• 제목/요약/키워드: Formation flight

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ISAR 영상을 이용한 효과적인 편대비행 표적식별 연구 (A Study on Effective Identification of Targets Flying in Formation ISAR Images)

  • 차상빈;최인오;정주호;박상홍
    • 대한임베디드공학회논문지
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    • 제17권1호
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    • pp.67-76
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    • 2022
  • Monostatic/Bistatic inverse synthetic aperture radar (ISAR) images are two-dimensional radar cross section (RCS) distributions of a target. When there are many targets in a single radar beam, ISAR images are generated with targets overlapped, so it is difficult to perform the targets identification using the trained database. In addition, it is inefficient to perform target identification using only single monostatic and bistatic ISAR images separately because each method has its own advantages and weaknesses. Therefore, this paper analyzes multiple targets identification performances using monostatic/bistatic ISAR images and proposes a method of identification through fusion of two ISAR images. To identify multiple targets, we use image combination technique using trained single target images. Simulation results show effectiveness of proposed method.

RMA를 이용한 Spotlight SAR 영상형성 및 품질평가를 위한 시뮬레이터 개발 및 구현 (Development and application of simulator for spotlight SAR image formation and quality assesment using RMA)

  • 곽준영
    • 한국항공우주학회지
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    • 제39권2호
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    • pp.183-194
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    • 2011
  • 합성 개구면 레이다(SAR: synthetic aperture radar)는 날씨 및 주/야간에 관계없이 고해상도의 영상을 형성할 수 있기 때문에 다양한 분야에서 활용되고 있다. 본 논문에서는 영상 형상 및 품질 평가, 분석을 위한 Spotlight SAR 시뮬레이터를 제안한다. SAR 영상 품질의 예측은 초기 개념 설계 단계부터 최종적인 비행 검증 및 보정 단계에 걸쳐 필수적이다. 제안된 SAR 시뮬레이터는 시스템 설계 변수들에 기반을 두고 있어 전체 시스템 개발과정에서 SAR 영상의 품질을 예측 분석할 수 있다. 이를 위해 영상 획득 기하구조와 다양한 SAR 시스템 설계변수들을 고려하여 이상적인 점표적에 대한 시뮬레이션 원시 데이터를 생성하고 Spotlight 영상 형성 알고리듬을 구현함으로서 점표적 응답특성을 추정한다. 마지막으로 공간 해상도, 최대 부엽 수준, 누적 부엽 수준 등의 주요 품질변수들을 중심으로 생성된 원시 데이터의 영상 품질을 분석한다.

쿼드콥터 편대비행 중 PID값 불일치 및 센서, 모듈 고장진단을 통해 2차사고 발생 방지를 위한 연구 (A Study for Preventing Secondary Incident Caused by Incoincidence of Individual Flights PID values or Sensor or Telecommunication Defects During Formation Flying)

  • 김효진;이강환
    • 한국정보통신학회:학술대회논문집
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    • 한국정보통신학회 2016년도 춘계학술대회
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    • pp.487-489
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    • 2016
  • 본 논문에서는 쿼드콥터 편대비행 중 오류로 인해 높은 공중에서 추락할 경우 발생 가능한 문제들을 예방하는 방법을 제안한다. 기존 연구에서는 쿼드콥터 편대비행을 실내에서 구현하기 때문에 추락할 경우를 생각할 필요가 없었다. 본 연구는 비행 중 헤더노드의 Proportional-Integral-Derivative(PID) 값과 일치하지 않거나 쿼드콥터에 부착된 센서나 통신모듈 이상이 생길시 자가진단을 한 뒤 비행을 중지하여 2차 사고를 방지한다. 제안하는 방안은 쿼드콥터 편대비행 중 한 노드에 문제가 발생했을 시 추락을 방지하기 위해 헤드노드가 현재 상태를 서버로 전송하고 자가 진단하여 고도를 조절하는 시스템이다. 따라서 헤더노드와 비교한 PID 값의 차이가 지정된 값 이상이거나 센서나 통신모듈을 진단을 하여 결함을 발견했을 시 정지하여 안전한 곳으로 이동한다. 이 시스템은 가속도센서, 자이로센서, 다양한 센서들의 결함을 자가진단을 통해 발견하며 고도를 조절함으로 추가적인 피해를 최소화할 수 있다.

