Restrictions on connections between non-terrestrial base stations and airborne communication devices

The communication control device addresses the inefficiency of non-terrestrial base station resource waste by airborne devices by restricting connections based on altitude or propagation time, improving communication resource utilization.

JP7770540B2Active Publication Date: 2025-11-14RAKUTEN MOBILE INC
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Patent Information

Application Number
JP2024510738
Authority / Receiving Office
JP · JP
Patent Type
Patents
Current Assignee / Owner
Filing Date
2022-03-28
Publication Date
2025-11-14
Estimated Expiration
2042-03-28

AI Technical Summary

Technical Problem

Communication resources of non-terrestrial base stations are wasted due to the high-speed movement of airborne communication devices, such as those on aircraft, which quickly pass through satellite communication cells, leading to inefficient use of limited satellite resources and potential disruption of communication for terrestrial devices.

Method used

A communication control device that detects airborne communication devices and restricts their connection to non-terrestrial base stations using altitude thresholds or propagation time criteria, thereby reducing unnecessary resource consumption.

Benefits of technology

Reduces the consumption of communication resources by non-terrestrial base stations by preventing excessive connection attempts from airborne devices, thereby enhancing communication availability for terrestrial devices.

✦ Generated by Eureka AI based on patent content.

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Patent Text Reader

Abstract

A communication control device 3 includes at least one processor that executes: detecting an overhead communication instrument 2F which is located upward of the ground, by an overhead communication instrument detection unit 31; and limiting the connection of a flying communication satellite 131 that supplies a satellite communication cell 132 to communication instruments and the overhead communication instrument 2F, by a connection limiting unit 33. The overhead communication instrument 2F is a communication instrument in a flying aircraft FL. The overhead communication instrument detection unit 31 is provided to the overhead communication instrument 2F and detects itself as an overhead communication instrument 2F on the basis of the altitude detected by a positioning sensor which is provided to the overhead communication instrument 2F. The connection limiting unit 33 is provided to the overhead communication instrument 2F and limits transmission of a connection request from the overhead communication instrument 2F to the communication satellite 131 (FIG. 2).
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Description

[Technical Field]

[0001] The present disclosure relates to a communication control technique in a communication system. [Background technology]

[0002] The number, types, and uses of wireless communication devices, such as smartphones and Internet of Things (IoT) devices, are steadily increasing, and wireless communication standards are continually being expanded and improved. For example, commercial service for the fifth-generation mobile communication system, known as "5G," began in 2018, and standardization is still underway at the Third Generation Partnership Project (3GPP). In addition, efforts have begun to develop standards for the sixth-generation mobile communication system, or "6G," as the next-generation wireless communication standard following 5G.

[0003] Mobile communication (hereinafter also referred to as mobile communication) networks for mobile or portable communication devices (hereinafter collectively referred to as communication devices), such as smartphones and mobile phones, have generally been constructed using communication cells (hereinafter also referred to as terrestrial communication cells) provided by base stations (hereinafter also referred to as terrestrial base stations) installed on the ground. However, in some areas, it is difficult to install a sufficient number of terrestrial base stations for various reasons, which has led to the problem of relatively low quality of mobile communication.

[0004] To address these regional disparities in mobile communication quality and the "out-of-area" problem of mobile communication devices being unable to communicate in some areas, non-terrestrial networks (NTNs) are being considered. In NTNs, communication satellites and unmanned aerial vehicles flying in the atmosphere, such as outer space and the stratosphere, serve as base stations (hereinafter referred to as non-terrestrial base stations, and communication satellites in particular are also referred to as satellite base stations) and provide communication cells on the ground (hereinafter referred to as non-terrestrial communication cells, and communication cells provided by communication satellites in particular are also referred to as satellite communication cells). Devices within non-terrestrial communication cells communicate with non-terrestrial base stations directly or indirectly via other communication devices. Providing non-terrestrial communication cells in areas where terrestrial communication cells are insufficient can improve the quality of mobile communication in those areas. [Prior art documents] [Patent documents]

[0005] [Patent Document 1] Japanese Patent Application Laid-Open No. 2010-278886 Summary of the Invention [Problem to be solved by the invention]

[0006] The present inventors recognized that the communication quality of non-terrestrial networks may be affected by communication devices used by aircraft passengers and the like. Communication devices inside aircraft (hereinafter referred to as in-flight communication devices (in-flight UEs), or generalized to communication devices located above the ground as in-the-sky communication devices (in-the-sky UEs)) are located closer to non-terrestrial base stations such as communication satellites than ground communication devices (hereinafter referred to as ground communication devices (ground UEs)). Therefore, they are more likely to attempt to connect to non-terrestrial base stations. However, because aircraft fly at high speeds in the sky, they pass through satellite communication cells provided by communication satellites in an extremely short time. Therefore, even if the in-flight communication devices are connected to a communication satellite, they are effectively unable to communicate. Meanwhile, if hundreds of in-flight communication devices per aircraft simultaneously attempt to connect to a communication satellite, the satellite's valuable communication resources are wasted in processing the signals.

[0007] The present disclosure has been made in consideration of these circumstances, and aims to provide a communication control device, etc. that can reduce the consumption of communication resources of non-terrestrial base stations by airborne communication devices located above the ground. [Means for solving the problem]

[0008] In order to solve the above problem, a communication control device of one aspect of the present disclosure includes at least one processor that detects an airborne communication device located above the ground using an airborne communication device detection unit, and restricts the connection of the airborne communication device to a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device using a connection restriction unit.

[0009] According to this aspect, the connection between the non-terrestrial base station and the airborne communication device is restricted, so that the consumption of communication resources of the non-terrestrial base station by the airborne communication device can be reduced.

[0010] Another aspect of the present disclosure is a communication control method, which includes detecting an airborne communication device located above the ground, and restricting connection of the airborne communication device to an airborne non-terrestrial base station that provides a non-terrestrial communication cell to the communication device.

