Sampling-aided wind estimation for air-to-surface missiles in flight tests공대지 유도탄의 비행시험에 대한 샘플링 기반의 바람 추정

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dc.contributor.advisorChoi, Han-Lim-
dc.contributor.advisor최한림-
dc.contributor.authorKim, Seok-Woo-
dc.date.accessioned2023-06-23T19:35:08Z-
dc.date.available2023-06-23T19:35:08Z-
dc.date.issued2021-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=1006568&flag=dissertationen_US
dc.identifier.urihttp://hdl.handle.net/10203/309353-
dc.description학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2021.2,[viii, 130 p. :]-
dc.description.abstractIn this study, three different estimation methods are proposed to estimate the winds experienced during the flight by short-range air-to-surface missiles. The wind estimation method is largely consisted into two parts. The one part is the high fidelity flight dynamics simulation of missile, and another part is the random wind generation. The proposed wind estimation methods can be distinguished by how to use the simulator and how to generate the random winds. The first method requires telemetry data of flight test and high-altitude wind database at the test site. The second method estimates wind by telemetry data of flight test without wind database. The third method is to estimate the wind in real time without any wind database. In this study, the estimation performance of three different estimation methods are presented and compared with various wind and flight conditions including sensor and modeling error.-
dc.languageeng-
dc.publisher한국과학기술원-
dc.subjectWind estimation▼aAir-to-surface missile▼aTime interval Monte-Carlo simulation▼aHigh fidelity 6 degree-of-freedom simulator▼aRandom wind generation-
dc.subject바람 추정▼a공대지 유도탄▼a시간간격 몬테카를로 시뮬레이션▼a고충실도 6자유도 시뮬레이션▼a무작위 바람 생성-
dc.titleSampling-aided wind estimation for air-to-surface missiles in flight tests-
dc.title.alternative공대지 유도탄의 비행시험에 대한 샘플링 기반의 바람 추정-
dc.typeThesis(Ph.D)-
dc.identifier.CNRN325007-
dc.description.department한국과학기술원 :항공우주공학과,-
dc.contributor.alternativeauthor김석우-
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