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WO2018043284A1 - Base station device, emergency alert notification system, and emergency alert notification method - Google Patents

Base station device, emergency alert notification system, and emergency alert notification method Download PDF

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Publication number
WO2018043284A1
WO2018043284A1 PCT/JP2017/030320 JP2017030320W WO2018043284A1 WO 2018043284 A1 WO2018043284 A1 WO 2018043284A1 JP 2017030320 W JP2017030320 W JP 2017030320W WO 2018043284 A1 WO2018043284 A1 WO 2018043284A1
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WO
WIPO (PCT)
Prior art keywords
base station
emergency
unmanned aircraft
information
aircraft
Prior art date
Application number
PCT/JP2017/030320
Other languages
French (fr)
Japanese (ja)
Inventor
鈴木 由剛
矢島 俊輔
琢也 大久保
堅田 裕之
靖夫 菅原
重人 鈴木
Original Assignee
シャープ株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by シャープ株式会社 filed Critical シャープ株式会社
Publication of WO2018043284A1 publication Critical patent/WO2018043284A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/36Other airport installations
    • GPHYSICS
    • G08SIGNALLING
    • G08BSIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B25/00Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems
    • G08B25/01Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium
    • G08B25/10Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium using wireless transmission systems
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04MTELEPHONIC COMMUNICATION
    • H04M11/00Telephonic communication systems specially adapted for combination with other electrical systems
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04MTELEPHONIC COMMUNICATION
    • H04M11/00Telephonic communication systems specially adapted for combination with other electrical systems
    • H04M11/04Telephonic communication systems specially adapted for combination with other electrical systems with alarm systems, e.g. fire, police or burglar alarm systems

Definitions

  • Some embodiments of the present invention relate to a base station apparatus, an emergency alert notification system, and an emergency alert notification method.
  • This application claims priority based on Japanese Patent Application No. 2016-172768 filed in Japan on September 5, 2016, the contents of which are incorporated herein by reference.
  • Patent Document 1 describes a technique in which an unmanned aerial vehicle detects an emergency and performs a flight corresponding to the emergency.
  • Patent Document 2 describes an unmanned airplane equipped with a navigation device.
  • Patent Document 3 describes a rotary wing drone that transmits an emergency message to a central controller when an engine fails.
  • Patent Document 4 describes a robot device having identification information.
  • JP 2014-181034 A Japanese Patent No. 5819555 Japanese Patent No. 5819641 Japanese Unexamined Patent Publication No. 2016-506094
  • Patent Documents 1 to 4 cannot notify the person under the flying unmanned aircraft of the failure of the unmanned aircraft, the person is unaware of the presence of the unmanned aircraft and falls. There is a problem that there is a danger of colliding with an unmanned aircraft.
  • the present invention has been made in view of the above circumstances, and a base station device, an emergency alert notification system, and an emergency alert notification that can notify the person around the unmanned aircraft in which a failure has occurred to the presence of the unmanned aircraft.
  • One of the purposes is to provide a method.
  • the first aspect of the present invention is a wireless communication unit that wirelessly communicates with an unmanned aircraft, and the unmanned aircraft becomes an emergency.
  • a control unit that outputs emergency information indicating an emergency situation of the unmanned aircraft when it is determined that the unmanned aircraft is in an emergency state.
  • a second aspect of the present invention is an emergency alert notification system including an unmanned aircraft and a base station device, wherein the unmanned aircraft includes a wireless communication unit that wirelessly communicates with the base station device.
  • An apparatus includes: a wireless communication unit that wirelessly communicates with an unmanned aircraft; and a control unit that outputs emergency information indicating an emergency situation of the unmanned aircraft when it is determined that the unmanned aircraft is in an emergency situation. System.
  • an emergency alert notification method in a base station apparatus wherein a wireless communication process for wirelessly communicating with an unmanned aircraft and when the unmanned aircraft is determined to be in an emergency situation, And a control process for outputting emergency information indicating an emergency situation of the aircraft.
  • FIG. 1 is a schematic diagram illustrating an example of a configuration of an emergency alert notification system 1 according to the present embodiment.
  • the emergency alert notification system 1 includes home base stations 10-1, 10-2, an unmanned aircraft 20, communication terminals 40-0, 40-1, 40-2, a drone control system 50, and a business. Members 60-1 and 60-2.
  • the home base stations 10-1 and 10-2 may be collectively referred to as the home base station 10.
  • the communication terminals 40-0, 40-1, and 40-2 may be collectively referred to as the communication terminal 40.
  • the business operators 60-1 and 60-2 may be collectively referred to as the business operators 60.
  • the home base station 10 is a small base station device (Home eNodeB [indoor base station device], micro cell eNodeB) that transmits and receives data wirelessly with a mobile station device (User Equipment) such as the communication terminal 40 or the unmanned aircraft 20.
  • a mobile station device User Equipment
  • Microcell base station apparatus small base station apparatus
  • pico cell eNodeB picocell base station apparatus
  • femto cell eNodeB femtocell base station apparatus
  • the radius of a cell (range in which radio waves reach) that the home base station 10 provides services is, for example, a relatively narrow range of several meters to several tens of meters.
  • the home base station 10 is a base station device that has a narrow communication range with the mobile station device (typically, a radius of several meters to several tens of meters).
  • the home base station 10 is installed, for example, in each residential space of an apartment.
  • the home base stations 10-1 and 10-2 are connected to be communicable with each other via a network.
  • the number of home base stations 10 is not limited to the two illustrated, and may be one or more than two.
  • the unmanned aerial vehicle 20 is a drone, for example, and is a small aircraft that can fly unattended by remote control or automatic control.
  • the unmanned aerial vehicle 20 is a mobile station device that wirelessly transmits and receives data to and from the home base station 10.
  • the number of unmanned aerial vehicles 20 is not limited to the illustrated one, and may be more than one.
  • the communication terminal 40 is a mobile station device that transmits and receives data to and from the home base station 10 wirelessly.
  • the communication terminal 40 is, for example, a mobile phone, a smart phone, or a personal digital assistant (Personal Digital Assistant, PDA).
  • PDA Personal Digital Assistant
  • the number of communication terminals 40 is not limited to the illustrated three, and may be one, two, or more than three.
  • the drone control system 50 is a system that manages the operation of the unmanned aircraft 20, and includes, for example, one or a plurality of server devices.
  • the business operator 60 is an information processing apparatus such as a computer managed by a business operator (for example, a delivery company) that owns the unmanned aircraft 20.
  • the number of business operators 60 is not limited to the two illustrated, and may be one or more than two.
  • the unmanned aerial vehicle 20 searches the surroundings to find a connectable home base station 10, and flies while connecting to the found home base station 10. At this time, the unmanned aircraft 20 transmits emergency information to the connected home base station 10 when a failure occurs.
  • the emergency information is data indicating that a failure has occurred in the unmanned aerial vehicle 20 (emergency of the unmanned aircraft 20).
  • the drone ID which is the identification information of the unmanned aircraft 20, the failure level, the position information, and the unmanned aircraft 20 And at least a part of the open / close state of the parachute included in the unmanned aerial vehicle 20.
  • the failure level indicates the degree of failure, and the higher the level, the more likely it will crash.
  • the position information is GPS coordinates acquired by GPS (Global Positioning System), and includes latitude, longitude, and altitude.
  • the home base station 10 When the home base station 10 determines that the unmanned aircraft 20 is in an emergency, the home base station 10 outputs an emergency warning based on the emergency information. For example, the home base station 10 determines that the unmanned aircraft 20 has become an emergency when it receives emergency information from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 is suddenly interrupted. When the home base station 10 receives the emergency information from the unmanned aircraft 20, the home base station 10 acquires the aircraft information of the unmanned aircraft 20 from the drone control system 50 based on the received emergency information.
  • the airframe information is data related to the unmanned aircraft 20 and includes, for example, the size, color, and photograph of the airframe.
  • the home base station 10 transmits an aircraft information request including the drone ID included in the emergency information to the drone control system 50.
  • the drone control system 50 When receiving the aircraft information request, the drone control system 50 acquires the aircraft information corresponding to the drone ID included in the received aircraft information request from the business operator 60. Then, the drone control system 50 returns an aircraft information response including the acquired
  • the home base station 10 When the home base station 10 receives the aircraft information response, the home base station 10 transmits an emergency alert to at least a part of the communication terminals 40 in the cell provided by the home base station 10 (may be broadcast or multicast).
  • an emergency alert For emergency alerts, mechanisms such as PWS (Public Warning System), ETWS (Earthquake Tsunami Warning System), CMAS (Commercial Mobile Alert Service), etc., system information (System 20) Is information based on emergency information.
  • the emergency alert may include the drone ID of the unmanned aircraft 20, position information, airframe information, an estimated required time to fall, and a failure level.
  • the estimated required time to fall is the required time to fall predicted based on the altitude of the unmanned aircraft 20 included in the emergency information, the acceleration of the unmanned aircraft 20 and the open / close state of the parachute.
  • the communication terminal 40 When receiving the emergency alert, the communication terminal 40 notifies the user that the unmanned aircraft 20 has been dropped (the unmanned aircraft 20 is in an emergency state). For example, the communication terminal 40 notifies the user that the unmanned aircraft 20 has fallen by outputting a warning sound different from the earthquake tsunami warning. The warning sound may be a melody, a volume, a tone, or a length according to the failure level of the unmanned aircraft 20. Further, the communication terminal 40 notifies the user that the unmanned aircraft 20 has been dropped by displaying the received emergency alert. At this time, the communication terminal 40 may display the position information of the unmanned aircraft 20 included in the emergency alert on the map. Further, the communication terminal 40 may display a nearby evacuation place on a map in order to evacuate the user to a safe place.
  • FIG. 2 is a schematic diagram illustrating an example of the configuration of the home base station 10 according to the present embodiment.
  • the home base station 10 includes a control unit 101, a wireless communication unit 102, a network communication unit 103, a storage unit 104, an audio output unit 105, and a display unit 106.
  • the control unit 101 controls the home base station 10. For example, when the control unit 101 determines that the connected unmanned aircraft 20 is in an emergency situation, the control unit 101 outputs an emergency warning. When the wireless communication unit 102 receives emergency information from the unmanned aircraft 20, the control unit 101 determines that the unmanned aircraft 20 has entered an emergency situation. Alternatively, the control unit 101 determines that the unmanned aircraft 20 has become an emergency when communication with the unmanned aircraft 20 is suddenly interrupted. When it is determined that the connected unmanned aerial vehicle 20 is in an emergency situation, the control unit 101 generates an emergency alert based on the emergency information. More specifically, the control unit 101 writes the received emergency information in the storage unit 104 and transmits a body information request including the drone ID included in the emergency information to the drone control system 50 via the network communication unit 103.
  • the control unit 101 receives the aircraft information response from the drone control system 50 via the network communication unit 103 and writes the received aircraft information response in the storage unit 104. And the control part 101 produces
  • the control unit 101 causes the audio output unit 105 to output a warning sound. Or the control part 101 blinks LED (light emitting diode) with which the display part 106 is provided. Alternatively, the control unit 101 causes the display unit 106
  • the wireless communication unit 102 performs wireless communication with mobile station devices such as the communication terminal 40 and the unmanned aircraft 20.
  • the network communication unit 103 communicates with communication devices such as other home base stations 10 and the drone control system 50 via the network.
  • the storage unit 104 stores various data used by the home base station 10. More specifically, the storage unit 104 stores the content of emergency information received from the unmanned aircraft 20 via the wireless communication unit 102. Further, the storage unit 104 provides necessary information to the control unit 101 when the control unit 101 transmits an aircraft information request to the drone control system 50 via the network communication unit 103. The storage unit 104 also stores the contents of the aircraft information response received from the drone control system 50 via the network communication unit 103.
  • the storage unit 104 is necessary for the control unit 101 when the control unit 101 transmits an emergency alert to the communication terminal 40 via the wireless communication unit 102 (may be notified or multicasted).
  • the audio output unit 105 is a speaker that outputs audio.
  • the display unit 106 includes an LED and a liquid crystal display, and displays information. The audio output unit 105 or the display unit 106 constitutes an output unit that outputs an alarm based on emergency information.
  • FIG. 3 is a schematic diagram illustrating an example of the configuration of the unmanned aerial vehicle 20 according to the present embodiment.
  • the unmanned aircraft 20 includes a control unit 201, a wireless communication unit 202, a storage unit 203, an imaging unit 204, a position information acquisition unit 205, a failure detection unit 206, an acceleration detection unit 207, a parachute opening / closing detection unit 208, and a flight control unit 209. Consists of.
  • the control unit 201 controls the unmanned aircraft 20. For example, when the failure detection unit 206 detects a failure, the control unit 201 generates emergency information when the failure level is higher than a predetermined level.
  • the predetermined level is a failure level that may crash.
  • the predetermined level may be, for example, a case where the flight control unit 209 attempts to move the unmanned aircraft 20 in a direction at a certain speed but cannot move the unmanned aircraft 20 at that speed or in that direction.
  • the predetermined level may be, for example, the case where the unmanned aircraft 20 moves at a speed exceeding the speed that can be controlled by the flight control unit 209.
  • the emergency information includes the drone ID stored in the storage unit 203, the position information acquired by the position information acquisition unit 205, the acceleration detected by the acceleration detection unit 207, and the opening / closing state of the parachute detected by the parachute opening / closing detection unit 208. , At least a part of the failure level detected by the failure detection unit 206 is included. Then, the control unit 201 transmits the generated emergency information from the wireless communication unit 202 to the connected home base station 10.
  • the wireless communication unit 202 performs wireless communication with a base station device such as the home base station 10.
  • the storage unit 203 stores various information such as the drone ID of the unmanned aircraft 20. More specifically, the storage unit 203 provides a drone ID to be stored to the control unit 201 when the control unit 201 generates emergency information.
  • the imaging unit 204 is a camera that images the surroundings.
  • the position information acquisition unit 205 acquires position information by GPS.
  • the failure detection unit 206 detects a failure of the unmanned aerial vehicle 20 and its failure level.
  • the acceleration detection unit 207 is a triaxial acceleration sensor, for example, and detects the acceleration of each of the three orthogonal axes.
  • the parachute open / close detection unit 208 detects the open / close state of the parachute included in the unmanned aircraft 20.
  • the flight control unit 209 controls the moving direction and moving speed of the unmanned aircraft 20.
  • FIG. 4 is a sequence diagram illustrating the notification process according to the present embodiment. This figure shows notification processing when the unmanned aircraft 20 is connected to the home base station 10 and a failure occurs during flight.
  • Step S ⁇ b> 101 The unmanned aircraft 20 transmits emergency information to the home base station 10.
  • Step S ⁇ b> 102 Upon receiving the emergency information, the home base station 10 transmits an aircraft information request to the drone control system 50.
  • Step S103 Upon receiving the aircraft information request, the drone control system 50 transmits an ID inquiry for inquiring the aircraft information of the drone ID included in the received aircraft information request to the business operator 60.
  • Step S ⁇ b> 104 Upon receipt of the ID inquiry, the business operator 60 returns the body information corresponding to the received ID inquiry to the drone control system 50.
  • Step S ⁇ b> 105) When the drone control system 50 receives the aircraft information, the drone control system 50 returns an aircraft information response including the received aircraft information to the home base station 10.
  • Step S106 Upon receiving the aircraft information response, the home base station 10 generates an emergency alert based on the received aircraft information response, and transmits the emergency alert to the communication terminal 40 in the cell provided by the home base station 10 (notification) Or multicast). Thereafter, the processing of the home base station 10 proceeds to step S108.
  • Step S107 Upon receiving the emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
  • Step S108 The home base station 10 outputs an emergency warning by outputting a warning sound or light. Thereafter, the process ends.
  • the emergency alert notification system 1 includes the home base station 10, the unmanned aircraft 20, the communication terminal 40, and the drone control system 50.
  • the unmanned aerial vehicle 20 communicates with the home base station 10 from the wireless communication unit 202 when the wireless communication unit 202 that wirelessly communicates with the home base station 10, the failure detection unit 206 that detects a failure, and the failure detection unit 206 detects a failure.
  • a control unit 201 that generates and transmits emergency information for notifying a failure.
  • the home base station 10 includes a wireless communication unit 102 that wirelessly communicates with the unmanned aircraft 20 and a control unit 101 that outputs an emergency alert based on emergency information when it is determined that the unmanned aircraft 20 has entered an emergency.
  • the control unit 101 determines that the unmanned aircraft 20 has entered an emergency situation. Further, the control unit 101 transmits an emergency alert to the communication terminal 40 that can communicate from the wireless communication unit 102. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
  • the home base station 10 also includes an audio output unit 105 and a display unit 106. When the wireless communication unit 102 receives emergency information from the unmanned aircraft 20 that notifies the malfunction of the unmanned aircraft 20, a warning sound is output to the audio output unit 105. Or an LED (light emitting diode) included in the display unit 106 is blinked or an emergency alarm is displayed on the display unit 106.
  • the home base station 10 to which the unmanned aircraft 20 is connected and the communication terminal 40 in the cell provided by the home base station 10. Can output an emergency alert. For this reason, the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
  • control unit 101 acquires the aircraft information corresponding to the drone ID from the drone control system 50 by transmitting the aircraft information request including the drone ID included in the emergency information to the drone control system 50. Output emergency alerts that contain information.
  • the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request.
