-03 | 2017-01-25 | 西安航空电子科技有限公司 | Low latitude airborne vehicle monitored control system |
| CN106504588A (en) * | 2016-10-25 | 2017-03-15 | 中国民航大学 | Based on Beidou II and the multi-platform low latitude domain monitoring system and method for mobile network |
| CN106533819A (en) * | 2015-09-11 | 2017-03-22 | 北京奇虎科技有限公司 | Method, device and system for monitoring online service errors |
| CN106546245A (en) * | 2016-10-30 | 2017-03-29 | 北京工业大学 | Aircraft trace based on ADS B datas is inferred and smoothing method |
| CN106788679A (en) * | 2016-12-21 | 2017-05-31 | 福建星海通信科技有限公司 | A kind of Beidou satellite communication device and method with speech identifying function |
| CN106969765A (en) * | 2015-11-27 | 2017-07-21 | 泰勒斯公司 | The method represented for the in-flight track of calculating aircraft |
| CN207232391U (en) * | 2017-08-11 | 2018-04-13 | 四川联丰云网科技有限公司 | A kind of low-altitude surveillance system based on Beidou satellite communication |
-
2017
- 2017-08-11 CN CN201710683355.9A patent/CN107356940A/en active Pending
Patent Citations (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5381140A (en) * | 1992-02-18 | 1995-01-10 | Kabushiki Kaisha Toshiba | Aircraft position monitoring system |
| EP1369665A2 (en) * | 2002-06-07 | 2003-12-10 | EADS Deutschland GmbH | Method for avoiding aircraft terrain collisions |
| US20060074559A1 (en) * | 2002-12-17 | 2006-04-06 | Thales | Onboard terrain anticollision display device |
| CN102540219A (en) * | 2010-12-31 | 2012-07-04 | 和芯星通科技(北京)有限公司 | Receiving method and receiver for signal of global navigation satellite system |
| CN102509475A (en) * | 2011-10-26 | 2012-06-20 | 南京航空航天大学 | Air traffic control system and method for four-dimensional (4D)-trajectory-based operation |
| CN202549080U (en) * | 2012-03-16 | 2012-11-21 | 中国民用航空总局第二研究所 | Fusion system of radar data, flight plan data and ADS-B data |
| CN103149937A (en) * | 2013-02-26 | 2013-06-12 | 北京航空航天大学 | Transverse lateral curve flight-path tracking method based on curvature compensation |
| CN103646569A (en) * | 2013-12-03 | 2014-03-19 | 海丰通航科技有限公司 | General aviation low-altitude monitor and service system |
| CN103853156A (en) * | 2014-02-07 | 2014-06-11 | 中山大学 | Small four-rotor aircraft control system and method based on airborne sensor |
| CN103873133A (en) * | 2014-03-13 | 2014-06-18 | 中国民用航空总局第二研究所 | Communication navigation monitoring system based on multi-mode data link |
| CN103927906A (en) * | 2014-04-29 | 2014-07-16 | 北京威胜通达科技有限公司 | Big Dipper autonomous navigation method based on Big Dipper short message and 4G communication mode |
| CN104267417A (en) * | 2014-07-29 | 2015-01-07 | 西安科远测控技术有限公司 | Beidou-based flight safety real-time monitoring system and method |
| CN104406580A (en) * | 2014-11-21 | 2015-03-11 | 北京科航军威科技有限公司 | Navigation method, device and system for general aviation aircraft |
| CN104501816A (en) * | 2015-01-08 | 2015-04-08 | 中国航空无线电电子研究所 | Multi-unmanned aerial vehicle coordination and collision avoidance guide planning method |
| CN204442701U (en) * | 2015-01-28 | 2015-07-01 | 张万松 | A kind of system utilizing big-dipper satellite short message to realize voice information communication |
| CN104598747A (en) * | 2015-01-29 | 2015-05-06 | 中国航空无线电电子研究所 | Method for evaluating flight performance of aviator |
| CN106033646A (en) * | 2015-03-11 | 2016-10-19 | 沈阳空管技术开发有限公司 | Air traffic control system based on Beidou short message function |
| CN106155079A (en) * | 2015-04-13 | 2016-11-23 | 张谦 | A kind of unmanned aerial vehicle station system |
| CN204595221U (en) * | 2015-04-21 | 2015-08-26 | 中国民用航空总局第二研究所 | A kind of common aero vehicle airborne communication navigational system |
| CN104865939A (en) * | 2015-04-22 | 2015-08-26 | 中国民用航空总局第二研究所 | Ground monitoring device, method and system |
| CN104851322A (en) * | 2015-05-28 | 2015-08-19 | 西安尚安隆软件科技有限公司 | Low-altitude flight target warning system and low-altitude flight target warning method based on Beidou satellite navigation system |
| CN105004321A (en) * | 2015-07-17 | 2015-10-28 | 湖北省电力勘测设计院 | Unmanned plane GPS-supported bundle djustment method in consideration of non-synchronous exposal |
| CN105100247A (en) * | 2015-07-29 | 2015-11-25 | 重庆赛乐威航空科技有限公司 | Low-altitude aircraft meteorological information interaction system |
| CN106533819A (en) * | 2015-09-11 | 2017-03-22 | 北京奇虎科技有限公司 | Method, device and system for monitoring online service errors |
| CN106969765A (en) * | 2015-11-27 | 2017-07-21 | 泰勒斯公司 | The method represented for the in-flight track of calculating aircraft |
| CN105676249A (en) * | 2016-04-20 | 2016-06-15 | 中国民航大学 | Navigation airplane communication navigation monitoring system and method based on 4G/3G/BDS |
| CN105894862A (en) * | 2016-05-05 | 2016-08-24 | 中国民用航空华东地区空中交通管理局 | Intelligent command system for air traffic control |
| CN105931497A (en) * | 2016-05-20 | 2016-09-07 | 中国民用航空总局第二研究所 | General aviation air collision detection method, device and general aircraft |
| CN205910527U (en) * | 2016-06-03 | 2017-01-25 | 西安航空电子科技有限公司 | Low latitude airborne vehicle monitored control system |
