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...
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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. |
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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&date=20190501&DB=EPODOC&CC=EP&NR=3477260A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190501&DB=EPODOC&CC=EP&NR=3477260A1$$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> |
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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 |
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