[0011] Yet another aspect of the present disclosure is a storage medium that stores a communication control program that causes a computer to detect an airborne communication device located above the ground, and restrict connections between the airborne communication device and a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device.

[0012] Any combination of the above components, or any conversion of these expressions into methods, devices, systems, recording media, computer programs, etc., are also encompassed within the present disclosure. [Effects of the Invention]

[0013] According to the present disclosure, it is possible to reduce the consumption of communication resources of non-terrestrial base stations by airborne communication devices located above the ground. [Brief explanation of the drawings]

[0014] [Figure 1] 1 shows a schematic overview of a wireless communication system to which a communication control device is applied. [Figure 2] 1 illustrates a schematic diagram of a communication satellite providing a satellite communication cell to a communication device. [Figure 3] 4 is a flowchart showing an example of processing in the first embodiment; [Figure 4] 1 illustrates a schematic diagram of a random access procedure. [Figure 5] 10 is a flowchart illustrating an example of processing in the second embodiment. [Figure 6] 10 is a flowchart illustrating an example of processing in a third embodiment. DETAILED DESCRIPTION OF THE INVENTION

[0015] 1 schematically illustrates an overview of a wireless communication system 1 to which a communication control device according to an embodiment of the present disclosure is applied. The wireless communication system 1 includes a 5G wireless communication system 11 conforming to a fifth-generation mobile communication system (5G) that uses NR (New Radio) or 5G NR (Fifth Generation New Radio) as a radio access technology (RAT) and 5GC (Fifth Generation Core) as a core network (CN), a 4G wireless communication system 12 conforming to a fourth-generation mobile communication system (4G) that uses LTE (Long Term Evolution) or LTE-Advanced as a radio access technology and EPC (Evolved Packet Core) as a core network, and a satellite communication system 13 that handles satellite communication via a communication satellite 131. Although not illustrated, the wireless communication system 1 may include a wireless communication system of a generation earlier than 4G, a wireless communication system of a generation later than 5G (e.g., 6G), or any wireless communication system that is not associated with a generation, such as Wi-Fi (registered trademark).

[0016] The 5G wireless communication system 11 includes communication devices 2A, 2B, 2C, and 2D (hereinafter sometimes collectively referred to as communication devices 2) such as smartphones that are installed on the ground and are also called UE (User Equipment), and multiple 5G base stations 111A, 111B, and 111C (hereinafter sometimes collectively referred to as 5G base stations 111) that can communicate via 5G NR. In 5G, the base station 111 is also called a gNodeB (gNB). The communication range or support range of each of the 5G base stations 111A, 111B, and 111C is called a cell, and is illustrated as 112A, 112B, and 112C, respectively (hereinafter sometimes collectively referred to as 5G cells 112 or cells 112).

[0017] The size of the 5G cell 112 of each 5G base station 111 is arbitrary, but typically ranges from a few meters to tens of kilometers in radius. Although there is no established definition, cells with a radius of a few meters to tens of meters are called femtocells, cells with a radius of tens to tens of meters are called picocells, cells with a radius of tens to hundreds of meters are called microcells, and cells with a radius of more than several hundred meters are called macrocells. 5G often uses high-frequency radio waves such as millimeter waves, and because of their high line-of-sight characteristics, the radio waves are blocked by obstacles, shortening the communication distance. For this reason, 5G tends to use smaller cells than 4G and earlier generations.

[0018] A communication device 2 can perform 5G communication if it is located within at least one of multiple 5G cells 112A, 112B, and 112C. In the illustrated example, a communication device 2B located within 5G cells 112A and 112B can communicate with both 5G base stations 111A and 111B via 5G NR. Furthermore, a communication device 2C located within 5G cell 112C can communicate with 5G base station 111C via 5G NR. Communication devices 2A and 2D are located outside all of the 5G cells 112A, 112B, and 112C and are therefore unable to communicate via 5G NR. 5G communication via 5G NR between each communication device 2 and each 5G base station 111 is managed by the 5GC, which is a core network. For example, the 5GC handles data transmission and reception between each 5G base station 111, data transmission and reception between EPC, a satellite communication system 13, and external networks such as the Internet, and mobility management of the communication device 2.

[0019] The 4G wireless communication system 12 includes multiple 4G base stations 121 (only one of which is shown in FIG. 1 ) that are installed on the ground and capable of communicating with the communication device 2 via LTE or LTE-Advanced. In 4G, the base station 121 is also called an eNodeB (eNB). Like each 5G base station 111, the coverage area or support area of ​​each 4G base station 121 is also called a cell, and is illustrated as 122.

[0020] If the communication device 2 is located inside the 4G cell 122, it can perform 4G communication. In the illustrated example, communication devices 2A and 2B located inside the 4G cell 122 can communicate with the 4G base station 121 via LTE or LTE-Advanced. Communication devices 2C and 2D are located outside the 4G cell 122 and are therefore unable to communicate via LTE or LTE-Advanced. 4G communication between each communication device 2 and each 4G base station 121 via LTE or LTE-Advanced is managed by the EPC, which is a core network. For example, the EPC handles the exchange of data with each 4G base station 121, the exchange of data with external networks such as 5GC, the satellite communication system 13, and the Internet, and the mobility management of the communication device 2.

[0021] Focusing on each of the communicators 2A, 2B, 2C, and 2D, in the illustrated example, communicator 2A is capable of 4G communication with 4G base station 121, communicator 2B is capable of 5G communication with 5G base stations 111A and 111B and 4G communication with 4G base station 121, and communicator 2C is capable of 5G communication with 5G base station 111C. In cases where there are multiple base stations (111A, 111B, 121) with which communicator 2B can communicate, one base station determined to be optimal in terms of communication quality, etc., is selected under the management of the 5G communication center (5GC) and / or the EPC core network, and communication with communicator 2B is performed. Furthermore, communicator 2D is not capable of communication with any of the 5G base stations 111 and 4G base station 121, and therefore performs communication via satellite communication system 13, which will be described next.

