• 제어로봇시스템학회논문지
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• 제5권1호
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• pp.62-68
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• 1999

The attitude of a vehicle can be precisely determined using GPS carrier phase measurements from more than two antennas attached to a vehicle and an efficient integer ambiguity resolution technique. Many methods utilizing the known baseline length as a constraint of independent elements of integer ambiguities are proposed to resolve integer ambiguity at real time. Three-dimensional search space is reduced to two-dimensional search space with this constraint. Thus the true integer ambiguity can be easily determined with less computational burden and fewer number of measurements. But there are still strong requirements for the real time integer ambiguity resolution, which uses single epoch measurement of long baseline. In this paper, a new constraint from the geometry of multiple baselines is derived. With this new constraint, two-dimensional search space is further reduced to one-dimensional search space. It makes possible to determine integer ambiguity with single epoch measurement. The proposed method is applied to real data to show its effectiveness.

• 한국조명전기설비학회지:조명전기설비
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• 제6권6호
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• pp.23-31
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• 1992

Charged particle in the polymers is supposed to affect the electrical conduction and to lead them th dielectrical breakdown finally. So we measured the space charge distribution made by application of high electric field and evaluated the polarity of the charged particle affected on electrical conduction and space charge formed in the insulating materials by using temperature gradient thermally stimulated current measurement method(TG-TSC measurement). As a result, in the cross-linked polyethylene, A-peak was caused from dipole polarization, C-peak was caused from ionic space charge polarization and D-peak was injected trap hole. Also we found it crossible the evaluated the polarity of injected trap carrier and electron(or hole) of carrier trap in the cross-lined polyethylene. We found that ${\gamma}$-ray irradiated low density polyethylene had a relation to the electronic trap and we also could get the value of electric field distribution in the samples of which evaluation was available.

• 대한전자공학회논문지
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• 제14권2호
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• pp.28-31
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• 1977

반도체내에서의 종변조로 독한 반송파의 정상모드를 정의하였다. 충돌효과 및 열확산 현상이 있을때 이 반송파의 산란관계식을 유도하고 상세히 검토하였다. 특수한 경우에 이 반송파는 널리 알려진 공간 전하파와 전기음향파로 됨을 또한 여기에 밝혔다.

• 항공우주정책ㆍ법학회지
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• 제5권
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• pp.13-52
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• 1993

• International Journal of Aeronautical and Space Sciences
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• 제13권2호
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• pp.250-259
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• 2012

The need for position information in indoor environments has been growing lately. Several indoor navigation systems have been studied. Among them, pseudolite-based indoor positioning systems are one of the best systems to obtain precise position measurements. However, the installation of such systems is very difficult because the calibration of pseudolite antenna position is complicated. For precise calibration, the use of carrier phase measurements is necessary, and whenever carrier phase measurements are considered, problems with cycle ambiguity appear. In this paper, a new approach to calibrate the positions of pseudolite antennas is proposed. By using a multi-antenna, the ambiguity can be eliminated, epoch by epoch, for every single carrier phase measurement. Moreover, the number of calibration points can be reduced down to 3 by use of measurements collected at unknown positions. Using the proposed methods, the process of the collection of carrier phase measurements becomes considerably simple and convenient. Simulation results are presented to verify the proposed algorithms.

• 한국통신학회논문지
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• 제34권10A호
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• pp.807-813
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• 2009

위성 트랜스폰더는 상향 링크 신호를 복원하여 신호처리를 수행 하고, 하향 링크를 통해 지상국으로 전송하기 위한 통신 시스템이다. 이때 고속 비행에 의해 발생하는 도플러 주파수 편이로 인한 주파수 추적 및 동기시스템이 필요하며, 이를 위해 아날로그 트랜스폰더 방식으로는 PLL (Phase Locked Loop)을 사용하여 수신시스템의 반송파 복원을 획득한다. 이러한 방식은 위성의 기능에 따라 PLL구조 및 Loop필터의 구조와 설계방식의 변경을 필요로 한다. 본 논문에서는 이러한 아날로그 트랜스폰더를 대체할 수 있는 디지털 방식의 반송파 복원방안을 제안하였다. 이러한 방식은 근거리통신 위성이나 심 우주용 통신 위성의 특성에 따른 회로설계 변경 없이 동일한 하드웨어 플랫폼에 소프트웨어 변경으로 최적의 동기화를 구현할 수 있다.

