STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT
To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a steering command, an aircraft steering angle control system that...
Gespeichert in:
| Hauptverfasser: | , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | YAMAGUCHI, Yasuhiro FUNABIKI, Kohei YAMAJI, Takuro SHINKAWA, Tomoko |
| description | To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a steering command, an aircraft steering angle control system that outputs an operation signal related to a steering angle S as a control command signal for a nose steering wheel incorporates a nose wheel envelope protection 4 including a reference steering angle setting unit 41 that calculates a reference steering angle S s on the assumption that the airframe is not skidding; a skid detection unit 42 that detects a skidding state of the airframe based on the reference steering angle S s ; and a switch unit 43 that selects a control command signal for a nose wheel in conjunction with the skid detection unit 42. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2447155A4</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2447155A4</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2447155A43</originalsourceid><addsrcrecordid>eNrjZNAKDnF1DfL0c1dw9HP3cVVw9vcLCfL3UQiOBEr4Krj5Byk4egY5Bzm6hfAwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXACMTE3NDU1NHE2MilAAAE2QkWA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT</title><source>esp@cenet</source><creator>YAMAGUCHI, Yasuhiro ; FUNABIKI, Kohei ; YAMAJI, Takuro ; SHINKAWA, Tomoko</creator><creatorcontrib>YAMAGUCHI, Yasuhiro ; FUNABIKI, Kohei ; YAMAJI, Takuro ; SHINKAWA, Tomoko</creatorcontrib><description>To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a steering command, an aircraft steering angle control system that outputs an operation signal related to a steering angle S as a control command signal for a nose steering wheel incorporates a nose wheel envelope protection 4 including a reference steering angle setting unit 41 that calculates a reference steering angle S s on the assumption that the airframe is not skidding; a skid detection unit 42 that detects a skidding state of the airframe based on the reference steering angle S s ; and a switch unit 43 that selects a control command signal for a nose wheel in conjunction with the skid detection unit 42.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; CONTROLLING ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRANSPORTING</subject><creationdate>2017</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=20170712&DB=EPODOC&CC=EP&NR=2447155A4$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170712&DB=EPODOC&CC=EP&NR=2447155A4$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YAMAGUCHI, Yasuhiro</creatorcontrib><creatorcontrib>FUNABIKI, Kohei</creatorcontrib><creatorcontrib>YAMAJI, Takuro</creatorcontrib><creatorcontrib>SHINKAWA, Tomoko</creatorcontrib><title>STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT</title><description>To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a steering command, an aircraft steering angle control system that outputs an operation signal related to a steering angle S as a control command signal for a nose steering wheel incorporates a nose wheel envelope protection 4 including a reference steering angle setting unit 41 that calculates a reference steering angle S s on the assumption that the airframe is not skidding; a skid detection unit 42 that detects a skidding state of the airframe based on the reference steering angle S s ; and a switch unit 43 that selects a control command signal for a nose wheel in conjunction with the skid detection unit 42.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAKDnF1DfL0c1dw9HP3cVVw9vcLCfL3UQiOBEr4Krj5Byk4egY5Bzm6hfAwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXACMTE3NDU1NHE2MilAAAE2QkWA</recordid><startdate>20170712</startdate><enddate>20170712</enddate><creator>YAMAGUCHI, Yasuhiro</creator><creator>FUNABIKI, Kohei</creator><creator>YAMAJI, Takuro</creator><creator>SHINKAWA, Tomoko</creator><scope>EVB</scope></search><sort><creationdate>20170712</creationdate><title>STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT</title><author>YAMAGUCHI, Yasuhiro ; FUNABIKI, Kohei ; YAMAJI, Takuro ; SHINKAWA, Tomoko</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2447155A43</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YAMAGUCHI, Yasuhiro</creatorcontrib><creatorcontrib>FUNABIKI, Kohei</creatorcontrib><creatorcontrib>YAMAJI, Takuro</creatorcontrib><creatorcontrib>SHINKAWA, Tomoko</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YAMAGUCHI, Yasuhiro</au><au>FUNABIKI, Kohei</au><au>YAMAJI, Takuro</au><au>SHINKAWA, Tomoko</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT</title><date>2017-07-12</date><risdate>2017</risdate><abstract>To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a steering command, an aircraft steering angle control system that outputs an operation signal related to a steering angle S as a control command signal for a nose steering wheel incorporates a nose wheel envelope protection 4 including a reference steering angle setting unit 41 that calculates a reference steering angle S s on the assumption that the airframe is not skidding; a skid detection unit 42 that detects a skidding state of the airframe based on the reference steering angle S s ; and a switch unit 43 that selects a control command signal for a nose wheel in conjunction with the skid detection unit 42.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP2447155A4 |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING |
| title | STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-03T17%3A17%3A52IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=YAMAGUCHI,%20Yasuhiro&rft.date=2017-07-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2447155A4%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |