AIRCRAFT DOCKING GUIDANCE SYSTEM WHICH TAKES POSITION REFERENCE IN ANTI-COLLISION LIGHT OF AIRCRAFT
A plurality of image pickup devices (15, 16) are set on the ground to pick up images of an anti-collision light located on an aircraft to be guided. A position reference producing section (17, 18, 19) produces a signal representing a position reference of the aircraft in accordance with picked-up im...
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| creator | SATO TETSUO MURANAKA SUSUMU |
| description | A plurality of image pickup devices (15, 16) are set on the ground to pick up images of an anti-collision light located on an aircraft to be guided. A position reference producing section (17, 18, 19) produces a signal representing a position reference of the aircraft in accordance with picked-up image signals from the plurality of image pickup devices (15, 16). A display data producing section (20) produces at least one of direction information and distance information as guidance information to be provided to pilots of the aircraft in accordance with the signal representing the position reference of the aircraft which is supplied from the position reference producing section (17, 18, 19). A display unit (11, 22) displays at least one of the direction information and distance information from the display data producing section (20) at a position on the ground where the pilots can see and recognize the information. |
| format | Patent |
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A position reference producing section (17, 18, 19) produces a signal representing a position reference of the aircraft in accordance with picked-up image signals from the plurality of image pickup devices (15, 16). A display data producing section (20) produces at least one of direction information and distance information as guidance information to be provided to pilots of the aircraft in accordance with the signal representing the position reference of the aircraft which is supplied from the position reference producing section (17, 18, 19). A display unit (11, 22) displays at least one of the direction information and distance information from the display data producing section (20) at a position on the ground where the pilots can see and recognize the information.</description><language>eng</language><subject>AIRCRAFT ; ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; AVIATION ; CONTROLLING ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; MEASURING ; PERFORMING OPERATIONS ; PHYSICS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; REGULATING ; SIGNALLING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TESTING ; TRAFFIC CONTROL SYSTEMS ; TRANSPORTING</subject><creationdate>1992</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=19921124&DB=EPODOC&CC=US&NR=5166746A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19921124&DB=EPODOC&CC=US&NR=5166746A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SATO; TETSUO</creatorcontrib><creatorcontrib>MURANAKA; SUSUMU</creatorcontrib><title>AIRCRAFT DOCKING GUIDANCE SYSTEM WHICH TAKES POSITION REFERENCE IN ANTI-COLLISION LIGHT OF AIRCRAFT</title><description>A plurality of image pickup devices (15, 16) are set on the ground to pick up images of an anti-collision light located on an aircraft to be guided. A position reference producing section (17, 18, 19) produces a signal representing a position reference of the aircraft in accordance with picked-up image signals from the plurality of image pickup devices (15, 16). A display data producing section (20) produces at least one of direction information and distance information as guidance information to be provided to pilots of the aircraft in accordance with the signal representing the position reference of the aircraft which is supplied from the position reference producing section (17, 18, 19). A display unit (11, 22) displays at least one of the direction information and distance information from the display data producing section (20) at a position on the ground where the pilots can see and recognize the information.</description><subject>AIRCRAFT</subject><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>AVIATION</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</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>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</subject><subject>MEASURING</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>RADIO DIRECTION-FINDING</subject><subject>RADIO NAVIGATION</subject><subject>REGULATING</subject><subject>SIGNALLING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TESTING</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1992</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqFjLEKwjAUALM4iPoNvh_oIGqcQ_qSPBoTSV4Rp1JKnEQL9f-Rgs5ON9xxSzEoSjopw1BH3VCwYFuqVdAI-ZYZz3B1pB2wajDDJWZiigESGkw4VxRABaZKR-8pz86TdQzRwG-9Fot7_5jK5suV2Bpk7aoyvroyjf1QnuXdtfm4k_J0kGr_v_gASk8zjg</recordid><startdate>19921124</startdate><enddate>19921124</enddate><creator>SATO; TETSUO</creator><creator>MURANAKA; SUSUMU</creator><scope>EVB</scope></search><sort><creationdate>19921124</creationdate><title>AIRCRAFT DOCKING GUIDANCE SYSTEM WHICH TAKES POSITION REFERENCE IN ANTI-COLLISION LIGHT OF AIRCRAFT</title><author>SATO; TETSUO ; MURANAKA; SUSUMU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US5166746A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1992</creationdate><topic>AIRCRAFT</topic><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>AVIATION</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</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>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</topic><topic>MEASURING</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>RADIO DIRECTION-FINDING</topic><topic>RADIO NAVIGATION</topic><topic>REGULATING</topic><topic>SIGNALLING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TESTING</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>SATO; TETSUO</creatorcontrib><creatorcontrib>MURANAKA; SUSUMU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SATO; TETSUO</au><au>MURANAKA; SUSUMU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT DOCKING GUIDANCE SYSTEM WHICH TAKES POSITION REFERENCE IN ANTI-COLLISION LIGHT OF AIRCRAFT</title><date>1992-11-24</date><risdate>1992</risdate><abstract>A plurality of image pickup devices (15, 16) are set on the ground to pick up images of an anti-collision light located on an aircraft to be guided. A position reference producing section (17, 18, 19) produces a signal representing a position reference of the aircraft in accordance with picked-up image signals from the plurality of image pickup devices (15, 16). A display data producing section (20) produces at least one of direction information and distance information as guidance information to be provided to pilots of the aircraft in accordance with the signal representing the position reference of the aircraft which is supplied from the position reference producing section (17, 18, 19). A display unit (11, 22) displays at least one of the direction information and distance information from the display data producing section (20) at a position on the ground where the pilots can see and recognize the information.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ANALOGOUS ARRANGEMENTS USING OTHER WAVES AVIATION CONTROLLING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PERFORMING OPERATIONS PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION REGULATING SIGNALLING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TESTING TRAFFIC CONTROL SYSTEMS TRANSPORTING |
| title | AIRCRAFT DOCKING GUIDANCE SYSTEM WHICH TAKES POSITION REFERENCE IN ANTI-COLLISION LIGHT OF AIRCRAFT |
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