• Proceedings of the Korean DIstribution Association Conference
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• 2007.08a
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• pp.67-84
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• 2007

세계경제는 국가간 자유무역협정(FTA)으로 개방과 통합이 가속화되고 있다. 이러한 교역환경의 변화는 국내 프랜차이즈기업의 해외진출 기회를 확대하고 있지만 동시에 선진국 프랜차이즈기업의 위협을 극복해야 한다는 과제를 안겨주고 있다. 본 연구는 국내 프랜차이즈기업을 대상으로 해외 진출기업과 미진출기업의 조직특성에서의 차이점을 규명하는 데 목적이 있다. 자원기반이론과 대리이론에 근거하여 본 연구는 몇 가지 조직특성이 국내 프랜차이즈기업의 해외진출을 촉진하는 것으로 가설을 설정하고 있으며 이를 국내 315개 프랜차이즈기업에 대한 서베이조사를 통해 검증하고 있다. 분석 결과, 해외 진출 프랜차이즈기업이 미진출 프랜차이즈기업에 비해 규모가 크고 역사가 오래되었으며, 국내시장에서 점포의 지리적 분포가 큰 것으로 나타났다. 성장성은 기대와 달리 해외 진출 기업이 미진출 기업보다 낮은 것으로 나타났다. 또한 가맹점에 대한 가격구속은 진출기업과 미진출기업간에 통계적으로 유의적인 차이가 없는 것으로 나타났다. 분석결과를 토대로 본 연구는 국내 프랜차이즈기업의 해외진출을 위한 몇가지 시사점을 향우 연구과제와 함께 제시하고 있다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1997.10a
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• pp.361-364
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• 1997

The re-enty guidance design involves trajectory optimization, generation of a reference drag acceleration profile with the satisfaction of trajectory constraints. This reference drag acceleration profile can be considered as the reference trajectory. This paper proposes the atmospheric re-entry system which is composed of longitudinal, later and range control. This paper shows the a performance of a re-entry guidance and control system using feedback linearization control and predictive control.

• Proceedings of the Korean Fiber Society Conference
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• 2003.10b
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• pp.155-156
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• 2003

시멘트는 압축강도가 크고 내구성이 좋으며 가격이 저렴한 우수한 토목건축재료이다. 그러나 인장강도가 낮아서 사용 시 발생하는 휨에 의한 인장변형에 의하거나 양생 후 해 표면 크랙이 발생하는 결점이 있다. 이러한 결점을 보완하기위해 크랙의 발생 억제, 성장 지연을 목적으로 시멘트에 보강용 섬유를 투입하고 있다[1]. 시멘트에서의 보강섬유의 역할은 크랙발생에 필요한 에너지를 최대한 증가시키켜 시멘트가 경화되기 시작할 때, 구속에 의해 발생하는 인장응력 및 균열을 억제하구 내부에 형성되는 결함을 방지함에 있다[2]. (중략)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.5
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• pp.56-64
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• 2006

Station collocation of closely placed multiple GEO spacecraft is required to avoid the problem of collision risk, attitude sensor interference and/or occultation. This paper presents the method of obtaining the orbit correction scheme for collocating two GEO spacecraft within a small station-keeping box. The relative motion of each spacecraft with respect to the virtual geostationary satellite is precisely expressed in terms of power and trigonometry functions. This closed-form orbit propagator is used to define the constraint conditions which meet the requirements for the station collocation. Finally, the technique of constrained optimization is used to find the orbit maneuver sequence. Nonlinear simulations are performed and their results are compared with those of the classical method.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.2
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• pp.141-149
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• 2010

This paper contains impulsive maneuver which considers fuel consumption balance of chief satellite and deputy satellite in satellite formation flying. Thrust input is obtained by Lagrange' Multiplier method which is constructed by cost function with weight parameter of each satellite. Energy matching constraint is applied for boundedness of relative orbit, and theoretical solutions are verified by simulation results. Simulations are divided into two scenarios, with or without air-drag effect. This paper's results are expected to be used in real satellite formation flying, when fuel-balancing impulsive maneuver for relative orbit boundedness is needed.

