AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION

An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios is provided. The method includes receiving a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data. These i...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DE VILLELE, Dorothee, CHAUBEY, Rajesh, ADVANI, Sharanabasappa
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 DE VILLELE, Dorothee
CHAUBEY, Rajesh
ADVANI, Sharanabasappa
description An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios is provided. The method includes receiving a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data. These inputs are processed to determine a reference approach profile and an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The approach stabilization criterion is used to determine, whether (a) an IMC criterion profile stabilizes the actual approach and whether (b) a VMC criterion profile stabilizes the actual approach. A display system is commanded to display the approach stabilization criterion; and, when conditions (a) and (b) occur concurrently, user selections responsive to the displayed approach stabilization criterion are processed to update the actual approach profile.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3477260A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3477260A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3477260A13</originalsourceid><addsrcrecordid>eNrjZDB39AxyDnJ0C1EIjgwOcfUNVnD0c1HwdQ3x8HcJVnDzD1JwDAgI8nd09lAIDnF08vTxjHIM8fT342FgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4Bxibm5kZmBo6GxkQoAQAA2Cf9</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION</title><source>esp@cenet</source><creator>DE VILLELE, Dorothee ; CHAUBEY, Rajesh ; ADVANI, Sharanabasappa</creator><creatorcontrib>DE VILLELE, Dorothee ; CHAUBEY, Rajesh ; ADVANI, Sharanabasappa</creatorcontrib><description>An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios is provided. The method includes receiving a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data. These inputs are processed to determine a reference approach profile and an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The approach stabilization criterion is used to determine, whether (a) an IMC criterion profile stabilizes the actual approach and whether (b) a VMC criterion profile stabilizes the actual approach. A display system is commanded to display the approach stabilization criterion; and, when conditions (a) and (b) occur concurrently, user selections responsive to the displayed approach stabilization criterion are processed to update the actual approach profile.</description><language>eng ; fre ; ger</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 ; GYROSCOPIC INSTRUMENTS ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PARACHUTES ; PERFORMING OPERATIONS ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; REGULATING ; SIGNALLING ; SURVEYING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TESTING ; TRAFFIC CONTROL SYSTEMS ; TRANSPORTING</subject><creationdate>2019</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&amp;date=20190501&amp;DB=EPODOC&amp;CC=EP&amp;NR=3477260A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20190501&amp;DB=EPODOC&amp;CC=EP&amp;NR=3477260A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DE VILLELE, Dorothee</creatorcontrib><creatorcontrib>CHAUBEY, Rajesh</creatorcontrib><creatorcontrib>ADVANI, Sharanabasappa</creatorcontrib><title>AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION</title><description>An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios is provided. The method includes receiving a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data. These inputs are processed to determine a reference approach profile and an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The approach stabilization criterion is used to determine, whether (a) an IMC criterion profile stabilizes the actual approach and whether (b) a VMC criterion profile stabilizes the actual approach. A display system is commanded to display the approach stabilization criterion; and, when conditions (a) and (b) occur concurrently, user selections responsive to the displayed approach stabilization criterion are processed to update the actual approach profile.</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>GYROSCOPIC INSTRUMENTS</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>SIGNALLING</subject><subject>SURVEYING</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB39AxyDnJ0C1EIjgwOcfUNVnD0c1HwdQ3x8HcJVnDzD1JwDAgI8nd09lAIDnF08vTxjHIM8fT342FgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4Bxibm5kZmBo6GxkQoAQAA2Cf9</recordid><startdate>20190501</startdate><enddate>20190501</enddate><creator>DE VILLELE, Dorothee</creator><creator>CHAUBEY, Rajesh</creator><creator>ADVANI, Sharanabasappa</creator><scope>EVB</scope></search><sort><creationdate>20190501</creationdate><title>AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION</title><author>DE VILLELE, Dorothee ; CHAUBEY, Rajesh ; ADVANI, Sharanabasappa</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3477260A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</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>GYROSCOPIC INSTRUMENTS</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>SIGNALLING</topic><topic>SURVEYING</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>DE VILLELE, Dorothee</creatorcontrib><creatorcontrib>CHAUBEY, Rajesh</creatorcontrib><creatorcontrib>ADVANI, Sharanabasappa</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DE VILLELE, Dorothee</au><au>CHAUBEY, Rajesh</au><au>ADVANI, Sharanabasappa</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION</title><date>2019-05-01</date><risdate>2019</risdate><abstract>An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios is provided. The method includes receiving a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data. These inputs are processed to determine a reference approach profile and an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The approach stabilization criterion is used to determine, whether (a) an IMC criterion profile stabilizes the actual approach and whether (b) a VMC criterion profile stabilizes the actual approach. A display system is commanded to display the approach stabilization criterion; and, when conditions (a) and (b) occur concurrently, user selections responsive to the displayed approach stabilization criterion are processed to update the actual approach profile.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3477260A1
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
GYROSCOPIC INSTRUMENTS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PARACHUTES
PERFORMING OPERATIONS
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
REGULATING
SIGNALLING
SURVEYING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TESTING
TRAFFIC CONTROL SYSTEMS
TRANSPORTING
title AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-23T15%3A47%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=DE%20VILLELE,%20Dorothee&rft.date=2019-05-01&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3477260A1%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