DC Field | Value | Language |
---|---|---|
dc.contributor.author | 김영주 | ko |
dc.contributor.author | 탁민제 | ko |
dc.contributor.author | 이종하 | ko |
dc.date.accessioned | 2013-02-24T14:02:20Z | - |
dc.date.available | 2013-02-24T14:02:20Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1994-04 | - |
dc.identifier.citation | 한국항공우주학회지, v.22, no.2, pp.81 - 92 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/57666 | - |
dc.description.abstract | A Hardware-In-The-Loop Simulation(HILS) is widely used in the test and evaluation(T&E) of complex guidance and control systems hardware for aerospace applications. The real time HILS was performed by using a Taxis flight motion simulator, real time computer, I/O system and flight control system hardware along with a flight trajectory of the guidance flight system. In this paper, we proved the validity of the proposed simulation method, real time HILS, in the guidance night system by comparing its simulation results with the software simulation results. | - |
dc.language | Korean | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | 비행제어 시스템의 실물 모의시험 연구 | - |
dc.title.alternative | A Study on Hirdware-in-the-loop Simulation of a Flight Control Systems | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 22 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 81 | - |
dc.citation.endingpage | 92 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.contributor.localauthor | 탁민제 | - |
dc.contributor.nonIdAuthor | 김영주 | - |
dc.contributor.nonIdAuthor | 이종하 | - |
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