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Conference Paper: Differential flatness based full authority helicopter control design

TitleDifferential flatness based full authority helicopter control design
Authors
Koo, TJohnSastry, Shankar
Issue Date1999
PublisherInstitute of Electrical and Electronics Engineers. The Journal's web site is located at http://www.ieeexplore.ieee.org/xpl/conhome.jsp?punumber=1000188
Citation
Proceedings Of The Ieee Conference On Decision And Control, 1999, v. 2, p. 1982-1987 How to Cite?
AbstractA full authority helicopter control design based on differential flatness is presented. The concept of outer flatness is deployed for the design. The position dynamics and attitude dynamics are treated as the outer and inner systems respectively. The proposed design is based on an approximate model which is differentially flat, and then modified for the exact model. Given a desired trajectory in trim flight condition, the proposed control scheme is proved to result in global exponentially stability and convergence in the trajectory error.
Persistent Identifierhttp://hdl.handle.net/10722/188697
ISSN
0191-2216
2020 SCImago Journal Rankings: 0.395

 

DC FieldValueLanguage
dc.contributor.authorKoo, TJohnen_US
dc.contributor.authorSastry, Shankaren_US
dc.date.accessioned2013-09-03T04:13:34Z-
dc.date.available2013-09-03T04:13:34Z-
dc.date.issued1999en_US
dc.identifier.citationProceedings Of The Ieee Conference On Decision And Control, 1999, v. 2, p. 1982-1987en_US
dc.identifier.issn0191-2216en_US
dc.identifier.urihttp://hdl.handle.net/10722/188697-
dc.description.abstractA full authority helicopter control design based on differential flatness is presented. The concept of outer flatness is deployed for the design. The position dynamics and attitude dynamics are treated as the outer and inner systems respectively. The proposed design is based on an approximate model which is differentially flat, and then modified for the exact model. Given a desired trajectory in trim flight condition, the proposed control scheme is proved to result in global exponentially stability and convergence in the trajectory error.en_US
dc.languageengen_US
dc.publisherInstitute of Electrical and Electronics Engineers. The Journal's web site is located at http://www.ieeexplore.ieee.org/xpl/conhome.jsp?punumber=1000188en_US
dc.relation.ispartofProceedings of the IEEE Conference on Decision and Controlen_US
dc.titleDifferential flatness based full authority helicopter control designen_US
dc.typeConference_Paperen_US
dc.identifier.emailKoo, TJohn: john.koo@siat.ac.cnen_US
dc.identifier.authorityKoo, TJohn=rp01787en_US
dc.description.naturelink_to_subscribed_fulltexten_US
dc.identifier.scopuseid_2-s2.0-0033345819en_US
dc.identifier.volume2en_US
dc.identifier.spage1982en_US
dc.identifier.epage1987en_US
dc.publisher.placeUnited Statesen_US
dc.identifier.scopusauthoridKoo, TJohn=7005428590en_US
dc.identifier.scopusauthoridSastry, Shankar=35560685800en_US
dc.identifier.issnl0191-2216-

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