FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASURING SYSTEM
To provide a flight control system for an unmanned aerial vehicle, in which a flight position of the unmanned aerial vehicle, the flight position being measured at a total station on the ground, is transmitted to an unmanned flight body.SOLUTION: A flight control system 1 for an unmanned aerial vehi...
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| creator | KUMAGAI KAORU RICCARDO LOTI |
| description | To provide a flight control system for an unmanned aerial vehicle, in which a flight position of the unmanned aerial vehicle, the flight position being measured at a total station on the ground, is transmitted to an unmanned flight body.SOLUTION: A flight control system 1 for an unmanned aerial vehicle is provided that comprises: an unmanned aerial vehicle (UAV) 3 mounted with a reflector 7; and a total station (TS) 2 for tracking the reflector and for acquiring measurement data of three-dimensional coordinates of the reflector, wherein the total station comprises: a tracking unit for tracking the reflector; a TS-data transmission unit which has an optical axis in parallel to an optical axis of tracking light 22 of the tracking unit, and emits TS-data transmission light 23; and a TS-arithmetic control unit, wherein the unmanned aerial vehicle comprises: a photodetector for receiving the TS-data transmission light; and a UAV-arithmetic control unit for controlling a flight of the unmanned aerial vehicle, and wherein the TS-arithmetic control unit superimposes the measurement data on the TS-data transmission light, and the UAV-arithmetic control unit separates the measurement data from a photodetecting signal and obtains a flight position of the unmanned aerial vehicle.SELECTED DRAWING: Figure 1
【課題】無人飛行機の飛行制御システムに於いて、地上のトータルステーションで測定した無人飛行機の飛行位置を無人飛行体に伝送するシステムを提供する。【解決手段】反射体７を搭載した無人飛行機（ＵＡＶ）３と、該反射体を追尾し、その３次元座標の測定データを取得するトータルステーション（ＴＳ）２とを具備する無人飛行機の飛行制御システム１であって、前記トータルステーションは前記反射体を追尾する追尾部と、該追尾部の追尾光２２の光軸と平行な光軸を有し、ＴＳ−データ伝送光２３を発するＴＳ−データ伝送部と、ＴＳ−演算制御部とを具備し、前記無人飛行機は、前記ＴＳ−データ伝送光を受光する受光器と前記無人飛行機の飛行を制御するＵＡＶ−演算制御部とを有し、前記ＴＳ−演算制御部は、前記測定データを前記ＴＳ−データ伝送光に重畳し、前記ＵＡＶ−演算制御部は受光信号から測定データを分離し、前記無人飛行機の飛行位置を取得する。【選択図】図１ |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2020203664A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2020203664A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2020203664A3</originalsourceid><addsrcrecordid>eNrjZAh08_F09whRcPb3Cwny91EIjgwOcfVVcPMPUgj183X083N1UXB0DfJ09FEIc_XwdPZxVXD0c1EI8Q_wdw9yDPCIVPB1dQwODfL0c4fq5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8V4BRgYgaGxmZuJoTJQiAB3iL_0</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASURING SYSTEM</title><source>esp@cenet</source><creator>KUMAGAI KAORU ; RICCARDO LOTI</creator><creatorcontrib>KUMAGAI KAORU ; RICCARDO LOTI</creatorcontrib><description>To provide a flight control system for an unmanned aerial vehicle, in which a flight position of the unmanned aerial vehicle, the flight position being measured at a total station on the ground, is transmitted to an unmanned flight body.SOLUTION: A flight control system 1 for an unmanned aerial vehicle is provided that comprises: an unmanned aerial vehicle (UAV) 3 mounted with a reflector 7; and a total station (TS) 2 for tracking the reflector and for acquiring measurement data of three-dimensional coordinates of the reflector, wherein the total station comprises: a tracking unit for tracking the reflector; a TS-data transmission unit which has an optical axis in parallel to an optical axis of tracking light 22 of the tracking unit, and emits TS-data transmission light 23; and a TS-arithmetic control unit, wherein the unmanned aerial vehicle comprises: a photodetector for receiving the TS-data transmission light; and a UAV-arithmetic control unit for controlling a flight of the unmanned aerial vehicle, and wherein the TS-arithmetic control unit superimposes the measurement data on the TS-data transmission light, and the UAV-arithmetic control unit separates the measurement data from a photodetecting signal and obtains a flight position of the unmanned aerial vehicle.SELECTED DRAWING: Figure 1
