CN105676246A - Airplane monitor system and method on the basis of real-time dynamic positioning and data link - Google Patents
Airplane monitor system and method on the basis of real-time dynamic positioning and data link Download PDFInfo
- Publication number
- CN105676246A CN105676246A CN201610005958.9A CN201610005958A CN105676246A CN 105676246 A CN105676246 A CN 105676246A CN 201610005958 A CN201610005958 A CN 201610005958A CN 105676246 A CN105676246 A CN 105676246A
- Authority
- CN
- China
- Prior art keywords
- reference station
- terrestrial reference
- aircraft
- information
- data transmission
- 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
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
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- 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
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/40—Correcting position, velocity or attitude
- G01S19/41—Differential correction, e.g. DGPS [differential GPS]
-
- 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
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/53—Determining attitude
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0073—Surveillance aids
- G08G5/0078—Surveillance aids for monitoring traffic from the aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radio Relay Systems (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention relates to an airplane monitor system and method on the basis of real-time dynamic positioning and data link. The system comprises an airborne device and a ground-based device. The airborne device is installed on an airplane and is used for receiving satellite signals and real-time differential update information, finishing the correction of airplane positioning data, and sending differentiated position information in real time; the ground-based device is installed on the approach tower and is used for receiving the real-time differential update information, sending the update information to airplanes in the airspace of the airport periodically, receiving differential positioning data sent in real time by airplanes in the air, and sending the received airplane position information to an flight monitor terminal. By use of the system and method, the safety factor of flight training and monitor level of the stage of airplane approaching landing are increased; The system and method can be applied in flight conducting and air traffic control. Position information of targets in the airspace of the airport can be monitored in real time. The system and method can be applied in flight conducting and guiding, especially in dangerous cases such as rough weather and decreasing visibility, providing auxiliary decision-making information for flight commanders, and increasing the safety factor of flight training.
Description
Technical field
The present invention relates to a kind of aircraft to enter closely to monitor system and method.
Background technology
During flight training, enter aircraft from crew, aircraft prepares to sliding race of flight landing to slow down until all personnel leaves the whole process of aircraft machine, is a complicated flight course. In this process, aircraft can face a series of flight safety test problem. Wherein, aircraft enters near to land the required precision in the speed of aircraft, height and orientation etc. is higher, and the control action that driver to complete is more, completes difficulty relatively big, and enters nearly landing period at aircraft, and aircraft configuration conversion greatly, causes easily occurring safety problem. Particularly awing occurring when climatic deterioration, visibility descend rapidly degradation dangerous situation, aircraft controller cannot effectively grasp the flight posture in flying area.
But existing supervision means are all grasp the flight condition of aircraft by radar plot, the information of this means transmission is few, poor real, precision are low, it is unfavorable for that aircraft controller grasps the skyborne state of flight of aircraft in real time, it is impossible to solve the flight control under IFR conditions and booting problem.
Summary of the invention
The technical problem to be solved in the present invention is in that: provide a kind of Aircraft surveillance systems based on real-time dynamic positioning and Data-Link and method, improve aircraft and enter the supervision level of nearly landing period and the safety coefficient of flight training, improve bad weather operations commander and guidance capability.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of Aircraft surveillance systems based on real-time dynamic positioning and Data-Link, including airborne equipment and ground installation, described airborne equipment is installed aboard, for receiving satellite-signal and real time differential update information, complete the correction of Plane location data, and differentiated positional information is sent to ground in real time; Described ground installation is arranged on approach tower, is used for obtaining real time differential update information, and periodically this update information is sent to the aircraft in Ben Chang spatial domain; Receive the Differential positioning data that aerospace plane sends in real time simultaneously, and the aircraft-position information received is sent to flight monitoring terminal.
