DC Field | Value | Language |
---|---|---|
dc.contributor.author | 이현재 | ko |
dc.contributor.author | 한진원 | ko |
dc.contributor.author | 방효충 | ko |
dc.date.accessioned | 2013-03-04T20:58:20Z | - |
dc.date.available | 2013-03-04T20:58:20Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2001-08 | - |
dc.identifier.citation | 한국항공우주학회지, v.29, no.5, pp.108 - 116 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/84114 | - |
dc.description.abstract | A software development of satellite attitude dynamics and control simulation is presented in this study. The software compromises two primary modules, 1). simulation and animation module, 2). operation module. It is developed in a PC platform by using C++ programming tool. The software development is intended to maintain generality to the extent possible through object oriented approach for future modification and expansion. Feedback attitude control using a reaction wheel assembly and open-loop control by multiple pulse thrusters are implemented in the S/W. The principal model and thruster control mode is taken from Koreasat 111 which is a geostationary satellite launched in 1999. | - |
dc.language | Korean | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | 인공위성 3축 자세제어 S/W 시뮬레이터 연구 :3차원 그래픽 포함 | - |
dc.title.alternative | S/W Simulator for Three-axis Attitude Control of Satellites | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 29 | - |
dc.citation.issue | 5 | - |
dc.citation.beginningpage | 108 | - |
dc.citation.endingpage | 116 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.contributor.localauthor | 방효충 | - |
dc.contributor.nonIdAuthor | 이현재 | - |
dc.contributor.nonIdAuthor | 한진원 | - |
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