CN108932875B - Intelligent airplane berth indicating system with high safety performance - Google Patents
Intelligent airplane berth indicating system with high safety performance Download PDFInfo
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- CN108932875B CN108932875B CN201810888875.8A CN201810888875A CN108932875B CN 108932875 B CN108932875 B CN 108932875B CN 201810888875 A CN201810888875 A CN 201810888875A CN 108932875 B CN108932875 B CN 108932875B
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0043—Traffic management of multiple aircrafts from the ground
Abstract
The invention discloses an aircraft berth intelligent indicating system with high safety performance, which comprises an information acquisition unit, a berth operation main control module, a corridor bridge automatic control module, a wireless communication module, a remote control center, an information receiving and transmitting module, an information processing and controlling module, an infrared signal receiving module, an aircraft positioning module, an intelligent voice prompting module, a real-time infrared image display module, a data storage module and a detection information display module, wherein the information acquisition unit comprises a video acquisition module, a berth infrared projection module, an infrared image acquisition module, a laser distance measurement sensing module, a speed measurement module, a middle shaft positioning sensing module, a corridor bridge positioning module, a first infrared signal transmitting module and a second infrared signal transmitting module. The invention has high safety performance, can effectively improve the airplane berthing precision, has the prompting function and the real-time data comparison function, can remotely control the airplane berthing, and meets the requirement of rapid, accurate and efficient berthing guidance.
Description
Technical Field
the invention relates to the technical field of airplane berth indicating systems, in particular to an airplane berth intelligent indicating system with high safety performance.
Background
The automatic indicating system for the airplane berth can provide accurate and normative guidance for safe and efficient berthing of the airplane on the parking apron and guide a pilot to berth the airplane in an optimal procedure. The airplane berthing process is a component in flight operation, and the use of auxiliary equipment for improving the efficiency and the safety of flight operation is also a component in the modernization construction of airports.
However, the conventional airplane berth indicating system mainly adopts a video measurement image identification method and a triggered coil induction detection method, wherein the video measurement image identification method is used for capturing an airplane running track through a video camera image tracking technology, but the influence of weather and light is large, a large error and a certain error probability exist, and potential safety hazards exist; the triggering type coil induction detection method is characterized in that the position of an airplane is determined through an induction coil buried under the ground, and the triggering type coil induction detection method has the defects of easiness in damage, low precision and low safety performance; an airplane berth intelligent indicating system which has high safety performance, a prompting function, a multi-time data comparison function, can remotely control an airplane to berth and meets the requirement of rapid, accurate and efficient berth guidance is urgently needed.
Therefore, the invention provides an intelligent indicating system for airplane berth with high safety performance to solve the problems.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an intelligent indicating system for airplane berth with high safety performance, and solves the problems that the indicating system for airplane berth has low safety performance, low indicating precision and low efficiency, and can not meet the requirement of rapid, accurate and efficient berth guidance.
In order to achieve the purpose, the invention is realized by the following technical scheme: an aircraft berth intelligent indicating system with high safety performance comprises an information acquisition unit, a berth operation main control module, a corridor bridge automatic control module, a wireless communication module, a remote control center, an information transceiving module, an information processing and control module, an infrared signal receiving module, an aircraft positioning module, an intelligent voice prompt module, a real-time infrared image display module, a data storage module and a detection information display module, wherein the information acquisition unit comprises a video acquisition module, a berth infrared projection module, an infrared image acquisition module, a laser ranging sensing module, a speed measurement module, a middle shaft positioning sensing module, a corridor bridge positioning module, a first infrared signal transmitting module and a second infrared signal transmitting module, the video acquisition module is connected with the berth operation main control module and is used for tracking and capturing an aircraft image running track running on an aircraft berth traction channel, the parking space infrared projection module is connected with the parking space operation main control module and used for carrying out infrared projection on a parking space on an airplane parking space traction channel, the infrared image acquisition module is connected with the parking space operation main control module and used for capturing an infrared projection image, an airplane image and a running track on the parking space in real time, the laser distance measurement sensing module and the speed measurement module are respectively connected with the parking space operation main control module and used for detecting the distance between the airplane and the two sides of the airplane parking space traction channel and the running speed of the airplane in real time, the middle shaft positioning sensing module is connected with the parking space operation main control module and used for indicating the airplane to run along the central line of the airplane parking space traction channel, the gallery bridge positioning module is connected with the parking space operation main control module and used for detecting the height difference between a gallery bridge and an airplane boarding gate, and the first infrared signal transmitting module and the second infrared signal transmitting module are respectively connected with the parking space operation main control module, the system is used for positioning and detecting the boarding gate of the airplane, the corridor bridge automatic control module is connected with the berth operation main control module and is used for controlling the corridor bridge to run to a position corresponding to the boarding gate of the airplane, the berth operation main control module is connected with a remote control center through a wireless communication module and is used for realizing remote control, the berth operation main control module is connected with the information processing and control module through an information transceiving module, the infrared signal receiving module is connected with the information processing and control module and is used for receiving infrared signals of a first infrared signal transmitting module and a second infrared signal transmitting module, the airplane positioning module is used for positioning the airplane in real time, the intelligent voice prompt module is connected with the information processing and control module and is used for prompting a pilot to lead the airplane running circuit to deviate from the central line of a berth traction channel of the airplane through voice, and the real-time infrared image display module is connected with the information, the data storage module is connected with the information processing and control module, is used for storing various detection data, calculation results and supplying the information processing and control module to extract standard data, displays the standard data through the detection information display module, compares the standard data with the real-time detection data, and is connected with the information processing and control module, is used for displaying various data, detection information and calculation results, and is convenient for a pilot to adjust the running track.