As the improvement of the present invention, described airborne equipment includes onboard satellite reception antenna and navigation neceiver, on-board data transmission equipment and airborne ultra-short wave antenna;Described onboard satellite reception antenna, is used for receiving satellite-signal; Described navigation neceiver, original almanac data for observing and record more than at least four same satellite positions information, utilize ground installation to send the real time differential update information come the positional information of the machine is modified, obtain precise position information and the time of the machine again by revised four location information, and precise position information and time are sent to on-board data transmission equipment; Described on-board data transmission equipment, sends, for receiving ground installation when receiving, the real time differential update information of coming, and gives navigation neceiver; When sending, give airborne ultra-short wave antenna according to the Networking protocol of regulation by forming radiofrequency signal behind aircraft exact position and temporal information framing, coding, modulation, power amplification; Described airborne ultra-short wave antenna and described on-board data transmission equipment coordinate, for receiving from the radiofrequency signal of ground installation and radiation from the radiofrequency signal of on-board data transmission equipment.
As a further improvement on the present invention, described ground installation includes terrestrial reference station satellite earth antenna, terrestrial reference station terminal unit, terrestrial reference station data transmission set and terrestrial reference station ultrashort wave antenna, flight monitoring terminal; Described terrestrial reference station satellite earth antenna, is used for receiving satellite-signal; Described terrestrial reference station terminal unit, for carrying out three-dimensional localization after observing four aeronautical satellites, calculate the coordinate of base station, poor with base station known coordinate, obtain Differential corrections, and Differential corrections is sent to terrestrial reference station data transmission set; Described terrestrial reference station data transmission set, for when sending, completing the coding of Differential corrections, modulation, amplification, and give terrestrial reference station ultrashort wave antenna; When receiving, receive, according to the procotol of regulation, the accurate position of this airplane and the temporal information that aerial every airplane sends; Described terrestrial reference station ultrashort wave antenna and described terrestrial reference station data transmission set coordinate, for receiving from aerial radiofrequency signal and radiating the radiofrequency signal from terrestrial reference station data transmission set; Described flight monitoring terminal, for receiving the exact position monitoring every airplane in spatial domain and temporal information that terrestrial reference station data transmission set sends here, by aircraft-position information with enter nearly channel information integrated display, for aircraft controller.
A kind of aircraft adopted based on real-time dynamic positioning and the Aircraft surveillance systems of Data-Link enters nearly supervision method, comprises the following steps:
Step 1: terrestrial reference station satellite earth antenna and terrestrial reference station terminal unit four aeronautical satellites of observation, calculates Differential corrections, and is sent to terrestrial reference station data transmission set;
Step 2: terrestrial reference station data transmission set completes the coding of Differential corrections, modulation, amplification, and by terrestrial reference station ultrashort wave antenna to external radiation;
Step 3: on-board data transmission equipment and airborne ultra-short wave antenna on every airplane receive Differential corrections, and deliver to navigation neceiver;
Step 4: every airplane utilizes the original almanac data location information that more than at least four same satellite were observed and recorded to onboard satellite reception antenna and navigation neceiver; The navigation neceiver positional information of Differential corrections correction the machine, and accurate position and temporal information are given the on-board data transmission equipment on aircraft;
Step 5: the on-board data transmission equipment on every airplane passes through airborne ultra-short wave antenna to the accurate position of this airplane of external radiation and temporal information according to the procotol of regulation;
Step 6: terrestrial reference station data receiver and terrestrial reference station ultrashort wave antenna receive the exact position and temporal information that monitor that in spatial domain, every airplane sends, and are sent to flight monitoring terminal;
Step 7: the aircraft-position information according to real-time reception, merges Aircraft Targets and is shown in three-dimensional scenic; According to flight training handbook, generate aircraft safety and enter nearly channel information, aircraft safety is entered nearly passage and is shown in three-dimensional scenic.