[0022] The satellite communication system 13 is a wireless communication system that uses a communication satellite 131, which is a low-orbit satellite flying in space at an altitude of approximately 500 km to 700 km above the Earth's surface, as a non-terrestrial base station. Similar to the 5G base station 111 and the 4G base station 121, the communication range or support area of ​​the communication satellite 131 is also called a cell and is illustrated as 132. In this way, the communication satellite 131, which is a non-terrestrial base station, provides the satellite communication cell 132, which is a non-terrestrial communication cell, to the ground. A terrestrial communication device 2 can perform satellite communication if it is located inside the satellite communication cell 132. Similar to the 5G base station 111 in the 5G wireless communication system 11 and the 4G base station 121 in the 4G wireless communication system 12, the communication satellite 131, which is a base station in the satellite communication system 13, can wirelessly communicate with the communication device 2 in the satellite communication cell 132 directly or indirectly via an aircraft or the like. The radio access technology that the communication satellite 131 uses for radio communication with the communication device 2 in the satellite communication cell 132 may be 5G NR, the same as the 5G base station 111, or LTE or LTE-Advanced, the same as the 4G base station 121, or any other radio access technology that can be used by the communication device 2. For this reason, the communication device 2 does not need to be provided with special functions or components for satellite communication.

[0023] The satellite communication system 13 includes a gateway 133 as a ground station installed on the ground and capable of communicating with a communication satellite 131. The gateway 133 includes a satellite antenna for communicating with the communication satellite 131 and is connected to a 5G base station 111 and a 4G base station 121 as terrestrial base stations that constitute a terrestrial network (TN). In this way, the gateway 133 connects the NTN formed by the communication satellite 131 to the TN formed by the terrestrial base stations 111 and 121 so that they can communicate with each other. When the communication satellite 131 performs 5G communication with a communication device 2 in a satellite communication cell 132 using 5G NR, the 5GC connected via the gateway 133 and the 5G base station 111 (or a 5G radio access network) in the TN is used as the core network. When the communication satellite 131 performs 4G communication with a communication device 2 in the satellite communication cell 132 using LTE or LTE-Advanced, the EPC connected via the gateway 133 and the 4G base station 121 (or a 4G radio access network) in the TN is used as the core network. In this way, appropriate cooperation is achieved between different wireless communication systems such as 5G communication, 4G communication, and satellite communication via the gateway 133.

[0024] Satellite communication using a communication satellite 131 is primarily used to cover areas where terrestrial base stations such as 5G base station 111 and 4G base station 121 are not installed or are few in number. In the illustrated example, a communication device 2D located outside the communication cells of all terrestrial base stations communicates with the communication satellite 131. Meanwhile, communication devices 2A, 2B, and 2C that can communicate satisfactorily with any terrestrial base station are also within a satellite communication cell 132 and can therefore communicate with the communication satellite 131. However, by communicating with a terrestrial base station rather than the communication satellite 131 as a satellite base station, the limited communication resources (including power) of the communication satellite 131 are conserved for the communication device 2D and the like. The communication satellite 131 improves the quality of communication with the communication device 2D by directing communication radio waves toward the communication device 2D within the satellite communication cell 132 using beamforming.

[0025] The size of the satellite communication cell 132 of the communication satellite 131 serving as a satellite base station can be set arbitrarily depending on the number of beams emitted by the communication satellite 131; for example, a satellite communication cell 132 with a diameter of approximately 24 km can be formed by combining up to 2,800 beams. As shown in the figure, the satellite communication cell 132 is typically larger than a terrestrial communication cell such as the 5G cell 112 or the 4G cell 122, and may include one or more 5G cells 112 and / or 4G cells 122 therein. Note that, although the above example illustrates a communication satellite 131 flying in low orbit at an altitude of approximately 500 km to 700 km above the Earth's surface as a flying non-terrestrial base station, a communication satellite flying in high orbit such as a geostationary orbit, or an unmanned or manned aircraft flying in the atmosphere at a lower altitude (for example, approximately 20 km above the Earth's surface) such as the stratosphere, may also be used as a non-terrestrial base station in addition to or instead of the communication satellite 131.

[0026] 2 schematically shows how a communication satellite 131 serving as a non-terrestrial base station provides a satellite communication cell 132 serving as a non-terrestrial communication cell to communication devices 2F and 2G. Communication device 2F is a communication device used by passengers of an aircraft FL flying in the air, and is hereinafter also referred to as an on-board communication device 2F. Furthermore, on-board communication device 2F is one type of communication device located within a satellite communication cell 132 in the sky above the ground, and is hereinafter also referred to as an airborne communication device 2F. Communication device 2G is a communication device located within the satellite communication cell 132 on the ground, and is hereinafter also referred to as a terrestrial communication device 2G. Since the airborne communication device 2F and the terrestrial communication device 2G are located within the satellite communication cell 132 in the sky and on the ground, respectively, both can connect to the communication satellite 131.

[0027] In particular, the airborne communication device 2F is located closer to the communication satellite 131 than the terrestrial communication device 2G, and therefore is more likely to attempt to connect to the communication satellite 131. However, because the aircraft FL flies in the sky at high speed, it passes through the satellite communication cell 132 provided by the communication satellite 131 in an extremely short time. As a result, even if the onboard communication device 2F connects to the communication satellite 131, it is practically unable to communicate. On the other hand, if several hundred onboard communication devices 2F per aircraft FL simultaneously attempt to connect to the communication satellite 131, the communication satellite 131's valuable communication resources will be wasted in processing the signals. As a result, the connection and communication between the terrestrial communication device 2G and the communication satellite 131 may be hindered by the large number of onboard communication devices 2F. In particular, since the communication satellite 131 often has limited available power and wireless bandwidth compared to the terrestrial base stations 111 and 121, the allocation of valuable communication resources to unnecessary processing with the onboard communication device 2F may result in a disconnection of communication with the terrestrial communication device 2G. This embodiment provides a communication control device 3 that can reduce the consumption or waste of communication resources of the communication satellite 131 by such an airborne communication device 2F.

