FLIGHT CONTROL SYSTEM, SERVER, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM
To provide a flight method that can prevent a collision of a drone and entanglement of a power supply cable.SOLUTION: A flight control system relating to flight control of electrically driven drones 3 that are connected respectively to power supply cables 4a for power supplied from the ground side c...
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| creator | AOYAGI JIN ABE TAKASHI |
| description | To provide a flight method that can prevent a collision of a drone and entanglement of a power supply cable.SOLUTION: A flight control system relating to flight control of electrically driven drones 3 that are connected respectively to power supply cables 4a for power supplied from the ground side comprises: first acquisition means 111 for acquiring respective flight distances when the plurality of drones 3 are caused to fly from parking stations 800 (departure sites) to respective corresponding destinations; determination means 112 for determining flight methods for the respective drones 3 on the basis of the respective flight distances acquired by the first acquisition means 111; first control means 113 for causing the drones 3 to fly in accordance with the flight methods determined by the determination means 112; and second control means 116 for causing the respective power supply cables 4a to be advanced or retracted at speed corresponding to flight speed of the respective drones 3.SELECTED DRAWING: Figure 1
【課題】ドローンの衝突や給電ケーブルの絡みを防止可能な飛行方法を提供する。【解決手段】地上側から供給される給電ケーブル４ａに接続された電気駆動式のドローン３の飛行制御に関する飛行制御システムにおいて、複数のドローン３を、駐機場８００（出発地）からそれぞれ対応する目的地まで飛行させる場合の各飛行距離を取得する第１取得手段１１１と、第１取得手段１１１により取得された各飛行距離に基づき各ドローン３の飛行方法を決定する決定手段１１２と、決定手段１１２により決定された飛行方法に従って各ドローン３を飛行させる第１制御手段１１３と、ドローン３の飛行速度に対応する速度で給電ケーブル４ａの送り受けを行わせる第２制御手段１１６と、を備える。【選択図】図１ |
| format | Patent |
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【課題】ドローンの衝突や給電ケーブルの絡みを防止可能な飛行方法を提供する。【解決手段】地上側から供給される給電ケーブル４ａに接続された電気駆動式のドローン３の飛行制御に関する飛行制御システムにおいて、複数のドローン３を、駐機場８００（出発地）からそれぞれ対応する目的地まで飛行させる場合の各飛行距離を取得する第１取得手段１１１と、第１取得手段１１１により取得された各飛行距離に基づき各ドローン３の飛行方法を決定する決定手段１１２と、決定手段１１２により決定された飛行方法に従って各ドローン３を飛行させる第１制御手段１１３と、ドローン３の飛行速度に対応する速度で給電ケーブル４ａの送り受けを行わせる第２制御手段１１６と、を備える。【選択図】図１</description><language>eng ; jpn</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; SIGNALLING ; TRAFFIC CONTROL SYSTEMS ; TRANSPORTING</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240228&DB=EPODOC&CC=JP&NR=2024025872A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240228&DB=EPODOC&CC=JP&NR=2024025872A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>AOYAGI JIN</creatorcontrib><creatorcontrib>ABE TAKASHI</creatorcontrib><title>FLIGHT CONTROL SYSTEM, SERVER, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM</title><description>To provide a flight method that can prevent a collision of a drone and entanglement of a power supply cable.SOLUTION: A flight control system relating to flight control of electrically driven drones 3 that are connected respectively to power supply cables 4a for power supplied from the ground side comprises: first acquisition means 111 for acquiring respective flight distances when the plurality of drones 3 are caused to fly from parking stations 800 (departure sites) to respective corresponding destinations; determination means 112 for determining flight methods for the respective drones 3 on the basis of the respective flight distances acquired by the first acquisition means 111; first control means 113 for causing the drones 3 to fly in accordance with the flight methods determined by the determination means 112; and second control means 116 for causing the respective power supply cables 4a to be advanced or retracted at speed corresponding to flight speed of the respective drones 3.SELECTED DRAWING: Figure 1
【課題】ドローンの衝突や給電ケーブルの絡みを防止可能な飛行方法を提供する。【解決手段】地上側から供給される給電ケーブル４ａに接続された電気駆動式のドローン３の飛行制御に関する飛行制御システムにおいて、複数のドローン３を、駐機場８００（出発地）からそれぞれ対応する目的地まで飛行させる場合の各飛行距離を取得する第１取得手段１１１と、第１取得手段１１１により取得された各飛行距離に基づき各ドローン３の飛行方法を決定する決定手段１１２と、決定手段１１２により決定された飛行方法に従って各ドローン３を飛行させる第１制御手段１１３と、ドローン３の飛行速度に対応する速度で給電ケーブル４ａの送り受けを行わせる第２制御手段１１６と、を備える。【選択図】図１</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>SIGNALLING</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAhw8_F09whRcPb3Cwny91EIjgwOcfXVUQh2DQpzDdJRQJP2dQ3x8HfRUXD0c0GXCgjydw9y9OVhYE1LzClO5YXS3AxKbq4hzh66qQX58anFBYnJqXmpJfFeAUYGRiYGRqYW5kaOxkQpAgDNaC90</recordid><startdate>20240228</startdate><enddate>20240228</enddate><creator>AOYAGI JIN</creator><creator>ABE TAKASHI</creator><scope>EVB</scope></search><sort><creationdate>20240228</creationdate><title>FLIGHT CONTROL SYSTEM, SERVER, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM</title><author>AOYAGI JIN ; ABE TAKASHI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2024025872A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2024</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>SIGNALLING</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>AOYAGI JIN</creatorcontrib><creatorcontrib>ABE TAKASHI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>AOYAGI JIN</au><au>ABE TAKASHI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FLIGHT CONTROL SYSTEM, SERVER, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM</title><date>2024-02-28</date><risdate>2024</risdate><abstract>To provide a flight method that can prevent a collision of a drone and entanglement of a power supply cable.SOLUTION: A flight control system relating to flight control of electrically driven drones 3 that are connected respectively to power supply cables 4a for power supplied from the ground side comprises: first acquisition means 111 for acquiring respective flight distances when the plurality of drones 3 are caused to fly from parking stations 800 (departure sites) to respective corresponding destinations; determination means 112 for determining flight methods for the respective drones 3 on the basis of the respective flight distances acquired by the first acquisition means 111; first control means 113 for causing the drones 3 to fly in accordance with the flight methods determined by the determination means 112; and second control means 116 for causing the respective power supply cables 4a to be advanced or retracted at speed corresponding to flight speed of the respective drones 3.SELECTED DRAWING: Figure 1
【課題】ドローンの衝突や給電ケーブルの絡みを防止可能な飛行方法を提供する。【解決手段】地上側から供給される給電ケーブル４ａに接続された電気駆動式のドローン３の飛行制御に関する飛行制御システムにおいて、複数のドローン３を、駐機場８００（出発地）からそれぞれ対応する目的地まで飛行させる場合の各飛行距離を取得する第１取得手段１１１と、第１取得手段１１１により取得された各飛行距離に基づき各ドローン３の飛行方法を決定する決定手段１１２と、決定手段１１２により決定された飛行方法に従って各ドローン３を飛行させる第１制御手段１１３と、ドローン３の飛行速度に対応する速度で給電ケーブル４ａの送り受けを行わせる第２制御手段１１６と、を備える。【選択図】図１</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PARACHUTES PERFORMING OPERATIONS PHYSICS SIGNALLING TRAFFIC CONTROL SYSTEMS TRANSPORTING |
| title | FLIGHT CONTROL SYSTEM, SERVER, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM |
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