Furthermore, the video acquisition module adopts a video camera and captures the running track of the airplane through an image tracking technology.
Furthermore, the infrared projection module of the parking space adopts an infrared projector to perform regional infrared projection on the parking space, the body shell of the airplane adopts a special material which does not reflect light but reflects an infrared light source, and the infrared image acquisition module captures the running track of the airplane.
Furthermore, the laser ranging sensing module adopts a laser sensor, the speed measuring module adopts a speed measuring sensor, the laser sensor and the speed measuring sensor are provided with a plurality of sensors and are correspondingly arranged at two sides of the aircraft berth traction channel, and the laser sensors and the speed measuring sensor at two sides are alternately arranged.
Furthermore, the middle shaft positioning induction module adopts a first satellite positioning antenna, and the first satellite positioning antenna is installed at the axial end part of the central line of the aircraft berth traction channel and is positioned at the outer end of the aircraft takeoff line and used for detecting the angle between the aircraft body and the central line when the aircraft runs.
Further, first infra-red signal emission module and second infra-red signal emission module adopt first infra-red transmitter and second infra-red transmitter respectively, the gallery bridge includes anterior segment, middle section and back end, and first infra-red transmitter corresponds the lateral part that sets up in the middle section, and second infra-red transmitter corresponds the top that sets up in the anterior segment, infra-red signal receiving module adopts the infra-red receiver who matches with first infra-red transmitter and second infra-red transmitter model, and infra-red receiver sets up in the upper end of aircraft gate, and infra-red receiver, first infra-red transmitter and second infra-red transmitter's height is the same, gallery bridge orientation module adopts second satellite positioning antenna, corresponds to install in the anterior segment top and be located one side of second infra-red transmitter for the difference in height of real-time detection anterior segment and aircraft gate.
Further, when the gallery bridge is in an initial state, an acute angle is formed between the axial direction of the middle section and the axial direction of the aircraft berth traction channel, the first infrared emitter is installed on the side portion, close to the aircraft, of the middle section, and the infrared signal direction transmitted by the first infrared emitter is perpendicular to the axial direction of the aircraft berth traction channel.
Furthermore, the detection information display module adopts a touch display screen, so that the man-machine interaction of a pilot is facilitated.
compared with the prior art, the invention has the advantages that:
1. This aircraft berth intelligence indicating system that security performance is high, through video acquisition module and berth position infrared projection module and the cooperation setting of infrared image acquisition module in the information acquisition unit, realize aircraft discernment and position detection through the mode of two image tracking and orbit seizure, effectively reduce detection error, improved the berth precision, the security is high.
2. This aircraft berth intelligence indicating system that security performance is high, through laser rangefinder sensing module among the information acquisition unit, the module tests the speed, axis location response module, shelter bridge orientation module, the cooperation setting of first infrared signal emission module and second infrared signal emission module, can assist and pull the aircraft and pull straight line traveling on the passageway at aircraft berth, for the aircraft provides quick, accurate, efficient berth guide, when further having improved the berth precision, cooperation shelter bridge automatic control module, can realize the automatic butt joint of shelter bridge, high work efficiency.
