Skip navigation
  • 中文
  • English

DSpace CRIS

  • DSpace logo
  • Home
  • Research Outputs
  • Researchers
  • Organizations
  • Projects
  • Explore by
    • Research Outputs
    • Researchers
    • Organizations
    • Projects
  • Communities & Collections
  • SDGs
  • Sign in
  • 中文
  • English
  1. National Taiwan Ocean University Research Hub
  2. 電機資訊學院
  3. 通訊與導航工程學系
Please use this identifier to cite or link to this item: http://scholars.ntou.edu.tw/handle/123456789/18134
DC FieldValueLanguage
dc.contributor.authorJih-Gau Juangen_US
dc.contributor.authorHao-Hsiang Changen_US
dc.contributor.authorKai-Chung Chengen_US
dc.date.accessioned2021-10-29T02:56:36Z-
dc.date.available2021-10-29T02:56:36Z-
dc.date.issued2002-
dc.identifier.isbn0-7803-7298-0-
dc.identifier.issn0743-1619-
dc.identifier.otherINSPEC Accession Number: 7426249-
dc.identifier.urihttp://scholars.ntou.edu.tw/handle/123456789/18134-
dc.description.abstractNeural network applications to aircraft automatic landing control based on linearized inverse aircraft model are presented. Conventional automatic landing systems can provide a smooth landing which is essential to the comfort of passengers. However, these systems work only within a specified operational safety envelope. When the conditions are beyond the envelope, such as turbulence or wind shear, they often cannot be used. The objective of this study is to investigate the use of neural networks with linearized inverse aircraft model in automatic landing systems and to make these systems more intelligent. Current flight control law is adopted in the intelligent controller design. Tracking performance and robustness are demonstrated through software simulations. This paper presents five different neural network controllers to improve the performance of conventional automatic landing systems based on the linearized inverse aircraft model. Simulation results show that the neural network controller can successfully expand the safety envelope to include more hostile environments such as severe turbulenceen_US
dc.language.isoenen_US
dc.publisherIEEEen_US
dc.subjectIntelligent controlen_US
dc.subjectAircraften_US
dc.subjectaerospace controlen_US
dc.subjectInverse problemsen_US
dc.subjectAutomatic controlen_US
dc.subjectNeural networksen_US
dc.subjectSafetyen_US
dc.subjectIntelligent systemsen_US
dc.subjectintelligent networksen_US
dc.subjectRobustnessen_US
dc.titleIntelligent Landing Control Using Linearized Inverse Aircraft Modelen_US
dc.typeconference paperen_US
dc.relation.conferenceProceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301)en_US
dc.relation.conferenceAnchorage, AK, USAen_US
dc.identifier.doi10.1109/ACC.2002.1025295-
dc.relation.journalvolume4en_US
dc.relation.pages3269-3274en_US
item.openairetypeconference paper-
item.fulltextno fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_5794-
item.grantfulltextnone-
item.cerifentitytypePublications-
item.languageiso639-1en-
crisitem.author.deptCollege of Electrical Engineering and Computer Science-
crisitem.author.deptDepartment of Communications, Navigation and Control Engineering-
crisitem.author.deptNational Taiwan Ocean University,NTOU-
crisitem.author.parentorgNational Taiwan Ocean University,NTOU-
crisitem.author.parentorgCollege of Electrical Engineering and Computer Science-
Appears in Collections:通訊與導航工程學系
Show simple item record

Page view(s)

103
Last Week
0
Last month
2
checked on Jun 30, 2025

Google ScholarTM

Check

Altmetric

Altmetric

Related Items in TAIR


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.

Explore by
  • Communities & Collections
  • Research Outputs
  • Researchers
  • Organizations
  • Projects
Build with DSpace-CRIS - Extension maintained and optimized by Logo 4SCIENCE Feedback