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The Effect of Word-of-Mouth on Purchase Intention: A Case Study of Low-Cost Carriers in Indonesia

  • SOELASIH, Yasintha;SUMANI, Sumani
    • The Journal of Asian Finance, Economics and Business
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    • 제8권4호
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    • pp.433-440
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    • 2021
  • This study aims at testing word-of-mouth (WOM) by mediating positive and negative perceptions of purchase intention on low-cost carriers (LCC) flights in Indonesia. One of the communications mixes that airlines can carry out is WOM. WOM is a form of communication between passengers after using a flight. The formation of a positive perception of WOM is expected by airlines. If a positive perception of WOM has formed, a purchase intention will arise. The study population included LCC flight passengers in Indonesia, involving 387 respondents. For indicators and variables, validity and reliability tests were conducted using CFA, CR, and AVE tools. Sampling locations were Soekarno-Hatta and Kualanamu airports. Sample collection was obtained through purposive sampling, and the analytical tool used was structural equation modeling (SEM) with Lisrel. The results showed that WOM influenced purchase intention through positive and negative perceptions of WOM. It can be seen that a positive perception of WOM has a direct effect, while a negative perception of WOM has the opposite effect. In conclusion, the mediation of perceptions influences purchase intention, whether it in the same direction or the opposite ones. To conclude, WOM is an antecedent for it influences purchase intention.

기내에서의 라포가 신뢰성과 안전성에 미치는 영향 - 팬데믹 상황을 기반으로 - (The Effect of Rapport on the Airplane on Reliability and Safety - Under the Pandemic -)

  • 김경은;전승준;정윤식
    • 한국항공운항학회지
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    • 제30권3호
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    • pp.65-75
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    • 2022
  • This study tried to confirm whether the public's negative emotions such as fear and anxiety about corona virus infection caused by the spatial nature of the aircraft were alleviated due to factors of in-flight services focusing on hygiene and quarantine and further had a positive effect on the formation of Rapport between cabin crews and passengers. We also investigated the impact on passengers' perceptions such as Reliability and Safety which can be viewed as a new measure and standard of customer satisfaction in the Pandemic era through Rapport. A survey was conducted online in December 2021 for passengers with experience in boarding aircraft after the COVID-19 outbreak, and a total of 211 responses were used for analysis. As a result of the analysis of the data, it was confirmed that aircraft in-flight service had a positive (+) effect on Rapport, and Rapport between passengers and cabin crews had a positive (+) effect on passenger Reliability and Safety.

Thermal Desorption-comprehensive Two Dimensional Gas Chromatography-time of Flight Mass Spectrometry (TD-GCxGC-TOFMS)을 이용한 서울 대기 중 PM2.5 유기성분 분석 (Analysis of Organic Compounds in Ambient PM2.5 over Seoul using Thermal Desorption-comprehensive Two Dimensional Gas Chromatography-time of Flight Mass Spectrometry (TD-GCxGC-TOFMS))

  • 이지이;;허종배;이승묵;김용표
    • 한국대기환경학회지
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    • 제25권5호
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    • pp.420-431
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    • 2009
  • Characteristics and advantages of the thermal desorption-comprehensive two dimensional gas chromatography-time of flight mass spectrometry (TD-GCxGC-TOFMS) were discussed and the organic compound's analysis result was shown for the ambient $PM_{2.5}$ sample collected in Seoul, Korea. Over 10,000 individual organic compounds were separated from about $70{\mu}g$ of aerosols in a single procedure with no sample pre-treatment. Among them, around 300 compounds were identified and classified based on the mass fragmentation patterns and GCxGC retention times. Several aliphatic compounds groups such as alkanes, alkenes, cycloalkanes, alkanoic acids, and alkan-2-ones were identified as well as 72 PAH compounds including alkyl substituted compounds and 8 hopanes. In Seoul aerosol, numerous oxidized aromatic compounds including major components of secondary organic aerosols were observed. The inventory of organic compounds in $PM_{2.5}$ of Seoul, Korea suggested that organic aerosol were constituted by the compounds of primary source emission as well as the formation of secondary organic aerosols.

The Flight Model of the NISS onboard NEXTSat-1

  • Jeong, Woong-Seob;Park, Sung-Joon;Moon, Bongkon;Lee, Dae-Hee;Pyo, Jeonghyun;Park, Won-Kee;Kim, Il-Joong;Park, Youngsik;Lee, Duk-Hang;Ko, Kyeongyeon;Kim, Mingyu;Nam, Ukwon;Kim, Minjin;Ko, Jongwan;Im, Myungshin;Lee, Hyung Mok;Lee, Jeong-Eun;Shin, Goo-Hwan;Chae, Jangsoo;Matsumoto, Toshio
    • 천문학회보
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    • 제41권2호
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    • pp.64.3-65
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    • 2016
  • The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared instrument optimized to the Next Generation of small satellite series (NEXTSat). The capability of both imaging and low spectral resolution spectroscopy in the near-infrared range is a unique function of the NISS. The major scientific mission is to study the cosmic star formation history in local and distant universe. For those purposes, the main observational targets are nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optical design is optimized to have a wide field of view ($2deg.{\times}2deg.$) as well as the wide wavelength range from 0.95 to $3.8{\mu}m$. Two linear variable filters are used to realize the imaging spectroscopy with the spectral resolution of ~20. The mechanical structure is considered to endure the launching condition as well as the space environment. The compact dewar is confirmed to operate the infrared detector as well as filters at 80K stage. The electronics is tested to obtain and process the signal from infrared sensor and to communicate with the satellite. After the test and calibration of the engineering qualification model (EQM), the flight model of the NSS is assembled and integrated into the satellite. To verify operations of the satellite in space, the space environment tests such as the vibration, shock and thermal-vacuum test were performed. Here, we report the test results of the flight model of the NISS.