Compared with prior art, the method have technical effect that:
The present invention is dynamically positioned by comprehensive integration real time differential and transmits with data, construct aircraft and enter nearly supervision system, obtain in real time in Ben Chang spatial domain aircraft-position information and automatically generate aircraft and enter nearly passage, by aircraft-position information and enter nearly channel information integrated display in flight monitoring terminal, compensate for the deficiency of existing supervision means, new hands section is provided for flight control, in visual mode, aircraft entered the precise position information in nearly stage real-time, continuously, stable sends aircraft controller to, ensure that on ground in the face of aircraft enters the monitoring of nearly landing period, aircraft controller or pilotinstructorpiston's real-time deviation correcting can be made, improve the safety coefficient of flight training and aircraft enters the supervision level of nearly landing period, the present invention can be used for flight control, air traffic control, particularly awing occur when climatic deterioration, visibility descend rapidly degradation dangerous situation, can realize the monitor in real time of aerial target positional information, attitude information in Ben Chang spatial domain, there is provided decision-making assistant information for aircraft controller, improve flight safety training coefficient.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in the following describes is some embodiments of the present invention, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the structural representation of the airborne equipment of the present invention;
Fig. 2 is the structural representation of the ground installation of the present invention;
In figure:
1-onboard satellite reception antenna 2-navigation neceiver 3-airborne ultra-short wave antenna
Satellite earth antenna 6-terrestrial reference station, 4-on-board data transmission equipment 5-terrestrial reference station terminal unit
Ultrashort wave antenna 8-terrestrial reference station, 7-terrestrial reference station data transmission set 9-flight monitoring terminal
Detailed description of the invention
For making the purpose of the embodiment of the present invention, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is a part of embodiment of the present invention, rather than whole embodiments. Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
As illustrated in fig. 1 and 2, a kind of Aircraft surveillance systems based on real-time dynamic positioning and Data-Link, including airborne equipment and ground installation, airborne equipment is installed aboard, for receiving satellite-signal and real time differential update information, complete the correction of Plane location data, and differentiated positional information is sent to ground in real time;Ground installation is arranged on approach tower, is used for obtaining real time differential update information, and periodically this update information is sent to the aircraft in Ben Chang spatial domain; Receive the Differential positioning data that aerospace plane sends in real time simultaneously, and the aircraft-position information received is sent to flight monitoring terminal 9.
As it is shown in figure 1, airborne equipment includes onboard satellite reception antenna 1 and navigation neceiver 2, on-board data transmission equipment 4 and airborne ultra-short wave antenna 3; Onboard satellite reception antenna 1 is used for receiving satellite-signal; Navigation neceiver 2, original almanac data for observing and record more than at least four same satellite positions information, utilize ground installation to send the real time differential update information come the positional information of the machine is modified, obtain precise position information and the time of the machine again by revised four location information, and precise position information and time are sent to on-board data transmission equipment 4; On-board data transmission equipment 4, sends, for receiving ground installation when receiving, the real time differential update information of coming, and gives navigation neceiver 2; When sending, give airborne ultra-short wave antenna 3 according to the Networking protocol of regulation by forming radiofrequency signal behind aircraft exact position and temporal information framing, coding, modulation, power amplification; Airborne ultra-short wave antenna 3 and on-board data transmission equipment 4 coordinate, for receiving from the radiofrequency signal of ground installation and radiation from the radiofrequency signal of on-board data transmission equipment 4.
As in figure 2 it is shown, ground installation includes terrestrial reference station satellite earth antenna 5, terrestrial reference station terminal unit 6, terrestrial reference station data transmission set 8 and terrestrial reference station ultrashort wave antenna 7, flight monitoring terminal 9; Terrestrial reference station satellite earth antenna 5, is used for receiving satellite-signal; Terrestrial reference station terminal unit 6, carries out three-dimensional localization after being used for observing four aeronautical satellites, calculates the coordinate of base station, poor with base station known coordinate, obtains Differential corrections, and Differential corrections is sent to terrestrial reference station data transmission set 8; Terrestrial reference station data transmission set 8, for when sending, completing the coding of Differential corrections, modulation, amplification, and give terrestrial reference station ultrashort wave antenna 7; When receiving, receive, according to the procotol of regulation, the accurate position of this airplane and the temporal information that aerial every airplane sends; Terrestrial reference station ultrashort wave antenna 7 and terrestrial reference station data transmission set 8 coordinate, for receiving from aerial radiofrequency signal and radiating the radiofrequency signal from terrestrial reference station data transmission set 8; Flight monitoring terminal 9, for receiving the exact position monitoring every airplane in spatial domain and temporal information that terrestrial reference station data transmission set 8 sends here, by aircraft-position information with enter nearly channel information integrated display, for aircraft controller.