[0028] The communication control device 3 includes an airborne communication device detection unit 31 that detects airborne communication devices 2F, such as the onboard communication device 2F; an orbit information acquisition unit 32 that acquires orbit information about the communication satellite 131; and a connection restriction unit 33 that restricts the connection between the communication satellite 131 and the airborne communication device 2F. These functional blocks are realized by the cooperation of hardware resources, such as a computer's central processing unit, memory, input devices, output devices, and peripheral devices connected to the computer, and software executed using these resources. Regardless of the type or location of the computer, each of the above functional blocks may be realized by the hardware resources of a single computer or by a combination of hardware resources distributed across multiple computers. In particular, in this embodiment, some or all of the functional blocks of the communication control device 3 may be realized in a centralized or distributed manner by computers and processors provided in the communication devices 2 (e.g., 2F), the communication satellite 131, the gateway 133, and a core network, such as a 5GC or EPC, directly or indirectly connected to the gateway 133.

[0029] In this embodiment, we will explain a first embodiment in which each functional block 31 to 33 of the communication control device 3 is mainly realized on the airborne communication device 2F side, and a second embodiment in which each functional block 31 to 33 of the communication control device 3 is mainly realized on the non-terrestrial network side constituted by a communication satellite 131 and a gateway 133.

[0030] In the first embodiment, the airborne communication device detection unit 31, orbit information acquisition unit 32, and connection restriction unit 33 are realized in the airborne communication device 2F. The airborne communication device detection unit 31 provided in the airborne communication device 2F detects itself as an airborne communication device 2F based on the altitude detected by a positioning sensor provided in the airborne communication device 2F. The airborne communication device 2F acquires its own three-dimensional position information by using a positioning sensor based on a satellite positioning system such as GPS (Global Positioning System) or GNSS (Global Navigation Satellite System) as the airborne communication device detection unit 31. In this embodiment, altitude information included in the three-dimensional position information is particularly used.

[0031] For example, the airspace communication device detection unit 31 may set an altitude threshold for the altitude of the airspace communication device 2F, and detect a communication device 2 whose altitude is detected as equal to or higher than the altitude threshold as the airspace communication device 2F. Specifically, if the altitude threshold is, for example, "5,000 m," each communication device 2 recognizes itself as an airspace communication device 2F when the altitude detected by its own positioning sensor is "5,000 m" or higher. The connection restriction unit 33 provided in such an airspace communication device 2F restricts the transmission of a connection request from itself (the airspace communication device 2F) to the communication satellite 131. For example, a communication device 2 (connection restriction unit 33) that recognizes itself as the airspace communication device 2F does not transmit a connection request to the communication satellite 131. In this way, the transmission of a connection request from the airspace communication device 2F to the communication satellite 131 is restricted, and as a result, the connection between the communication satellite 131 and the airspace communication device 2F is restricted, thereby reducing the consumption of communication resources of the communication satellite 131 by the airspace communication device 2F.

[0032] In addition to the above, the airborne communication device detection unit 31 provided in the airborne communication device 2F may detect itself as the airborne communication device 2F when the difference between the altitude information of the communication satellite 131 notified to the airborne communication device 2F by a non-terrestrial network including the communication satellite 131 and its own altitude detected by a positioning sensor is equal to or less than a predetermined value. Specifically, the orbit information acquisition unit 32 provided in the airborne communication device 2F receives broadcast information such as an SIB (System Information Block) periodically or aperiodically transmitted by the communication satellite 131 within the satellite communication cell 132, and extracts the orbit information (ephemeris information) of the communication satellite 131 contained therein.

[0033] The airborne communication device detection unit 31 can recognize the altitude of the communication satellite 131 based on the orbit information of the communication satellite 131 acquired by the orbit information acquisition unit 32. In this case, the airborne communication device 2F as the airborne communication device detection unit 31 can compare its own altitude determined by the positioning sensor with the altitude of the communication satellite 131 determined by the orbit information acquisition unit 32. For example, the airborne communication device detection unit 31 may detect itself as an airborne communication device 2F when the difference in altitude between the communication satellite 131 and itself (the airborne communication device 2F) is equal to or less than a predetermined altitude difference threshold. Specifically, if the altitude difference threshold is, for example, "2,000 m," and the altitude of the communication satellite 131 determined by the orbit information acquisition unit 32 is, for example, "10,000 m," each communication device 2 recognizes itself as an airborne communication device 2F for that communication satellite 131 when the altitude detected by its own positioning sensor is equal to or greater than "8,000 m" and equal to or less than "12,000 m." As a result, the connection between the communication satellite 131 and the airborne communication device 2F is restricted by the connection restriction unit 33, thereby reducing the consumption of communication resources of the communication satellite 131 by the airborne communication device 2F. Note that the altitude information of the communication satellite 131 can also be acquired or calculated through MDT (Minimization of Drive Tests) introduced by 3GPP.

[0034] Note that the broadcast information such as SIBs transmitted periodically or aperiodically by the non-terrestrial network may include altitude range information of the communication device 2 for which connection is restricted or permitted, in addition to or instead of the orbit information and altitude information of the communication satellite 131. For example, if the broadcast information such as SIBs includes an altitude range with a lower limit of "8,000 m" and an upper limit of "12,000 m" as altitude range information for restricting connection, the upper air communication device 2F serving as the upper air communication device detection unit 31 that receives it recognizes itself as the upper air communication device 2F for the communication satellite 131 if the altitude measured by its own positioning sensor is within the altitude range. As a result, the connection between the communication satellite 131 and the upper air communication device 2F is restricted by the connection restriction unit 33, thereby reducing the consumption of communication resources of the communication satellite 131 by the upper air communication device 2F.