| CN106302055A (en) * | 2016-09-26 | 2017-01-04 | Tcl集团股份有限公司 | The synchronous updating method of a kind of smart machine state and system |
| CN106504588A (en) * | 2016-10-25 | 2017-03-15 | 中国民航大学 | Based on Beidou II and the multi-platform low latitude domain monitoring system and method for mobile network |
| CN106546245A (en) * | 2016-10-30 | 2017-03-29 | 北京工业大学 | Aircraft trace based on ADS B datas is inferred and smoothing method |
| CN106788679A (en) * | 2016-12-21 | 2017-05-31 | 福建星海通信科技有限公司 | A kind of Beidou satellite communication device and method with speech identifying function |
| CN207232391U (en) * | 2017-08-11 | 2018-04-13 | 四川联丰云网科技有限公司 | A kind of low-altitude surveillance system based on Beidou satellite communication |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108196578A (en) * | 2018-01-24 | 2018-06-22 | 广东容祺智能科技有限公司 | A kind of digitlization unmanned plane during flying Performance Test System |
| CN108768492A (en) * | 2018-03-29 | 2018-11-06 | 中国人民解放军国防科技大学 | Aerial target tracking method based on satellite-borne ADS-B special telegraph text |
| CN109116348A (en) * | 2018-07-23 | 2019-01-01 | 北京理工大学 | A kind of remote trace simulation method taken off towards insect communities with cruise |
| CN113382364A (en) * | 2021-04-30 | 2021-09-10 | 航天恒星科技有限公司 | Return type aircraft track measuring and communication device based on Beidou short message |
| CN113382364B (en) * | 2021-04-30 | 2022-07-05 | 航天恒星科技有限公司 | Return type aircraft track measuring and communication device based on Beidou short message |
| CN113362655A (en) * | 2021-05-24 | 2021-09-07 | 东方红卫星移动通信有限公司 | Remote information aggregation method based on ADS-B |
| CN113537344A (en) * | 2021-07-15 | 2021-10-22 | 北京东进航空科技股份有限公司 | Processing method, equipment and medium for multi-source flight monitoring data fusion |
| CN113532471A (en) * | 2021-07-15 | 2021-10-22 | 浙江东进航科信息技术有限公司 | Processing method, equipment and medium for multi-source flight trajectory data fusion |
| CN114360298A (en) * | 2021-12-21 | 2022-04-15 | 芜湖通航产业技术研究院有限公司 | Low-altitude airspace ground supervision service system |
| CN115226051A (en) * | 2022-08-19 | 2022-10-21 | 王震 | Simple flight test real-time monitoring system based on short message of Beidou navigation system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107356940A (en) | Low-altitude surveillance system based on Beidou satellite communication | |
| CN101192350B (en) | Airplane anti-collision and navigation system and method for actively launching three-dimensional stereo flight information | |
| CN103869822B (en) | The perception of many rotor wing unmanned aerial vehicles and avoidance system and bypassing method thereof | |
| CN104035106B (en) | Salvage system and method based on beidou navigation and communication | |
| US10795055B2 (en) | Distributed weather monitoring system | |
| CN110109480A (en) | A kind of unmanned plane inspection search and rescue system and rescue method based on Multi-sensor Fusion | |
| CN105676249B (en) | A kind of navigation aircraft communication navigation observ and method based on 4G/3G/BDS | |
| CN107808551A (en) | A kind of General Aviation operation monitoring system and its monitoring method based on the Big Dipper | |
| CN103310578B (en) | Forest aviatic firefighting water fire extinguishing system and method | |
| CN103048670A (en) | System and method for positioning and navigating unattended flyer | |
| CN107605537A (en) | Coal and gas prominent tunnel the condition of a disaster intelligent detecting system and detection method | |
| CN106249752A (en) | A kind of unmanned plane networking flight monitoring and collaborative collision avoidance method and device | |
| KR102208152B1 (en) | System and method for response disaster situations in mountain area using UAS | |
| CN104316900B (en) | Aerial radio monitoring intelligent robot | |
| CN102109595A (en) | Search and rescue system and search and rescue method using personal positioning terminal | |
| WO2021079108A1 (en) | Flight control systems, ground-based control centres, remotely piloted aircraft, and methods | |
| CN104316899B (en) | A kind of on-air radio pyroelectric monitor intelligent robot | |
| CN204013537U (en) | A kind of communication and navigation surveillance based on multimode data link | |
| CN207232391U (en) | A kind of low-altitude surveillance system based on Beidou satellite communication | |
| CN105372722B (en) | A kind of spatial domain Wind measurement method and its device | |
| KR20180042655A (en) | Ship emergency response system | |
| CN106411388A (en) | Unmanned aerial vehicle information transmission system based on FPGA | |
| CN107229290A (en) | Unmanned plane search and rescue system and method | |
| CN104316901A (en) | Aerial intelligent robot used for radio monitoring | |
| CN205721375U (en) | A kind of many rotor wing unmanned aerial vehicles communication and safety monitoring system |
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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171117 |