The present invention is dynamically positioned by comprehensive integration real time differential and transmits with data, construct aircraft and enter nearly supervision system, obtain in real time in Ben Chang spatial domain aircraft-position information and automatically generate aircraft and enter nearly passage, by aircraft-position information and enter nearly channel information integrated display in flight monitoring terminal, compensate for the deficiency of existing supervision means, new hands section is provided for flight control, in visual mode, aircraft entered the precise position information in nearly stage real-time, continuously, stable sends aircraft controller to, ensure that on ground in the face of aircraft enters the monitoring of nearly landing period, aircraft controller or pilotinstructorpiston's real-time deviation correcting can be made, improve the safety coefficient of flight training and aircraft enters the supervision level of nearly landing period,The present invention can be used for flight control, air traffic control, particularly awing occur when climatic deterioration, visibility descend rapidly degradation dangerous situation, can realize the monitor in real time of aerial target positional information, attitude information in Ben Chang spatial domain, there is provided decision-making assistant information for aircraft controller, improve flight safety training coefficient.
A kind of aircraft adopted based on real-time dynamic positioning and the Aircraft surveillance systems of Data-Link enters nearly supervision method, comprises the following steps:
Step 1: terrestrial reference station satellite earth antenna 5 and terrestrial reference station terminal unit 6 observe four aeronautical satellites, calculates Differential corrections, and is sent to terrestrial reference station data transmission set 8;
Step 2: terrestrial reference station data transmission set 8 completes the coding of Differential corrections, modulation, amplification, and by terrestrial reference station ultrashort wave antenna 7 to external radiation;
Step 3: on-board data transmission equipment 4 and airborne ultra-short wave antenna 3 on every airplane receive Differential corrections, and deliver to navigation neceiver 2;
Step 4: every airplane utilizes the original almanac data location information that more than at least four same satellite were observed and recorded to onboard satellite reception antenna 1 and navigation neceiver 2; Navigation neceiver 2 positional information of Differential corrections correction the machine, and accurate position and temporal information are given the on-board data transmission equipment 4 on aircraft;
Step 5: the on-board data transmission equipment 4 on every airplane passes through airborne ultra-short wave antenna 3 to the accurate position of this airplane of external radiation and temporal information according to the procotol of regulation;
Step 6: terrestrial reference station data receiver and terrestrial reference station ultrashort wave antenna 7 receive the exact position and temporal information that monitor that in spatial domain, every airplane sends, and are sent to flight monitoring terminal 9;
Step 7: the aircraft-position information according to real-time reception, merges Aircraft Targets and is shown in three-dimensional scenic; According to flight training handbook, generate aircraft safety and enter nearly channel information, aircraft safety is entered nearly passage and is shown in three-dimensional scenic.
Last it is noted that above example is only in order to illustrate technical scheme, it is not intended to limit; Although the present invention being described in detail with reference to previous embodiment, it will be understood by those within the art that: the technical scheme described in foregoing embodiments still can be modified by it, or wherein portion of techniques feature is carried out equivalent replacement; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.
Claims (4)
1. based on an Aircraft surveillance systems for real-time dynamic positioning and Data-Link, including airborne equipment and ground installation, it is characterised in that:
Described airborne equipment is installed aboard, is used for receiving satellite-signal and real time differential update information, completes the correction of Plane location data, and differentiated positional information is sent to ground in real time;
Described ground installation is arranged on approach tower, is used for obtaining real time differential update information, and periodically this update information is sent to the aircraft in Ben Chang spatial domain; Receive the Differential positioning data that aerospace plane sends in real time simultaneously, and the aircraft-position information received is sent to flight monitoring terminal.