【課題】無人飛行機の飛行制御システムに於いて、地上のトータルステーションで測定した無人飛行機の飛行位置を無人飛行体に伝送するシステムを提供する。【解決手段】反射体７を搭載した無人飛行機（ＵＡＶ）３と、該反射体を追尾し、その３次元座標の測定データを取得するトータルステーション（ＴＳ）２とを具備する無人飛行機の飛行制御システム１であって、前記トータルステーションは前記反射体を追尾する追尾部と、該追尾部の追尾光２２の光軸と平行な光軸を有し、ＴＳ−データ伝送光２３を発するＴＳ−データ伝送部と、ＴＳ−演算制御部とを具備し、前記無人飛行機は、前記ＴＳ−データ伝送光を受光する受光器と前記無人飛行機の飛行を制御するＵＡＶ−演算制御部とを有し、前記ＴＳ−演算制御部は、前記測定データを前記ＴＳ−データ伝送光に重畳し、前記ＵＡＶ−演算制御部は受光信号から測定データを分離し、前記無人飛行機の飛行位置を取得する。【選択図】図１</description><language>eng ; jpn</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CONTROLLING ; 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 ; GYROSCOPIC INSTRUMENTS ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HELICOPTERS ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PARACHUTES ; PERFORMING OPERATIONS ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; REGULATING ; SURVEYING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TESTING ; TRANSPORTING</subject><creationdate>2020</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=20201224&DB=EPODOC&CC=JP&NR=2020203664A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201224&DB=EPODOC&CC=JP&NR=2020203664A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KUMAGAI KAORU</creatorcontrib><creatorcontrib>RICCARDO LOTI</creatorcontrib><title>FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASURING SYSTEM</title><description>To provide a flight control system for an unmanned aerial vehicle, in which a flight position of the unmanned aerial vehicle, the flight position being measured at a total station on the ground, is transmitted to an unmanned flight body.SOLUTION: A flight control system 1 for an unmanned aerial vehicle is provided that comprises: an unmanned aerial vehicle (UAV) 3 mounted with a reflector 7; and a total station (TS) 2 for tracking the reflector and for acquiring measurement data of three-dimensional coordinates of the reflector, wherein the total station comprises: a tracking unit for tracking the reflector; a TS-data transmission unit which has an optical axis in parallel to an optical axis of tracking light 22 of the tracking unit, and emits TS-data transmission light 23; and a TS-arithmetic control unit, wherein the unmanned aerial vehicle comprises: a photodetector for receiving the TS-data transmission light; and a UAV-arithmetic control unit for controlling a flight of the unmanned aerial vehicle, and wherein the TS-arithmetic control unit superimposes the measurement data on the TS-data transmission light, and the UAV-arithmetic control unit separates the measurement data from a photodetecting signal and obtains a flight position of the unmanned aerial vehicle.SELECTED DRAWING: Figure 1