[0035] Furthermore, notification information such as SIB does not necessarily have to be notified to the communication device 2 from the communication satellite 131 to be connected, but may be notified to the communication device 2 from other communication satellites 131 that the aircraft FL passed nearby before the communication satellite 131 to be connected, other communication satellites 131 around the communication satellite 131 to be connected, or from terrestrial base stations 111, 121 or gateways 133, etc., if the communication device 2F in the sky can receive radio waves from the ground.

[0036] FIG. 3 is a flowchart showing a processing example of the first embodiment. In the flowchart, "S" denotes a step or a process. This flowchart mainly shows the processing executed by the onboard communication device 2F. In S1, the orbit information acquisition unit 32 provided in the onboard communication device 2F determines whether or not orbit information of the communication satellite 131 can be acquired. Specifically, it determines whether or not the orbit information of the communication satellite 131 to be connected is included in the broadcast information such as the SIB received by the onboard communication device 2F from the communication satellite 131 to be connected or other non-terrestrial base stations and / or terrestrial base stations. If the determination in S1 is No, the process proceeds to S2, and the onboard communication device 2F performs normal connection and communication operations similar to those of the terrestrial communication device 2G. Note that, as described above, the onboard communication device 2F may limit the transmission of a connection request to the communication satellite 131 based on the comparison result between the altitude detected by its own positioning sensor and a predetermined altitude threshold, regardless of the orbit information (altitude information) of the communication satellite 131.

[0037] If S1 determines Yes, the process proceeds to S3, where the orbit information acquisition unit 32 provided in the on-board communication device 2F determines whether there are multiple communication satellites 131 to which the on-board communication device 2F can connect. Specifically, the on-board communication device 2F can recognize the number of non-terrestrial base stations to which it can potentially connect, based on the broadcast information such as the SIB received in S1. If S3 determines No, the process proceeds to S4, where the airborne communication device detection unit 31 provided in the on-board communication device 2F determines whether the altitude detected by its own positioning sensor is within the allowable altitude range for connection of the communication satellite 131 set in the broadcast information such as the SIB received in S1.

[0038] If S3 and / or S4 determine "Yes," the process proceeds to S5, where the connection restriction unit 33 provided in the on-board communication device 2F does not restrict the connection between the communication satellite 131 and the on-board communication device 2F, and the on-board communication device 2F transmits a connection request to the communication satellite 131 in accordance with a normal random access procedure. If S3 determines "Yes," there are multiple communication satellites 131 to which the on-board communication device 2F can connect, and the satellite communication system 13 as a whole is considered to have relatively abundant communication resources, so it is permitted to allocate communication resources to the on-board communication device 2F, which has low connection possibility and communication efficiency. Also, if S4 determines "Yes," the altitude of the on-board communication device 2F is within the allowable connection altitude range of the communication satellite 131 (for example, below the lower threshold "8,000 m" or above the upper threshold "12,000 m"), and it is expected that the on-board communication device 2F will stay within the satellite communication cell 132 for a relatively long time, so it is permitted to allocate communication resources to the on-board communication device 2F as well as to the ground communication device 2G.

[0039] If the determinations in S3 and S4 are No, the process proceeds to S6, where the connection restriction unit 33 provided in the on-board communication device 2F restricts the transmission of a connection request from the on-board communication device 2F determined to be an overhead communication device 2F in S3 and S4 to the communication satellite 131. In this way, the connection restriction unit 33 restricts the connection between the on-board communication device 2F and the communication satellite 131 when there is only one communication satellite 131 to which the on-board communication device 2F can connect (No in S3) and when the altitude of the on-board communication device 2F is outside the allowable altitude range for connection of the communication satellite 131 (for example, greater than the lower threshold "8,000 m" and less than the upper threshold "12,000 m") (No in S4). After a predetermined time has elapsed since the processing of S6, the process returns to S3, and the processing of S3 to S6 is repeated periodically (for example, every 5 to 10 seconds) (ending in S5).

[0040] In the second embodiment, the airborne communication device detection unit 31 and the connection restriction unit 33 are realized in a non-terrestrial network including a communication satellite 131 and a gateway 133. Note that the non-terrestrial network recognizes the orbital information of the communication satellite 131 that constitutes the non-terrestrial network, and therefore, in this embodiment, there is no need to provide an orbital information acquisition unit 32. The airborne communication device detection unit 31 provided in the non-terrestrial network (for example, the communication satellite 131 or the gateway 133) detects, as an airborne communication device 2F, a communication device 2 whose signal propagation time with the communication satellite 131 is equal to or shorter than a predetermined value. The signal for detecting the airborne communication device 2F may be any signal communicated between the airborne communication device 2F and the communication satellite 131, but, for example, a message transmitted by the airborne communication device 2F to the communication satellite 131 in a random access procedure for establishing a connection with the communication satellite 131 is used.

[0041] 4 schematically shows a contention-based random access (CBRA) procedure between a communication device 2 (UE) and a communication satellite 131 (Satellite). The CBRA procedure is composed of four messages exchanged between the communication device 2 and the communication satellite 131. The first message (Msg1) is a random access request (RA Request) sent by the communication device 2 to the communication satellite 131. When the communication device 2 attempts random access to establish a connection to the communication satellite 131, it selects any one preamble from a maximum of 64 predetermined, mutually orthogonal random access preambles (hereinafter simply referred to as preambles) that the communication satellite 131 can accept, and transmits the selected preamble in a first message to the communication satellite 131 on a physical random access channel (PRACH).

[0042] The second message (Msg2) is a random access response (RA Response) that the communication satellite 131 transmits to the communication device 2. When the communication satellite 131 receives a preamble from the communication device 2 through the physical random access channel and there is no other communication device 2 that has transmitted the same preamble to the communication satellite 131 on the same physical random access channel (when there is no preamble collision), the communication satellite 131 transmits a random access response (hereinafter simply referred to as a response) to the communication device 2.

