인공위성 3축 자세제어 지상 검증 Testbed 연구 - I. 개발 연구A Study on Ground Verification Testbed for Three Axis Attitude Control of Satellites - Part I. Develoopment Study

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dc.contributor.author박영웅ko
dc.contributor.author한정엽ko
dc.contributor.author방효충ko
dc.contributor.author박봉규ko
dc.date.accessioned2013-03-03T00:12:52Z-
dc.date.available2013-03-03T00:12:52Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1999-04-
dc.identifier.citation한국항공우주학회지, v.27, no.5, pp.113 - 121-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/76190-
dc.description.abstractA study on the development of spacecraft attitude control system using a 3 axis spacecraft attitude control ground testbed is discussed in this paper. The testbed structure is made of aluminum structure width a configuration for general satellites. The testbed is connected to an air bearing for the 3 axis attitude control and some panels are located in the testbed holding experimental equipments. Experimental equipments are connected by wires to transfer power and signal. An OBC(On Board Computer) is used as a controller with on-board signal processing software developed. RF modems are installed between the testbed and a PC used as a ground station. Telemetry & command data processing software is also designed.-
dc.languageKorean-
dc.publisher한국항공우주학회-
dc.title인공위성 3축 자세제어 지상 검증 Testbed 연구 - I. 개발 연구-
dc.title.alternativeA Study on Ground Verification Testbed for Three Axis Attitude Control of Satellites - Part I. Develoopment Study-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume27-
dc.citation.issue5-
dc.citation.beginningpage113-
dc.citation.endingpage121-
dc.citation.publicationname한국항공우주학회지-
dc.contributor.localauthor방효충-
dc.contributor.nonIdAuthor박영웅-
dc.contributor.nonIdAuthor한정엽-
dc.contributor.nonIdAuthor박봉규-
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AE-Journal Papers(저널논문)
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