  • the emergency information includes position information of the unmanned aircraft 20. Thereby, the position of the unmanned aerial vehicle 20 where the failure has occurred can be known.
  • the emergency information includes the acceleration of the unmanned aircraft 20. Thereby, it is possible to know the drop speed of the unmanned aerial vehicle 20 in which a failure has occurred, and it is possible to predict the time required for the drop.
  • the emergency information includes the open / close state of the parachute included in the unmanned aircraft 20. Thereby, the time required until the unmanned aerial vehicle 20 in which a failure has occurred can be predicted more accurately.
  • the home base station 10 transmits an emergency alert only to the communication terminal 40 in its own cell, but in this embodiment, the home base station 10 is another home base station 10 in the vicinity.
  • the point which transmits an emergency alert also differs from the first embodiment.
  • the control unit 101 of the home base station 10 transmits an emergency alert to the adjacent home base station 10 via the network communication unit 103.
  • Information regarding the adjacent home base station 10 is set in advance, and is stored in the storage unit 104.
  • the control unit 101 receives at least one of the communication terminals 40 in the cell provided by the control unit 101 via the wireless communication unit 102.
  • the received alarm information is transmitted to the part (may be broadcast or multicast). Since the other configuration of the home base station 10 is the same as that of the first embodiment, the description thereof is omitted.
  • FIG. 5 is a sequence diagram illustrating a notification process according to the present embodiment. This figure shows the notification process when the unmanned aircraft 20 is connected to the home base station 10-1 and a failure occurs during the flight.
  • the home base station 10-2 is close to the home base station 10-1.
  • the communication terminal 40-1 is in a cell provided by the home base station 10-1.
  • the communication terminal 40-2 is in a cell provided by the home base station 10-2.
  • step S201 to step S207 Since the processing from step S201 to step S207 is the same as the processing from step S101 to step S107 described above, description thereof is omitted.
  • Step S208 The home base station 10-1 transmits an emergency alert to the adjacent home base station 10-2. Thereafter, the processing of the home base station 10-1 proceeds to Step S212.
  • Step S209 Upon receiving the emergency alert, the home base station 10-2 transmits the received emergency alert to the communication terminal 40-2 in the cell provided by the home base station 10-2 (may be broadcast or multicast). Thereafter, the processing of the home base station 10-2 proceeds to Step S211.
  • Step S210 Upon receiving the emergency alert, the communication terminal 40 (40-2) displays and outputs the received emergency alert.
  • the home base station 10-2 outputs an emergency warning by outputting a warning sound or light.
  • Step S212 The home base station 10-1 outputs an emergency warning by outputting a warning sound or light. Thereafter, the process ends.
  • the emergency alert notification system 1 includes the home base station 10, the unmanned aircraft 20, the communication terminal 40, and the drone control system 50.
  • the unmanned aerial vehicle 20 communicates with the home base station 10 from the wireless communication unit 202 when the wireless communication unit 202 that wirelessly communicates with the home base station 10, the failure detection unit 206 that detects a failure, and the failure detection unit 206 detects a failure.
  • a control unit 201 that generates and transmits emergency information for notifying a failure.
  • the home base station 10 includes a wireless communication unit 102 that wirelessly communicates with the unmanned aircraft 20, a control unit 101 that outputs an emergency alert based on emergency information when it is determined that the unmanned aircraft 20 has entered an emergency, A network communication unit 103 that communicates with the station device.
  • the control unit 101 determines that the unmanned aircraft 20 has entered an emergency situation.
  • the control unit 101 transmits an emergency alert from the network communication unit 103 to another home base station 10 in the vicinity.
  • the communication terminal 40 displays and outputs the received emergency alert.
  • the home base station 10 includes an audio output unit 105 and a display unit 106, and the wireless communication unit 102 receives emergency information from the unmanned aircraft 20 for notifying a failure of the unmanned aircraft 20, or the network communication unit 103 is an emergency.
  • the sound output unit 105 outputs a warning sound
  • the LED provided in the display unit 106 blinks, or the display unit 106 displays an emergency alarm.
  • control unit 101 acquires the aircraft information corresponding to the drone ID from the drone control system 50 by transmitting the aircraft information request including the drone ID included in the emergency information to the drone control system 50. Output emergency alerts that contain information.
  • the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request.
  • FIG. 6 is a schematic diagram illustrating an example of the configuration of the emergency alert notification system 1A according to the present embodiment.
  • the emergency alert notification system 1A in the present embodiment includes a macro cell base station 30 in addition to the configuration of the emergency alert notification system 1 in the first embodiment. Since other configurations are the same as those of the first embodiment, the description thereof is omitted.
  • the macro cell base station 30 is a macro cell base station device (macro cell eNodeB) that transmits and receives data wirelessly to and from the mobile station device.
  • the radius of the cell provided by the macrocell base station 30 is, for example, a relatively wide range of several hundred meters to several tens km. That is, the macrocell base station 30 is a base station device that has a wide communication range with the mobile station device (typically, a radius of several hundred m to several tens km).
  • the macro cell base station 30 is communicably connected to the home base station 10 via a network.
  • the unmanned aerial vehicle 20 searches the surroundings to find a connectable macrocell base station 30 or home base station 10 and performs a flight while connecting to the found macrocell base station 30 or home base station 10.
  • the operation when a failure occurs while the unmanned aircraft 20 is connected to the home base station 10 is the same as that in the first embodiment or the second embodiment.
  • the unmanned aerial vehicle 20 transmits emergency information to the connected macro cell base station 30 when a failure occurs during connection with the macro cell base station 30.
  • the macrocell base station 30 determines that the unmanned aircraft 20 is in an emergency situation, the macrocell base station 30 outputs an emergency warning based on the emergency information.
  • the macro cell base station 30 determines that the unmanned aircraft 20 has entered an emergency when emergency information is received from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 is suddenly interrupted.
  • the macro cell base station 30 acquires the aircraft information of the unmanned aircraft 20 from the drone control system 50 based on the received emergency information.
  • the macro cell base station 30 generates an emergency alert based on the emergency information and the aircraft information, and transmits the generated emergency alert to the home base station 10 and / or the communication terminal 40 in the cell provided by the macro cell base station 30.
  • the home base station 10 When receiving the emergency alert, the home base station 10 transmits the received emergency alert to at least a part of the communication terminals 40 in the cell provided by the home base station 10 (may be broadcast or multicast). When each of the communication terminals 40 receives an emergency alert, the communication terminal 40 notifies the user that the unmanned aircraft 20 has fallen.
  • FIG. 7 is a schematic diagram illustrating an example of the configuration of the macro cell base station 30 according to the present embodiment.
  • the macrocell base station 30 includes a control unit 301, a wireless communication unit 302, a network communication unit 303, and a storage unit 304.
  • the control unit 301 controls the macro cell base station 30.
  • the control unit 301 determines that the connected unmanned aircraft 20 is in an emergency, the control unit 301 outputs an alarm.
  • the control unit 301 determines that the unmanned aircraft 20 has entered an emergency situation.
  • the control unit 301 determines that the unmanned aircraft 20 has entered an emergency when communication with the unmanned aircraft 20 is suddenly interrupted.
  • the control unit 301 generates an emergency alert based on the emergency information.
  • the control unit 301 writes the received emergency information in the storage unit 304 and transmits a body information request including the drone ID included in the emergency information to the drone control system 50 via the network communication unit 303. To do. Thereafter, the control unit 301 receives the aircraft information response from the drone control system 50 via the network communication unit 303 and writes the received aircraft information response in the storage unit 304. And the control part 301 produces
  • the wireless communication unit 302 performs wireless communication with mobile station devices such as the communication terminal 40 and the unmanned aircraft 20.
  • the network communication unit 303 communicates with a communication device such as the home base station 10 via the network.
  • the storage unit 304 stores various information used by the macrocell base station 30. More specifically, the storage unit 304 stores the content of emergency information received from the unmanned aircraft 20 via the wireless communication unit 302. In addition, the storage unit 304 provides necessary information to the control unit 301 when the control unit 301 transmits an aircraft information request to the drone control system 50 via the network communication unit 303. In addition, the storage unit 304 stores the contents of the aircraft information response received from the drone control system 50 via the network communication unit 303. The storage unit 304 provides necessary information to the control unit 301 when the control unit 301 transmits an emergency alert.
  • FIG. 8 is a sequence diagram illustrating a notification process according to the present embodiment. This figure shows notification processing when the unmanned aircraft 20 is connected to the macrocell base station 30 and a failure occurs during flight.
  • the home base stations 10-1 and 10-2 are in cells provided by the macro cell base station 30.
  • the communication terminal 40-1 is in a cell provided by the home base station 10-1.
  • the communication terminal 40-2 is in a cell provided by the home base station 10-2.
  • the communication terminal 40-3 is in a cell provided by the macrocell base station 30, but is not in a cell provided by the home base station 10-1 or in a cell provided by the home base station 10-1.
  • Step S ⁇ b> 301 The unmanned aerial vehicle 20 transmits emergency information to the macrocell base station 30.
  • Step S ⁇ b> 302 Upon receiving the emergency information, the macro cell base station 30 transmits a body information request to the drone control system 50.
  • Step S303 Upon receiving the aircraft information request, the drone control system 50 transmits an ID inquiry for inquiring the aircraft information of the drone ID included in the received aircraft information request to the business operator 60.
  • Step S ⁇ b> 304 Upon receipt of the ID inquiry, the business operator 60 returns the aircraft information corresponding to the received ID inquiry to the drone control system 50.
  • Step S ⁇ b> 305) Upon receiving the aircraft information, the drone control system 50 returns a aircraft information response including the received aircraft information to the macrocell base station 30.
  • Step S306 Upon receiving the aircraft information response, the macro cell base station 30 generates an emergency alert based on the received aircraft information response, and transmits the emergency alert to the home base station 10-1 in the cell provided by the macro cell base station 30 To do. Thereafter, the processing of the macrocell base station 30 proceeds to step S310.
  • Step S307 Upon receiving the emergency alert, the home base station 10-1 transmits the received emergency alert to the communication terminal 40-1 in the cell provided by the home base station 10-1. Thereafter, the processing of the home base station 10-1 proceeds to step S309.
  • Step S308 Upon receiving the emergency alert, the communication terminal 40-1 displays and outputs the received emergency alert.
  • Step S309 The home base station 10-1 outputs an emergency warning by outputting a warning sound or light.
  • Step S310 The macrocell base station 30 transmits an emergency alert to the home base station 10-2 in the cell provided by the macrocell base station 30.
  • Step S311 Upon receiving the emergency alert, the home base station 10-2 transmits the received emergency alert to the communication terminal 40-2 in the cell provided by the home base station 10-2. Thereafter, the process of the home base station 10-2 proceeds to the process of step S313.
  • Step S312 Upon receiving the emergency alert, the communication terminal 40-2 displays and outputs the received emergency alert.
  • Step S313 The home base station 10-2 outputs an emergency warning by outputting a warning sound or light.
  • Step S314 The macro cell base station 30 transmits an emergency alert to the communication terminal 40-3 in the cell provided by the macro cell base station 30.
  • Step S315) Upon receiving the emergency alert, the communication terminal 40-3 displays and outputs the received emergency alert. Thereafter, the process ends.
  • Step S310, Step S306, and Step S314 are described separately, it is desirable that they are transmitted at the same timing.
  • the emergency alert notification system 1A includes the home base station 10, the unmanned aircraft 20, the macro cell base station 30, the communication terminal 40, and the drone control system 50.
  • the unmanned aircraft 20 includes a wireless communication unit 202 that wirelessly communicates with the home base station 10 or the macrocell base station 30, a failure detection unit 206 that detects a failure, and a wireless communication unit 202 when the failure detection unit 206 detects a failure.
  • a control unit 201 that generates and transmits emergency information for notifying the home base station 10 or the macrocell base station 30 of the failure.
  • the wireless communication unit 302 that wirelessly communicates with the unmanned aircraft 20 outputs an emergency alert based on emergency information that notifies the emergency of the unmanned aircraft 20 And a network communication unit 303 that communicates with other base station devices.
  • the control unit 301 determines that the unmanned aircraft 20 has entered an emergency situation.
  • the control unit 301 transmits an emergency alert from the network communication unit 303 or the wireless communication unit 302 to the home base station 10 (that is, the adjacent home base station 10) and the communication terminal 40 in its own cell.
  • the home base station 10 When receiving the emergency alert, the home base station 10 transmits the received emergency alert to the communication terminal 40 in its own cell. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
  • the home base station 10 includes a voice output unit 105 and a display unit 106, and when receiving an emergency warning, causes the voice output unit 105 to output a warning sound, or blinks an LED provided in the display unit 106, or An emergency warning is displayed on the display unit 106.
  • the communication terminal 40, the home base station 10 in the cell provided by the macro cell base station 30 to which the unmanned aircraft 20 is connected and An emergency alert can be output to the communication terminal 40 in the cell provided by the home base station 10.
  • the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
  • the control part 301 acquires the airframe information corresponding to the said drone ID from the drone control system 50 by transmitting the airframe information request
  • the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request.
  • FIG. 9 is a schematic diagram illustrating an example of the configuration of the emergency alert notification system 1B according to the present embodiment.
  • the emergency alert notification system 1B in the present embodiment includes a macro cell base station 30 instead of the home base station 10 with respect to the emergency alert notification system 1 in the first embodiment. Since other configurations are the same as those of the first embodiment, the description thereof is omitted.
  • the control unit 301 of the macrocell base station 30 in the present embodiment generates an emergency alert when it determines that the connected unmanned aircraft 20 is in an emergency situation. Since the emergency determination method and the emergency alert generation method are the same as those in the third embodiment, description thereof is omitted. And the control part 301 transmits the emergency information produced
  • FIG. 10 is a sequence diagram illustrating a notification process according to the present embodiment. This figure shows notification processing when the unmanned aircraft 20 is connected to the macrocell base station 30 and a failure occurs during flight.
  • Step S ⁇ b> 401 The unmanned aircraft 20 transmits emergency information to the macro cell base station 30.
  • Step S ⁇ b> 402 Upon receiving the emergency information, the macro cell base station 30 transmits a body information request to the drone control system 50.
  • Step S403 Upon receiving the aircraft information request, the drone control system 50 transmits an ID inquiry for inquiring the aircraft information of the drone ID included in the received aircraft information request to the business operator 60.
  • Step S ⁇ b> 404 Upon receiving the ID inquiry, the business operator 60 returns the aircraft information corresponding to the received ID inquiry to the drone control system 50.
  • Step S ⁇ b> 405 When the drone control system 50 receives the aircraft information, the drone control system 50 returns an aircraft information response including the received aircraft information to the macro cell base station 30.
  • Step S406 Upon receiving the aircraft information response, the macro cell base station 30 generates an emergency alert based on the received aircraft information response, and transmits the emergency alert to the communication terminal 40 in the cell provided by the macro cell base station 30 (notification) Or multicast).
  • Step S407 Upon receiving the emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
  • the emergency alert notification system 1B includes the macro cell base station 30, the unmanned aircraft 20, the communication terminal 40, and the drone control system 50.
  • the unmanned aerial vehicle 20 includes a wireless communication unit 202 that wirelessly communicates with the macro cell base station 30, a failure detection unit 206 that detects a failure, and the wireless communication unit 202 to the macro cell base station 30 when the failure detection unit 206 detects a failure.
  • a control unit 201 that generates and transmits emergency information for notifying a failure.
  • the macrocell base station 30 includes a wireless communication unit 302 that wirelessly communicates with the unmanned aircraft 20 and a control unit 301 that outputs an emergency alert based on emergency information when it is determined that the unmanned aircraft 20 has entered an emergency.
  • the control unit 301 determines that the unmanned aircraft 20 has entered an emergency situation. In addition, the control unit 301 transmits an emergency alert to the communication terminal 40 that can communicate from the wireless communication unit 102. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
  • an emergency warning is output to the communication terminal 40 in the cell provided by the macro cell base station 30 to which the unmanned aircraft 20 is connected. Can do. For this reason, the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
  • the control part 301 acquires the airframe information corresponding to the said drone ID from the drone control system 50 by transmitting the airframe information request
  • the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request.
  • control part 101, control part 201, or control part 301 with a computer.
  • the program for realizing the control function may be recorded on a computer-readable recording medium, and the program recorded on the recording medium may be read by a computer system and executed.
  • the “computer system” is a computer system built in the home base station 10, the unmanned aircraft 20 or the macrocell base station 30, and includes hardware such as an OS and peripheral devices.
  • the “computer-readable recording medium” refers to a storage device such as a flexible medium, a magneto-optical disk, a portable medium such as a ROM or a CD-ROM, and a hard disk incorporated in a computer system. Furthermore, the “computer-readable recording medium” is a medium that dynamically holds a program for a short time, such as a communication line when transmitting a program via a network such as the Internet or a communication line such as a telephone line, In such a case, a volatile memory inside a computer system serving as a server or a client may be included and a program that holds a program for a certain period of time.
  • the program may be a program for realizing a part of the functions described above, and may be a program capable of realizing the functions described above in combination with a program already recorded in a computer system.
  • a part of the home base station 10, the unmanned aircraft 20 or the macro cell base station 30 in the above-described embodiment, for example, the control unit 101, the control unit 201, or the control unit 301 is integrated with LSI (Large Scale Integration) or the like. It may be realized as a circuit.
  • LSI Large Scale Integration
  • each of the control unit 101, the control unit 201, or the control unit 301 may be integrated into a processor.
