Robust time-Optimal Control for Flexible Structure Vibration Control by Augmented Dynamics
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Bang, Hyochoong | ko |
| dc.contributor.author | Lee, Hyunjae | ko |
| dc.contributor.author | Eun, Yeonju | ko |
| dc.date.accessioned | 2017-12-19T03:12:10Z | - |
| dc.date.available | 2017-12-19T03:12:10Z | - |
| dc.date.created | 2017-01-12 | - |
| dc.date.created | 2017-01-12 | - |
| dc.date.created | 2017-01-12 | - |
| dc.date.issued | 2004-05 | - |
| dc.identifier.citation | International Journal of Aeronautical and Space Sciences, v.5, no.1, pp.19 - 29 | - |
| dc.identifier.issn | 2093-274X | - |
| dc.identifier.uri | http://hdl.handle.net/10203/228696 | - |
| dc.description.abstract | Robust optimal control problem for flexible spacecraft/structures using on-off type discrete actuators has been a subject of intensive research. Optimization by switching time parameterization can be used to minimize the maneuver time subject to equality. | - |
| dc.language | English | - |
| dc.publisher | The Korean Society for Aeronautical & Space Sciences | - |
| dc.title | Robust time-Optimal Control for Flexible Structure Vibration Control by Augmented Dynamics | - |
| dc.type | Article | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 5 | - |
| dc.citation.issue | 1 | - |
| dc.citation.beginningpage | 19 | - |
| dc.citation.endingpage | 29 | - |
| dc.citation.publicationname | International Journal of Aeronautical and Space Sciences | - |
| dc.identifier.doi | 10.5139/IJASS.2004.5.1.019 | - |
| dc.contributor.localauthor | Bang, Hyochoong | - |
| dc.description.isOpenAccess | N | - |
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