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Status Report of the Flight Model of the NISS onboard NEXTSat-1

  • Jeong, Woong-Seob;Moon, Bongkon;Park, Sung-Joon;Lee, Dae-Hee;Pyo, Jeonghyun;Park, Won-Kee;Kim, Il-Joong;Park, Youngsik;Lee, Duk-Hang;Ko, Kyeongyeon;Kim, Mingyu;Nam, Ukwon;Kim, Minjin;Ko, Jongwan;Im, Myungshin;Lee, Hyung Mok;Lee, Jeong-Eun;Shin, Goo-Hwan;Chae, Jangsoo;Matsumoto, Toshio
    • 천문학회보
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    • 제42권1호
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    • pp.40.1-40.1
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    • 2017
  • The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared spectro-photometric instrument optimized to the Next Generation of small satellite series (NEXTSat). To achieve the major scientific objectives for the study of the cosmic star formation in local and distant universe, the spectro-photometric survey covering more than 100 square degree will be performed. The main observational targets will be nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optics was developed to cover a wide field of view ($2deg.{\times}2deg.$) as well as the wide wavelength range from 0.95 to $2.5{\mu}m$, which were revised based upon the recent test and evaluation of the NISS instrument. The mechanical structure were tested under the launching condition as well as the space environment. The signal processing from infrared sensor and the communication with the satellite were evaluated after the integration into the satellite. The flight model of the NSS was assembled and integrated into the satellite. To verify operations of the satellite in space, the space environment tests such as the vibration, shock and thermal-vacuum test were performed. The accurate calibration data were obtained in our test facilities. Here, we report the test results of the flight model of the NISS.

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피에조 잉크젯 헤드의 액적 토출 형상 전산해석 (Numerical Simulation of Inkjet Drop Formation in Piezo Inkjet Head)

  • 주영철;박상국;권계시
    • 한국산학기술학회논문지
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    • 제17권7호
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    • pp.641-647
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    • 2016
  • 피에조 DOD(drop-on-demand) 잉크젯 프린팅 방식은 다양한 종류의 잉크를 사용할 수 있기 때문에 최근에 첨단 산업에 적용이 활발히 연구되고 있다. 피에조 잉크젯 헤드에서 토출되는 액적의 형성 과정을 VOF(Volume-of-Fluid) 기법을 이용한 전산해석으로 예측하고 이를 측정결과와 비교하였다. 작동유체는 에틸렌 글리콜 50%와 IPA(Isopropil alchol) 50%의 혼합액을 사용하였다. 노즐 출구에서 메니스커스 변위의 시간에 따른 변화를 직접 측정하여 노즐 입구의 속도분포를 예측하고 이를 해석의 초기조건 입력자료로 사용하였다. 측정치와 해석치를 비교한 결과 전산해석이 측정치의 액적 형성 과정을 잘 예측함을 알 수 있었다. 주액적 형성과정보다 위성액적 형성과정 예측에 오차가 약간 컸는데, 이는 정지중의 공기에 큰 질량의 주액적이 날아가는 것을 예측할 때는 해석오차가 적지만 주액적에 의해서 주변 공기 유동이 활발해진 상태에서 적은 질량의 위성액적이 날아가는 것을 예측할 때는 해석오차가 상대적으로 커지기 때문이다. 또한 에틸렌 글리콜과 IPA의 혼합 비율을 달리하여 물성치를 변화시킨 다른 잉크에 대해서도 잉크 액적 형상을 예측한 결과 실험 결과를 비교적 정확히 예측할 수 있었다.

Computational Investigation of Lightning Strike Effects on Aircraft Components

  • Ranjith, Ravichandran;Myong, Rho Shin;Lee, Sangwook
    • International Journal of Aeronautical and Space Sciences
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    • 제15권1호
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    • pp.44-53
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    • 2014
  • A lightning strike to the aircraft seriously affects the aircraft and its components in various ways. As one of the most critical threats to the flight safety of an aircraft, fuel vapour ignition by lightning can occur through various means, notably through hot spot formation on the fuel tank skins. In this study, a coupled thermal-electrical approach using the commercial software ABAQUS is used to study the effects of a lightning strike on aircraft fuel tanks. This approach assumes that the electrical conductivity of a material depends on temperature, and that a temperature rise in a material due to Joule heat generation depends on electrical current. The inter-dependence of thermal and electrical properties-the thermal-electrical coupling-is analyzed by a coupled thermal-electrical analysis module. The analysis elucidates the effects of different material properties and thicknesses of tank skins and identifies the worst case of lightning zones.