  • the method of circuit integration is not limited to LSI, and may be realized by a dedicated circuit or a general-purpose processor.
  • an integrated circuit based on the technology may be used.
  • the unmanned aerial vehicle 20 detects a failure and transmits emergency information.
  • the present invention is not limited to this, and the operator who remotely operates the unmanned aircraft 20 is determined to be urgent.
  • emergency information may be transmitted by operating the unmanned aircraft 20.
  • the home base station 10 transmits an emergency alert to the communication terminal 40 in the cell provided by the home base station 10.
  • An alarm may be sent.
  • the home base station 10 may send an emergency alert by e-mail to a user's pre-registered e-mail address.
  • the home base station 10 or the macro cell base station 30 may send an emergency alert to the police or fire department in charge for notification.
  • the home base station 10 or the macro cell base station 30 identifies an operator (for example, a courier company) of the unmanned aircraft 20 based on the drone ID, and sends an emergency alert to the identified operator for notification. Good.
  • the operator information may be included in the emergency information.
  • an emergency warning is output when a failure occurs in the unmanned aircraft 20, but not limited to this, until the unmanned aircraft 20 falls after the failure occurs in the unmanned aircraft 20.
  • Emergency warnings including the progress information may be output sequentially.
  • the progress information includes position information (latitude, longitude, and altitude) of the unmanned aircraft 20.
  • the unmanned aerial vehicle 20 transmits emergency information to the home base station 10 or the macro cell base station 30 that is connected every predetermined time until it falls.
  • the home base station 10 or the macro cell base station 30 generates and outputs an emergency alert each time emergency information is received. Thereby, the person around the unmanned aerial vehicle 20 can know the state of the unmanned aircraft 20 falling.
  • the unmanned aircraft 20 transmits recovery information notifying the recovery to the home base station 10 or the macrocell base station 30.
  • the home base station 10 or the macro cell base station 30 receives the recovery information, the home base station 10 or the macro cell base station 30 generates and outputs an emergency warning cancel code.
  • the home base station 10 or the macro cell base station 30 may output the release code after a certain time has elapsed since the emergency information was received. Thereby, the person around the unmanned aerial vehicle 20 can know that the unmanned aerial vehicle 20 has recovered from the failure.
  • the home base station 10 or the macro cell base station 30 may transmit and notify information for notifying that the unmanned aircraft 20 has landed (falling completed). Thereby, the person around the unmanned aerial vehicle 20 can know that the unmanned aerial vehicle 20 has landed.
  • the emergency alert transmitted from the home base station 10 or the macro cell base station 30 may be in two stages.
  • the home base station 10 or the macro cell base station 30 transmits at least a part of the emergency information acquired from the unmanned aircraft 30 at the first time, and among the information acquired from the drone control system 50 at the second time. You may transmit at least one part.
  • the home base station 10 or the macro cell base station 30 may transmit the information transmitted during the first transmission in an overlapping manner.
  • the home base station 10 or the macro cell base station 30 may update the position information and the estimated required time transmitted by the first warning based on time lapse, wind information, and the like. .
  • a base station apparatus comprising: a wireless communication unit that wirelessly communicates with an unmanned aircraft; and a control unit that outputs emergency information indicating an emergency situation of the unmanned aircraft when it is determined that the unmanned aircraft has become an emergency.
  • the base station device according to (1) wherein the control unit determines that the unmanned aircraft is in an emergency when the emergency information is received from the unmanned aircraft.
  • a communication unit that communicates with another base station device is provided, and the control unit transmits information based on emergency information from the communication unit to the other base station device, according to any one of (1) to (4) The base station apparatus as described.
  • the base station apparatus according to any one of (1) to (5), wherein the emergency information includes position information of the unmanned aircraft. (7) The base station apparatus according to any one of (1) to (6), wherein the emergency information includes an acceleration of the unmanned aircraft. (8) The base station apparatus according to any one of (1) to (7), wherein the emergency information includes an open / closed state of a parachute included in the unmanned aircraft. (9) The base station apparatus according to any one of (1) to (8), further including an output unit, wherein the control unit causes the output unit to output an alarm based on emergency information.
  • An emergency alert notification system including an unmanned aircraft and a base station device, wherein the unmanned aircraft includes a wireless communication unit that wirelessly communicates with the base station device, and the base station device wirelessly communicates with the unmanned aircraft.
  • An emergency alert notification system comprising: a control unit that outputs emergency information indicating an emergency of the unmanned aircraft when it is determined that the unmanned aircraft has entered an emergency.
  • An emergency alert notification method in a base station device wherein a wireless communication process for wirelessly communicating with an unmanned aircraft and outputting emergency information indicating an unmanned aircraft emergency when it is determined that the unmanned aircraft has become an emergency And an emergency alert notification method.
  • Some aspects of the present invention are applied to a base station apparatus, an emergency warning notification system, an emergency warning notification method, and the like that are required to notify a person in the vicinity of an unmanned aircraft in which a failure has occurred to the presence of the unmanned aircraft. be able to.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Signal Processing (AREA)
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Abstract

Provided is a base station device, comprising: a wireless communication unit which wirelessly communicates with an unmanned aerial vehicle; and a control unit which, if it is determined that an emergency situation has occurred with the unmanned aerial vehicle, outputs emergency information which indicates the emergency situation of the unmanned aerial vehicle.

Description

基地局装置、緊急警報通知システム及び緊急警報通知方法Base station apparatus, emergency alert notification system, and emergency alert notification method
 本発明のいくつかの態様は、基地局装置、緊急警報通知システム及び緊急警報通知方法に関する。
 本願は、2016年9月5日に、日本に出願された特願2016-172768号に基づき優先権を主張し、その内容をここに援用する。
Some embodiments of the present invention relate to a base station apparatus, an emergency alert notification system, and an emergency alert notification method.
This application claims priority based on Japanese Patent Application No. 2016-172768 filed in Japan on September 5, 2016, the contents of which are incorporated herein by reference.
 現在、ドローン等の小型の無人航空機が普及してきているが、飛行中にこれらの無人航空機に故障が発生した場合には、墜落する恐れがある。特許文献1には、無人航空機が緊急事態を検出し、緊急事態に対応する飛行を行う技術が記載されている。また、特許文献2には、ナビゲーション装置を搭載した無人飛行機が記載されている。また、特許文献3には、エンジンが故障した場合に、中央コントローラに緊急メッセージを送信する回転翼無人機が記載されている。また、特許文献4には、識別情報を備えたロボットデバイスが記載されている。 Currently, small unmanned aerial vehicles such as drones have become widespread, but if these unmanned aerial vehicles break down during flight, they may crash. Patent Document 1 describes a technique in which an unmanned aerial vehicle detects an emergency and performs a flight corresponding to the emergency. Patent Document 2 describes an unmanned airplane equipped with a navigation device. Patent Document 3 describes a rotary wing drone that transmits an emergency message to a central controller when an engine fails. Patent Document 4 describes a robot device having identification information.
特開2014-181034号公報JP 2014-181034 A 特許第5819555号公報Japanese Patent No. 5819555 特許第5819641号公報Japanese Patent No. 5819641 特開2016-506094号公報Japanese Unexamined Patent Publication No. 2016-506094
 しかしながら、特許文献1~4に記載された技術では、飛行している無人航空機の下にいる人に当該無人航空機の故障を知らせることができないため、その人は無人航空機の存在に気付かず、落下する無人航空機と衝突する危険がある、という問題がある。 However, since the techniques described in Patent Documents 1 to 4 cannot notify the person under the flying unmanned aircraft of the failure of the unmanned aircraft, the person is unaware of the presence of the unmanned aircraft and falls. There is a problem that there is a danger of colliding with an unmanned aircraft.
 本発明は、上記した事情に鑑みてなされたもので、故障が発生した無人航空機の周囲にいる人に、当該無人航空機の存在を知らせることができる基地局装置、緊急警報通知システム及び緊急警報通知方法を提供することを目的の一つとする。 The present invention has been made in view of the above circumstances, and a base station device, an emergency alert notification system, and an emergency alert notification that can notify the person around the unmanned aircraft in which a failure has occurred to the presence of the unmanned aircraft. One of the purposes is to provide a method.
 本発明のいくつかの態様は上記の課題を解決するためになされたものであり、本発明の第1の態様は、無人航空機と無線通信する無線通信部と、前記無人航空機が緊急事態になったと判定した場合に、前記無人航空機の緊急事態を示す緊急情報を出力する制御部と、を備える基地局装置である。 Some aspects of the present invention have been made to solve the above-described problems. The first aspect of the present invention is a wireless communication unit that wirelessly communicates with an unmanned aircraft, and the unmanned aircraft becomes an emergency. A control unit that outputs emergency information indicating an emergency situation of the unmanned aircraft when it is determined that the unmanned aircraft is in an emergency state.
 また、本発明の第2の態様は、無人航空機と基地局装置とを備える緊急警報通知システムであって、前記無人航空機は、前記基地局装置と無線通信する無線通信部を備え、前記基地局装置は、無人航空機と無線通信する無線通信部と、前記無人航空機が緊急事態になったと判定した場合に、前記無人航空機の緊急事態を示す緊急情報を出力する制御部と、を備える緊急警報通知システムである。 A second aspect of the present invention is an emergency alert notification system including an unmanned aircraft and a base station device, wherein the unmanned aircraft includes a wireless communication unit that wirelessly communicates with the base station device. An apparatus includes: a wireless communication unit that wirelessly communicates with an unmanned aircraft; and a control unit that outputs emergency information indicating an emergency situation of the unmanned aircraft when it is determined that the unmanned aircraft is in an emergency situation. System.
 また、本発明の第3の態様は、基地局装置における緊急警報通知方法であって、無人航空機と無線通信する無線通信過程と、前記無人航空機が緊急事態になったと判定した場合に、前記無人航空機の緊急事態を示す緊急情報を出力する制御過程と、を有する緊急警報通知方法である。 According to a third aspect of the present invention, there is provided an emergency alert notification method in a base station apparatus, wherein a wireless communication process for wirelessly communicating with an unmanned aircraft and when the unmanned aircraft is determined to be in an emergency situation, And a control process for outputting emergency information indicating an emergency situation of the aircraft.
 本発明のいくつかの態様によれば、故障が発生した無人航空機の周囲にいる人に、当該無人航空機の存在を知らせることができる。 According to some aspects of the present invention, it is possible to notify the person around the unmanned aerial vehicle where the failure has occurred to the presence of the unmanned aerial vehicle.
本発明の第1の実施形態に係る緊急警報通知システムの構成の一例を示す概略図である。It is the schematic which shows an example of a structure of the emergency alert notification system which concerns on the 1st Embodiment of this invention. 本実施形態に係るホーム基地局の構成の一例を示す概略図である。It is the schematic which shows an example of a structure of the home base station which concerns on this embodiment. 本実施形態に係る無人航空機の構成の一例を示す概略図である。It is the schematic which shows an example of a structure of the unmanned aircraft which concerns on this embodiment. 本実施形態に係る通知処理を表すシーケンス図である。It is a sequence diagram showing the notification process which concerns on this embodiment. 本発明の第2の実施形態に係る通知処理を表すシーケンス図である。It is a sequence diagram showing the notification process which concerns on the 2nd Embodiment of this invention. 本発明の第3の実施形態に係る緊急警報通知システムの構成の一例を示す概略図である。It is the schematic which shows an example of a structure of the emergency alert notification system which concerns on the 3rd Embodiment of this invention. 本実施形態に係るマクロセル基地局の構成の一例を示す概略図である。It is the schematic which shows an example of a structure of the macrocell base station which concerns on this embodiment. 本実施形態に係る通知処理を表すシーケンス図である。It is a sequence diagram showing the notification process which concerns on this embodiment. 本発明の第4の実施形態に係る緊急警報通知システムの構成の一例を示す概略図である。It is the schematic which shows an example of a structure of the emergency alert notification system which concerns on the 4th Embodiment of this invention. 本実施形態に係る通知処理を表すシーケンス図である。It is a sequence diagram showing the notification process which concerns on this embodiment.
 以下、図面を参照しながら本発明の実施形態について詳しく説明する。なお、各図において同一部分には同一符号を付している。 Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings. In the drawings, the same parts are denoted by the same reference numerals.
(第1の実施形態)
 まず、本発明の第1の実施形態について説明する。
 図1は、本実施形態に係る緊急警報通知システム1の構成の一例を示す概略図である。
 本図に示すように、緊急警報通知システム1は、ホーム基地局10-1、10-2、無人航空機20、通信端末40-0、40-1、40-2、ドローン管制システム50、及び事業者60-1、60-2を含んで構成される。以下、ホーム基地局10-1、10-2をホーム基地局10と総称することがある。また、通信端末40-0、40-1、40-2を通信端末40と総称することがある。また、事業者60-1、60-2を事業者60と総称することがある。
(First embodiment)
First, a first embodiment of the present invention will be described.
FIG. 1 is a schematic diagram illustrating an example of a configuration of an emergency alert notification system 1 according to the present embodiment.
As shown in the figure, the emergency alert notification system 1 includes home base stations 10-1, 10-2, an unmanned aircraft 20, communication terminals 40-0, 40-1, 40-2, a drone control system 50, and a business. Members 60-1 and 60-2. Hereinafter, the home base stations 10-1 and 10-2 may be collectively referred to as the home base station 10. In addition, the communication terminals 40-0, 40-1, and 40-2 may be collectively referred to as the communication terminal 40. Further, the business operators 60-1 and 60-2 may be collectively referred to as the business operators 60.
 ホーム基地局10は、通信端末40や無人航空機20などの移動局装置(User Equipment)との間で、無線でデータを送受信する小型基地局装置(Home eNodeB[屋内基地局装置]、micro cell eNodeB[マイクロセル基地局装置]、pico cell eNodeB[ピコセル基地局装置]、femto cell eNodeB[フェムトセル基地局装置]とも呼ばれる)である。ホーム基地局10がサービスを提供するセル(電波が到達する範囲)の半径は、例えば数m~数十mの比較的狭い範囲である。即ち、ホーム基地局10とは、移動局装置との通信可能な範囲が狭い(典型的には、半径数m~数十m)基地局装置である。ホーム基地局10は、例えば、マンションの各住居スペース等に設置されている。また、ホーム基地局10-1、10-2は、ネットワークを介して、互いに通信可能に接続されている。本実施形態では、ホーム基地局10の個数は図示した2個に限られず、1個、又は2個よりも多くてもよい。 The home base station 10 is a small base station device (Home eNodeB [indoor base station device], micro cell eNodeB) that transmits and receives data wirelessly with a mobile station device (User Equipment) such as the communication terminal 40 or the unmanned aircraft 20. [Microcell base station apparatus], pico cell eNodeB [picocell base station apparatus], and femto cell eNodeB [femtocell base station apparatus]). The radius of a cell (range in which radio waves reach) that the home base station 10 provides services is, for example, a relatively narrow range of several meters to several tens of meters. That is, the home base station 10 is a base station device that has a narrow communication range with the mobile station device (typically, a radius of several meters to several tens of meters). The home base station 10 is installed, for example, in each residential space of an apartment. The home base stations 10-1 and 10-2 are connected to be communicable with each other via a network. In the present embodiment, the number of home base stations 10 is not limited to the two illustrated, and may be one or more than two.
 無人航空機20は、例えばドローンであり、遠隔操作や自動制御によって無人で飛行できる小型の航空機である。無人航空機20は、ホーム基地局10との間で、無線でデータを送受信する移動局装置である。本実施形態では、無人航空機20の個数は図示した1個に限られず、1個よりも多くてもよい。 The unmanned aerial vehicle 20 is a drone, for example, and is a small aircraft that can fly unattended by remote control or automatic control. The unmanned aerial vehicle 20 is a mobile station device that wirelessly transmits and receives data to and from the home base station 10. In the present embodiment, the number of unmanned aerial vehicles 20 is not limited to the illustrated one, and may be more than one.
 通信端末40は、ホーム基地局10との間で、無線でデータを送受信する移動局装置である。通信端末40は、例えば、携帯電話機、スマートフォン、携帯情報端末装置(Personal Digital Assistant、PDA)である。本実施形態では、通信端末40の個数は図示した3個に限られず、1個、2個又は3個よりも多くてもよい。 The communication terminal 40 is a mobile station device that transmits and receives data to and from the home base station 10 wirelessly. The communication terminal 40 is, for example, a mobile phone, a smart phone, or a personal digital assistant (Personal Digital Assistant, PDA). In the present embodiment, the number of communication terminals 40 is not limited to the illustrated three, and may be one, two, or more than three.
 ドローン管制システム50は、無人航空機20の運航を管理するシステムであり、例えば、1または複数のサーバ装置を含む。事業者60は、無人航空機20を所有する事業者(例えば、宅配事業者)が管理するコンピュータ等の情報処理装置である。本実施形態では、事業者60の個数は図示した2個に限られず、1個、又は2個よりも多くてもよい。 The drone control system 50 is a system that manages the operation of the unmanned aircraft 20, and includes, for example, one or a plurality of server devices. The business operator 60 is an information processing apparatus such as a computer managed by a business operator (for example, a delivery company) that owns the unmanned aircraft 20. In the present embodiment, the number of business operators 60 is not limited to the two illustrated, and may be one or more than two.
