• 한국응용곤충학회지
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• 제34권1호
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• pp.20-32
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• 1995

Adult diapause in insects is characterized by suppression of reproductive development. It is induced by environmental cues such as photoperiod, temperature, food availability, and other conditions Diapause-inducing environment is recognized and analyzed by the brain of the insects. The interpreted information is conveyed via endocrine system to target tissues such as ovaries, fat body, and other tissues. From this signal hierarchy of a brain-endocrine-target tissue axis, several factors are involved to express a diapause trait in a quantitative mode, even though the insects show a binomial phenotye between being in diapause or not. Recent works estimated that the number of the factors is relatively small by a series of crossing trials between high and low diapause lines. Heritability of the diapause is quite high (ca. 70%) in some species. Epistasis, sex-linkage, pleiotropism, and other nongenetic components also affect diapause inheritance. Most physiological studies have been focused on control mechanisms of the juvenile hormone (JH) synthesis in corpora allata (CA) because JH level in hemolymph of teneral adults is critical to decide a later developmental mode. Allatostatin, an antagonizer of JH synthesis, has been believed to be a potent brain message to CA for adult diapause induction.

• International Journal of Aeronautical and Space Sciences
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• 제11권1호
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• pp.49-57
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• 2010

Several pyrotechnic devices are employed over the course of satellite's missions, generally for the separation of structural subsystems and deployment of appendages. Firing of pyrotechnic devices results in impulsive loads characterized by high peak acceleration and high frequency content which can cause failures of various flight hardware elements and small components. Thus, accurate prediction of acceleration level in various components of spacecraft due to pyrotechnic devices is important. In this paper, two methods for pyroshock prediction, an empirical model and statistical energy analysis in conjunction with virtual mode synthesis, are applied to predict shock response of a low altitude earth observation satellite during launch vehicle separation. The predicted results are then evaluated through comparison with the shock test results.

• 한국전자파학회논문지
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• 제14권12호
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• pp.1283-1291
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• 2003

원하는 주파수 응답을 갖는 불균일 전송선로(NTL)는 일차원 역산란 문제에서 결합모드 Zakharov-Shabat(ZS) 방정식으로부터 포텐셜을 합성함으로서 구현할 수 있다. 본 연구에서는 ZS 방정식을 사용하여 제한된 포텐셜범위를 갖도록 하는 임의 반사계수를 갖는 NTL을 효율적으로 합성하는 방법을 제안한다. 이 방법은 특정한 윈도우 함수를 사용한 반사계수를 목표치로 한 경우보다 합성된 선로의 길이가 짧아지는 장점을 가진다. 또한 ZS 역변환시 연쇄법을 사용함으로서 기존의 반복법에 의한 계산과정을 간소화시켰다. 분산특성을 갖는 NTL 필터 설계에 제안한 방법을 적용함으로서 특정한 윈도우를 목표치로 한 기존의 방법과 비교, 분석하였으며, chain 행렬을 사용한 2-포트 해석을 통해 타당성을 검증하였다.

• 해양환경안전학회지
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• 제25권3호
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• pp.306-312
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• 2019

This paper investigates to design a controller for maritime autonomous surface ship (MASS) by means of adaptive super-twisting algorithm (ASTA). A input-out feedback linearization method is considered for multi-input multi-output (MIMO) system. Sliding Mode Controller (SMC) is suitable for MASS subject to ocean environments due to its robustness against parameter uncertainties and disturbances. However, conventional SMC has inherent disadvantages so-called, chattering phenomenon, which resulted from the high frequency of switching terms. Chattering may cause harmful failure of actuators such as propeller and rudder of ships. The main contribution of this work is to address an appropriate controller for MASS, simultaneously controls surge and yaw motion in severe step inputs. Proposed control mechanism well provides convergence bewildered by external disturbances in the middle of steady-state responses as well as chattering attenuation. Also, the adaptive algorithm is contributed to reducing non-overestimated value of control gains. Control inputs of surge and yaw motion are displayed by smoother curves without excessive control activities of actuators. Finally, no overshoot can be seen in transient responses.

• 한국전자파학회논문지
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• 제16권1호
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• pp.19-25
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• 2005

본 논문에서는 각 통과대역이 군지연 등화된 두 개의 통과대역을 갖는 필터의 합성 방법에 관하여 언급하였다. 각 통과대역이 군지연 등화된 특성을 가지게 함으로써, 기존의 이중 통과대역 필터보다 디지털 데이터 전송에 있어서 비트 에러율(BER)을 감소시킬 수 있고, 군지연 변화를 등화시키기 위하여 외부 등화기가 별도로 필요하지 않다. 본 논문에서의 합성 방법 타당성 검증을 위하여 각 통과대역이 군지연 등화된 5차 타원 응답특성을 갖는 두 개의 통과대역을 갖는 10차 이중모드 필터를 합성하였다.