2. a kind of Aircraft surveillance systems based on real-time dynamic positioning and Data-Link according to claim 1, it is characterised in that: wherein said airborne equipment includes onboard satellite reception antenna and navigation neceiver, on-board data transmission equipment and airborne ultra-short wave antenna;
Described onboard satellite reception antenna, is used for receiving satellite-signal;
Described navigation neceiver, original almanac data for observing and record more than at least four same satellite positions information, utilize ground installation to send the real time differential update information come the positional information of the machine is modified, obtain precise position information and the time of the machine again by revised four location information, and precise position information and time are sent to on-board data transmission equipment;
Described on-board data transmission equipment, sends, for receiving ground installation when receiving, the real time differential update information of coming, and gives navigation neceiver; When sending, give airborne ultra-short wave antenna according to the Networking protocol of regulation by forming radiofrequency signal behind aircraft exact position and temporal information framing, coding, modulation, power amplification;
Described airborne ultra-short wave antenna and described on-board data transmission equipment coordinate, for receiving from the radiofrequency signal of ground installation and radiation from the radiofrequency signal of on-board data transmission equipment.
3. a kind of Aircraft surveillance systems based on real-time dynamic positioning and Data-Link according to claim 1 and 2, it is characterised in that: wherein said ground installation includes terrestrial reference station satellite earth antenna, terrestrial reference station terminal unit, terrestrial reference station data transmission set and terrestrial reference station ultrashort wave antenna, flight monitoring terminal;
Described terrestrial reference station satellite earth antenna, is used for receiving satellite-signal;
Described terrestrial reference station terminal unit, for carrying out three-dimensional localization after observing four aeronautical satellites, calculate the coordinate of base station, poor with base station known coordinate, obtain Differential corrections, and Differential corrections is sent to terrestrial reference station data transmission set;
Described terrestrial reference station data transmission set, for when sending, completing the coding of Differential corrections, modulation, amplification, and give terrestrial reference station ultrashort wave antenna; When receiving, receive, according to the procotol of regulation, the accurate position of this airplane and the temporal information that aerial every airplane sends;
Described terrestrial reference station ultrashort wave antenna and described terrestrial reference station data transmission set coordinate, for receiving from aerial radiofrequency signal and radiating the radiofrequency signal from terrestrial reference station data transmission set;
Described flight monitoring terminal, for receiving the exact position monitoring every airplane in spatial domain and temporal information that terrestrial reference station data transmission set sends here, by aircraft-position information with enter nearly channel information integrated display, for aircraft controller.
4. one kind adopts the aircraft based on real-time dynamic positioning and the Aircraft surveillance systems of Data-Link as claimed in claim 1 to enter nearly supervision method, it is characterised in that comprise the following steps:
Step 1: terrestrial reference station satellite earth antenna and terrestrial reference station terminal unit four aeronautical satellites of observation, calculates Differential corrections, and is sent to terrestrial reference station data transmission set;
Step 2: terrestrial reference station data transmission set completes the coding of Differential corrections, modulation, amplification, and by terrestrial reference station ultrashort wave antenna to external radiation;
Step 3: on-board data transmission equipment and airborne ultra-short wave antenna on every airplane receive Differential corrections, and deliver to navigation neceiver;