 続いて、緊急警報通知システム1の概要について説明する。
 無人航空機20は、周辺をサーチして接続可能なホーム基地局10を見付け、見付けたホーム基地局10と接続しながら飛行を行う。このとき、無人航空機20は、故障が発生した場合には、接続しているホーム基地局10に対して緊急情報を送信する。緊急情報は、無人航空機20に故障が発生したこと(無人航空機20の緊急事態)を示すデータであり、無人航空機20の識別情報であるドローンIDと、故障レベルと、位置情報と、無人航空機20の加速度と、無人航空機20が備えるパラシュートの開閉状態のうちの少なくとも一部を含む。故障レベルは、故障の度合いを示し、そのレベルが高いほど墜落する可能性が高い。位置情報は、GPS(Global Positioning System)により取得したGPS座標であって、緯度、経度、及び高度を含む。
Then, the outline | summary of the emergency alert notification system 1 is demonstrated.
The unmanned aerial vehicle 20 searches the surroundings to find a connectable home base station 10, and flies while connecting to the found home base station 10. At this time, the unmanned aircraft 20 transmits emergency information to the connected home base station 10 when a failure occurs. The emergency information is data indicating that a failure has occurred in the unmanned aerial vehicle 20 (emergency of the unmanned aircraft 20). The drone ID, which is the identification information of the unmanned aircraft 20, the failure level, the position information, and the unmanned aircraft 20 And at least a part of the open / close state of the parachute included in the unmanned aerial vehicle 20. The failure level indicates the degree of failure, and the higher the level, the more likely it will crash. The position information is GPS coordinates acquired by GPS (Global Positioning System), and includes latitude, longitude, and altitude.
 ホーム基地局10は、無人航空機20が緊急事態になったと判定した場合に、緊急情報に基づく緊急警報を出力する。例えば、ホーム基地局10は、無人航空機20から緊急情報を受信した場合、或いは、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。ホーム基地局10は、無人航空機20から緊急情報を受信すると、受信した緊急情報に基づいて、ドローン管制システム50から無人航空機20の機体情報を取得する。機体情報は、無人航空機20に関するデータであって、例えば、機体の大きさや色、写真等を含む。具体的には、ホーム基地局10は、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信する。ドローン管制システム50は、機体情報要求を受信すると、受信した機体情報要求に含まれるドローンIDに対応する機体情報を事業者60から取得する。そして、ドローン管制システム50は、取得した機体情報を含む機体情報応答をホーム基地局10に返信する。 When the home base station 10 determines that the unmanned aircraft 20 is in an emergency, the home base station 10 outputs an emergency warning based on the emergency information. For example, the home base station 10 determines that the unmanned aircraft 20 has become an emergency when it receives emergency information from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 is suddenly interrupted. When the home base station 10 receives the emergency information from the unmanned aircraft 20, the home base station 10 acquires the aircraft information of the unmanned aircraft 20 from the drone control system 50 based on the received emergency information. The airframe information is data related to the unmanned aircraft 20 and includes, for example, the size, color, and photograph of the airframe. Specifically, the home base station 10 transmits an aircraft information request including the drone ID included in the emergency information to the drone control system 50. When receiving the aircraft information request, the drone control system 50 acquires the aircraft information corresponding to the drone ID included in the received aircraft information request from the business operator 60. Then, the drone control system 50 returns an aircraft information response including the acquired aircraft information to the home base station 10.
 ホーム基地局10は、機体情報応答を受信すると、自身が提供するセル内にいる通信端末40の少なくとも一部に緊急警報を送信する(報知またはマルチキャストしても良い)。緊急警報は、PWS(Public Warning System)、ETWS(Earthquake Tsunami Warning System)、CMAS(Commercial Mobile Alert Service)等の仕組みや、システム情報(System Information)等を用いて送信される、無人航空機20の落下を警報する情報であって、緊急情報に基づく情報である。緊急警報には、無人航空機20のドローンIDと、位置情報と、機体情報と、落下までの予測所要時間と、故障レベルとが含まれていてもよい。落下までの予測所要時間は、緊急情報に含まれる無人航空機20の高度と無人航空機20の加速度とパラシュートの開閉状態とに基づいて予測した落下までの所要時間である。 When the home base station 10 receives the aircraft information response, the home base station 10 transmits an emergency alert to at least a part of the communication terminals 40 in the cell provided by the home base station 10 (may be broadcast or multicast). For emergency alerts, mechanisms such as PWS (Public Warning System), ETWS (Earthquake Tsunami Warning System), CMAS (Commercial Mobile Alert Service), etc., system information (System 20) Is information based on emergency information. The emergency alert may include the drone ID of the unmanned aircraft 20, position information, airframe information, an estimated required time to fall, and a failure level. The estimated required time to fall is the required time to fall predicted based on the altitude of the unmanned aircraft 20 included in the emergency information, the acceleration of the unmanned aircraft 20 and the open / close state of the parachute.
 通信端末40は、緊急警報を受信すると、無人航空機20の落下(無人航空機20が緊急状態であること)をユーザに通知する。例えば、通信端末40は、地震津波警報とは異なる警告音を出力することにより、無人航空機20の落下をユーザに通知する。当該警告音は、無人航空機20の故障レベルに応じたメロディ、音量、トーンまたは長さであってもよい。また、通信端末40は、受信した緊急警報を表示することにより、無人航空機20の落下をユーザに通知する。このとき、通信端末40は、緊急警報に含まれる無人航空機20の位置情報を地図上に表示してもよい。また、通信端末40は、ユーザを安全な場所に退避させるため、近隣の避難場所を地図上に表示してもよい。 When receiving the emergency alert, the communication terminal 40 notifies the user that the unmanned aircraft 20 has been dropped (the unmanned aircraft 20 is in an emergency state). For example, the communication terminal 40 notifies the user that the unmanned aircraft 20 has fallen by outputting a warning sound different from the earthquake tsunami warning. The warning sound may be a melody, a volume, a tone, or a length according to the failure level of the unmanned aircraft 20. Further, the communication terminal 40 notifies the user that the unmanned aircraft 20 has been dropped by displaying the received emergency alert. At this time, the communication terminal 40 may display the position information of the unmanned aircraft 20 included in the emergency alert on the map. Further, the communication terminal 40 may display a nearby evacuation place on a map in order to evacuate the user to a safe place.
 次に、本実施形態に係るホーム基地局10の構成について説明する。
 図2は、本実施形態に係るホーム基地局10の構成の一例を示す概略図である。ホーム基地局10は、制御部101、無線通信部102、ネットワーク通信部103、記憶部104、音声出力部105及び表示部106を含んで構成される。
Next, the configuration of the home base station 10 according to the present embodiment will be described.
FIG. 2 is a schematic diagram illustrating an example of the configuration of the home base station 10 according to the present embodiment. The home base station 10 includes a control unit 101, a wireless communication unit 102, a network communication unit 103, a storage unit 104, an audio output unit 105, and a display unit 106.
 制御部101は、ホーム基地局10を制御する。例えば、制御部101は、接続している無人航空機20が緊急事態になったと判定した場合に、緊急警報を出力する。制御部101は、無線通信部102が無人航空機20から緊急情報を受信した場合に、無人航空機20が緊急事態になったと判定する。或いは、制御部101は、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。制御部101は、接続している無人航空機20が緊急事態になったと判定した場合には、緊急情報に基づく緊急警報を生成する。より具体的には、制御部101は、受信した緊急情報を記憶部104に書き込むとともに、ネットワーク通信部103を介して、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信する。その後、制御部101は、ネットワーク通信部103を介して、ドローン管制システム50から機体情報応答を受信し、受信した機体情報応答を記憶部104に書き込む。そして、制御部101は、受信した機体情報応答に基づいて緊急警報を生成する。その後、制御部101は、生成した緊急警報を出力する。具体的には、制御部101は、無線通信部102を介して、ホーム基地局10が提供するセル内にいる(即ち、通信可能な)通信端末40の少なくとも一部に緊急警報を送信する(報知またはマルチキャストしても良い)。また、制御部101は、音声出力部105に警告音を出力させる。或いは、制御部101は、表示部106が備えるLED(light emitting diode)を点滅させる。或いは、制御部101は、表示部106に緊急警報を表示させる。 The control unit 101 controls the home base station 10. For example, when the control unit 101 determines that the connected unmanned aircraft 20 is in an emergency situation, the control unit 101 outputs an emergency warning. When the wireless communication unit 102 receives emergency information from the unmanned aircraft 20, the control unit 101 determines that the unmanned aircraft 20 has entered an emergency situation. Alternatively, the control unit 101 determines that the unmanned aircraft 20 has become an emergency when communication with the unmanned aircraft 20 is suddenly interrupted. When it is determined that the connected unmanned aerial vehicle 20 is in an emergency situation, the control unit 101 generates an emergency alert based on the emergency information. More specifically, the control unit 101 writes the received emergency information in the storage unit 104 and transmits a body information request including the drone ID included in the emergency information to the drone control system 50 via the network communication unit 103. To do. Thereafter, the control unit 101 receives the aircraft information response from the drone control system 50 via the network communication unit 103 and writes the received aircraft information response in the storage unit 104. And the control part 101 produces | generates an emergency alert based on the received airframe information response. Thereafter, the control unit 101 outputs the generated emergency alert. Specifically, the control unit 101 transmits an emergency alert to at least a part of the communication terminals 40 in the cell provided by the home base station 10 (that is, capable of communication) via the wireless communication unit 102 ( Broadcast or multicast). In addition, the control unit 101 causes the audio output unit 105 to output a warning sound. Or the control part 101 blinks LED (light emitting diode) with which the display part 106 is provided. Alternatively, the control unit 101 causes the display unit 106 to display an emergency alert.
 無線通信部102は、通信端末40や無人航空機20等の移動局装置と無線通信する。
ネットワーク通信部103は、ネットワークを介して、他のホーム基地局10やドローン管制システム50等の通信装置と通信する。記憶部104は、ホーム基地局10が使用する種々のデータを記憶する。より具体的には、記憶部104は、無線通信部102を介して、無人航空機20から受信した緊急情報の内容を記憶する。また、記憶部104は、制御部101が、ネットワーク通信部103を介して、ドローン管制システム50に機体情報要求を送信する際は、制御部101に対して、必要な情報を提供する。また、記憶部104は、ネットワーク通信部103を介して、ドローン管制システム50から受信した機体情報応答の内容を記憶する。また、記憶部104は、制御部101が、無線通信部102を介して、通信端末40に緊急警報を送信する(報知またはマルチキャストしても良い)際は、制御部101に対して、必要な情報を提供する。音声出力部105は、音声を出力するスピーカである。表示部106は、LEDや液晶ディスプレイを備え、情報を表示する。音声出力部105又は表示部106が、緊急情報に基づく警報を出力する出力部を構成する。
The wireless communication unit 102 performs wireless communication with mobile station devices such as the communication terminal 40 and the unmanned aircraft 20.
The network communication unit 103 communicates with communication devices such as other home base stations 10 and the drone control system 50 via the network. The storage unit 104 stores various data used by the home base station 10. More specifically, the storage unit 104 stores the content of emergency information received from the unmanned aircraft 20 via the wireless communication unit 102. Further, the storage unit 104 provides necessary information to the control unit 101 when the control unit 101 transmits an aircraft information request to the drone control system 50 via the network communication unit 103. The storage unit 104 also stores the contents of the aircraft information response received from the drone control system 50 via the network communication unit 103. Further, the storage unit 104 is necessary for the control unit 101 when the control unit 101 transmits an emergency alert to the communication terminal 40 via the wireless communication unit 102 (may be notified or multicasted). Provide information. The audio output unit 105 is a speaker that outputs audio. The display unit 106 includes an LED and a liquid crystal display, and displays information. The audio output unit 105 or the display unit 106 constitutes an output unit that outputs an alarm based on emergency information.
 次に、本実施形態に係る無人航空機20の構成について説明する。
 図3は、本実施形態に係る無人航空機20の構成の一例を示す概略図である。無人航空機20は、制御部201、無線通信部202、記憶部203、撮像部204、位置情報取得部205、故障検出部206、加速度検出部207、パラシュート開閉検出部208及び飛行制御部209を含んで構成される。
Next, the configuration of the unmanned aircraft 20 according to the present embodiment will be described.
FIG. 3 is a schematic diagram illustrating an example of the configuration of the unmanned aerial vehicle 20 according to the present embodiment. The unmanned aircraft 20 includes a control unit 201, a wireless communication unit 202, a storage unit 203, an imaging unit 204, a position information acquisition unit 205, a failure detection unit 206, an acceleration detection unit 207, a parachute opening / closing detection unit 208, and a flight control unit 209. Consists of.
 制御部201は、無人航空機20を制御する。例えば、制御部201は、故障検出部206が故障を検出した場合に、その故障レベルが所定のレベルより大きいときに、緊急情報を生成する。当該所定のレベルは、墜落する可能性がある故障レベルである。当該所定のレベルは、例えば、飛行制御部209がある速度である方向に無人航空機20を移動させようとしても、その速度で又はその方向に無人航空機20を移動させることができない場合でも良い。また、当該所定のレベルは、例えば、飛行制御部209が制御可能な速度を超える速度で無人航空機20が移動してしまう場合でも良い。緊急情報には、記憶部203が記憶するドローンIDと、位置情報取得部205が取得する位置情報と、加速度検出部207が検出する加速度と、パラシュート開閉検出部208が検出するパラシュートの開閉状態と、故障検出部206が検出した故障レベルの少なくとも一部が含まれる。そして、制御部201は、生成した緊急情報を無線通信部202から、接続しているホーム基地局10に送信する。 The control unit 201 controls the unmanned aircraft 20. For example, when the failure detection unit 206 detects a failure, the control unit 201 generates emergency information when the failure level is higher than a predetermined level. The predetermined level is a failure level that may crash. The predetermined level may be, for example, a case where the flight control unit 209 attempts to move the unmanned aircraft 20 in a direction at a certain speed but cannot move the unmanned aircraft 20 at that speed or in that direction. The predetermined level may be, for example, the case where the unmanned aircraft 20 moves at a speed exceeding the speed that can be controlled by the flight control unit 209. The emergency information includes the drone ID stored in the storage unit 203, the position information acquired by the position information acquisition unit 205, the acceleration detected by the acceleration detection unit 207, and the opening / closing state of the parachute detected by the parachute opening / closing detection unit 208. , At least a part of the failure level detected by the failure detection unit 206 is included. Then, the control unit 201 transmits the generated emergency information from the wireless communication unit 202 to the connected home base station 10.
 無線通信部202は、ホーム基地局10等の基地局装置と無線通信する。記憶部203は、無人航空機20のドローンID等の種々の情報を記憶する。より具体的には、記憶部203は、制御部201が緊急情報を生成するときは、制御部201に対して、記憶するドローンIDを提供する。撮像部204は、周囲を撮像するカメラである。位置情報取得部205は、GPSにより位置情報を取得する。故障検出部206は、無人航空機20の故障とその故障レベルを検出する。加速度検出部207は、例えば3軸加速度センサであり、直交する3軸それぞれの加速度を検出する。パラシュート開閉検出部208は、無人航空機20が備えるパラシュートの開閉状態を検出する。飛行制御部209は、無人航空機20の移動方向や移動速度等を制御する。 The wireless communication unit 202 performs wireless communication with a base station device such as the home base station 10. The storage unit 203 stores various information such as the drone ID of the unmanned aircraft 20. More specifically, the storage unit 203 provides a drone ID to be stored to the control unit 201 when the control unit 201 generates emergency information. The imaging unit 204 is a camera that images the surroundings. The position information acquisition unit 205 acquires position information by GPS. The failure detection unit 206 detects a failure of the unmanned aerial vehicle 20 and its failure level. The acceleration detection unit 207 is a triaxial acceleration sensor, for example, and detects the acceleration of each of the three orthogonal axes. The parachute open / close detection unit 208 detects the open / close state of the parachute included in the unmanned aircraft 20. The flight control unit 209 controls the moving direction and moving speed of the unmanned aircraft 20.
 次に、本実施形態に係る通知処理について説明する。
 図4は、本実施形態に係る通知処理を表すシーケンス図である。
 本図には、無人航空機20がホーム基地局10と接続しており、飛行中に故障が発生した場合における通知処理を示す。
Next, notification processing according to the present embodiment will be described.
FIG. 4 is a sequence diagram illustrating the notification process according to the present embodiment.
This figure shows notification processing when the unmanned aircraft 20 is connected to the home base station 10 and a failure occurs during flight.
 (ステップS101)無人航空機20は、緊急情報をホーム基地局10に送信する。
 (ステップS102)ホーム基地局10は、緊急情報を受信すると、機体情報要求をドローン管制システム50に送信する。
(Step S <b> 101) The unmanned aircraft 20 transmits emergency information to the home base station 10.
(Step S <b> 102) Upon receiving the emergency information, the home base station 10 transmits an aircraft information request to the drone control system 50.
 (ステップS103)ドローン管制システム50は、機体情報要求を受信すると、受信した機体情報要求に含まれるドローンIDの機体情報を問い合わせるID問い合わせを事業者60に送信する。
 (ステップS104)事業者60は、ID問い合わせを受信すると、受信したID問い合わせに対応する機体情報をドローン管制システム50に返信する。
 (ステップS105)ドローン管制システム50は、機体情報を受信すると、受信した機体情報を含む機体情報応答をホーム基地局10に返信する。
 (ステップS106)ホーム基地局10は、機体情報応答を受信すると、受信した機体情報応答に基づいて緊急警報を生成し、自身の提供するセル内にいる通信端末40に緊急警報を送信する(報知またはマルチキャストしても良い)。この後、ホーム基地局10の処理は、ステップS108に進む。
(Step S103) Upon receiving the aircraft information request, the drone control system 50 transmits an ID inquiry for inquiring the aircraft information of the drone ID included in the received aircraft information request to the business operator 60.
