• 한국전산유체공학회지
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• 제19권4호
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• pp.37-44
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• 2014

A detailed satellite panel thermal model composed of more than thousands nodes can not be directly integrated into a spacecraft thermal model due to its node size and the limitation of commercial satellite thermal analysis programs. For the integration of the panel into the satellite thermal model, a reduced thermal model having proper accuracy is required. A thermal model reduction method was developed and validated by using a geostationary satellite panel. The temperature differences of main components between the detailed and the reduced thermal model were less than $1^{\circ}C$ in steady state analysis. Also, the dynamic responses of the detailed and the reduced thermal model show very similar trends. Thus, the developed reduction method can be applicable to actual satellite thermal design and analysis with resonable accuracy and convenience.

• International Journal of Aeronautical and Space Sciences
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• 제17권4호
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• pp.476-490
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• 2016

This paper defines mode shape function of a composite solar panel assumed as Kirchhoff-Love plate for considering a torsional mode of composite solar panel. It then goes on to define dynamic model of a high-agility satellite considering the flexibility of composite solar panel as well as stiffness of a solar panel's hinge using Lagrange's theorem, Ritz method and the mode shape function. Furthermore, this paper verifies the validity of dynamic model by comparing numerical results from the finite element analysis. In addition, this paper performs a dynamic response analysis of a rigid satellite which includes only natural modes for solar panel's hinges and a flexible satellite which includes not only natural modes of solar panel's hinges, but also structural modes of composite solar panels. According to the results, we confirm that the torsional mode of solar panel should be considered for the structural design of high-agility satellite. Finally, we performed optimization of high-agility satellite for minimizing mass with solar panel's area limit using the defined dynamic model. Consequently, we observed that the defined dynamic model for a high-agility satellite and result of the optimal design are very useful not only because of their optimal structural design but also because of the dynamic analysis of the satellite.

• 한국항공우주학회지
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• 제37권9호
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• pp.837-842
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• 2009

구성 모드(Component mode) 합성법을 이용하여, 태양전지판의 유연구조 진동특성을 고려한 위성의 축약된 동적 모델링 기법을 수립하였다. 유연구조 위성의 본체와 태양전지판을 서로 다른 두 개의 부구조물로 나누고, 각각의 국부좌표계에 대하여 유도된 부구조물 표현식들을 위성 전체의 기준좌표계에 대해서 합성하였다. 수립된 부구조물 합성법은 단일 태양전지판을 갖는 유연구조 위성의 수치적 예제에 적용되었으며, 태양전지판의 회전을 고려한 전달함수 결과의 고찰을 통하여 동적 모델링 기법의 타당성을 확인하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.304-306
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• 2003

Oceanic pycnocline depth is usually obtained from in situ measurements. As ocean internal waves occur on and propagate along oceanic pycnocline, it is possible to estimate the depth remotely. This paper presents a method for retrieving pycnocline depth from synthetic aperture radar (SAR) imagery where internal waves are visible. This model is constructed by combining a two-layer ocean model and a nonlinear internal wave model. It is also assumed that the observed groups of internal wave packets on SAR imagery are generated by local semidiurnal tides. Case study in East China Sea shows a good agreement with in situ CTD data.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 추계학술대회논문집 II
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• pp.933-939
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• 2001

A Satellite shipping container must afford the satellite a relatively benign thermal, vibration, and particle environment that is oblivious to the extreme temperatures, sand, dust, vibrations and shocks that can accompany the transportation. In this study, we have designed a vibration isolation system of a spacecraft container that will be used to transport a satellite called KOMPSAT (KOrea Multi-Purpose SATellite) -2 from KARI (Korea Aerospace Research Institute) Taejon to its launch site. To identify the dynamic characteristics of the system, a 1/3-scaled mockup of the container was developed. A large electro-magnetic shaker (Max. 240 KN) was used to excite the mockup, and vibration signals from 20 points were collected for modal tests. Numerical simulations through CATIA 3D Modeling were performed to identify the behavior of isolation springs. The results showed that a simplified model predicts the behavior in a reasonable accuracy. Moreover, the model guides us how to design a full-scaled satellite-shipping container.