【課題】無人飛行機の飛行制御システムに於いて、地上のトータルステーションで測定した無人飛行機の飛行位置を無人飛行体に伝送するシステムを提供する。【解決手段】反射体７を搭載した無人飛行機（ＵＡＶ）３と、該反射体を追尾し、その３次元座標の測定データを取得するトータルステーション（ＴＳ）２とを具備する無人飛行機の飛行制御システム１であって、前記トータルステーションは前記反射体を追尾する追尾部と、該追尾部の追尾光２２の光軸と平行な光軸を有し、ＴＳ−データ伝送光２３を発するＴＳ−データ伝送部と、ＴＳ−演算制御部とを具備し、前記無人飛行機は、前記ＴＳ−データ伝送光を受光する受光器と前記無人飛行機の飛行を制御するＵＡＶ−演算制御部とを有し、前記ＴＳ−演算制御部は、前記測定データを前記ＴＳ−データ伝送光に重畳し、前記ＵＡＶ−演算制御部は受光信号から測定データを分離し、前記無人飛行機の飛行位置を取得する。【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>CONTROLLING</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>GYROSCOPIC INSTRUMENTS</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HELICOPTERS</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SURVEYING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAh08_F09whRcPb3Cwny91EIjgwOcfVVcPMPUgj183X083N1UXB0DfJ09FEIc_XwdPZxVXD0c1EI8Q_wdw9yDPCIVPB1dQwODfL0c4fq5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8V4BRgYgaGxmZuJoTJQiAB3iL_0</recordid><startdate>20201224</startdate><enddate>20201224</enddate><creator>KUMAGAI KAORU</creator><creator>RICCARDO LOTI</creator><scope>EVB</scope></search><sort><creationdate>20201224</creationdate><title>FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASURING SYSTEM</title><author>KUMAGAI KAORU ; RICCARDO LOTI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2020203664A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2020</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROLLING</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>GYROSCOPIC INSTRUMENTS</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HELICOPTERS</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SURVEYING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>KUMAGAI KAORU</creatorcontrib><creatorcontrib>RICCARDO LOTI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KUMAGAI KAORU</au><au>RICCARDO LOTI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASURING SYSTEM</title><date>2020-12-24</date><risdate>2020</risdate><abstract>To provide a flight control system for an unmanned aerial vehicle, in which a flight position of the unmanned aerial vehicle, the flight position being measured at a total station on the ground, is transmitted to an unmanned flight body.SOLUTION: A flight control system 1 for an unmanned aerial vehicle is provided that comprises: an unmanned aerial vehicle (UAV) 3 mounted with a reflector 7; and a total station (TS) 2 for tracking the reflector and for acquiring measurement data of three-dimensional coordinates of the reflector, wherein the total station comprises: a tracking unit for tracking the reflector; a TS-data transmission unit which has an optical axis in parallel to an optical axis of tracking light 22 of the tracking unit, and emits TS-data transmission light 23; and a TS-arithmetic control unit, wherein the unmanned aerial vehicle comprises: a photodetector for receiving the TS-data transmission light; and a UAV-arithmetic control unit for controlling a flight of the unmanned aerial vehicle, and wherein the TS-arithmetic control unit superimposes the measurement data on the TS-data transmission light, and the UAV-arithmetic control unit separates the measurement data from a photodetecting signal and obtains a flight position of the unmanned aerial vehicle.SELECTED DRAWING: Figure 1
【課題】無人飛行機の飛行制御システムに於いて、地上のトータルステーションで測定した無人飛行機の飛行位置を無人飛行体に伝送するシステムを提供する。【解決手段】反射体７を搭載した無人飛行機（ＵＡＶ）３と、該反射体を追尾し、その３次元座標の測定データを取得するトータルステーション（ＴＳ）２とを具備する無人飛行機の飛行制御システム１であって、前記トータルステーションは前記反射体を追尾する追尾部と、該追尾部の追尾光２２の光軸と平行な光軸を有し、ＴＳ−データ伝送光２３を発するＴＳ−データ伝送部と、ＴＳ−演算制御部とを具備し、前記無人飛行機は、前記ＴＳ−データ伝送光を受光する受光器と前記無人飛行機の飛行を制御するＵＡＶ−演算制御部とを有し、前記ＴＳ−演算制御部は、前記測定データを前記ＴＳ−データ伝送光に重畳し、前記ＵＡＶ−演算制御部は受光信号から測定データを分離し、前記無人飛行機の飛行位置を取得する。【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 CONTROLLING 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 GYROSCOPIC INSTRUMENTS HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS REGULATING SURVEYING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TESTING TRANSPORTING |
| title | FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASURING SYSTEM |
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