[0043] Upon receiving a normal response (second message) from the communication satellite 131, the communication device 2 transmits a third message (Msg3) to the communication satellite 131 in accordance with the timing information and scheduling permission (which specify resources in the uplink frame or a Physical Uplink Shared Channel (PUSCH) that can be used to transmit the third message) contained in the second message. The third message includes communication device identification information of the communication device 2, etc. Upon receiving the third message, the communication satellite 131, in cooperation with the core network as appropriate, identifies or authenticates the communication device 2 based on the communication device identification information, etc., and transmits a completion notification to the communication device 2 as a fourth message (Msg4). After the above series of four messages have been successfully exchanged, a connection between the communication device 2 and the communication satellite 131 is established.

[0044] In a random access procedure for a non-terrestrial network including a communication satellite 131, the distance between the communication device 2 and the base station (communication satellite 131) is greater than in a terrestrial network, so communication of each message involves a non-negligible propagation delay (typically greater than 20 ms). In FIG. 4, the propagation delay or propagation time for the first message is illustrated as TA (Timing Advance). The propagation time TA of each message is recognized by the message receiver, for example, as the difference between the timestamp (transmission time) assigned to the message by the message sender (communication device 2 for the first message) and the reception time of the message by the message receiver (communication satellite 131 for the first message). For example, the communication satellite 131 that receives the first message can detect the propagation time TA of the signal between itself and the communication device 2 as the difference between the transmission time according to the timestamp assigned to the first message and the reception time of the first message by itself. The airborne communication device detection unit 31 of the non-terrestrial network that has detected the propagation time TA in this way detects the communication device 2 whose propagation time TA is less than a predetermined value (for example, "10 ms") as an airborne communication device 2F.

[0045] The connection restriction unit 33 provided in the non-terrestrial network may not transmit a response (e.g., a second message in a random access procedure) to a message (e.g., a first message in a random access procedure) received from an airborne communication device 2F detected by the airborne communication device detection unit 31, to the airborne communication device 2F. In addition to or instead of this, the connection restriction unit 33 provided in the non-terrestrial network transmits a connection restriction request to the communication satellite 131 to the airborne communication device 2F detected by the airborne communication device detection unit 31. The connection restriction request may prohibit or restrict the transmission of a connection request (second random access) from the airborne communication device 2F to the communication satellite 131, or may be an indication of a relatively long waiting time (e.g., a backoff indicator) until the airborne communication device 2F can transmit the next connection request to the communication satellite 131.

[0046] In this way, the connection restriction unit 33 provided in the non-terrestrial network prohibits or restricts connection between the communication satellite 131 and the airborne communication device 2F. This makes it possible to reduce the consumption of communication resources of the communication satellite 131 by the airborne communication device 2F. However, in the second embodiment, in order for the airborne communication device detection unit 31 provided in the non-terrestrial network to detect the airborne communication device 2F, it is necessary to calculate the propagation time based on a signal received from the airborne communication device 2F (for example, a first message in the random access procedure). This consumes communication resources of the communication satellite 131. In contrast, in the first embodiment described above, when the communication device 2 recognizes that it is the airborne communication device 2F, it autonomously restricts the transmission of a connection request to the communication satellite 131, thereby minimizing the consumption of communication resources of the communication satellite 131.

[0047] FIG. 5 is a flowchart showing a processing example of the second embodiment. The flowchart in FIG. 5 mainly shows processing executed by the non-terrestrial network (NTN). In S7, the airborne communication device detection unit 31 provided in the non-terrestrial network receives a message (e.g., a first message in a random access procedure) from the communication device 2 at the communication satellite 131. In S8, the airborne communication device detection unit 31 provided in the non-terrestrial network determines whether there is another communication satellite 131 to which the communication device 2 that transmitted the message of S7 can connect, in the vicinity of the communication satellite 131 that received the message of S7. Because the non-terrestrial network recognizes the positions and orbits of communication satellites 131 that belong to its own or other affiliated non-terrestrial networks, the determination in S8 can be made in the non-terrestrial network. If the determination in S8 is No, the process proceeds to S9, where the airborne communication device detection unit 31 provided in the non-terrestrial network determines whether the propagation time TA of the signal between the communication device 2 and the communication satellite 131 detected based on the message received in S7 exceeds a predetermined value (e.g., 10 ms).

[0048] If the determination in S8 and / or S9 is Yes, the process proceeds to S10, where the connection restriction unit 33 provided in the non-terrestrial network does not send a connection restriction request to the communication satellite 131 to the communication device 2, and the communication satellite 131 transmits a second message to the communication device 2 as a response to the first message received in S7 in accordance with the normal random access procedure. If the determination in S8 is Yes, there are multiple communication satellites 131 to which the communication device 2 that sent the message in S7 can connect, and it is considered that the communication resources of the satellite communication system 13 as a whole are relatively abundant, so it is permissible to allocate communication resources to the on-board communication device 2F etc. that have low connection possibility and communication efficiency. Furthermore, if the answer to S9 is Yes, the signal propagation time TA between the communication device 2 that sent the message in S7 and the communication satellite 131 exceeds a predetermined value (e.g., 10 ms), and since the communication device 2 is expected to stay within the satellite communication cell 132 for a relatively long time, it is permissible to allocate communication resources to the communication device 2 (such as the onboard communication device 2F) in the same way as to the terrestrial communication device 2G.

[0049] If the determinations in S8 and S9 are No, the process proceeds to S11, where the connection restriction unit 33 provided in the non-terrestrial network transmits a connection restriction request to the communication satellite 131 to the communication device 2 determined to be the airborne communication device 2F in S8 and S9. In this way, the connection restriction unit 33 restricts the connection between the communication satellite 131 and the communication device 2 (such as the on-board communication device 2F) when there is only one communication satellite 131 to which the communication device 2 can connect (No in S8) or when the signal propagation time TA between the communication device 2 and the communication satellite 131 is equal to or less than a predetermined value (e.g., 10 ms) (No in S9). In addition, the connection restriction unit 33 does not transmit a response to the message received in S7 to the airborne communication device 2F. After a predetermined time has elapsed since the process of S11, the process returns to S8, and the processes of S8 to S11 are repeated periodically (e.g., every 5 to 10 seconds) (ending in S10).

