DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING
The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre |
| 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 | HUYNH, JEAN-PHILIPPE ROUQUETTE, PATRICE |
| description | The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA2640318A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA2640318A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA2640318A13</originalsourceid><addsrcrecordid>eNrjZEh0cQ3zdHZVcPMPUnD0dPH0c1cI8XBVCPD08Q8BcfzdFBz9gDJBzkGObiEKLqFBIFGQUEBAkL-js4dCgIdjMEQ_WGNoUIA_kA_U5-PoBzKPh4E1LTGnOJUXSnMzKLi5hjh76KYW5MenFhckJqfmpZbEOzsamZkYGBtaOBoaE6EEANiZMlc</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING</title><source>esp@cenet</source><creator>HUYNH, JEAN-PHILIPPE ; ROUQUETTE, PATRICE</creator><creatorcontrib>HUYNH, JEAN-PHILIPPE ; ROUQUETTE, PATRICE</creatorcontrib><description>The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13).</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CONTROLLING ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; SIGNALLING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRAFFIC CONTROL SYSTEMS ; TRANSPORTING</subject><creationdate>2007</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=20070830&DB=EPODOC&CC=CA&NR=2640318A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20070830&DB=EPODOC&CC=CA&NR=2640318A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUYNH, JEAN-PHILIPPE</creatorcontrib><creatorcontrib>ROUQUETTE, PATRICE</creatorcontrib><title>DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING</title><description>The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13).</description><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>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SIGNALLING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2007</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZEh0cQ3zdHZVcPMPUnD0dPH0c1cI8XBVCPD08Q8BcfzdFBz9gDJBzkGObiEKLqFBIFGQUEBAkL-js4dCgIdjMEQ_WGNoUIA_kA_U5-PoBzKPh4E1LTGnOJUXSnMzKLi5hjh76KYW5MenFhckJqfmpZbEOzsamZkYGBtaOBoaE6EEANiZMlc</recordid><startdate>20070830</startdate><enddate>20070830</enddate><creator>HUYNH, JEAN-PHILIPPE</creator><creator>ROUQUETTE, PATRICE</creator><scope>EVB</scope></search><sort><creationdate>20070830</creationdate><title>DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING</title><author>HUYNH, JEAN-PHILIPPE ; ROUQUETTE, PATRICE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2640318A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2007</creationdate><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>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SIGNALLING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>HUYNH, JEAN-PHILIPPE</creatorcontrib><creatorcontrib>ROUQUETTE, PATRICE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUYNH, JEAN-PHILIPPE</au><au>ROUQUETTE, PATRICE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING</title><date>2007-08-30</date><risdate>2007</risdate><abstract>The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13).</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre |
| recordid | cdi_epo_espacenet_CA2640318A1 |
| source | esp@cenet |
| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONTROLLING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING SIGNALLING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRAFFIC CONTROL SYSTEMS TRANSPORTING |
| title | DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-02T18%3A01%3A30IST&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=HUYNH,%20JEAN-PHILIPPE&rft.date=2007-08-30&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECA2640318A1%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 |