Step 4: every airplane utilizes the original almanac data location information that more than at least four same satellite were observed and recorded to onboard satellite reception antenna and navigation neceiver; The navigation neceiver positional information of Differential corrections correction the machine, and accurate position and temporal information are given the on-board data transmission equipment on aircraft;
Step 5: the on-board data transmission equipment on every airplane passes through airborne ultra-short wave antenna to the accurate position of this airplane of external radiation and temporal information according to the procotol of regulation;
Step 6: terrestrial reference station data receiver and terrestrial reference station ultrashort wave antenna receive the exact position and temporal information that monitor that in spatial domain, every airplane sends, and are sent to flight monitoring terminal;
Step 7: the aircraft-position information according to real-time reception, merges Aircraft Targets and is shown in three-dimensional scenic; According to flight training handbook, generate aircraft safety and enter nearly channel information, aircraft safety is entered nearly passage and is shown in three-dimensional scenic.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610005958.9A CN105676246A (en) | 2016-01-06 | 2016-01-06 | Airplane monitor system and method on the basis of real-time dynamic positioning and data link |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610005958.9A CN105676246A (en) | 2016-01-06 | 2016-01-06 | Airplane monitor system and method on the basis of real-time dynamic positioning and data link |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105676246A true CN105676246A (en) | 2016-06-15 |
Family
ID=56299058
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610005958.9A Pending CN105676246A (en) | 2016-01-06 | 2016-01-06 | Airplane monitor system and method on the basis of real-time dynamic positioning and data link |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105676246A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107310735A (en) * | 2017-01-19 | 2017-11-03 | 中国人民解放军海军航空工程学院青岛校区 | A kind of multi-mode enters nearly Landing Guidance System |
| CN107356230A (en) * | 2017-07-12 | 2017-11-17 | 深圳市武测空间信息有限公司 | A kind of digital mapping method and system based on outdoor scene threedimensional model |
| CN107590757A (en) * | 2017-08-25 | 2018-01-16 | 乐琦（北京）科技有限公司 | A kind of unmanned plane Driving Test method and its intelligent apparatus |
| CN109150282A (en) * | 2018-06-15 | 2019-01-04 | 上海卫星工程研究所 | Ground fortune control network system suitable for the real-time continuous monitoring in the space-based whole world |
| WO2019095122A1 (en) * | 2017-11-14 | 2019-05-23 | 华为技术有限公司 | Data transmission method, network device, and server |
| CN109839650A (en) * | 2019-01-04 | 2019-06-04 | 哈瓦国际航空技术（深圳）有限公司 | A kind of compatible RTK localization method of unmanned plane, system, equipment and storage medium |
| CN111986522A (en) * | 2020-07-29 | 2020-11-24 | 广州市新航科技有限公司 | Airborne equipment positioning method based on ADS-B signal, airborne equipment and storage medium thereof |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050125142A1 (en) * | 2003-10-07 | 2005-06-09 | Akihiro Yamane | Navigation apparatus and navigation method with image recognition |
| CN101989363A (en) * | 2009-07-30 | 2011-03-23 | 中国商用飞机有限责任公司 | System and method for processing digital air data |
| CN105720369A (en) * | 2014-12-03 | 2016-06-29 | 中航通飞研究院有限公司 | Novel telemetry antenna tracking method |
-
2016
- 2016-01-06 CN CN201610005958.9A patent/CN105676246A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050125142A1 (en) * | 2003-10-07 | 2005-06-09 | Akihiro Yamane | Navigation apparatus and navigation method with image recognition |
| CN101989363A (en) * | 2009-07-30 | 2011-03-23 | 中国商用飞机有限责任公司 | System and method for processing digital air data |
| CN105720369A (en) * | 2014-12-03 | 2016-06-29 | 中航通飞研究院有限公司 | Novel telemetry antenna tracking method |
Non-Patent Citations (2)
| Title |
|---|
| 贾绍文 等: "飞机飞行数据实时传输系统", 《兵工自动化》 * |
| 马捷中 等: "飞行数据管理记录系统的数据采集技术实现", 《计算机工程与设计》 * |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107310735A (en) * | 2017-01-19 | 2017-11-03 | 中国人民解放军海军航空工程学院青岛校区 | A kind of multi-mode enters nearly Landing Guidance System |