(Step S <b> 104) Upon receipt of the ID inquiry, the business operator 60 returns the body information corresponding to the received ID inquiry to the drone control system 50.
(Step S <b> 105) When the drone control system 50 receives the aircraft information, the drone control system 50 returns an aircraft information response including the received aircraft information to the home base station 10.
(Step S106) Upon receiving the aircraft information response, the home base station 10 generates an emergency alert based on the received aircraft information response, and transmits the emergency alert to the communication terminal 40 in the cell provided by the home base station 10 (notification) Or multicast). Thereafter, the processing of the home base station 10 proceeds to step S108.
 (ステップS107)通信端末40は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。
 (ステップS108)ホーム基地局10は、警告音や光などを出力することにより、緊急警報を出力する。その後、処理を終了する。
(Step S107) Upon receiving the emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
(Step S108) The home base station 10 outputs an emergency warning by outputting a warning sound or light. Thereafter, the process ends.
 以上説明してきたように、本実施形態によれば、緊急警報通知システム1は、ホーム基地局10と、無人航空機20と、通信端末40と、ドローン管制システム50とを備える。無人航空機20は、ホーム基地局10と無線通信する無線通信部202と、故障を検出する故障検出部206と、故障検出部206が故障を検出した場合に、無線通信部202からホーム基地局10に故障を通知する緊急情報を生成して送信する制御部201とを備える。ホーム基地局10は、無人航空機20と無線通信する無線通信部102と、無人航空機20が緊急事態になったと判定した場合に、緊急情報に基づく緊急警報を出力する制御部101と、を備える。制御部101は、無線通信部102が緊急情報を無人航空機20から受信した場合、或いは、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。また、制御部101は、無線通信部102から通信可能な通信端末40に緊急警報を送信する。通信端末40は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。また、ホーム基地局10は、音声出力部105と表示部106を備え、無線通信部102が無人航空機20の故障を通知する緊急情報を無人航空機20から受信すると、音声出力部105に警告音を出力させ、或いは、表示部106が備えるLED(light emitting diode)を点滅させ、或いは、表示部106に緊急警報を表示させる。 As described above, according to the present embodiment, the emergency alert notification system 1 includes the home base station 10, the unmanned aircraft 20, the communication terminal 40, and the drone control system 50. The unmanned aerial vehicle 20 communicates with the home base station 10 from the wireless communication unit 202 when the wireless communication unit 202 that wirelessly communicates with the home base station 10, the failure detection unit 206 that detects a failure, and the failure detection unit 206 detects a failure. And a control unit 201 that generates and transmits emergency information for notifying a failure. The home base station 10 includes a wireless communication unit 102 that wirelessly communicates with the unmanned aircraft 20 and a control unit 101 that outputs an emergency alert based on emergency information when it is determined that the unmanned aircraft 20 has entered an emergency. When the wireless communication unit 102 receives emergency information from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 suddenly stops, the control unit 101 determines that the unmanned aircraft 20 has entered an emergency situation. Further, the control unit 101 transmits an emergency alert to the communication terminal 40 that can communicate from the wireless communication unit 102. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert. The home base station 10 also includes an audio output unit 105 and a display unit 106. When the wireless communication unit 102 receives emergency information from the unmanned aircraft 20 that notifies the malfunction of the unmanned aircraft 20, a warning sound is output to the audio output unit 105. Or an LED (light emitting diode) included in the display unit 106 is blinked or an emergency alarm is displayed on the display unit 106.
 これにより、故障が発生して墜落しそうな無人航空機20がある場合には、当該無人航空機20が接続しているホーム基地局10、及び当該ホーム基地局10が提供するセル内にいる通信端末40に緊急警報を出力させることができる。このため、故障が発生して墜落しそうな無人航空機20の周囲にいる人に当該無人航空機20の存在を知らせることができる。よって、周囲にいる人は回避や警戒をすることができるため、人身事故を防ぐことができる。 Thereby, when there is an unmanned aircraft 20 that is likely to crash due to a failure, the home base station 10 to which the unmanned aircraft 20 is connected, and the communication terminal 40 in the cell provided by the home base station 10. Can output an emergency alert. For this reason, the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
 また、制御部101は、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信することにより、当該ドローンIDに対応する機体情報をドローン管制システム50から取得し、取得した機体情報を含む緊急警報を出力する。ドローン管制システム50は、機体情報要求を受信すると、当該機体情報要求に対応する機体情報を含む機体情報応答を返信する。これにより、無線航空機20から送信されたドローンIDに基づいて、故障が発生して墜落しそうな無線航空機20がどういった機体であるかを特定することができる。 In addition, the control unit 101 acquires the aircraft information corresponding to the drone ID from the drone control system 50 by transmitting the aircraft information request including the drone ID included in the emergency information to the drone control system 50. Output emergency alerts that contain information. When the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request. Thereby, based on the drone ID transmitted from the wireless aircraft 20, it is possible to identify the type of the aircraft that is likely to crash due to a failure.
 また、緊急情報は、無人航空機20の位置情報を含む。これにより、故障が発生している無人航空機20の位置を知ることができる。 Further, the emergency information includes position information of the unmanned aircraft 20. Thereby, the position of the unmanned aerial vehicle 20 where the failure has occurred can be known.
 また、緊急情報は、無人航空機20の加速度を含む。これにより、故障が発生している無人航空機20の落下速度を知ることができ、落下までの所要時間を予測することが可能である。また、緊急情報は、無人航空機20が備えるパラシュートの開閉状態を含む。これにより、故障が発生している無人航空機20の落下までの所要時間をより精度良く予測することができる。 The emergency information includes the acceleration of the unmanned aircraft 20. Thereby, it is possible to know the drop speed of the unmanned aerial vehicle 20 in which a failure has occurred, and it is possible to predict the time required for the drop. The emergency information includes the open / close state of the parachute included in the unmanned aircraft 20. Thereby, the time required until the unmanned aerial vehicle 20 in which a failure has occurred can be predicted more accurately.
(第2の実施形態)
 次に、本発明の第2の実施形態について説明する。本実施形態における緊急警報通知システム1の構成は、第1の実施形態と同様であるため、その説明を省略する。第1の実施形態では、ホーム基地局10は自身のセル内にいる通信端末40にのみ緊急警報を送信しているが、本実施形態では、ホーム基地局10は近接する他のホーム基地局10にも緊急警報を送信する点が、第1の実施形態と異なる。
(Second Embodiment)
Next, a second embodiment of the present invention will be described. Since the configuration of the emergency alert notification system 1 in the present embodiment is the same as that in the first embodiment, the description thereof is omitted. In the first embodiment, the home base station 10 transmits an emergency alert only to the communication terminal 40 in its own cell, but in this embodiment, the home base station 10 is another home base station 10 in the vicinity. The point which transmits an emergency alert also differs from the first embodiment.
 本実施形態におけるホーム基地局10の制御部101は、ネットワーク通信部103を介して、近接するホーム基地局10に緊急警報を送信する。近接するホーム基地局10に関する情報は予め設定されており、記憶部104が記憶している。また、制御部101は、ネットワーク通信部103を介して、他のホーム基地局10から緊急警報を受信すると、無線通信部102を介して、自身が提供するセル内にいる通信端末40の少なくとも一部に、受信した警報情報を送信する(報知またはマルチキャストしても良い)。ホーム基地局10の他の構成は、第1の実施形態と同様であるため、その説明を省略する。 In the present embodiment, the control unit 101 of the home base station 10 transmits an emergency alert to the adjacent home base station 10 via the network communication unit 103. Information regarding the adjacent home base station 10 is set in advance, and is stored in the storage unit 104. In addition, when receiving an emergency alert from another home base station 10 via the network communication unit 103, the control unit 101 receives at least one of the communication terminals 40 in the cell provided by the control unit 101 via the wireless communication unit 102. The received alarm information is transmitted to the part (may be broadcast or multicast). Since the other configuration of the home base station 10 is the same as that of the first embodiment, the description thereof is omitted.
 次に、本実施形態に係る通知処理について説明する。
 図5は、本実施形態に係る通知処理を表すシーケンス図である。
 本図には、無人航空機20がホーム基地局10-1と接続しており、飛行中に故障が発生した場合における通知処理を示す。また、ホーム基地局10-2は、ホーム基地局10-1と近接する。また、通信端末40-1は、ホーム基地局10-1が提供するセル内にいる。また、通信端末40-2は、ホーム基地局10-2が提供するセル内にいる。
Next, notification processing according to the present embodiment will be described.
FIG. 5 is a sequence diagram illustrating a notification process according to the present embodiment.
This figure shows the notification process when the unmanned aircraft 20 is connected to the home base station 10-1 and a failure occurs during the flight. The home base station 10-2 is close to the home base station 10-1. Further, the communication terminal 40-1 is in a cell provided by the home base station 10-1. The communication terminal 40-2 is in a cell provided by the home base station 10-2.
 ステップS201からステップS207までの処理は、上述したステップS101からステップS107までの処理と同様であるため、その説明を省略する。 Since the processing from step S201 to step S207 is the same as the processing from step S101 to step S107 described above, description thereof is omitted.
 (ステップS208)ホーム基地局10-1は、近接するホーム基地局10-2に緊急警報を送信する。この後、ホーム基地局10-1の処理は、ステップS212に進む。
 (ステップS209)ホーム基地局10-2は、緊急警報を受信すると、自身の提供するセル内にいる通信端末40-2に受信した緊急警報を送信する(報知またはマルチキャストしても良い)。この後、ホーム基地局10-2の処理は、ステップS211に進む。
(Step S208) The home base station 10-1 transmits an emergency alert to the adjacent home base station 10-2. Thereafter, the processing of the home base station 10-1 proceeds to Step S212.
(Step S209) Upon receiving the emergency alert, the home base station 10-2 transmits the received emergency alert to the communication terminal 40-2 in the cell provided by the home base station 10-2 (may be broadcast or multicast). Thereafter, the processing of the home base station 10-2 proceeds to Step S211.
 (ステップS210)通信端末40(40-2)は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。
 (ステップS211)ホーム基地局10-2は、警告音や光などを出力することにより、緊急警報を出力する。
 (ステップS212)ホーム基地局10-1は、警告音や光などを出力することにより、緊急警報を出力する。その後、処理を終了する。
(Step S210) Upon receiving the emergency alert, the communication terminal 40 (40-2) displays and outputs the received emergency alert.
(Step S211) The home base station 10-2 outputs an emergency warning by outputting a warning sound or light.
(Step S212) The home base station 10-1 outputs an emergency warning by outputting a warning sound or light. Thereafter, the process ends.
 以上説明してきたように、本実施形態によれば、緊急警報通知システム1は、ホーム基地局10と、無人航空機20と、通信端末40と、ドローン管制システム50とを備える。無人航空機20は、ホーム基地局10と無線通信する無線通信部202と、故障を検出する故障検出部206と、故障検出部206が故障を検出した場合に、無線通信部202からホーム基地局10に故障を通知する緊急情報を生成して送信する制御部201とを備える。ホーム基地局10は、無人航空機20と無線通信する無線通信部102と、無人航空機20が緊急事態になったと判定した場合に、緊急情報に基づく緊急警報を出力する制御部101と、他の基地局装置と通信するネットワーク通信部103と、を備える。制御部101は、無線通信部102が緊急情報を無人航空機20から受信した場合、或いは、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。また、制御部101は、ネットワーク通信部103から近接する他のホーム基地局10に緊急警報を送信する。通信端末40は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。また、ホーム基地局10は、音声出力部105と表示部106を備え、無線通信部102が無人航空機20の故障を通知する緊急情報を無人航空機20から受信する、或いは、ネットワーク通信部103が緊急警報を受信すると、音声出力部105に警告音を出力させ、或いは、表示部106が備えるLEDを点滅させ、或いは、表示部106に緊急警報を表示させる。 As described above, according to the present embodiment, the emergency alert notification system 1 includes the home base station 10, the unmanned aircraft 20, the communication terminal 40, and the drone control system 50. The unmanned aerial vehicle 20 communicates with the home base station 10 from the wireless communication unit 202 when the wireless communication unit 202 that wirelessly communicates with the home base station 10, the failure detection unit 206 that detects a failure, and the failure detection unit 206 detects a failure. And a control unit 201 that generates and transmits emergency information for notifying a failure. The home base station 10 includes a wireless communication unit 102 that wirelessly communicates with the unmanned aircraft 20, a control unit 101 that outputs an emergency alert based on emergency information when it is determined that the unmanned aircraft 20 has entered an emergency, A network communication unit 103 that communicates with the station device. When the wireless communication unit 102 receives emergency information from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 suddenly stops, the control unit 101 determines that the unmanned aircraft 20 has entered an emergency situation. In addition, the control unit 101 transmits an emergency alert from the network communication unit 103 to another home base station 10 in the vicinity. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert. In addition, the home base station 10 includes an audio output unit 105 and a display unit 106, and the wireless communication unit 102 receives emergency information from the unmanned aircraft 20 for notifying a failure of the unmanned aircraft 20, or the network communication unit 103 is an emergency. When the alarm is received, the sound output unit 105 outputs a warning sound, the LED provided in the display unit 106 blinks, or the display unit 106 displays an emergency alarm.
 これにより、故障が発生して墜落しそうな無人航空機20がある場合には、当該無線航空機20が接続しているホーム基地局10が提供するセル内にいる通信端末40だけでなく、そのホーム基地局10に近接する他のホーム基地局10が提供するセル内にいる通信端末40にも、緊急警報を出力させることができる。このため、故障が発生して墜落しそうな無人航空機20の周囲にいる人に当該無人航空機20の存在を知らせることができる。よって、周囲にいる人は回避や警戒をすることができるため、人身事故を防ぐことができる。 As a result, when there is an unmanned aircraft 20 that is likely to crash due to a failure, not only the communication terminal 40 in the cell provided by the home base station 10 to which the wireless aircraft 20 is connected, but also its home base An emergency alert can also be output to the communication terminal 40 in a cell provided by another home base station 10 in the vicinity of the station 10. For this reason, the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
 また、制御部101は、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信することにより、当該ドローンIDに対応する機体情報をドローン管制システム50から取得し、取得した機体情報を含む緊急警報を出力する。ドローン管制システム50は、機体情報要求を受信すると、当該機体情報要求に対応する機体情報を含む機体情報応答を返信する。これにより、無線航空機20から送信されたドローンIDに基づいて、故障が発生して墜落しそうな無線航空機20がどういった機体であるかを特定することができる。 In addition, the control unit 101 acquires the aircraft information corresponding to the drone ID from the drone control system 50 by transmitting the aircraft information request including the drone ID included in the emergency information to the drone control system 50. Output emergency alerts that contain information. When the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request. Thereby, based on the drone ID transmitted from the wireless aircraft 20, it is possible to identify the type of the aircraft that is likely to crash due to a failure.
(第3の実施形態)
 次に、本発明の第3の実施形態について説明する。
 図6は、本実施形態に係る緊急警報通知システム1Aの構成の一例を示す概略図である。
 本実施形態における緊急警報通知システム1Aは、第1の実施形態における緊急警報通知システム1の構成に加えて、マクロセル基地局30を備える。他の構成は、第1の実施形態と同様であるため、その説明を省略する。
(Third embodiment)
Next, a third embodiment of the present invention will be described.
FIG. 6 is a schematic diagram illustrating an example of the configuration of the emergency alert notification system 1A according to the present embodiment.
The emergency alert notification system 1A in the present embodiment includes a macro cell base station 30 in addition to the configuration of the emergency alert notification system 1 in the first embodiment. Since other configurations are the same as those of the first embodiment, the description thereof is omitted.
 マクロセル基地局30は、移動局装置との間で、無線でデータを送受信するマクロセル基地局装置(macro cell eNodeB)である。マクロセル基地局30が提供するセルの半径は、例えば数百m~数十kmの比較的広い範囲である。即ち、マクロセル基地局30とは、移動局装置との通信可能な範囲が広い(典型的には、半径数百m~数十km)基地局装置である。マクロセル基地局30は、ネットワークを介して、ホーム基地局10と通信可能に接続されている。 The macro cell base station 30 is a macro cell base station device (macro cell eNodeB) that transmits and receives data wirelessly to and from the mobile station device. The radius of the cell provided by the macrocell base station 30 is, for example, a relatively wide range of several hundred meters to several tens km. That is, the macrocell base station 30 is a base station device that has a wide communication range with the mobile station device (typically, a radius of several hundred m to several tens km). The macro cell base station 30 is communicably connected to the home base station 10 via a network.
 続いて、緊急警報通知システム1Aの概要について説明する。
 無人航空機20は、周辺をサーチして接続可能なマクロセル基地局30またはホーム基地局10を見付け、見付けたマクロセル基地局30またはホーム基地局10と接続しながら飛行を行う。無人航空機20がホーム基地局10と接続中に故障が発生した際の動作は、第1の実施形態または第2の実施形態と同様である。
Next, an outline of the emergency alert notification system 1A will be described.