3. This aircraft berth intelligence indicating system that security performance is high, through berth operation host system, information transceiver module, information processing and control module, the cooperation setting of data storage module and detection information display module, through berth operation host system with the detection data and the operation result of gathering send for information processing and control module through information transceiver module, carry out data display through detection information display module, the standard data information that returns back through data storage module is shown simultaneously, through comparing detection data and standard data in real time, the pilot of being convenient for carries out flight path adjustment, realize accurate berth.
4. The intelligent indicating system for the airplane berth with high safety performance can intelligently prompt a pilot to carry out berth adjustment and simultaneously realize the remote control of the airplane berth through the matching arrangement of the berth operation main control module, the wireless communication module, the remote control center, the information processing and control module and the intelligent voice prompt module.
Drawings
FIG. 1 is a simplified schematic illustration of an aircraft berth towing corridor according to the present invention;
FIG. 2 is a simplified illustration of infrared projection of a parking lot in accordance with the present invention;
FIG. 3 is a schematic block diagram of an information acquisition unit and a berthing operation main control module according to the present invention;
FIG. 4 is a schematic block diagram of a berthing operation main control module and an information processing and controlling module according to the present invention;
FIG. 5 is a schematic block diagram of an information processing and control module and various modules according to the present invention;
Fig. 6 is a simplified illustration of the relationship between the aircraft and the veranda bridge in the present invention, both docked and undocked.
In the figure: 1. an information acquisition unit; 101. a video acquisition module; 102. a dock infrared projection module; 103. an infrared image acquisition module; 104. a laser ranging sensing module; 105. a speed measuring module; 106. a middle shaft positioning induction module; 107. a gallery bridge positioning module; 108. a first infrared signal transmitting module; 109. a second infrared signal transmitting module; 2. a berth operation main control module; 3. a corridor bridge automatic control module; 4. a wireless communication module; 5. a remote control center; 6. an information transceiving module; 7. an information processing and control module; 8. an infrared signal receiving module; 9. an aircraft positioning module; 10. an intelligent voice prompt module; 11. a real-time infrared image display module; 12. a data storage module; 13. an aircraft berth traction channel; 14. an aircraft; 15. a parking place; 16. a gallery bridge; 1601. a front section; 1602. a middle section; 1603. a rear section; 17. and detecting an information display module.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
as shown in fig. 1 to 6, the present invention provides a technical solution: an aircraft berth intelligent indicating system with high safety performance comprises an information acquisition unit 1, a berth operation main control module 2, a corridor bridge automatic control module 3, a wireless communication module 4, a remote control center 5, an information receiving and transmitting module 6, an information processing and controlling module 7, an infrared signal receiving module 8, an aircraft positioning module 9, an intelligent voice prompting module 10, a real-time infrared image display module 11, a data storage module 12 and a detection information display module 17, wherein the information acquisition unit 1 comprises a video acquisition module 101, a berth infrared projection module 102, an infrared image acquisition module 103, a laser ranging sensing module 104, a speed measuring module 105, a middle shaft positioning sensing module 106, a corridor bridge positioning module 107, a first infrared signal transmitting module 108 and a second infrared signal transmitting module 109, wherein the video acquisition module 101 is connected with the berth operation main control module 2, the system is used for tracking images and capturing a running track of an airplane 14 running on an airplane berth traction channel 13, a berth infrared projection module 102 is connected with a berth operation main control module 2 and is used for performing infrared projection on a berth 15 on the airplane berth traction channel, an infrared image acquisition module 103 is connected with the berth operation main control module 2 and is used for capturing infrared projection images on the berth 15 and images and running tracks of the airplane 14 in real time, a laser ranging sensing module 104 and a speed measuring module 105 are respectively connected with the berth operation main control module 2 and are used for detecting the distance between the airplane 14 and the two sides of the airplane berth traction channel 13 and the running speed of the airplane 14 in real time, a middle shaft positioning sensing module 106 is connected with the berth operation main control module 2 and is used for indicating the airplane 14 to run along a central line of the airplane berth traction channel 13, and a corridor bridge positioning module 107 is connected with the berth operation main control, the device is used for detecting the height difference between a corridor bridge 16 and a boarding gate of an airplane 14, a first infrared signal transmitting module 108 and a second infrared signal transmitting module 109 are respectively connected with a berth operation main control module 2 and used for positioning and detecting the boarding gate of the airplane 14, a corridor bridge automatic control module 3 is connected with the berth operation main control module 2 and used for controlling the corridor bridge 16 to run to a position corresponding to the boarding gate of the airplane 14, the berth operation main control module 2 is connected with a remote control center 5 through a wireless communication module 4 and used for realizing remote control, the berth operation main control module 2 is connected with an information processing and control module 7 through an information transceiver module 6, an infrared signal receiving module 8 is connected with the information processing and control module 7 and used for receiving infrared signals of the first infrared signal transmitting module 108 and the second infrared signal transmitting module 109, and an airplane positioning module 9 is used for positioning the airplane 14 in real time, the intelligent voice prompt module 10 is connected with the information processing and control module 7 and used for voice prompting a pilot that an operation line of an airplane 14 deviates from a central line of an airplane berth traction channel 13, the real-time infrared image display module 11 is connected with the information processing and control module 7 and used for displaying infrared projection information acquired by receiving the infrared image acquisition module 103 in real time, the data storage module 12 is connected with the information processing and control module 7 and used for storing various detection data, calculation results and extracting standard data for the information processing and control module 7, the standard data are displayed through the detection information display module 17 and are compared with the real-time detection data, and the detection information display module 17 is connected with the information processing and control module 7 and used for displaying various data, detection information and calculation results, so that the pilot can conveniently adjust an operation track.
