유연 우주 구조물 제어를 위한 최적 보상기 설계Optimal Compensator Design for Flexible Space Structure Control
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 방효충 | ko |
| dc.contributor.author | 김위대 | ko |
| dc.date.accessioned | 2013-02-28T04:46:09Z | - |
| dc.date.available | 2013-02-28T04:46:09Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 1996-04 | - |
| dc.identifier.citation | 한국항공우주학회지, v.24, no.1, pp.130 - 141 | - |
| dc.identifier.issn | 1225-1348 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/72839 | - |
| dc.description.abstract | An optimal compensator design approach for high precision pointing maneuver of flexible spacecraft by using adaptive structure is investigated in this paper. The Positive Position Feedback controller gains with a stability condition are the main design parameters resulting in the optimal compensator. A parameter optimization technique. is used to find out controller parameters which minimize a desired objective function. The objective function is selected to represent the pointing performance of a flexible space structure. The optimization result is a set of stabilizing feedback gains in conjunction with a set of second order compensators. | - |
| dc.language | English | - |
| dc.publisher | 한국항공우주학회 | - |
| dc.title | 유연 우주 구조물 제어를 위한 최적 보상기 설계 | - |
| dc.title.alternative | Optimal Compensator Design for Flexible Space Structure Control | - |
| dc.type | Article | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 24 | - |
| dc.citation.issue | 1 | - |
| dc.citation.beginningpage | 130 | - |
| dc.citation.endingpage | 141 | - |
| dc.citation.publicationname | 한국항공우주학회지 | - |
| dc.contributor.localauthor | 방효충 | - |
| dc.contributor.nonIdAuthor | 김위대 | - |
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