The unmanned aerial vehicle 20 searches the surroundings to find a connectable macrocell base station 30 or home base station 10 and performs a flight while connecting to the found macrocell base station 30 or home base station 10. The operation when a failure occurs while the unmanned aircraft 20 is connected to the home base station 10 is the same as that in the first embodiment or the second embodiment.
 一方、無人航空機20は、マクロセル基地局30と接続中に故障が発生した場合には、接続しているマクロセル基地局30に対して緊急情報を送信する。マクロセル基地局30は、無人航空機20が緊急事態になったと判定した場合に、緊急情報に基づく緊急警報を出力する。例えば、マクロセル基地局30は、無人航空機20から緊急情報を受信した場合、或いは、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。マクロセル基地局30は、無人航空機20から緊急情報を受信すると、受信した緊急情報に基づいて、ドローン管制システム50から無人航空機20の機体情報を取得する。そして、マクロセル基地局30は、緊急情報及び機体情報に基づいて緊急警報を生成し、自身が提供するセル内にあるホーム基地局10及び/又は通信端末40に生成した緊急警報を送信する。 On the other hand, the unmanned aerial vehicle 20 transmits emergency information to the connected macro cell base station 30 when a failure occurs during connection with the macro cell base station 30. When the macrocell base station 30 determines that the unmanned aircraft 20 is in an emergency situation, the macrocell base station 30 outputs an emergency warning based on the emergency information. For example, the macro cell base station 30 determines that the unmanned aircraft 20 has entered an emergency when emergency information is received from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 is suddenly interrupted. When receiving the emergency information from the unmanned aircraft 20, the macro cell base station 30 acquires the aircraft information of the unmanned aircraft 20 from the drone control system 50 based on the received emergency information. The macro cell base station 30 generates an emergency alert based on the emergency information and the aircraft information, and transmits the generated emergency alert to the home base station 10 and / or the communication terminal 40 in the cell provided by the macro cell base station 30.
 ホーム基地局10は、緊急警報を受信した場合、自身が提供するセル内にいる通信端末40の少なくとも一部に受信した緊急警報を送信する(報知またはマルチキャストしても良い)。通信端末40は、それぞれ緊急警報を受信すると、無人航空機20の落下をユーザに通知する。 When receiving the emergency alert, the home base station 10 transmits the received emergency alert to at least a part of the communication terminals 40 in the cell provided by the home base station 10 (may be broadcast or multicast). When each of the communication terminals 40 receives an emergency alert, the communication terminal 40 notifies the user that the unmanned aircraft 20 has fallen.
 次に、本実施形態に係るマクロセル基地局30の構成について説明する。
 図7は、本実施形態に係るマクロセル基地局30の構成の一例を示す概略図である。マクロセル基地局30は、制御部301、無線通信部302、ネットワーク通信部303及び記憶部304を含んで構成される。
Next, the configuration of the macro cell base station 30 according to the present embodiment will be described.
FIG. 7 is a schematic diagram illustrating an example of the configuration of the macro cell base station 30 according to the present embodiment. The macrocell base station 30 includes a control unit 301, a wireless communication unit 302, a network communication unit 303, and a storage unit 304.
 制御部301は、マクロセル基地局30を制御する。制御部301は、接続している無人航空機20が緊急事態になったと判定した場合に、警報を出力する。例えば、制御部301は、無線通信部302が緊急情報を無人航空機20から受信した場合に、無人航空機20が緊急事態になったと判定する。或いは、制御部301は、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。制御部301は、接続している無人航空機20が緊急事態になったと判定した場合には、緊急情報に基づく緊急警報を生成する。より具体的には、制御部301は、受信した緊急情報を記憶部304に書き込むとともに、ネットワーク通信部303を介して、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信する。その後、制御部301は、ネットワーク通信部303を介して、ドローン管制システム50から機体情報応答を受信し、受信した機体情報応答を記憶部304に書き込む。そして、制御部301は、受信した機体情報応答に基づいて緊急警報を生成する。制御部301は、ネットワーク通信部303または無線通信部302を介して、自身が提供するセル内にあるホーム基地局10及び通信端末40の少なくとも一部に生成した緊急情報を送信する(報知またはマルチキャストしても良い)。セル内にあるホーム基地局10に関する情報は予め設定されており、記憶部304が記憶している。 The control unit 301 controls the macro cell base station 30. When the control unit 301 determines that the connected unmanned aircraft 20 is in an emergency, the control unit 301 outputs an alarm. For example, when the wireless communication unit 302 receives emergency information from the unmanned aircraft 20, the control unit 301 determines that the unmanned aircraft 20 has entered an emergency situation. Alternatively, the control unit 301 determines that the unmanned aircraft 20 has entered an emergency when communication with the unmanned aircraft 20 is suddenly interrupted. When it is determined that the connected unmanned aerial vehicle 20 is in an emergency, the control unit 301 generates an emergency alert based on the emergency information. More specifically, the control unit 301 writes the received emergency information in the storage unit 304 and transmits a body information request including the drone ID included in the emergency information to the drone control system 50 via the network communication unit 303. To do. Thereafter, the control unit 301 receives the aircraft information response from the drone control system 50 via the network communication unit 303 and writes the received aircraft information response in the storage unit 304. And the control part 301 produces | generates an emergency alert based on the received airframe information response. The control unit 301 transmits the generated emergency information to at least a part of the home base station 10 and the communication terminal 40 in the cell provided by the control unit 301 via the network communication unit 303 or the wireless communication unit 302 (notification or multicast). You may). Information regarding the home base station 10 in the cell is set in advance, and is stored in the storage unit 304.
 無線通信部302は、通信端末40や無人航空機20等の移動局装置と無線通信する。
ネットワーク通信部303は、ネットワークを介して、ホーム基地局10等の通信装置と通信する。記憶部304は、マクロセル基地局30が使用する種々の情報を記憶する。より具体的には、記憶部304は、無線通信部302を介して、無人航空機20から受信した緊急情報の内容を記憶する。また、記憶部304は、制御部301が、ネットワーク通信部303を介して、ドローン管制システム50に機体情報要求を送信する際は、制御部301に対して、必要な情報を提供する。また、記憶部304は、ネットワーク通信部303を介して、ドローン管制システム50から受信した機体情報応答の内容を記憶する。
また、記憶部304は、制御部301が緊急警報を送信する際は、制御部301に対して、必要な情報を提供する。
The wireless communication unit 302 performs wireless communication with mobile station devices such as the communication terminal 40 and the unmanned aircraft 20.
The network communication unit 303 communicates with a communication device such as the home base station 10 via the network. The storage unit 304 stores various information used by the macrocell base station 30. More specifically, the storage unit 304 stores the content of emergency information received from the unmanned aircraft 20 via the wireless communication unit 302. In addition, the storage unit 304 provides necessary information to the control unit 301 when the control unit 301 transmits an aircraft information request to the drone control system 50 via the network communication unit 303. In addition, the storage unit 304 stores the contents of the aircraft information response received from the drone control system 50 via the network communication unit 303.
The storage unit 304 provides necessary information to the control unit 301 when the control unit 301 transmits an emergency alert.
 次に、本実施形態に係る通知処理について説明する。
 図8は、本実施形態に係る通知処理を表すシーケンス図である。
 本図には、無人航空機20がマクロセル基地局30と接続しており、飛行中に故障が発生した場合における通知処理を示す。また、ホーム基地局10-1、10-2は、マクロセル基地局30が提供するセル内にある。また、通信端末40-1は、ホーム基地局10-1が提供するセル内にいる。また、通信端末40-2は、ホーム基地局10-2が提供するセル内にいる。通信端末40-3は、マクロセル基地局30が提供するセル内にいるが、ホーム基地局10-1が提供するセル内にも、ホーム基地局10-1が提供するセル内にもいない。
Next, notification processing according to the present embodiment will be described.
FIG. 8 is a sequence diagram illustrating a notification process according to the present embodiment.
This figure shows notification processing when the unmanned aircraft 20 is connected to the macrocell base station 30 and a failure occurs during flight. The home base stations 10-1 and 10-2 are in cells provided by the macro cell base station 30. Further, the communication terminal 40-1 is in a cell provided by the home base station 10-1. The communication terminal 40-2 is in a cell provided by the home base station 10-2. The communication terminal 40-3 is in a cell provided by the macrocell base station 30, but is not in a cell provided by the home base station 10-1 or in a cell provided by the home base station 10-1.
 (ステップS301)無人航空機20は、緊急情報をマクロセル基地局30に送信する。
 (ステップS302)マクロセル基地局30は、緊急情報を受信すると、機体情報要求をドローン管制システム50に送信する。
(Step S <b> 301) The unmanned aerial vehicle 20 transmits emergency information to the macrocell base station 30.
(Step S <b> 302) Upon receiving the emergency information, the macro cell base station 30 transmits a body information request to the drone control system 50.
 (ステップS303)ドローン管制システム50は、機体情報要求を受信すると、受信した機体情報要求に含まれるドローンIDの機体情報を問い合わせるID問い合わせを事業者60に送信する。
 (ステップS304)事業者60は、ID問い合わせを受信すると、受信したID問い合わせに対応する機体情報をドローン管制システム50に返信する。
 (ステップS305)ドローン管制システム50は、機体情報を受信すると、受信した機体情報を含む機体情報応答をマクロセル基地局30に返信する。
 (ステップS306)マクロセル基地局30は、機体情報応答を受信すると、受信した機体情報応答に基づいて緊急警報を生成し、自身の提供するセル内にいるホーム基地局10-1に緊急警報を送信する。この後、マクロセル基地局30の処理は、ステップS310に進む。
(Step S303) Upon receiving the aircraft information request, the drone control system 50 transmits an ID inquiry for inquiring the aircraft information of the drone ID included in the received aircraft information request to the business operator 60.
(Step S <b> 304) Upon receipt of the ID inquiry, the business operator 60 returns the aircraft information corresponding to the received ID inquiry to the drone control system 50.
(Step S <b> 305) Upon receiving the aircraft information, the drone control system 50 returns a aircraft information response including the received aircraft information to the macrocell base station 30.
(Step S306) Upon receiving the aircraft information response, the macro cell base station 30 generates an emergency alert based on the received aircraft information response, and transmits the emergency alert to the home base station 10-1 in the cell provided by the macro cell base station 30 To do. Thereafter, the processing of the macrocell base station 30 proceeds to step S310.
 (ステップS307)ホーム基地局10-1は、緊急警報を受信すると、自身の提供するセル内にいる通信端末40-1に受信した緊急警報を送信する。この後、ホーム基地局10-1の処理は、ステップS309に進む。
 (ステップS308)通信端末40-1は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。
 (ステップS309)ホーム基地局10-1は、警告音や光などを出力することにより、緊急警報を出力する。
(Step S307) Upon receiving the emergency alert, the home base station 10-1 transmits the received emergency alert to the communication terminal 40-1 in the cell provided by the home base station 10-1. Thereafter, the processing of the home base station 10-1 proceeds to step S309.
(Step S308) Upon receiving the emergency alert, the communication terminal 40-1 displays and outputs the received emergency alert.
(Step S309) The home base station 10-1 outputs an emergency warning by outputting a warning sound or light.
 (ステップS310)マクロセル基地局30は、自身の提供するセル内にいるホーム基地局10-2に緊急警報を送信する。
 (ステップS311)ホーム基地局10-2は、緊急警報を受信すると、自身の提供するセル内にいる通信端末40-2に受信した緊急警報を送信する。この後、ホーム基地局10-2の処理は、ステップS313の処理に進む。
(Step S310) The macrocell base station 30 transmits an emergency alert to the home base station 10-2 in the cell provided by the macrocell base station 30.
(Step S311) Upon receiving the emergency alert, the home base station 10-2 transmits the received emergency alert to the communication terminal 40-2 in the cell provided by the home base station 10-2. Thereafter, the process of the home base station 10-2 proceeds to the process of step S313.
 (ステップS312)通信端末40-2は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。
 (ステップS313)ホーム基地局10-2は、警告音や光などを出力することにより、緊急警報を出力する。
(Step S312) Upon receiving the emergency alert, the communication terminal 40-2 displays and outputs the received emergency alert.
(Step S313) The home base station 10-2 outputs an emergency warning by outputting a warning sound or light.
 (ステップS314)マクロセル基地局30は、自身の提供するセル内にいる通信端末40-3に緊急警報を送信する。
 (ステップS315)通信端末40-3は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。その後、処理を終了する。
 尚、ステップS310とステップS306とステップS314とは、別々に記載されているが、同一のタイミングで送信されることが望ましい。
(Step S314) The macro cell base station 30 transmits an emergency alert to the communication terminal 40-3 in the cell provided by the macro cell base station 30.
(Step S315) Upon receiving the emergency alert, the communication terminal 40-3 displays and outputs the received emergency alert. Thereafter, the process ends.
Although Step S310, Step S306, and Step S314 are described separately, it is desirable that they are transmitted at the same timing.
 以上説明してきたように、本実施形態によれば、緊急警報通知システム1Aは、ホーム基地局10と、無人航空機20と、マクロセル基地局30と、通信端末40と、ドローン管制システム50とを備える。無人航空機20は、ホーム基地局10またはマクロセル基地局30と無線通信する無線通信部202と、故障を検出する故障検出部206と、故障検出部206が故障を検出した場合に、無線通信部202からホーム基地局10またはマクロセル基地局30に故障を通知する緊急情報を生成して送信する制御部201とを備える。マクロセル基地局30は、無人航空機20と無線通信する無線通信部302と、無人航空機20が緊急事態になったと判定した場合に、無人航空機20の緊急事態を通知する緊急情報に基づく緊急警報を出力する制御部301と、他の基地局装置と通信するネットワーク通信部303と、を備える。制御部301は、無線通信部302が緊急情報を無人航空機20から受信した場合、或いは、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。また、制御部301は、ネットワーク通信部303または無線通信部302から自身のセル内にあるホーム基地局10(即ち、近接するホーム基地局10)及び通信端末40に緊急警報を送信する。ホーム基地局10は、緊急警報を受信すると、受信した緊急警報を自身のセル内にいる通信端末40に送信する。通信端末40は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。また、ホーム基地局10は、音声出力部105と表示部106を備え、緊急警報を受信すると、音声出力部105に警告音を出力させ、或いは、表示部106が備えるLEDを点滅させ、或いは、表示部106に緊急警報を表示させる。 As described above, according to the present embodiment, the emergency alert notification system 1A includes the home base station 10, the unmanned aircraft 20, the macro cell base station 30, the communication terminal 40, and the drone control system 50. . The unmanned aircraft 20 includes a wireless communication unit 202 that wirelessly communicates with the home base station 10 or the macrocell base station 30, a failure detection unit 206 that detects a failure, and a wireless communication unit 202 when the failure detection unit 206 detects a failure. A control unit 201 that generates and transmits emergency information for notifying the home base station 10 or the macrocell base station 30 of the failure. When the macrocell base station 30 determines that the unmanned aircraft 20 is in an emergency, the wireless communication unit 302 that wirelessly communicates with the unmanned aircraft 20 outputs an emergency alert based on emergency information that notifies the emergency of the unmanned aircraft 20 And a network communication unit 303 that communicates with other base station devices. When the wireless communication unit 302 receives emergency information from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 suddenly stops, the control unit 301 determines that the unmanned aircraft 20 has entered an emergency situation. In addition, the control unit 301 transmits an emergency alert from the network communication unit 303 or the wireless communication unit 302 to the home base station 10 (that is, the adjacent home base station 10) and the communication terminal 40 in its own cell. When receiving the emergency alert, the home base station 10 transmits the received emergency alert to the communication terminal 40 in its own cell. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert. The home base station 10 includes a voice output unit 105 and a display unit 106, and when receiving an emergency warning, causes the voice output unit 105 to output a warning sound, or blinks an LED provided in the display unit 106, or An emergency warning is displayed on the display unit 106.
 これにより、故障が発生して墜落しそうな無人航空機20がある場合には、当該無人航空機20が接続しているマクロセル基地局30が提供するセル内にいる通信端末40、ホーム基地局10、及び当該ホーム基地局10が提供するセル内にいる通信端末40に、緊急警報を出力させることができる。このため、故障が発生して墜落しそうな無人航空機20の周囲にいる人に当該無人航空機20の存在を知らせることができる。よって、周囲にいる人は回避や警戒をすることができるため、人身事故を防ぐことができる。 Thereby, when there is an unmanned aerial vehicle 20 that is likely to crash due to a failure, the communication terminal 40, the home base station 10 in the cell provided by the macro cell base station 30 to which the unmanned aircraft 20 is connected, and An emergency alert can be output to the communication terminal 40 in the cell provided by the home base station 10. For this reason, the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
 また、制御部301は、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信することにより、当該ドローンIDに対応する機体情報をドローン管制システム50から取得し、取得した機体情報を含む緊急警報を出力する。ドローン管制システム50は、機体情報要求を受信すると、当該機体情報要求に対応する機体情報を含む機体情報応答を返信する。これにより、無線航空機20から送信されたドローンIDに基づいて、故障が発生して墜落しそうな無線航空機20がどういった機体であるかを特定することができる。 Moreover, the control part 301 acquires the airframe information corresponding to the said drone ID from the drone control system 50 by transmitting the airframe information request | requirement containing drone ID contained in emergency information to the drone control system 50, and acquired the airframe Output emergency alerts that contain information. When the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request. Thereby, based on the drone ID transmitted from the wireless aircraft 20, it is possible to identify the type of the aircraft that is likely to crash due to a failure.