• 한국위성정보통신학회논문지
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• 제12권4호
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• pp.120-124
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• 2017

본 논문은 동역학 모델을 적용한 양방향 군 탐색구조 시스템의 시작품 제작에 대한 내용을 기술한다. USRP 개발 플랫폼과 단말기와 위성간의 통신을 상용 LTE망에 COSPAS-SARSAT 규격인 Spread Spectrum 방식의 신호체계를 USRP에 구현한 결과이다. 또한 구현된 결과의 정당성을 확인하기 위해 동역학 모델을 적용한 COSPAS-SARSAT 기반의 RF신호 처리를 USRP 테스트베드에 적용하여 실제적인 성능평가를 수행하였다. 향후 TDOA와 FDOA의 상관관계를 이용하는 CAF 알고리즘을 이용하여 보다 정확한 지상측위에 적용하고자 한다.

• International Journal of Aeronautical and Space Sciences
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• 제11권3호
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• pp.240-245
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• 2010

The controller of a model reference adaptive control monitors the plant's inputs and outputs to acknowledge its characteristics. It then adapts itself to the characteristics it encounters instead of behaving in a fixed manner. An important part of every adaptive scheme is the adaptive law for estimating the unknown parameters on line. A more precise model is required to improve performance and to stabilize a given dynamic system, such as a satellite in which performance varies over time and the coefficients change due to disturbances, etc. After model identification, the robust controller ($H{\infty}$) is designed to stabilize the rigid body and flexible body of a satellite, which can be perturbed due to disturbance. The result obtained by the $H{\infty}$ controller is compared with that of the proportional and integration controller which is commonly used for stabilizing a satellite.

• 한국위성정보통신학회논문지
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• 제6권1호
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• pp.12-18
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• 2011

고주파수 대역을 사용하는 위성통신 시스템의 링크 성능 저하의 가장 큰 요인 중의 하나가 강우 감쇠라고 할 수 있으며, 이러한 강우 감쇠를 보상하기 위한 가장 효율적인 방법으로써, 적응형 전송방식을 사용하고 있다. 강우 감쇠에 대처하기 위한 적응형 전송 방식을 개발하고 설계하는데 있어서 중요한 요소 중의 하나가 실제 발생하는 강우 감쇠에 대한 동적 시뮬레이션 모델이다. 본 논문에서는 초 단위 강우 감쇠 실측 데이터에 대한 통계치를 바탕으로 Markov 프로세스 모델을 이용하여 모델링하는 절차를 기술한다. 먼저 실측된 데이터의 통계적 특성을 추출하여 4가지 상태를 가지는 Markov 프로세스를 정의하고, 이를 이용하여 모델링된 데이터와 실측 데이터를 비교 분석한 결과를 제시한다.

• ETRI Journal
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• 제33권4호
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• pp.487-496
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• 2011

Korea Multi-Purpose Satellite-5 (KOMPSAT-5) is the first satellite in Korea that provides 1 m resolution synthetic aperture radar (SAR) images. Precise orbit determination (POD) using a dual-frequency IGOR receiver data is performed to conduct high-resolution SAR images. We suggest orbit determination strategies based on a differential GPS technique. Double-differenced phase observations are sampled every 30 seconds. A dynamic model approach using an estimation of general empirical acceleration every 6 minutes through a batch least-squares estimator is applied. The orbit accuracy is validated using real data from GRACE and KOMPSAT-2 as well as simulated KOMPSAT-5 data. The POD results using GRACE satellite are adjusted through satellite laser ranging data and compared with publicly available reference orbit data. Operational orbit determination satisfies 5 m root sum square (RSS) in one sigma, and POD meets the orbit accuracy requirements of less than 20 cm and 0.003 cm/s RSS in position and velocity, respectively.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.323-326
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• 1996

In a simple system, the control schemes work well provided that the characteristic of the plant or the coefficients are known and fixed. But the condition is not met in the system like satellite, for example, varying over time and the coefficients of dynamic system change due to disturbance, etc, and the better precise model is required to control the given dynamic system well. Conversely, the fixed controller make the unmodel dynamic system with a wide class of modelling error be stable within the error tolerance limits. Also, a robust model reference adaptive control scheme is designed for the plant, paying attention to the derivation of the appropriate parametric model and the design of the normalizing signal to guarantee that it has the desired properties.