Method and apparatus for an improved autopilot system providing for late runway change
An improvement to an autopilot flight director system allows the flight crew to make a late runway change without disengaging the autopilot. The improved system allows a transition to a new runway assignment if radio altitude is greater than 1500 feet. Control logic determines whether or not localiz...
Gespeichert in:
Hauptverfasser: | , , , , , , , , , , , , , , , , , , , |
---|---|
Format: | Patent |
Sprache: | eng |
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 | CASHMAN JOHN E CHANEY ROBERT E AGATE ROBERT M LILISCHKIES RONALD GRIFFIN, III JOHN C MCROBERTS TIMOTHY C BLOOM RONALD J HOVLAND CHARLES A MACDONALD JOSEPH M SANTONI, JR. FRANK P |
description | An improvement to an autopilot flight director system allows the flight crew to make a late runway change without disengaging the autopilot. The improved system allows a transition to a new runway assignment if radio altitude is greater than 1500 feet. Control logic determines whether or not localizer and/or glideslope have been captured and enters predetermined modes as a function thereof to effect a transition to the new approach while enabling instrument landing system retuning while maintaining autopilot engagement. Flight crew workload during approach is significantly reduced as a result of implementation of the improved system. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US5523949A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US5523949A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US5523949A3</originalsourceid><addsrcrecordid>eNrjZAjzTS3JyE9RSMwD4oKCxKLEktJihbT8IqCIQmZuQVF-WSpQprQkvyAzJ79EobiyuCQ1VwEknpmSmZcOVpqTWJKqUFSaV55YqZCckZiXnsrDwJqWmFOcyguluRnk3VxDnD10Uwvy41OLCxKTU_NSS-JDg01NjYwtTSwdjQmrAABuOTlj</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Method and apparatus for an improved autopilot system providing for late runway change</title><source>esp@cenet</source><creator>CASHMAN; JOHN E ; CHANEY; ROBERT E ; AGATE; ROBERT M ; LILISCHKIES; RONALD ; GRIFFIN, III; JOHN C ; MCROBERTS; TIMOTHY C ; BLOOM; RONALD J ; HOVLAND; CHARLES A ; MACDONALD; JOSEPH M ; SANTONI, JR.; FRANK P</creator><creatorcontrib>CASHMAN; JOHN E ; CHANEY; ROBERT E ; AGATE; ROBERT M ; LILISCHKIES; RONALD ; GRIFFIN, III; JOHN C ; MCROBERTS; TIMOTHY C ; BLOOM; RONALD J ; HOVLAND; CHARLES A ; MACDONALD; JOSEPH M ; SANTONI, JR.; FRANK P</creatorcontrib><description>An improvement to an autopilot flight director system allows the flight crew to make a late runway change without disengaging the autopilot. The improved system allows a transition to a new runway assignment if radio altitude is greater than 1500 feet. Control logic determines whether or not localizer and/or glideslope have been captured and enters predetermined modes as a function thereof to effect a transition to the new approach while enabling instrument landing system retuning while maintaining autopilot engagement. Flight crew workload during approach is significantly reduced as a result of implementation of the improved system.</description><edition>6</edition><language>eng</language><subject>CONTROLLING ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><creationdate>1996</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=19960604&DB=EPODOC&CC=US&NR=5523949A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19960604&DB=EPODOC&CC=US&NR=5523949A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CASHMAN; JOHN E</creatorcontrib><creatorcontrib>CHANEY; ROBERT E</creatorcontrib><creatorcontrib>AGATE; ROBERT M</creatorcontrib><creatorcontrib>LILISCHKIES; RONALD</creatorcontrib><creatorcontrib>GRIFFIN, III; JOHN C</creatorcontrib><creatorcontrib>MCROBERTS; TIMOTHY C</creatorcontrib><creatorcontrib>BLOOM; RONALD J</creatorcontrib><creatorcontrib>HOVLAND; CHARLES A</creatorcontrib><creatorcontrib>MACDONALD; JOSEPH M</creatorcontrib><creatorcontrib>SANTONI, JR.; FRANK P</creatorcontrib><title>Method and apparatus for an improved autopilot system providing for late runway change</title><description>An improvement to an autopilot flight director system allows the flight crew to make a late runway change without disengaging the autopilot. The improved system allows a transition to a new runway assignment if radio altitude is greater than 1500 feet. Control logic determines whether or not localizer and/or glideslope have been captured and enters predetermined modes as a function thereof to effect a transition to the new approach while enabling instrument landing system retuning while maintaining autopilot engagement. Flight crew workload during approach is significantly reduced as a result of implementation of the improved system.