| CN107356230A (en) * | 2017-07-12 | 2017-11-17 | 深圳市武测空间信息有限公司 | A kind of digital mapping method and system based on outdoor scene threedimensional model |
| CN107356230B (en) * | 2017-07-12 | 2020-10-27 | 深圳市武测空间信息有限公司 | Digital mapping method and system based on live-action three-dimensional model |
| CN107590757A (en) * | 2017-08-25 | 2018-01-16 | 乐琦（北京）科技有限公司 | A kind of unmanned plane Driving Test method and its intelligent apparatus |
| WO2019095122A1 (en) * | 2017-11-14 | 2019-05-23 | 华为技术有限公司 | Data transmission method, network device, and server |
| CN111345070A (en) * | 2017-11-14 | 2020-06-26 | 华为技术有限公司 | Data transmission method, network equipment and server |
| CN111345070B (en) * | 2017-11-14 | 2021-06-22 | 华为技术有限公司 | Data transmission method, network equipment and server |
| US11546265B2 (en) | 2017-11-14 | 2023-01-03 | Huawei Technologies Co., Ltd. | Data transmission method, network device, and server for transmitting assistance data |
| CN109150282A (en) * | 2018-06-15 | 2019-01-04 | 上海卫星工程研究所 | Ground fortune control network system suitable for the real-time continuous monitoring in the space-based whole world |
| CN109839650A (en) * | 2019-01-04 | 2019-06-04 | 哈瓦国际航空技术（深圳）有限公司 | A kind of compatible RTK localization method of unmanned plane, system, equipment and storage medium |
| CN111986522A (en) * | 2020-07-29 | 2020-11-24 | 广州市新航科技有限公司 | Airborne equipment positioning method based on ADS-B signal, airborne equipment and storage medium thereof |
| CN111986522B (en) * | 2020-07-29 | 2022-03-22 | 广州市新航科技有限公司 | Airborne equipment positioning method based on ADS-B signal, airborne equipment and storage medium thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105676246A (en) | Airplane monitor system and method on the basis of real-time dynamic positioning and data link | |
| RU2692306C2 (en) | Tracking system for unmanned aerial vehicles | |
| CN103592948B (en) | Unmanned plane flight collision avoidance method | |
| CN109147398B (en) | Target monitoring and tracking performance optimization method for airborne collision avoidance system | |
| KR101494654B1 (en) | Method and Apparatus for Guiding Unmanned Aerial Vehicle and Method and Apparatus for Controlling Unmanned Aerial Vehicle | |
| US10911132B2 (en) | Low earth orbit satellite for air traffic control | |
| US20180181125A1 (en) | On-ground vehicle collision avoidance utilizing unmanned aerial vehicles | |
| RU2703412C2 (en) | Automatic aircraft landing method | |
| CN112486199A (en) | Unmanned aerial vehicle inspection control system and method suitable for remote power transmission tower group | |
| US10771993B2 (en) | Method for determining a quality of at least one mobile radio network | |
| RU100836U1 (en) | COMPLEX OF CONTROL AND CONTROL FOR SELF-DRIVING ON LOCAL AIRLINES ON THE BASIS OF MODERN TECHNOLOGIES | |
| WO2019170649A1 (en) | Air position information- and traffic management system for unmanned and manned aircraft | |
| CN109613929B (en) | Flight precision approach and landing method and system | |
| DE10120537A1 (en) | Procedure with an interferometric ROSAR device | |
| CN107579768B (en) | Aviation control system based on wireless laser communication | |
| CN103213685A (en) | Aircraft fixed point landing image guide method and landing image system thereof | |
| CN104539906A (en) | Image/laser ranging/ABS-B monitoring integrated system | |
| CN110850456A (en) | Positioning equipment, positioning method and monitoring device of high-altitude unmanned aerial vehicle | |
| CN102706350A (en) | Method for indicating yaw navigation of airplane | |
| CN203318684U (en) | Aircraft fixed-point landing image system | |
| RU2710983C1 (en) | Method of multi-position observation, control and management over flights of manned and unmanned aerial systems in common air space | |
| GB2165427A (en) | Dynamic graphic displays in vehicles | |
| Eltahier et al. | Review of instrument landing system | |
| CN111813141A (en) | Flight mission control system and method for remotely controlling unmanned aerial vehicle | |
| JPH11345399A (en) | Landing guide system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160615 |
|
| WD01 | Invention patent application deemed withdrawn after publication |