• 항공우주시스템공학회지
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• 제1권4호
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• pp.13-21
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• 2007

As one of YHF digital data link technologies, VDL Mode 2 is designed to be an air-to-ground subnetwork of the Aeronautical Telecommunication Network (ATN) based on the Open System Interconnection (OSI) architecture. VDL Mode 2 can be used in ATS Applications especially for CPDLC and ADS. And it is also expected to replace ACARS (Aircraft Communications Addressing and Reporting System) which has broadly been used in AOC for over 20 years. This paper presents the design result of VDL Mode 2 system under AOA (ACARS Over AVLC) environment for the implementation of bit-oriented ATS applications. The system is composed of airborne and ground subsystem. Airborne subsystem consists of VDR, CMU and an aircraft test equipment with CPDLC/ADS client applications for operational test and ground system consists of Ground Station which includes ground VDR and ground communication controller, simple DSP (Datalink Service Processor) and a ground test equipment with CPDLC/ADS server applications.

• International Journal of Aeronautical and Space Sciences
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• 제18권3호
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• pp.545-554
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• 2017

Among various applications of the High Altitude Long Endurance (HALE) Unmanned Aerial Vehicle (UAV), this paper has a focus on the Global Positioning System (GPS) utilizing pseudolite and its improved performance, particularly during the multi-purpose missions. In a multi-purpose mission, the HALE UAV follows a specified flight trajectory for both navigation applications and missions. Some of the representative HALE missions are remote exploration, surveillance, reconnaissance, and communication relay. During these operations, the HALE UAV can also be an additional positioning signal source as it broadcast signals using pseudolite. The pseudolite signal can improve the availability, accuracy, and reliability of the GPS particularly in areas with poor signal reception, such as shadowed regions between tall buildings. The improvement in performance of navigation is validated through simulations of multi-purpose missions of the solar-powered HALE UAV in an urban canyon. The simulation includes UAV trajectory generation at stratosphere and uses actual geographical building data. The results indicate that the pseudolite-equipped HALE UAV has the potential to enhance the performance of the satellite navigation system in navigationally degraded regions even during multi-purpose operations.

• 항공우주시스템공학회지
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• 제17권2호
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• pp.94-102
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• 2023

큐브위성용 태양전지판 분리장치는 열선 또는 저항소자의 발열로 나일론선을 절단하여 구조물의 구속을 해제하는 나일론선 절단방식 구속분리장치가 주로 적용되고 있다. 일반적으로 태양전지판 조립체의 발사하중을 고려한 구조해석을 수행하여 구속분리장치의 설계가 이루어지고 있으나, 발사 이후 궤도 열환경에 대한 구속분리장치의 열적 검토 및 분석사례는 전무한 실정이다. 따라서, 본 논문에서는 현재 개발중인 큐브위성 STEP Cube Lab-II에 적용되는 나일론선 절단 기반 구속분리장치의 열적 안정성 평가를 수행하고자 한다. 위성이 POD (Picosatellite Orbital Deployer)에서 사출되고 태양전지판이 전개되기까지의 분리장치 온도 분포를 검토하여 분리장치의 허용온도 범위 내에서 안정적인 구속 분리가 될 수 있도록 분리장치에 대한 궤도 열해석을 수행하였다. 또한, 열해석 결과를 기반으로 열진공시험을 수행하여 분리장치의 설계를 검증하였다.

• International Journal of Aeronautical and Space Sciences
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• 제8권1호
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• pp.1-9
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• 2007

As a first step toward a complete CFD-CSD coupling for helicopter rotor load analysis, the present study attempts to loosely couple a CFD code with a source-double panel method. The far-field wake effects were calculated by a time-marching free vortex wake method and were implemented into the CFD module via field velocity approach. Unlike the lifting line method, the air loads correction process is not trivial for the source-doublet panel method. The air loads correction process between the source-doublet method and CFD is newly suggested in this work and the computation results are validated against available data for well-known hovering flight conditions.

• 항공우주시스템공학회지
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• 제8권2호
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• pp.27-32
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• 2014

From the flight safety and the performance point of views, a new engine installation impacts an helicopter development or upgrade program significantly. More than a close relationship between an aircraft manufacturer and an engine manufacturer is necessary for the best integration work from the program initiation phase. In this paper, technical cooperation between aircraft and engine companies, and technical supports by the engine manufacturer for the T700/701K engine during the Surion development program are summarized. The applications of official technical program documents, US Mil-spec, France airworthiness regulations as the standard of the engine installation work, and engineering activities at each phase such as contract, design and manufacturing, flight clearance, ground and flight tests are described. This paper would be a cornerstone for the future domestic helicopter development program.

• Journal of electromagnetic engineering and science
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• 제6권4호
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• pp.217-221
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• 2006

Multipactor-free S-band duplexer based on inter-digital cavity type filter is proposed and demonstrated by in-house mulitpactor test facility for satellite RF components. Multipactor sensitivity of designed duplexer is analyzed by checking it out the maximum field accumulated region inside duplexer and calculating the electric field intensities at each resonator using 3D EM simulation in order to restrict the minimum gap distance as 2.5 mm which handles 43.13 dBm RF input power. Multipactor threshold was finally detected at 44 dBm in experiment for pulse mode test. The developed multipactor test method is cost effective, simple structure and gives a good agreement compared with the previous high cost MP test methodologies.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.270-308
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• 2006

• Carbon letters
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• 제4권4호
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• pp.192-201
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• 2003

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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• pp.798-802
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• 2002

Data provider and data user are linked together by suitable data. This implies that for a successful relationship the provider knows what kind of data, whether original or processed, is needed by the user and that the user articulates his needs to the provider. The co-operation between Korea and Austria aims at identifying these needs and to provide suitable routines for the processing of satellite data. Partners of this co-operation are the Korea Aerospace Research Institute, ARC Seibersdorf research and GeoVille. While the focus of the former lies in the development and running of satellite systems, the latter two have experience in the development and set up of applications in the field of remote sensing. Based on the complementary know-how by the institutions involved, projects were set up in Korea and Austria to fulfill this need and establish a pilot data feed for governmental applications.

• 한국항행학회논문지
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• 제21권3호
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• pp.213-219
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• 2017

대형 위성들은 수십억 달러가 넘는 개발 비용이 사용되고, 우주환경에서 운영하기까지 수십 년이 걸릴 수도 있다. 이에 비해 소형 위성은 상용 소프트웨어, 센서 등을 활용해서 비용을 절감할 수 있으며 개발 기간을 2년 이내로 단축시킬 수 있다. 본 논문에서는 이렇게 많은 이점을 가지고 있는 소형위성의 국내외 개발현황을 살펴보고, 소형위성을 군에서 활용하기 위한 몇 가지 방안을 제안한다. 먼저, 해외 개발현황으로 미국, 일본의 소형위성 개발현황을 소개하고, 국내 소형위성 개발현황을 소개한다. 군사적 활용방안은 크게 교육, 연구, 작전 분야로 분류하여 제안한다. 최근 소형위성은 상업 분야에서 빠르게 발전하고 있으며 향후 군에서도 중요한 역할을 할 것이다. 따라서 향후 스타워즈를 준비하고 있는 군에게 소형위성은 반드시 필요한 자산이며, 연구개발을 통해 지속적으로 발전시켜 나가야 한다.