Specifically, the video capture module 101 uses a video camera to capture the operation track of the airplane 14 by using an image tracking technology.
Specifically, the parking lot infrared projection module 102 uses an infrared projector to perform regional infrared projection on the parking lot 15, the airframe shell of the airplane 14 uses a special material which does not reflect light but reflects an infrared light source, and the infrared image collection module 103 captures the moving track of the airplane 14.
Specifically, the laser distance measuring sensing module 104 adopts a laser sensor, the speed measuring module 105 adopts a speed measuring sensor, the laser sensors and the speed measuring sensor are provided in a plurality, the laser sensors and the speed measuring sensor are correspondingly arranged on two sides of the aircraft berth traction channel 13, and the laser sensors and the speed measuring sensor on the two sides are alternately arranged.
specifically, the middle shaft positioning sensing module 106 adopts a first satellite positioning antenna, which is installed at the axial end of the central line of the aircraft berth traction channel 13 and located at the outer end of the takeoff line of the aircraft 14, and is used for detecting the angle between the body and the central line when the aircraft 14 runs.
Specifically, first infrared signal transmitting module 108 and second infrared signal transmitting module 109 adopt first infrared transmitter and second infrared transmitter respectively, gallery bridge 16 includes anterior segment 1601, middle section 1602 and back end 1603, first infrared transmitter corresponds the lateral part that sets up in middle section 1602, the second infrared transmitter corresponds the top that sets up in anterior segment 1601, infrared signal receiving module 8 adopts the infrared receiver who matches with first infrared transmitter and second infrared transmitter model, infrared receiver sets up in the upper end of 14 gates of aircraft, infrared receiver, first infrared transmitter and second infrared transmitter's height is the same, gallery bridge positioning module 107 adopts the second satellite positioning antenna, correspond to install in anterior segment 1601 top and be located one side of second infrared transmitter, be used for the difference in height of real-time detection anterior segment 1601 and 14 gates.
Specifically, when the gallery bridge 16 is in the initial state, the axial direction of the middle section 1602 and the axial direction of the aircraft berth traction channel 13 are arranged at an acute angle, the first infrared emitter is installed at the side part of the middle section 1602 close to the aircraft 14, and the direction of the infrared signal emitted by the first infrared emitter is perpendicular to the axial direction of the aircraft berth traction channel 13.
Specifically, the detection information display module 17 adopts a touch display screen, so that the human-computer interaction of the pilot is facilitated.
when the airplane 14 identification and position detection device is used, the airplane 14 identification and position detection are realized in a double-image tracking and running track capturing mode through the matched arrangement of the video acquisition module 101, the berth position infrared projection module 102 and the infrared image acquisition module 103 in the information acquisition unit 1; through the matching arrangement of the laser ranging sensing module 104, the speed measuring module 105, the middle shaft positioning sensing module 106, the corridor bridge positioning module 107, the first infrared signal transmitting module 108 and the second infrared signal transmitting module 109 in the information acquisition unit 1, the airplane 14 can be assisted to be dragged to run on the airplane berth traction channel 13 in a straight line, and fast, accurate and efficient berth guidance is provided for the airplane; through the matching arrangement of the berth operation main control module 2, the information transceiving module 6, the information processing and control module 7, the data storage module 12 and the detection information display module 17, the acquired detection data and operation results are sent to the information processing and control module 7 through the information transceiving module 6 through the berth operation main control module 2, data display is carried out through the detection information display module 17, meanwhile, standard data information returned back through the data storage module 12 is displayed, and by comparing the detection data with the standard data in real time, a pilot can conveniently carry out flight track adjustment, so that accurate berthing is realized; through the matching arrangement of the berthing operation main control module 2, the wireless communication module 4, the remote control center 5, the information processing and control module 7 and the intelligent voice prompt module 10, the pilot can be intelligently prompted to carry out berthing adjustment, and meanwhile, the remote control of the berthing of the airplane 14 is realized.
