1축 회전 시뮬레이터를 이용한 인공위성 지상 자세제어 실험 연구An Experimental Study on Attitude Control of Spacecraft using Single Axis Rotational Simulator

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dc.contributor.author한정엽ko
dc.contributor.author박영웅ko
dc.contributor.author방효충ko
dc.contributor.author황보한ko
dc.date.accessioned2013-02-27T09:41:33Z-
dc.date.available2013-02-27T09:41:33Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1998-04-
dc.identifier.citation한국항공우주학회지, v.26, no.4, pp.83 - 91-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/67801-
dc.description.abstractA spacecraft attitude control ground hardware simulator development is introduced in this paper. The simulator is called KT/KARI HILSSAT(Korea Telecom/Korea Aerospace Research Institute Hardware-In-the-Loop Simulator Single Axis Testbed). The main structure consists of a single axis bearing and a satellite main body model connected to the bearing The single axis simulator as an experimental hardware evaluates performance and applicability of satellite attitude control logic. Some useful experiments on attitude control of spacecraft by using air thrusters and a reaction wheel are presented. Time optimal controllers with dead zone and with PWM(Pulse Width Modulation) are applied to experiments. In particular, performance of PWM as one of the popular spacecraft attitude control technique is evaluated. A proportional-derivative controller for the reaction wheel control is tested producing successful results.-
dc.languageKorean-
dc.publisher한국항공우주학회-
dc.title1축 회전 시뮬레이터를 이용한 인공위성 지상 자세제어 실험 연구-
dc.title.alternativeAn Experimental Study on Attitude Control of Spacecraft using Single Axis Rotational Simulator-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume26-
dc.citation.issue4-
dc.citation.beginningpage83-
dc.citation.endingpage91-
dc.citation.publicationname한국항공우주학회지-
dc.contributor.localauthor방효충-
dc.contributor.nonIdAuthor한정엽-
dc.contributor.nonIdAuthor박영웅-
dc.contributor.nonIdAuthor황보한-
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AE-Journal Papers(저널논문)
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