(第4の実施形態)
 次に、本発明の第4の実施形態について説明する。
 図9は、本実施形態に係る緊急警報通知システム1Bの構成の一例を示す概略図である。
 本実施形態における緊急警報通知システム1Bは、第1の実施形態における緊急警報通知システム1に対して、ホーム基地局10に代えてマクロセル基地局30を備える。他の構成は、第1の実施形態と同様であるため、その説明を省略する。
(Fourth embodiment)
Next, a fourth embodiment of the present invention will be described.
FIG. 9 is a schematic diagram illustrating an example of the configuration of the emergency alert notification system 1B according to the present embodiment.
The emergency alert notification system 1B in the present embodiment includes a macro cell base station 30 instead of the home base station 10 with respect to the emergency alert notification system 1 in the first embodiment. Since other configurations are the same as those of the first embodiment, the description thereof is omitted.
 本実施形態におけるマクロセル基地局30の制御部301は、接続している無人航空機20が緊急事態になったと判定した場合に、緊急警報を生成する。緊急事態の判定方法及び緊急警報の生成方法は、第3の実施形態と同様であるため、その説明を省略する。そして、制御部301は、無線通信部302を介して、自身が提供するセル内にいる通信端末40の少なくとも一部に生成した緊急情報を送信する(報知またはマルチキャストしても良い)。マクロセル基地局30の他の構成は、第3の実施形態と同様であるため、その説明を省略する。 The control unit 301 of the macrocell base station 30 in the present embodiment generates an emergency alert when it determines that the connected unmanned aircraft 20 is in an emergency situation. Since the emergency determination method and the emergency alert generation method are the same as those in the third embodiment, description thereof is omitted. And the control part 301 transmits the emergency information produced | generated to at least one part of the communication terminal 40 in the cell which self provides via the wireless communication part 302 (it may alert | report or multicast). Since the other structure of the macrocell base station 30 is the same as that of 3rd Embodiment, the description is abbreviate | omitted.
 次に、本実施形態に係る通知処理について説明する。
 図10は、本実施形態に係る通知処理を表すシーケンス図である。
 本図には、無人航空機20がマクロセル基地局30と接続しており、飛行中に故障が発生した場合における通知処理を示す。
Next, notification processing according to the present embodiment will be described.
FIG. 10 is a sequence diagram illustrating a notification process according to the present embodiment.
This figure shows notification processing when the unmanned aircraft 20 is connected to the macrocell base station 30 and a failure occurs during flight.
 (ステップS401)無人航空機20は、緊急情報をマクロセル基地局30に送信する。
 (ステップS402)マクロセル基地局30は、緊急情報を受信すると、機体情報要求をドローン管制システム50に送信する。
(Step S <b> 401) The unmanned aircraft 20 transmits emergency information to the macro cell base station 30.
(Step S <b> 402) Upon receiving the emergency information, the macro cell base station 30 transmits a body information request to the drone control system 50.
 (ステップS403)ドローン管制システム50は、機体情報要求を受信すると、受信した機体情報要求に含まれるドローンIDの機体情報を問い合わせるID問い合わせを事業者60に送信する。
 (ステップS404)事業者60は、ID問い合わせを受信すると、受信したID問い合わせに対応する機体情報をドローン管制システム50に返信する。
 (ステップS405)ドローン管制システム50は、機体情報を受信すると、受信した機体情報を含む機体情報応答をマクロセル基地局30に返信する。
(Step S403) Upon receiving the aircraft information request, the drone control system 50 transmits an ID inquiry for inquiring the aircraft information of the drone ID included in the received aircraft information request to the business operator 60.
(Step S <b> 404) Upon receiving the ID inquiry, the business operator 60 returns the aircraft information corresponding to the received ID inquiry to the drone control system 50.
(Step S <b> 405) When the drone control system 50 receives the aircraft information, the drone control system 50 returns an aircraft information response including the received aircraft information to the macro cell base station 30.
 (ステップS406)マクロセル基地局30は、機体情報応答を受信すると、受信した機体情報応答に基づいて緊急警報を生成し、自身の提供するセル内にいる通信端末40に緊急警報を送信する(報知またはマルチキャストしても良い)。
 (ステップS407)通信端末40は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。
(Step S406) Upon receiving the aircraft information response, the macro cell base station 30 generates an emergency alert based on the received aircraft information response, and transmits the emergency alert to the communication terminal 40 in the cell provided by the macro cell base station 30 (notification) Or multicast).
(Step S407) Upon receiving the emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
 以上説明してきたように、本実施形態によれば、緊急警報通知システム1Bは、マクロセル基地局30と、無人航空機20と、通信端末40と、ドローン管制システム50とを備える。無人航空機20は、マクロセル基地局30と無線通信する無線通信部202と、故障を検出する故障検出部206と、故障検出部206が故障を検出した場合に、無線通信部202からマクロセル基地局30に故障を通知する緊急情報を生成して送信する制御部201とを備える。マクロセル基地局30は、無人航空機20と無線通信する無線通信部302と、無人航空機20が緊急事態になったと判定した場合に、緊急情報に基づく緊急警報を出力する制御部301と、を備える。制御部301は、無線通信部302が緊急情報を無人航空機20から受信した場合、或いは、無人航空機20との通信が突然途絶えた場合に、無人航空機20が緊急事態になったと判定する。また、制御部301は、無線通信部102から通信可能な通信端末40に緊急警報を送信する。通信端末40は、緊急警報を受信すると、受信した緊急警報を表示する等して出力する。 As described above, according to the present embodiment, the emergency alert notification system 1B includes the macro cell base station 30, the unmanned aircraft 20, the communication terminal 40, and the drone control system 50. The unmanned aerial vehicle 20 includes a wireless communication unit 202 that wirelessly communicates with the macro cell base station 30, a failure detection unit 206 that detects a failure, and the wireless communication unit 202 to the macro cell base station 30 when the failure detection unit 206 detects a failure. And a control unit 201 that generates and transmits emergency information for notifying a failure. The macrocell base station 30 includes a wireless communication unit 302 that wirelessly communicates with the unmanned aircraft 20 and a control unit 301 that outputs an emergency alert based on emergency information when it is determined that the unmanned aircraft 20 has entered an emergency. When the wireless communication unit 302 receives emergency information from the unmanned aircraft 20 or when communication with the unmanned aircraft 20 suddenly stops, the control unit 301 determines that the unmanned aircraft 20 has entered an emergency situation. In addition, the control unit 301 transmits an emergency alert to the communication terminal 40 that can communicate from the wireless communication unit 102. When receiving an emergency alert, the communication terminal 40 displays and outputs the received emergency alert.
 これにより、故障が発生して墜落しそうな無人航空機20がある場合には、当該無人航空機20が接続しているマクロセル基地局30が提供するセル内にいる通信端末40に緊急警報を出力させることができる。このため、故障が発生して墜落しそうな無人航空機20の周囲にいる人に当該無人航空機20の存在を知らせることができる。よって、周囲にいる人は回避や警戒をすることができるため、人身事故を防ぐことができる。 Thereby, when there is an unmanned aerial vehicle 20 that is likely to crash due to a failure, an emergency warning is output to the communication terminal 40 in the cell provided by the macro cell base station 30 to which the unmanned aircraft 20 is connected. Can do. For this reason, the presence of the unmanned aerial vehicle 20 can be notified to a person around the unmanned aerial vehicle 20 that is likely to crash due to a failure. Therefore, people in the vicinity can avoid and be alert, so personal injury can be prevented.
 また、制御部301は、緊急情報に含まれるドローンIDを含む機体情報要求をドローン管制システム50に送信することにより、当該ドローンIDに対応する機体情報をドローン管制システム50から取得し、取得した機体情報を含む緊急警報を出力する。ドローン管制システム50は、機体情報要求を受信すると、当該機体情報要求に対応する機体情報を含む機体情報応答を返信する。これにより、無線航空機20から送信されたドローンIDに基づいて、故障が発生して墜落しそうな無線航空機20がどういった機体であるかを特定することができる。 Moreover, the control part 301 acquires the airframe information corresponding to the said drone ID from the drone control system 50 by transmitting the airframe information request | requirement containing drone ID contained in emergency information to the drone control system 50, and acquired the airframe Output emergency alerts that contain information. When the drone control system 50 receives the aircraft information request, the drone control system 50 returns an aircraft information response including the aircraft information corresponding to the aircraft information request. Thereby, based on the drone ID transmitted from the wireless aircraft 20, it is possible to identify the type of the aircraft that is likely to crash due to a failure.
 なお、上述した実施形態におけるホーム基地局10、無人航空機20またはマクロセル基地局30の一部、例えば、制御部101、制御部201または制御部301をコンピュータで実現するようにしても良い。その場合、この制御機能を実現するためのプログラムをコンピュータ読み取り可能な記録媒体に記録して、この記録媒体に記録されたプログラムをコンピュータシステムに読み込ませ、実行することによって実現しても良い。なお、ここでいう「コンピュータシステム」とは、ホーム基地局10、無人航空機20またはマクロセル基地局30に内蔵されたコンピュータシステムであって、OSや周辺機器等のハードウェアを含むものとする。また、「コンピュータ読み取り可能な記録媒体」とは、フレキシブルディスク、光磁気ディスク、ROM、CD-ROM等の可搬媒体、コンピュータシステムに内蔵されるハードディスク等の記憶装置のことをいう。さらに「コンピュータ読み取り可能な記録媒体」とは、インターネット等のネットワークや電話回線等の通信回線を介してプログラムを送信する場合の通信線のように、短時間、動的にプログラムを保持するもの、その場合のサーバやクライアントとなるコンピュータシステム内部の揮発性メモリのように、一定時間プログラムを保持しているものも含んでも良い。また上記プログラムは、前述した機能の一部を実現するためのものであっても良く、さらに前述した機能をコンピュータシステムにすでに記録されているプログラムとの組み合わせで実現できるものであっても良い。
 また、上述した実施形態におけるホーム基地局10、無人航空機20またはマクロセル基地局30の一部、例えば、制御部101、制御部201または制御部301のそれぞれを、LSI(Large Scale Integration)等の集積回路として実現してもよい。また、例えば、制御部101、制御部201または制御部301のそれぞれを集積してプロセッサ化してもよい。また、集積回路化の手法はLSIに限らず専用回路、または汎用プロセッサで実現してもよい。また、半導体技術の進歩によりLSIに代替する集積回路化の技術が出現した場合、当該技術による集積回路を用いてもよい。
In addition, you may make it implement | achieve a part of home base station 10, unmanned aircraft 20 or macrocell base station 30 in embodiment mentioned above, for example, control part 101, control part 201, or control part 301 with a computer. In that case, the program for realizing the control function may be recorded on a computer-readable recording medium, and the program recorded on the recording medium may be read by a computer system and executed. Here, the “computer system” is a computer system built in the home base station 10, the unmanned aircraft 20 or the macrocell base station 30, and includes hardware such as an OS and peripheral devices. The “computer-readable recording medium” refers to a storage device such as a flexible medium, a magneto-optical disk, a portable medium such as a ROM or a CD-ROM, and a hard disk incorporated in a computer system. Furthermore, the “computer-readable recording medium” is a medium that dynamically holds a program for a short time, such as a communication line when transmitting a program via a network such as the Internet or a communication line such as a telephone line, In such a case, a volatile memory inside a computer system serving as a server or a client may be included and a program that holds a program for a certain period of time. The program may be a program for realizing a part of the functions described above, and may be a program capable of realizing the functions described above in combination with a program already recorded in a computer system.
Further, a part of the home base station 10, the unmanned aircraft 20 or the macro cell base station 30 in the above-described embodiment, for example, the control unit 101, the control unit 201, or the control unit 301 is integrated with LSI (Large Scale Integration) or the like. It may be realized as a circuit. Further, for example, each of the control unit 101, the control unit 201, or the control unit 301 may be integrated into a processor. Further, the method of circuit integration is not limited to LSI, and may be realized by a dedicated circuit or a general-purpose processor. In addition, when an integrated circuit technology that replaces LSI appears due to the advancement of semiconductor technology, an integrated circuit based on the technology may be used.
 以上、図面を参照してこの発明の一実施形態について詳しく説明してきたが、具体的な構成は上述のものに限られることはなく、この発明の要旨を逸脱しない範囲内において様々な設計変更等をすることが可能である。例えば、上述の第1~4の実施形態において説明した各構成は、任意に組み合わせることができる。 As described above, the embodiment of the present invention has been described in detail with reference to the drawings. However, the specific configuration is not limited to the above, and various design changes and the like can be made without departing from the scope of the present invention. It is possible to For example, the configurations described in the first to fourth embodiments can be arbitrarily combined.
 また、上述した実施形態では、無人航空機20が故障を検知して緊急情報を送信しているが、これに限らず、無人航空機20を遠隔操作している操作者が緊急であると判断した場合に、無人航空機20を操作して緊急情報を送信してもよい。 In the above-described embodiment, the unmanned aerial vehicle 20 detects a failure and transmits emergency information. However, the present invention is not limited to this, and the operator who remotely operates the unmanned aircraft 20 is determined to be urgent. In addition, emergency information may be transmitted by operating the unmanned aircraft 20.
 また、上述した実施形態では、ホーム基地局10は、自身が提供するセル内にいる通信端末40に緊急警報を送信しているが、これに限らず、予め登録してある通信端末40に緊急警報を送信してもよい。或いは、ホーム基地局10は、予め登録してある利用者のメールアドレス宛にメールで緊急警報を送信してもよい。また、ホーム基地局10またはマクロセル基地局30は、所轄の警察や消防等に緊急警報を送信して通知してもよい。また、ホーム基地局10またはマクロセル基地局30は、ドローンIDに基づいて無人航空機20の運用者(例えば、宅配業者等)を特定し、特定した運用者に緊急警報を送信して通知してもよい。或いは、緊急情報に運用者の情報に含めてもよい。 In the above-described embodiment, the home base station 10 transmits an emergency alert to the communication terminal 40 in the cell provided by the home base station 10. An alarm may be sent. Alternatively, the home base station 10 may send an emergency alert by e-mail to a user's pre-registered e-mail address. Further, the home base station 10 or the macro cell base station 30 may send an emergency alert to the police or fire department in charge for notification. Further, the home base station 10 or the macro cell base station 30 identifies an operator (for example, a courier company) of the unmanned aircraft 20 based on the drone ID, and sends an emergency alert to the identified operator for notification. Good. Alternatively, the operator information may be included in the emergency information.
 また、上述した実施形態では、無人航空機20に故障が発生した際に、緊急警報を出力しているが、これに限らず、無人航空機20に故障が発生してから無人航空機20が落下するまでの経過情報を含む緊急警報を逐次出力するようにしてもよい。例えば、経過情報には、無人航空機20の位置情報(緯度、経度、及び高度)が含まれる。この場合には、無人航空機20は、落下するまで所定時間毎に接続しているホーム基地局10またはマクロセル基地局30に緊急情報を送信する。ホーム基地局10またはマクロセル基地局30は、緊急情報を受信する毎に緊急警報を生成して出力する。これにより、無人航空機20の周囲にいる人は、無人航空機20の落下の状態を知ることができる。 Further, in the embodiment described above, an emergency warning is output when a failure occurs in the unmanned aircraft 20, but not limited to this, until the unmanned aircraft 20 falls after the failure occurs in the unmanned aircraft 20. Emergency warnings including the progress information may be output sequentially. For example, the progress information includes position information (latitude, longitude, and altitude) of the unmanned aircraft 20. In this case, the unmanned aerial vehicle 20 transmits emergency information to the home base station 10 or the macro cell base station 30 that is connected every predetermined time until it falls. The home base station 10 or the macro cell base station 30 generates and outputs an emergency alert each time emergency information is received. Thereby, the person around the unmanned aerial vehicle 20 can know the state of the unmanned aircraft 20 falling.
 また、無人航空機20が故障から復旧したことを通知する緊急警報の解除コードを出力するようにしてもよい。この場合には、無人航空機20は、故障から復旧すると、復旧したことを通知する復旧情報をホーム基地局10またはマクロセル基地局30に送信する。
ホーム基地局10またはマクロセル基地局30は、復旧情報を受信すると、緊急警報の解除コードを生成して出力する。或いは、ホーム基地局10またはマクロセル基地局30は、緊急情報を受信してから一定時間経過後に解除コードを出力してもよい。これにより、無人航空機20の周囲にいる人は、無人航空機20が故障から復旧したことを知ることができる。また、ホーム基地局10またはマクロセル基地局30は、無人航空機20が着陸(落下完了)したことを通知する情報を送信して通知するようにしてもよい。これにより、無人航空機20の周囲にいる人は、無人航空機20が着陸したということを知ることができる。
Moreover, you may make it output the cancellation code | symbol of the emergency alert which notifies that the unmanned aircraft 20 was recovered from failure. In this case, when the unmanned aircraft 20 recovers from the failure, the unmanned aircraft 20 transmits recovery information notifying the recovery to the home base station 10 or the macrocell base station 30.