• 한국항공우주학회지
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• 제33권3호
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• pp.65-70
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• 2005

잘못된 미지정수는 잘못된 위치값을 사용자에게 제공하여 자세결정에 큰 오차를 발생시킨다. 본 논문에서는 이동하는 항체에 4개 이상의 GPS 안테나를 고정시켜 정확한 자세결정을 수행할 때 다중경로를 추정하는 방법을 제안하였다. 4개 이상의 GPS 안테나에서 얻은 측정값이 같은 수신기 시계오차를 갖게 되면, 안테나 사이의 기하학적 관계를 이용하여 자세결정을 보다 효과적으로 수행할 수 있다. 안테나 사이의 거리를 반파장으로 만들어 미지정수 검색의 과정 없이 미지정수를 결정하고, GPS 반송파 측정값에 존재하는 다중경로 오차를 추정할 수 있다. 본 논문은 GPS 반송파 측정값의 다중경로 오차를 추정하는 알고리즘을 제시하고 수학적인 증명을 하였으며, 이 결과를 시뮬레이션을 통해 검증하였다.

• Journal of Periodontal and Implant Science
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• 제29권3호
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• pp.447-472
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• 1999

The preclinical and clinical studies reviewed herein show that rhBMP-2 induces normal physiologic bone in relevant defects in the craniofacial skeleton. The newly formed bone assumes characteristics of the adjacent resident bone, and allows placement and osseointegration of dental implants. Clearly, the bone inducing capacity of rhBMP-2 is carrier and site dependent. rhBMP-2 in an absorbable collagen sponge carrier induces relevant bone formation in space providing defects. Space providing carries extends this possibility to non-space providing sites. Notably, some ceramic and polymeric biomaterials may substantially interfere with rhBMP-2 induced osteogenesis.

• 대한기계학회논문집B
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• 제23권2호
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• pp.281-287
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• 1999

The turbulent natural convection in the membrane type LNG carrier cofferdam with heating points has been studied by numerical method. As the numerical methods, we introduced the three turbulence model, a standard $k-{\varepsilon}$ model and two case of a low Reynolds number models. The parameters considered for this study ore number and capacity of heating points i.e., $1{\leq}Ns{\leq}12$ and $1.0{\times}10^5{\leq}Qs(W/m^3){\leq}1.0{\times}10^8$. The results of the isotherms and velocity vectors have been represented for various parameters. The temperature and velocity at upper position in the space ore shown to be higher than those at lower position. For obtaining the optimal temperatures, $20{\sim}30^{\circ}C$ in the cofferdam space, the heating capacities show $2.0{\times}10^7W/m^3$ at g-heating points and $1.0{\times}10^7W/m^3$ at 12-points. The mean temperature in the cofferdam space can be expressed as a function of number and capacity of heating points.

• 한국항만경제학회지
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• 제21권3호
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• pp.115-148
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• 2005

In the liner market, a strategy is hard to sustain as competitors can easily imitate the strategy. For examples, when a number of shipping companies pursue this space exchange strategy in a liner market, their competitors are likely to build a cooperative alliance, following similar strategic pattern without any difficulty. Such strategic imitations are universal in international liner market. Therefore, the success of global alliance requires following critical considerations. First, the strategy of global alliance should be designed the way it gives the liner operators an economy of scale, which could be a key advantage in the competitive market. Second, thorough global alliance the lines should be able to improve their transport service through the reduction of operating costs and the business rationalization. The international alliance today is characterized by a strategic cooperation among a limited number of 'mega-carriers'. Such cooperation between the large-sized operators has come in many different forms. However, the trend has been towards the space exchange agreement, where a carrier on a route offers to another carrier a fixed number of spaces for a fixed period of time. the major carriers have been entered into groupings by integrating their services structures to increase market power. With reference to the above, this study has the following primary objectives: (1) to explore the present status of global alliance in liner shipping industry, (2) to prospect the future trend of the global alliance.