In conclusion, the invention has high safety performance, can effectively improve the parking precision of the airplane 14, has the prompting function and the real-time data comparison function, can remotely control the parking of the airplane 14, and meets the requirements of quick, accurate and efficient parking guidance.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents, it being noted that the electrical components appearing therein are each electrically connected to an external master controller and 220V mains, and the master controller may be a conventionally known device, such as a computer, which controls the electrical components.
Claims (7)
1. The utility model provides an aircraft berth intelligence indicating system that security performance is high which characterized in that: comprises an information acquisition unit (1), a berth operation main control module (2), a corridor bridge automatic control module (3), a wireless communication module (4), a remote control center (5), an information transceiving module (6), an information processing and control module (7), an infrared signal receiving module (8), an airplane positioning module (9), an intelligent voice prompt module (10), a real-time infrared image display module (11), a data storage module (12) and a detection information display module (17), wherein the information acquisition unit (1) comprises a video acquisition module (101), a berth infrared projection module (102), an infrared image acquisition module (103), a laser ranging sensing module (104), a speed measuring module (105), a middle shaft positioning sensing module (106), a corridor bridge positioning module (107), a first infrared signal transmitting module (108) and a second infrared signal transmitting module (109), the system comprises a video acquisition module (101), a berth operation main control module (2), a berth infrared projection module (102), a berth operation main control module (2), an infrared image acquisition module (103), a berth operation main control module (2), a laser ranging sensing module (104) and a speed measurement module (105), wherein the video acquisition module (101) is connected with the berth operation main control module (2) and used for tracking images of an airplane (14) running on an airplane berth traction channel (13) and capturing running tracks, the infrared image acquisition module (102) is connected with the berth operation main control module (2) and used for performing infrared projection on the berth (15) on the berth traction channel, capturing images and running tracks of the airplane (14) in real time, the laser ranging sensing module (104) and the speed measurement module (105) are respectively connected with the berth operation main control module (2) and used for detecting the distance between the airplane (14) and two sides of the airplane berth traction channel (13) and, the central shaft positioning induction module (106) is connected with the berth operation main control module (2) and used for indicating the airplane (14) to linearly run along the central line of the airplane berth traction channel (13), the corridor bridge positioning module (107) is connected with the berth operation main control module (2) and used for detecting the height difference between a corridor bridge (16) and the boarding gate of the airplane (14), the first infrared signal transmitting module (108) and the second infrared signal transmitting module (109) are respectively connected with the berth operation main control module (2) and used for positioning and detecting the boarding gate of the airplane (14), the corridor bridge automatic control module (3) is connected with the berth operation main control module (2) and used for controlling the corridor bridge (16) to run to the position corresponding to the boarding gate of the airplane (14), the berth operation main control module (2) is connected with the remote control center (5) through the wireless communication module (4), the berth operation main control module (2) is connected with the information processing and control module (7) through the information transceiving module (6), the infrared signal receiving module (8) is connected with the information processing and control module (7) and is used for receiving infrared signals of the first infrared signal transmitting module (108) and the second infrared signal transmitting module (109), the airplane positioning module (9) is used for positioning an airplane (14) in real time, the intelligent voice prompt module (10) is connected with the information processing and control module (7) and is used for prompting the pilot that the operation line of the airplane (14) deviates from the central line of the airplane berth traction channel (13) in a voice mode, the real-time infrared image display module (11) is connected with the information processing and control module (7) and is used for displaying infrared projection information collected by the infrared image collecting module (103) in real time, the data storage module (12) is connected with the information processing and control module (7) and is used for storing various detection data and calculation results and providing for the information processing and control module (7) to extract standard data, the standard data are displayed through the detection information display module (17) and are compared with real-time detection data, and the detection information display module (17) is connected with the information processing and control module (7) and is used for displaying various data, detection information and calculation results, so that a pilot can conveniently adjust the running track; the first infrared signal transmitting module (108) and the second infrared signal transmitting module (109) respectively adopt a first infrared transmitter and a second infrared transmitter, the gallery bridge (16) comprises a front section (1601), a middle section (1602) and a rear section (1603), a first infrared emitter is correspondingly arranged on the side of the middle section (1602), a second infrared emitter is correspondingly arranged on the top end of the front section (1601), the infrared signal receiving module (8) adopts an infrared receiver matched with the first infrared transmitter and the second infrared transmitter in model, the infrared receiver is arranged at the upper end of a boarding gate of the airplane (14), the heights of the infrared receiver, the first infrared transmitter and the second infrared transmitter are the same, the gallery bridge positioning module (107) adopts a second satellite positioning antenna, and the second infrared emitter is correspondingly arranged at the top end of the front section (1601) and positioned at one side of the second infrared emitter, and is used for detecting the height difference between the front section (1601) and the boarding gate of the airplane (14) in real time.