</description><subject>CONTROLLING</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1996</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAjzTS3JyE9RSMwD4oKCxKLEktJihbT8IqCIQmZuQVF-WSpQprQkvyAzJ79EobiyuCQ1VwEknpmSmZcOVpqTWJKqUFSaV55YqZCckZiXnsrDwJqWmFOcyguluRnk3VxDnD10Uwvy41OLCxKTU_NSS-JDg01NjYwtTSwdjQmrAABuOTlj</recordid><startdate>19960604</startdate><enddate>19960604</enddate><creator>CASHMAN; JOHN E</creator><creator>CHANEY; ROBERT E</creator><creator>AGATE; ROBERT M</creator><creator>LILISCHKIES; RONALD</creator><creator>GRIFFIN, III; JOHN C</creator><creator>MCROBERTS; TIMOTHY C</creator><creator>BLOOM; RONALD J</creator><creator>HOVLAND; CHARLES A</creator><creator>MACDONALD; JOSEPH M</creator><creator>SANTONI, JR.; FRANK P</creator><scope>EVB</scope></search><sort><creationdate>19960604</creationdate><title>Method and apparatus for an improved autopilot system providing for late runway change</title><author>CASHMAN; JOHN E ; CHANEY; ROBERT E ; AGATE; ROBERT M ; LILISCHKIES; RONALD ; GRIFFIN, III; JOHN C ; MCROBERTS; TIMOTHY C ; BLOOM; RONALD J ; HOVLAND; CHARLES A ; MACDONALD; JOSEPH M ; SANTONI, JR.; FRANK P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US5523949A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1996</creationdate><topic>CONTROLLING</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><toplevel>online_resources</toplevel><creatorcontrib>CASHMAN; JOHN E</creatorcontrib><creatorcontrib>CHANEY; ROBERT E</creatorcontrib><creatorcontrib>AGATE; ROBERT M</creatorcontrib><creatorcontrib>LILISCHKIES; RONALD</creatorcontrib><creatorcontrib>GRIFFIN, III; JOHN C</creatorcontrib><creatorcontrib>MCROBERTS; TIMOTHY C</creatorcontrib><creatorcontrib>BLOOM; RONALD J</creatorcontrib><creatorcontrib>HOVLAND; CHARLES A</creatorcontrib><creatorcontrib>MACDONALD; JOSEPH M</creatorcontrib><creatorcontrib>SANTONI, JR.; FRANK P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CASHMAN; JOHN E</au><au>CHANEY; ROBERT E</au><au>AGATE; ROBERT M</au><au>LILISCHKIES; RONALD</au><au>GRIFFIN, III; JOHN C</au><au>MCROBERTS; TIMOTHY C</au><au>BLOOM; RONALD J</au><au>HOVLAND; CHARLES A</au><au>MACDONALD; JOSEPH M</au><au>SANTONI, JR.; FRANK P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method and apparatus for an improved autopilot system providing for late runway change</title><date>1996-06-04</date><risdate>1996</risdate><abstract>An improvement to an autopilot flight director system allows the flight crew to make a late runway change without disengaging the autopilot. The improved system allows a transition to a new runway assignment if radio altitude is greater than 1500 feet. Control logic determines whether or not localizer and/or glideslope have been captured and enters predetermined modes as a function thereof to effect a transition to the new approach while enabling instrument landing system retuning while maintaining autopilot engagement. Flight crew workload during approach is significantly reduced as a result of implementation of the improved system.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_US5523949A |
source | esp@cenet |
subjects | CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES |
title | Method and apparatus for an improved autopilot system providing for late runway change |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-09T19%3A25%3A33IST&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=CASHMAN;%20JOHN%20E&rft.date=1996-06-04&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS5523949A%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 |