DC Field | Value | Language |
---|---|---|
dc.contributor.author | Bang, Hyochoong | ko |
dc.contributor.author | Lee, JS | ko |
dc.contributor.author | Eun, YJ | ko |
dc.date.accessioned | 2010-02-09T02:03:46Z | - |
dc.date.available | 2010-02-09T02:03:46Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2004-02 | - |
dc.identifier.citation | KSME INTERNATIONAL JOURNAL, v.18, no.2, pp.203 - 210 | - |
dc.identifier.issn | 1226-4865 | - |
dc.identifier.uri | http://hdl.handle.net/10203/16529 | - |
dc.description.abstract | Attitude control law design for spacecraft large angle maneuvers is investigated in this paper. The feedback linearization technique is applied to the design of a nonlinear tracking control law. The output function to be tracked is the quaternion attitude parameter. The designed control law turns out to be a combination of attitude and attitude rate tracking commands. The attitude-only output function, therefore, leads to a stable closed-loop system following the given reference trajectory. The principal advantage of the proposed method is that it is relatively easy to produce reference trajectories and associated controller. | - |
dc.description.sponsorship | The Present work was supported by National Research Lab.(NRL) Program(MI-0203-00-0006) by the Ministry of Science and Technology, Korea. Auther fully appreciate the finalcial support | en |
dc.language | English | - |
dc.language.iso | en_US | en |
dc.publisher | KOREAN SOC MECHANICAL ENGINEERS | - |
dc.subject | LARGE-ANGLE MANEUVERS | - |
dc.subject | EIGENAXIS ROTATIONS | - |
dc.subject | QUATERNION FEEDBACK | - |
dc.title | Nonlinear attitude control for a rigid spacecraft by feedback linearization | - |
dc.type | Article | - |
dc.identifier.wosid | 000226596600003 | - |
dc.identifier.scopusid | 2-s2.0-21844479259 | - |
dc.type.rims | ART | - |
dc.citation.volume | 18 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 203 | - |
dc.citation.endingpage | 210 | - |
dc.citation.publicationname | KSME INTERNATIONAL JOURNAL | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | Bang, Hyochoong | - |
dc.contributor.nonIdAuthor | Lee, JS | - |
dc.contributor.nonIdAuthor | Eun, YJ | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | spacecraft attitude control | - |
dc.subject.keywordAuthor | feedback linearization | - |
dc.subject.keywordAuthor | quaternion parameter | - |
dc.subject.keywordAuthor | output tracking control | - |
dc.subject.keywordAuthor | singularity avoidance strategy | - |
dc.subject.keywordAuthor | sliding mode control | - |
dc.subject.keywordPlus | LARGE-ANGLE MANEUVERS | - |
dc.subject.keywordPlus | EIGENAXIS ROTATIONS | - |
dc.subject.keywordPlus | QUATERNION FEEDBACK | - |
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