A Full-Authority 4D Guidance Algorithm for Conventional Aircraft

A Full-Authority 4D Guidance Algorithm for Conventional Aircraft

A full-authority 4D guidance algorithm for a conventional aircraft is developed using Nonlinear Inverse Dynamics (NID) theory. The control task is simplified by the use of a forced singular perturbation, overall system dynamics being separated into fast and slow reduced-order systems. An analytical...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Stiharu-Alexe, Ilie, Stiharu-Alexe, Carmen
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Aerodynamics
Aircraft
Attitude control
Control systems
Elevators
Error correction
Feedback control
Force control
Iron
Neodymium
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 424
container_issue
container_start_page 420
container_title
container_volume
creator Stiharu-Alexe, Ilie
Stiharu-Alexe, Carmen
description A full-authority 4D guidance algorithm for a conventional aircraft is developed using Nonlinear Inverse Dynamics (NID) theory. The control task is simplified by the use of a forced singular perturbation, overall system dynamics being separated into fast and slow reduced-order systems. An analytical solution to inverting the slow time-scale dynamics is found through the Inverse Kinematics Problem (IKP). The algorithm's performance is evaluated in the terms of the tracking error.
doi_str_mv 10.23919/ACC.1993.4792887
format Conference Proceeding
fullrecord <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_4792887</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>4792887</ieee_id><sourcerecordid>4792887</sourcerecordid><originalsourceid>FETCH-LOGICAL-i105t-9839967ca346953b37eb41e81ca4a9f81aafef16f63c1a766b4397f0295951213</originalsourceid><addsrcrecordid>eNotj81Kw0AURgekUK19AHEzL5A4N3f-7s4h2ioU3Oi6TOKMHUkTmSRC317FfpsDZ3HgY-wGRFkhAd25ui6BCEtpqLLWXLArYaxAYbXABVtSVShpDC3Zehw_xe-UMiThkt07vpm7rnDzdBhymk5cPvDtnN593wbuuo8_eTjyOGReD_136Kc09L7jLuU2-zhds0X03RjWZ67Y2-bxtX4qdi_b59rtigRCTQVZJNKm9Sg1KWzQhEZCsNB66Sla8D6GCDpqbMEbrRuJZKKoSJGCCnDFbv-7KYSw_8rp6PNpf_6LP-liR-Q</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>A Full-Authority 4D Guidance Algorithm for Conventional Aircraft</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Stiharu-Alexe, Ilie ; Stiharu-Alexe, Carmen</creator><creatorcontrib>Stiharu-Alexe, Ilie ; Stiharu-Alexe, Carmen</creatorcontrib><description>A full-authority 4D guidance algorithm for a conventional aircraft is developed using Nonlinear Inverse Dynamics (NID) theory. The control task is simplified by the use of a forced singular perturbation, overall system dynamics being separated into fast and slow reduced-order systems. An analytical solution to inverting the slow time-scale dynamics is found through the Inverse Kinematics Problem (IKP). The algorithm's performance is evaluated in the terms of the tracking error.</description><identifier>ISBN: 0780308603</identifier><identifier>ISBN: 9780780308602</identifier><identifier>DOI: 10.23919/ACC.1993.4792887</identifier><identifier>LCCN: 92-54779</identifier><language>eng</language><publisher>IEEE</publisher><subject>Aerodynamics ; Aircraft ; Attitude control ; Control systems ; Elevators ; Error correction ; Feedback control ; Force control ; Iron ; Neodymium</subject><ispartof>1993 American Control Conference, 1993, p.420-424</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/4792887$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,27902,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4792887$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Stiharu-Alexe, Ilie</creatorcontrib><creatorcontrib>Stiharu-Alexe, Carmen</creatorcontrib><title>A Full-Authority 4D Guidance Algorithm for Conventional Aircraft</title><title>1993 American Control Conference</title><addtitle>ACC</addtitle><description>A full-authority 4D guidance algorithm for a conventional aircraft is developed using Nonlinear Inverse Dynamics (NID) theory. The control task is simplified by the use of a forced singular perturbation, overall system dynamics being separated into fast and slow reduced-order systems. An analytical solution to inverting the slow time-scale dynamics is found through the Inverse Kinematics Problem (IKP). The algorithm's performance is evaluated in the terms of the tracking error.