유연구조를 갖는 인공위성의 자세제어에 관한 연구A Study on Attitude Control of Flexible Satellites
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 황인석 | ko |
| dc.contributor.author | 탁민제 | ko |
| dc.date.accessioned | 2013-02-25T14:02:01Z | - |
| dc.date.available | 2013-02-25T14:02:01Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 1994-02 | - |
| dc.identifier.citation | 한국항공우주학회지, v.22, no.1, pp.46 - 56 | - |
| dc.identifier.issn | 1225-1348 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/62704 | - |
| dc.description.abstract | In this paper a new LOG method is proposed for attitude control design of flexible satellites. This method. referred to as Frequency-Weighted LQG with Model Error Sensitivity Suppression (FWL/MESS). is derived from Frequency-Weighted LQG(FWL) and Model Error Sensitivity Suppression (MESS) to incorporate the advantages of the two precedent methods. The proposed method is applied to a design example for which an MSC/NASTRAN model of KOREASAT is used. Simulation study is also conducted to compare the controller performance with other design techniques. | - |
| dc.language | Korean | - |
| dc.publisher | 한국항공우주학회 | - |
| dc.title | 유연구조를 갖는 인공위성의 자세제어에 관한 연구 | - |
| dc.title.alternative | A Study on Attitude Control of Flexible Satellites | - |
| dc.type | Article | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 22 | - |
| dc.citation.issue | 1 | - |
| dc.citation.beginningpage | 46 | - |
| dc.citation.endingpage | 56 | - |
| dc.citation.publicationname | 한국항공우주학회지 | - |
| dc.contributor.localauthor | 탁민제 | - |
| dc.contributor.nonIdAuthor | 황인석 | - |
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