When the home base station 10 or the macro cell base station 30 receives the recovery information, the home base station 10 or the macro cell base station 30 generates and outputs an emergency warning cancel code. Alternatively, the home base station 10 or the macro cell base station 30 may output the release code after a certain time has elapsed since the emergency information was received. Thereby, the person around the unmanned aerial vehicle 20 can know that the unmanned aerial vehicle 20 has recovered from the failure. In addition, the home base station 10 or the macro cell base station 30 may transmit and notify information for notifying that the unmanned aircraft 20 has landed (falling completed). Thereby, the person around the unmanned aerial vehicle 20 can know that the unmanned aerial vehicle 20 has landed.
 また、ホーム基地局10またはマクロセル基地局30が送信する緊急警報は、2段階であってもよい。例えば、ホーム基地局10またはマクロセル基地局30は、1回目には、無人航空機30から取得した緊急情報のうち少なくとも一部を送信し、2回目には、ドローン管制システム50から取得した情報のうち少なくとも一部を送信してもよい。この場合には、ホーム基地局10またはマクロセル基地局30は、2回目を送信するときに、1回目の送信時に送信した情報を重複して送信してもよい。また、ホーム基地局10またはマクロセル基地局30は、2回目を送信するときは、1回目の警報で送信した位置情報及び予測所要時間を時間経過や風の情報等に基づいて更新してもよい。 Further, the emergency alert transmitted from the home base station 10 or the macro cell base station 30 may be in two stages. For example, the home base station 10 or the macro cell base station 30 transmits at least a part of the emergency information acquired from the unmanned aircraft 30 at the first time, and among the information acquired from the drone control system 50 at the second time. You may transmit at least one part. In this case, when transmitting the second time, the home base station 10 or the macro cell base station 30 may transmit the information transmitted during the first transmission in an overlapping manner. In addition, when transmitting the second time, the home base station 10 or the macro cell base station 30 may update the position information and the estimated required time transmitted by the first warning based on time lapse, wind information, and the like. .
 (1)無人航空機と無線通信する無線通信部と、無人航空機が緊急事態になったと判定した場合に、無人航空機の緊急事態を示す緊急情報を出力する制御部と、を備える基地局装置。
 (2)制御部は、緊急情報を無人航空機から受信した場合に、無人航空機が緊急事態になったと判定する(1)に記載の基地局装置。
 (3)制御部は、無人航空機との通信が途絶えた場合に、無人航空機が緊急事態になったと判定する(1)または(2)に記載の基地局装置。
(1) A base station apparatus comprising: a wireless communication unit that wirelessly communicates with an unmanned aircraft; and a control unit that outputs emergency information indicating an emergency situation of the unmanned aircraft when it is determined that the unmanned aircraft has become an emergency.
(2) The base station device according to (1), wherein the control unit determines that the unmanned aircraft is in an emergency when the emergency information is received from the unmanned aircraft.
(3) The base station device according to (1) or (2), wherein the control unit determines that the unmanned aircraft is in an emergency when communication with the unmanned aircraft is interrupted.
 (4)制御部は、無線通信部において通信可能な移動局装置に緊急情報に基づく情報を送信する(1)から(3)のいずれか1項に記載の基地局装置。 (4) The base station device according to any one of (1) to (3), wherein the control unit transmits information based on the emergency information to a mobile station device capable of communicating in the wireless communication unit.
 (5)他の基地局装置と通信する通信部を備え、制御部は、通信部から他の基地局装置に緊急情報に基づく情報を送信する(1)から(4)のいずれか1項に記載の基地局装置。 (5) A communication unit that communicates with another base station device is provided, and the control unit transmits information based on emergency information from the communication unit to the other base station device, according to any one of (1) to (4) The base station apparatus as described.
 (6)緊急情報は、無人航空機の位置情報を含む(1)から(5)のいずれか1項に記載の基地局装置。
 (7)緊急情報は、無人航空機の加速度を含む(1)から(6)のいずれか1項に記載の基地局装置。
 (8)緊急情報は、無人航空機が備えるパラシュートの開閉状態を含む(1)から(7)のいずれか1項に記載の基地局装置。
 (9)出力部を備え、制御部は、緊急情報に基づく警報を出力部に出力させる(1)から(8)のいずれか1項に記載の基地局装置。
(6) The base station apparatus according to any one of (1) to (5), wherein the emergency information includes position information of the unmanned aircraft.
(7) The base station apparatus according to any one of (1) to (6), wherein the emergency information includes an acceleration of the unmanned aircraft.
(8) The base station apparatus according to any one of (1) to (7), wherein the emergency information includes an open / closed state of a parachute included in the unmanned aircraft.
(9) The base station apparatus according to any one of (1) to (8), further including an output unit, wherein the control unit causes the output unit to output an alarm based on emergency information.
 (10)無人航空機と基地局装置とを備える緊急警報通知システムであって、無人航空機は、基地局装置と無線通信する無線通信部を備え、基地局装置は、無人航空機と無線通信する無線通信部と、無人航空機が緊急事態になったと判定した場合に、無人航空機の緊急事態を示す緊急情報を出力する制御部と、を備える緊急警報通知システム。 (10) An emergency alert notification system including an unmanned aircraft and a base station device, wherein the unmanned aircraft includes a wireless communication unit that wirelessly communicates with the base station device, and the base station device wirelessly communicates with the unmanned aircraft. An emergency alert notification system comprising: a control unit that outputs emergency information indicating an emergency of the unmanned aircraft when it is determined that the unmanned aircraft has entered an emergency.
 (11)基地局装置における緊急警報通知方法であって、無人航空機と無線通信する無線通信過程と、無人航空機が緊急事態になったと判定した場合に、無人航空機の緊急事態を示す緊急情報を出力する制御過程と、を有する緊急警報通知方法。 (11) An emergency alert notification method in a base station device, wherein a wireless communication process for wirelessly communicating with an unmanned aircraft and outputting emergency information indicating an unmanned aircraft emergency when it is determined that the unmanned aircraft has become an emergency And an emergency alert notification method.
 本発明のいくつかの態様は、故障が発生した無人航空機の周囲にいる人に、当該無人航空機の存在を知らせることが必要な基地局装置、緊急警報通知システム及び緊急警報通知方法などに適用することができる。 Some aspects of the present invention are applied to a base station apparatus, an emergency warning notification system, an emergency warning notification method, and the like that are required to notify a person in the vicinity of an unmanned aircraft in which a failure has occurred to the presence of the unmanned aircraft. be able to.
1,1A,1B・・・緊急警報通知システム、10・・・ホーム基地局、20・・・無人航空機、30・・・マクロセル基地局、40・・・通信端末、50・・・ドローン管制システム、60・・・事業者、101・・・制御部、102・・・無線通信部、103・・・ネットワーク通信部、104・・・記憶部、105・・・音声出力部、106・・・表示部、201・・・制御部、202・・・無線通信部、203・・・記憶部、204・・・撮像部、205・・・位置情報取得部、206・・・故障検出部、207・・・加速度検出部、208・・パラシュート開閉検出部、209・・・飛行制御部、301・・・制御部、302・・・無線通信部、303・・・ネットワーク通信部、304・・・記憶部 DESCRIPTION OF SYMBOLS 1,1A, 1B ... Emergency alert notification system, 10 ... Home base station, 20 ... Unmanned aerial vehicle, 30 ... Macrocell base station, 40 ... Communication terminal, 50 ... Drone control system , 60 ... operator, 101 ... control unit, 102 ... wireless communication unit, 103 ... network communication unit, 104 ... storage unit, 105 ... audio output unit, 106 ... Display unit 201 ... Control unit 202 ... Wireless communication unit 203 ... Storage unit 204 ... Imaging unit 205 ... Position information acquisition unit 206 ... Failure detection unit 207・ ・ ・ Acceleration detection unit, 208... Parachute opening / closing detection unit, 209 ... Flight control unit, 301 ... control unit, 302 ... wireless communication unit, 303 ... network communication unit, 304 ... Memory

Claims (11)

  1.  無人航空機と無線通信する無線通信部と、
     前記無人航空機が緊急事態になったと判定した場合に、前記無人航空機の緊急事態を示す緊急情報を出力する制御部と、
     を備える基地局装置。
    A wireless communication unit for wireless communication with an unmanned aerial vehicle;
    When it is determined that the unmanned aircraft is in an emergency, a control unit that outputs emergency information indicating an emergency of the unmanned aircraft;
    A base station apparatus comprising:
  2.  前記制御部は、前記緊急情報を前記無人航空機から受信した場合に、前記無人航空機が緊急事態になったと判定する
     請求項1に記載の基地局装置。
    The base station apparatus according to claim 1, wherein the control unit determines that the unmanned aircraft is in an emergency when the emergency information is received from the unmanned aircraft.
  3.  前記制御部は、前記無人航空機との通信が途絶えた場合に、前記無人航空機が緊急事態になったと判定する
     請求項1または2に記載の基地局装置。
    The base station apparatus according to claim 1 or 2, wherein the control unit determines that the unmanned aircraft is in an emergency when communication with the unmanned aircraft is interrupted.
  4.  前記制御部は、前記無線通信部から通信可能な移動局装置に前記緊急情報を送信する
     請求項1から3のいずれか1項に記載の基地局装置。
    The base station apparatus according to any one of claims 1 to 3, wherein the control unit transmits the emergency information to a mobile station apparatus capable of communication from the wireless communication unit.
  5.  他の基地局装置と通信する通信部を備え、
     前記制御部は、前記通信部から前記他の基地局装置に前記緊急情報を送信する
     請求項1から4のいずれか1項に記載の基地局装置。
    A communication unit that communicates with other base station devices,
    The base station apparatus according to claim 1, wherein the control unit transmits the emergency information from the communication unit to the other base station apparatus.
  6.  前記緊急情報は、前記無人航空機の位置情報を含む
     請求項1から5のいずれか1項に記載の基地局装置。
    The base station apparatus according to any one of claims 1 to 5, wherein the emergency information includes position information of the unmanned aircraft.
  7.  前記緊急情報は、前記無人航空機の加速度を含む
     請求項1から6のいずれか1項に記載の基地局装置。
    The base station apparatus according to any one of claims 1 to 6, wherein the emergency information includes an acceleration of the unmanned aircraft.
  8.  前記緊急情報は、前記無人航空機が備えるパラシュートの開閉状態を含む
     請求項1から7のいずれか1項に記載の基地局装置。
    The base station apparatus according to any one of claims 1 to 7, wherein the emergency information includes a parachute opening / closing state of the unmanned aerial vehicle.
  9.  出力部を備え、
     前記制御部は、前記緊急情報に基づく警報を前記出力部に出力させる
     請求項1から8のいずれか1項に記載の基地局装置。
    With an output section,
    The base station apparatus according to any one of claims 1 to 8, wherein the control unit causes the output unit to output an alarm based on the emergency information.
  10.  無人航空機と基地局装置とを備える緊急警報通知システムであって、
     前記無人航空機は、
     前記基地局装置と無線通信する無線通信部
     を備え、
     前記基地局装置は、
     無人航空機と無線通信する無線通信部と、
     前記無人航空機が緊急事態になったと判定した場合に、前記無人航空機の緊急事態を示す緊急情報を出力する制御部と、
     を備える
     緊急警報通知システム。
    An emergency alert notification system comprising an unmanned aerial vehicle and a base station device,
    The unmanned aircraft
    A wireless communication unit that wirelessly communicates with the base station device;
    The base station device
    A wireless communication unit for wireless communication with an unmanned aerial vehicle;
    When it is determined that the unmanned aircraft is in an emergency, a control unit that outputs emergency information indicating an emergency of the unmanned aircraft;
    Equipped with emergency alert notification system.
  11.  基地局装置における緊急警報通知方法であって、
     無人航空機と無線通信する無線通信過程と、
     前記無人航空機が緊急事態になったと判定した場合に、前記無人航空機の緊急事態を示す緊急情報を出力する制御過程と、
     を有する緊急警報通知方法。
    An emergency alert notification method in a base station device,
    A wireless communication process for wireless communication with an unmanned aerial vehicle;
    When it is determined that the unmanned aircraft has become an emergency, a control process of outputting emergency information indicating an emergency of the unmanned aircraft,
    Having emergency alert notification method.
PCT/JP2017/030320 2016-09-05 2017-08-24 Base station device, emergency alert notification system, and emergency alert notification method WO2018043284A1 (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018070011A (en) * 2016-10-31 2018-05-10 キヤノンマーケティングジャパン株式会社 Unmanned aircraft controlling system, controlling method and program thereof
WO2019176423A1 (en) * 2018-03-13 2019-09-19 Kddi株式会社 Flight management device and flying device
WO2019181214A1 (en) * 2018-03-22 2019-09-26 パナソニックIpマネジメント株式会社 Optical device and optical detection system
JP2020502659A (en) * 2016-12-14 2020-01-23 テレフオンアクチーボラゲット エルエム エリクソン(パブル) Methods and entities for alerting unmanned aerial vehicle failure
JP2020067881A (en) * 2018-10-25 2020-04-30 株式会社Nttドコモ Information processing device
WO2021070464A1 (en) * 2019-10-07 2021-04-15 ソニー株式会社 Mobile body, mobile body control method, mobile body control program, management device, management control method, management control program, and mobile body system
JP2021086387A (en) * 2019-11-27 2021-06-03 ソフトバンク株式会社 Information processor, information processing method, and information processing program
WO2021255871A1 (en) * 2020-06-17 2021-12-23 日本電気株式会社 Flight setting method
US20220080478A1 (en) * 2020-09-14 2022-03-17 Shang-Jung Wu Management station of multi-point time-sharing water quality monitoring system
CN114518107A (en) * 2022-02-16 2022-05-20 中国地质大学(北京) Wireless synchronous control system based on unmanned aerial vehicle remote control seismic source
CN114967738A (en) * 2022-05-19 2022-08-30 中国航空工业集团公司沈阳飞机设计研究所 Emergency disposal system and method for unmanned aerial vehicle fault

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20010048050A1 (en) * 2000-05-27 2001-12-06 Wolfram Grieser Method for deploying a parachute on a drone
JP2005199902A (en) * 2004-01-16 2005-07-28 Seiko Epson Corp Airship and airship system
JP2007230367A (en) * 2006-03-01 2007-09-13 Yamaha Motor Co Ltd Monitor displaying system for unmanned helicopter base station, and abnormality judging system for unmanned helicopter using it
US20150254988A1 (en) * 2014-04-17 2015-09-10 SZ DJI Technology Co., Ltd Flight control for flight-restricted regions

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20010048050A1 (en) * 2000-05-27 2001-12-06 Wolfram Grieser Method for deploying a parachute on a drone
JP2005199902A (en) * 2004-01-16 2005-07-28 Seiko Epson Corp Airship and airship system
JP2007230367A (en) * 2006-03-01 2007-09-13 Yamaha Motor Co Ltd Monitor displaying system for unmanned helicopter base station, and abnormality judging system for unmanned helicopter using it
US20150254988A1 (en) * 2014-04-17 2015-09-10 SZ DJI Technology Co., Ltd Flight control for flight-restricted regions

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018070011A (en) * 2016-10-31 2018-05-10 キヤノンマーケティングジャパン株式会社 Unmanned aircraft controlling system, controlling method and program thereof
JP2020502659A (en) * 2016-12-14 2020-01-23 テレフオンアクチーボラゲット エルエム エリクソン(パブル) Methods and entities for alerting unmanned aerial vehicle failure
US11756344B2 (en) 2016-12-14 2023-09-12 Telefonaktiebolaget Lm Ericsson (Publ) Methods and entities for alerting about failure of an unmanned aerial vehicle
US11195345B2 (en) 2016-12-14 2021-12-07 Telefonaktiebolaget Lm Ericsson (Publ) Methods and entities for alerting about failure of an unmanned aerial vehicle
JP7030571B2 (en) 2018-03-13 2022-03-07 Kddi株式会社 Flight management system
WO2019176423A1 (en) * 2018-03-13 2019-09-19 Kddi株式会社 Flight management device and flying device
JP2019159811A (en) * 2018-03-13 2019-09-19 Kddi株式会社 Flight management system and flight device
US11341862B2 (en) 2018-03-13 2022-05-24 Kddi Corporation Flight management device and flying device
WO2019181214A1 (en) * 2018-03-22 2019-09-26 パナソニックIpマネジメント株式会社 Optical device and optical detection system
JP2020067881A (en) * 2018-10-25 2020-04-30 株式会社Nttドコモ Information processing device
JP7260281B2 (en) 2018-10-25 2023-04-18 株式会社Nttドコモ Information processing equipment
US20220332416A1 (en) * 2019-10-07 2022-10-20 Sony Group Corporation Mobile body, mobile body control method, mobile body control program, management device, management control method, management control program, and mobile body system
WO2021070464A1 (en) * 2019-10-07 2021-04-15 ソニー株式会社 Mobile body, mobile body control method, mobile body control program, management device, management control method, management control program, and mobile body system
JP2021086387A (en) * 2019-11-27 2021-06-03 ソフトバンク株式会社 Information processor, information processing method, and information processing program
JP7098596B2 (en) 2019-11-27 2022-07-11 ソフトバンク株式会社 Information processing equipment, information processing methods, and information processing programs
WO2021255871A1 (en) * 2020-06-17 2021-12-23 日本電気株式会社 Flight setting method
US20220080478A1 (en) * 2020-09-14 2022-03-17 Shang-Jung Wu Management station of multi-point time-sharing water quality monitoring system
CN114518107A (en) * 2022-02-16 2022-05-20 中国地质大学(北京) Wireless synchronous control system based on unmanned aerial vehicle remote control seismic source
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