[0050] The propagation time TA of the signal between the communication device 2 and the communication satellite 131 can be detected not only by the non-terrestrial network side that receives the first message in the random access procedure as in the second embodiment, but also by the communication device 2 side that receives the second message in the random access procedure and other signals from the communication satellite 131. Alternatively, the communication device 2 can estimate the relative distance and propagation time TA between itself and the communication satellite 131 based on its own position detected by a positioning sensor and the orbit information of the communication satellite 131 included in broadcast information such as an SIB transmitted from the communication satellite 131. An example of processing based on the propagation time TA that can be recognized on the communication device 2 side in this way is shown in Fig. 6 as a third embodiment.

[0051] The third embodiment essentially combines part of the processing of the first embodiment with part of the processing of the second embodiment. Processing similar to that of each embodiment is assigned the same reference numerals and redundant explanations will be omitted. In the third embodiment, the airborne communication device detection unit 31, orbit information acquisition unit 32, and connection restriction unit 33 are realized in the airborne communication device 2F.

[0052] The airborne communication device detection unit 31 provided in the airborne communication device 2F estimates the propagation time TA between the airborne communication device 2F and the communication satellite 131 based on the position of the airborne communication device 2F detected by its own positioning sensor and the orbit information of the communication satellite 131 contained in the broadcast information such as SIB from the communication satellite 131 etc. acquired by the orbit information acquisition unit 32. The broadcast information such as SIB transmitted periodically or aperiodically by the non-terrestrial network may include range information of the propagation time TA that restricts or allows connection. For example, if the broadcast information such as SIB specifies "10 ms or less" as the range information of the propagation time TA that restricts connection, the airborne communication device 2F serving as the airborne communication device detection unit 31 that receives the broadcast information recognizes itself as the airborne communication device 2F for the communication satellite 131 if the propagation time TA it detects is within that range. As a result, the connection between the communication satellite 131 and the airborne communication device 2F is restricted by the connection restriction unit 33, so that the consumption of communication resources of the communication satellite 131 by the airborne communication device 2F can be reduced.

[0053] In S1, the orbit information acquisition unit 32 provided in the on-board communication device 2F determines whether or not orbit information of the communication satellite 131 can be acquired. If the determination in S1 is No, the process proceeds to S2, where the on-board communication device 2F performs normal connection and communication operations similar to those of the terrestrial communication device 2G. If the determination in S1 is Yes, the process proceeds to S3, where the orbit information acquisition unit 32 provided in the on-board communication device 2F determines whether or not there are multiple communication satellites 131 to which the on-board communication device 2F can connect. If the determination in S3 is No, the process proceeds to S9, where the airborne communication device detection unit 31 provided in the on-board communication device 2F determines whether the propagation time TA of the signal between the on-board communication device 2F and the communication satellite 131 exceeds a predetermined value (for example, "10 ms").

[0054] If the determination in S3 and / or S9 is Yes, the process proceeds to S5, where the connection restriction unit 33 provided in the on-board communication device 2F does not restrict the connection between the communication satellite 131 and the on-board communication device 2F, and the on-board communication device 2F transmits a connection request to the communication satellite 131 in accordance with the normal random access procedure. If the determination in S3 and S9 is No, the process proceeds to S6, where the connection restriction unit 33 provided in the on-board communication device 2F restricts the transmission of a connection request to the communication satellite 131 from the on-board communication device 2F determined to be an overhead communication device 2F in S3 and S9. After a predetermined time has elapsed since the processing of S6, the process returns to S3, and the processing of S3, S9, and S6 is repeated periodically (for example, every 5 to 10 seconds) (ending in S5).

[0055] The present disclosure has been described above based on the embodiments. The embodiments are merely examples, and it will be understood by those skilled in the art that various modifications are possible in the combination of the respective components and treatment processes, and that such modifications are also within the scope of the present disclosure.

[0056] The functional configuration of each device described in the embodiments can be realized by hardware resources, software resources, or a combination of hardware and software resources. Examples of hardware resources include processors, ROMs, RAMs, and other LSIs. Examples of software resources include operating systems, applications, and other programs.

[0057] This disclosure may be expressed in the following terms:

[0058] Item 1: detecting an airborne communication device located above the ground by an airborne communication device detection unit; restricting a connection between a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device and the airborne communication device by a connection restriction unit; A communication control device comprising at least one processor that executes the above. Item 2: Item 1: A communication control device according to item 1, wherein the airborne communication device is a communication device within a flying aircraft. Item 3: The communication control device described in item 1 or 2, wherein the airborne communication device detection unit is provided in the airborne communication device and detects itself as an airborne communication device based on the altitude detected by a positioning sensor provided in the airborne communication device. Item 4: The communication control device described in item 3, wherein the airborne communication device detection unit detects itself as an airborne communication device when the difference between the altitude information of the non-terrestrial base station notified to the airborne communication device by the non-terrestrial network constituted by the non-terrestrial base station and the altitude of the airborne communication device detected by the positioning sensor is less than a predetermined value. Item 5: 5. The communication control device according to item 3 or 4, wherein the connection restriction unit is provided in the airborne communication device and restricts transmission of a connection request from the airborne communication device to the non-terrestrial base station. Item 6: The communication control device described in any one of items 1 to 5, wherein the airborne communication device detection unit is provided in a non-terrestrial network configured by the non-terrestrial base stations, and detects a communication device as an airborne communication device when the signal propagation time between the non-terrestrial base station and the non-terrestrial base station is less than a predetermined value. Item 7: 7. The communication control device according to item 6, wherein the signal is a message transmitted by the airborne communication device to the non-terrestrial base station in a random access procedure. Item 8: 8. The communication control device according to item 7, wherein the connection restriction unit is provided in the non-terrestrial network and does not transmit a response to the message to the airborne communication device. Item 9: 9. The communication control device according to any one of items 6 to 8, wherein the connection restriction unit is provided in the non-terrestrial network and transmits a connection restriction request to the non-terrestrial base station to the airborne communication device. Item 10: 8. A communication control device according to any one of items 1 to 7, wherein the connection restriction unit restricts the connection between the non-terrestrial base station and the airborne communication device when there is only one non-terrestrial base station to which the airborne communication device can connect. Item 11: 11. The communication control device according to any one of items 1 to 10, wherein the non-terrestrial base station is a communication satellite flying in outer space. Item 12: Detecting an airborne communication device located above the ground; a flying non-terrestrial base station providing a non-terrestrial communication cell to a communication device, and restricting connectivity of said flying communication device; A communication control method comprising: Item 13: Detecting an airborne communication device located above the ground; a flying non-terrestrial base station providing a non-terrestrial communication cell to a communication device, and restricting connectivity of said flying communication device; A storage medium that stores a communication control program that causes a computer to execute the above. [Industrial Applicability]