</description><subject>Aerodynamics</subject><subject>Aircraft</subject><subject>Attitude control</subject><subject>Control systems</subject><subject>Elevators</subject><subject>Error correction</subject><subject>Feedback control</subject><subject>Force control</subject><subject>Iron</subject><subject>Neodymium</subject><isbn>0780308603</isbn><isbn>9780780308602</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>1993</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotj81Kw0AURgekUK19AHEzL5A4N3f-7s4h2ioU3Oi6TOKMHUkTmSRC317FfpsDZ3HgY-wGRFkhAd25ui6BCEtpqLLWXLArYaxAYbXABVtSVShpDC3Zehw_xe-UMiThkt07vpm7rnDzdBhymk5cPvDtnN593wbuuo8_eTjyOGReD_136Kc09L7jLuU2-zhds0X03RjWZ67Y2-bxtX4qdi_b59rtigRCTQVZJNKm9Sg1KWzQhEZCsNB66Sla8D6GCDpqbMEbrRuJZKKoSJGCCnDFbv-7KYSw_8rp6PNpf_6LP-liR-Q</recordid><startdate>199306</startdate><enddate>199306</enddate><creator>Stiharu-Alexe, Ilie</creator><creator>Stiharu-Alexe, Carmen</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>199306</creationdate><title>A Full-Authority 4D Guidance Algorithm for Conventional Aircraft</title><author>Stiharu-Alexe, Ilie ; Stiharu-Alexe, Carmen</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i105t-9839967ca346953b37eb41e81ca4a9f81aafef16f63c1a766b4397f0295951213</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>1993</creationdate><topic>Aerodynamics</topic><topic>Aircraft</topic><topic>Attitude control</topic><topic>Control systems</topic><topic>Elevators</topic><topic>Error correction</topic><topic>Feedback control</topic><topic>Force control</topic><topic>Iron</topic><topic>Neodymium</topic><toplevel>online_resources</toplevel><creatorcontrib>Stiharu-Alexe, Ilie</creatorcontrib><creatorcontrib>Stiharu-Alexe, Carmen</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Stiharu-Alexe, Ilie</au><au>Stiharu-Alexe, Carmen</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>A Full-Authority 4D Guidance Algorithm for Conventional Aircraft</atitle><btitle>1993 American Control Conference</btitle><stitle>ACC</stitle><date>1993-06</date><risdate>1993</risdate><spage>420</spage><epage>424</epage><pages>420-424</pages><isbn>0780308603</isbn><isbn>9780780308602</isbn><abstract>A full-authority 4D guidance algorithm for a conventional aircraft is developed using Nonlinear Inverse Dynamics (NID) theory. The control task is simplified by the use of a forced singular perturbation, overall system dynamics being separated into fast and slow reduced-order systems. An analytical solution to inverting the slow time-scale dynamics is found through the Inverse Kinematics Problem (IKP). The algorithm's performance is evaluated in the terms of the tracking error.</abstract><pub>IEEE</pub><doi>10.23919/ACC.1993.4792887</doi><tpages>5</tpages></addata></record>
fulltext fulltext_linktorsrc
identifier ISBN: 0780308603
ispartof 1993 American Control Conference, 1993, p.420-424
issn
language eng
recordid cdi_ieee_primary_4792887
source IEEE Electronic Library (IEL) Conference Proceedings
subjects Aerodynamics
Aircraft
Attitude control
Control systems
Elevators
Error correction
Feedback control
Force control
Iron
Neodymium
title A Full-Authority 4D Guidance Algorithm for Conventional Aircraft
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-29T04%3A24%3A10IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=A%20Full-Authority%204D%20Guidance%20Algorithm%20for%20Conventional%20Aircraft&rft.btitle=1993%20American%20Control%20Conference&rft.au=Stiharu-Alexe,%20Ilie&rft.date=1993-06&rft.spage=420&rft.epage=424&rft.pages=420-424&rft.isbn=0780308603&rft.isbn_list=9780780308602&rft_id=info:doi/10.23919/ACC.1993.4792887&rft_dat=%3Cieee_6IE%3E4792887%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=4792887&rfr_iscdi=true