2. The intelligent indicating system of the airplane berth with high safety performance as claimed in claim 1, characterized in that: the video acquisition module (101) adopts a video camera to capture the running track of the airplane (14) through an image tracking technology.
3. The intelligent indicating system of the airplane berth with high safety performance as claimed in claim 1, characterized in that: the infrared projection module (102) of the parking position adopts an infrared projector to perform regional infrared projection on the parking position (15), the body shell of the airplane (14) adopts special materials which do not reflect light but reflect infrared light sources, and the running track of the airplane (14) is captured through the infrared image acquisition module (103).
4. The intelligent indicating system of the airplane berth with high safety performance as claimed in claim 1, characterized in that: the laser ranging sensor module (104) adopts a laser sensor, the speed measuring module (105) adopts a speed measuring sensor, the laser sensor and the speed measuring sensor are provided with a plurality of sensors and are correspondingly arranged on two sides of the aircraft berth traction channel (13), and the laser sensor and the speed measuring sensor on the two sides are alternately arranged.
5. The intelligent indicating system of the airplane berth with high safety performance as claimed in claim 1, characterized in that: the middle shaft positioning induction module (106) adopts a first satellite positioning antenna, the first satellite positioning antenna is installed at the axial end part of the central line of the aircraft berth traction passage (13) and is positioned at the outer end of the takeoff line of the aircraft (14), and the first satellite positioning antenna is used for detecting the angle between the aircraft body and the central line when the aircraft (14) runs.
6. The intelligent indicating system of the airplane berth with high safety performance as claimed in claim 1, characterized in that: when gallery bridge (16) is in initial condition, be the acute angle setting between middle section (1602) axial and the axial of aircraft berth traction passageway (13), first infrared emitter installs in the lateral part that middle section (1602) is close to aircraft (14), and the infrared ray signal direction that first infrared emitter sent is perpendicular setting with the axial of aircraft berth traction passageway (13).
7. The intelligent indicating system of the airplane berth with high safety performance as claimed in claim 1, characterized in that: the detection information display module (17) adopts a touch display screen, so that the pilot can conveniently carry out human-computer interaction.
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| US11538349B2 (en) | 2020-08-03 | 2022-12-27 | Honeywell International Inc. | Multi-sensor data fusion-based aircraft detection, tracking, and docking |
| CN116778760A (en) * | 2023-08-22 | 2023-09-19 | 中国科学院空天信息创新研究院 | Guiding device and guiding method for warehousing of large aircraft |
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| CN1664877A (en) * | 2005-03-07 | 2005-09-07 | 张积洪 | Airplane berth plane type automatic identification and indication system |
| CN102252619A (en) * | 2011-04-21 | 2011-11-23 | 中国民航大学 | Displacement distance measuring and displaying system in airplane berthing process |
| CN103786893A (en) * | 2014-01-24 | 2014-05-14 | 中国民用航空总局第二研究所 | Aircraft berthing automatic guide method and device based on laser ranging technology |
| CN106448275A (en) * | 2014-12-30 | 2017-02-22 | 大连现代高技术集团有限公司 | Visualization-based airplane berth real-time guiding system |
| CN106251711A (en) * | 2016-08-24 | 2016-12-21 | 桂林信通科技有限公司 | A kind of aircraft docking guidance and distance display and information system |
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