[0059] The present disclosure relates to a communication control technique in a communication system. [Explanation of symbols]

[0060] 1 wireless communication system, 2 communication device, 2F airborne communication device, 2G ground communication device, 3 communication control device, 11 5G wireless communication system, 12 4G wireless communication system, 13 satellite communication system, 31 airborne communication device detection unit, 32 orbit information acquisition unit, 33 connection restriction unit, 111 5G base station, 112 5G cell, 121 4G base station, 122 4G cell, 131 communication satellite, 132 satellite communication cell, 133 gateway.

Claims

1. an airborne communication device detection unit that detects an airborne communication device located above the ground; a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device; and a connection limiting unit that limits connection of the airborne communication device when a signal propagation time between the non-terrestrial base station and the flying non-terrestrial base station is less than a predetermined value; A communication control device comprising:

2. A communication control device as described in Claim 1, wherein the airborne communication device whose connection is restricted belongs to a non-terrestrial network constituted by the non-terrestrial base station.

3. The communication control device according to claim 1 , wherein the airborne communication device is a communication device inside a flying aircraft.

4. The communication control device according to claim 1 , wherein the airborne communication aircraft detection unit detects itself as an airborne communication aircraft.

5. The communication control device according to claim 4 , wherein the connection restriction unit restricts transmission of a connection request from the airborne communication device to the non-terrestrial base station.

6. The communication control device according to claim 1 , wherein the signal is a message transmitted by the airborne communication device to the non-terrestrial base station in a random access procedure.

7. The communication control device according to claim 6 , wherein the connection restriction unit is provided in a non-terrestrial network configured by the non-terrestrial base stations, and does not transmit a response to the message to the airborne communication device.

8. The communication control device according to claim 1 , wherein the connection restriction unit is provided in a non-terrestrial network configured by the non-terrestrial base stations, and transmits a connection restriction request to the airborne communication device for the non-terrestrial base stations.

9. The communication control device according to claim 1 , wherein the connection restriction unit restricts the connection between the non-terrestrial base station and the airborne communication device when the non-terrestrial base station to which the airborne communication device can be connected is one.

10. The communication control device according to claim 1 , wherein the non-terrestrial base station is a communication satellite flying in outer space.

11. An airborne communication device detection unit that detects that the device itself corresponds to an airborne communication device located above the ground based on the altitude detected by a positioning sensor that detects the device's own altitude; a connection restriction unit that restricts connection between itself and the non-terrestrial base station when a difference between the altitude of the non-terrestrial base station notified to the airborne communication device by a non-terrestrial network configured by flying non-terrestrial base stations that provide non-terrestrial communication cells to the communication device and the altitude of the airborne communication device detected by the positioning sensor is equal to or less than a predetermined value; A communication device comprising:

12. Detecting an airborne communication device located above the ground; restricting connection of the airborne communication device to a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device when a signal propagation time between the non-terrestrial base station is equal to or less than a predetermined value; A communication control method comprising:

13. A communication control method as described in Claim 12, wherein the airborne communication device whose connection is restricted belongs to a non-terrestrial network constituted by the non-terrestrial base station.

14. A communication control method as described in claim 12, wherein the airborne communication device is a communication device inside a flying aircraft.

15. A communication control method as described in claim 12, wherein the communication device that executes the communication control method is itself detected as an airborne communication device.

16. A communication control method as described in claim 12, wherein the non-terrestrial base station is a communication satellite flying in outer space.

17. A communication control method executed by a communication device, comprising: a step of detecting that the communication device itself is an airborne communication device located above the ground based on an altitude detected by a positioning sensor that detects the altitude of the communication device itself; a step of restricting connection between the non-terrestrial base station and the airborne communication device when a difference between the altitude of the non-terrestrial base station notified to the airborne communication device by a non-terrestrial network constituted by a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device and the altitude of the airborne communication device detected by the positioning sensor is equal to or less than a predetermined value; A communication control method comprising:

18. Detecting an airborne communication device located above the ground; restricting connection of the airborne communication device to a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device when a signal propagation time between the non-terrestrial base station is equal to or less than a predetermined value; A communication control program that causes a computer to execute the above.

19. A communication control program as described in Claim 18, wherein the airborne communication device whose connection is restricted belongs to a non-terrestrial network constituted by the non-terrestrial base station.

20. A step of detecting that the communication device itself is an airborne communication device located above the ground based on an altitude detected by a positioning sensor that detects the altitude of the communication device itself; a step of restricting connection between the non-terrestrial base station and the airborne communication device when a difference between the altitude of the non-terrestrial base station notified to the airborne communication device by a non-terrestrial network constituted by a flying non-terrestrial base station that provides a non-terrestrial communication cell to the communication device and the altitude of the airborne communication device detected by the positioning sensor is equal to or less than a predetermined value; A communication control program that causes a computer in the communication device to execute the above.

Citation Information

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