• Journal of the Korean Society for Precision Engineering
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• v.17 no.6
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• pp.111-118
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• 2000

The design of reference trajectory with respect to drag acceleration is necessary to decelerate from hypersonic speed safely after atmosphere re-entry of space vehicle. The re-entry guidance design involves trajectory optimization, generation of a reference drag acceleration profile with the satisfaction of 6 trajectory constraints during the re-entry flight. This reference drag acceleration profile can be considered as the reference trajectory. The cost function is composed of the accumulated total heating on vehicle due to the reduction of weight. And a regularization is needed to prevent optimal drag profile from varying too fast and achieve realized trajectory. This paper shows the relations between velocity, drag acceleration and altitude in drag acceleration profile, and how to determine the reference trajectory.

• Proceedings of the Korea Concrete Institute Conference
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• 1995.04a
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• pp.305-310
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• 1995

토목 및 건축재료로서 폴리프로필렌 섬유 모르타르 및 콘크리트의 사용은 미국, 영 국 등지에서 개발되기 시작하여 많은 연구가 진행되어 왔는데, 가격이 저렴하고, 화학적인 안정성과 내구성이 우수하여 그 사용이 점차 증대되고 있는 실정이다. 이러한 폴리프로필렌 섬유의 사용은 모르타르 및 콘크리트가 건조나 냉각에 의해 수축될 때 구속에 의해 발생하 는 인장응력 및 균연을 제어하고, 인성의 증가와 충격, 마모, 피로에 대한 저항성, 내구성을 증대시키는 등의 장점을 가지는 것으로 보고되고 있다. 본 연구에서는 이러한 폴리프로필렌 섬유 모르타르 및 콘크리트의 역학적 거동특성인 압축강도, 인장강도, 인성, 유동성과 균열 특성을 실험적으로 규명하고자 하였다. 실험결과 폴리프로필렌의 혼입량이 증가할수록 압축 강도, 인장강도, 인성의 증가를 보였으나, 혼입향 0.2%를 초과할 경우 유동성, 강도 모두 감 소하는 것을 볼 수 있었다. 그리고 단섬유형 보다는 메쉬 형태의 폴리프로필렌 섬유가 역학 적 특성면에서 우수한 것으로 관찰되었으며, Kraai 방법에 의한 소성수축균열제어 특성 실 험에서 약 45% 이상으 균열감소 (0.1%혼입) 효과를 볼 수 있었다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.18 no.12
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• pp.3236-3245
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• 1994

The nesting of two-dimensional patterns onto a given raw sheet has applications in a number industries. It is a common problem often faced by designers in the shipbuilding, garment making, blanking die design, glass and wood industries. This paper presents a multi-stage layout approach for nesting two-dimensional patterns by using artificial intelligence techniques with a relatively short computation time. The raw material with irregular boundaries and internal defects which must be considered in various cases of nesting was also investigated in this study. The proposed nesting approach consists of two stages : initial layout stage and layout improvement stage. The initial layout configuration is achieved by the self-organizing assisted layout(SOAL) algorithm while in the layout improvement stage, the simulated annealing(SA) is adopted for a finer optimization.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.13 no.12
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• pp.5704-5708
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• 2012

In this paper, the algorithm to determine the optimal condition of traverse grinding is proposed by using differential evolution algorithm(DEA). The cost function to determine the optimal grinding condition is designed with considering process cost, production rate, surface roughness. Also, the constraint conditions for grinding such as thermal damage effect, machine tool stiffness, wear parameter of grinding wheel, surface roughness are considered. The algorithm is implemented with LabView software which is widely used at the industrial field. The performance of proposed algorithm is verified by comparing with the result of genetic algorithm(GA) through computer simulation.

• The Journal of the Korea Contents Association
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• v.15 no.2
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• pp.433-443
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• 2015

This study aims to analyze key antecedents of customer loyalty based on dedication-based and constraint-based mechanisms. Our framework provides a theoretical lens of how two distinctive mechanisms influence customer loyalty in a coffee chain context. In this regard, this study examines the effects of customer satisfaction and switching costs on customer loyalty in a coffee shop market. In order to test the proposed model, data collected from 263 university students were empirically tested by using partial least squares regression. The analysis results reveal that customer loyalty is jointly influenced by both a dedication-based and a constraint-based mechanisms. Coffee quality service quality, price and value, and service atmosphere significantly affect user satisfaction. Habit and brand image were found to be the key factors of forming perceived switching costs.