• 대한기계학회논문집B
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• 제28권9호
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• pp.1081-1092
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• 2004

The synthesis of Ni-catalyzed multi-walled carbon nanotubes and nanofibers on a catalytic metal substrate, using an ethylene fueled inverse diffusion flame as a heat source, was investigated. When the gas temperature was varied from 1,400K to 900K, approximately, carbon nanotubes with diameters of 20∼60nm were formed on the substrate. In the regions where the gas temperature was higher than 1,400K or lower than 900K, iron nanorods or carbon nanofibers were synthesized, respectively. Based on the quantitative analyses of large amount of SEM and TEM images, the nanotubes formed closer to the flame had a tendency of having larger diameters. HR-TEM images and Raman spectra revealed that carbon nanotubes synthesized had multi-walled structures with some defective graphite layers at the wall. Based on the graphite mode of the Raman spectra, it was believed that the optimal synthesis could be obtained as the substrate was positioned at between 5.5mm and 5.0mm, from the flame axis.

• 한국소음진동공학회논문집
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• 제15권7호
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• pp.813-820
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• 2005

A deployable missile control fin has some structural nonlinearities because of the worn or loose hinges and the manufacturing tolerance. The structural nonlinearity cannot be eliminated completely, and exerts significant effects on the static and dynamic characteristics of the control fin. Thus, It is important to establish the accurate deployable missile control fin model. In the present study, the nonlinear dynamic model of 4he deployable missile control fin is developed using a substructure synthesis method. The deployable missile control fin can be subdivided Into two substructures represented by linear dynamic models and a nonlinear hinge with structural nonlinearities. The nonlinear hinge model is established by using a system identification method, and the substructure modes are improved using the Frequency Response Method. A substructure synthesis method Is expanded to couple the substructure models and the nonlinear hinge model, and the nonlinear dynamic model of the fin is developed. Finally, the established nonlinear dynamic model of the deployable missile control fin is verified by dynamic tests. The established model is In good agreement with test results, showing that the present approach is useful in aeroelastic stability analyses such as time-domain nonlinear flutter analysis.

• Nuclear Engineering and Technology
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• 제39권1호
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• pp.51-62
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• 2007

To efficiently design safety-critical systems such as nuclear power plants, with the requirement of high reliability, methodologies allowing for rigorous interactions between the synthesis and analysis processes have been proposed. This paper attempts to develop a reliability-centered design framework through an interactive process between Axiomatic Design (AD) and Fault Tree Analysis (FTA). Integrating AD and FTA into a single framework appears to be a viable solution, as they compliment each other with their unique advantages. AD provides a systematic synthesis tool while FTA is commonly used as a safety analysis tool. These methodologies build a design process that is less subjective, and they enable designers to develop insights that lead to solutions with improved reliability. Due to the nature of the two methodologies, the information involved in each process is complementary: a success tree versus a fault tree. Thus, at each step a system using AD is synthesized, and its reliability is then quantified using the FT derived from the AD synthesis process. The converted FT provides an opportunity to examine the completeness of the outcome from the synthesis process. This study presents an example of the design of a Containment Heat Removal System (CHRS). A case study illustrates the process of designing the CHRS with an interactive design framework focusing on the conversion of the AD process to FTA.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2014년도 제46회 동계 정기학술대회 초록집
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• pp.380.2-380.2
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• 2014

Direct synthesis of graphene using a chemical vapor deposition (CVD) has been considered a facile way to produce large-area and uniform graphene film, which is an accessible method from an application standpoint. Hence, their fundamental understanding is highly required. Unfortunately, the CVD growth mechanism of graphene on Cu remains elusive and controversial. Here, we present the effect of graphene growth parameters on the number of graphene layers were systematically studied and growth mechanism on copper substrate was proposed. Parameters that could affect the thickness of graphene growth include the pressure in the system, gas flow rate, growth pressure, growth temperature, and cooling rate. We hypothesis that the partial pressure of both the carbon sources and hydrogen gas in the growth process, which is set by the total pressure and the mole fraction of the feedstock, could be the factor that controls the thickness of the graphene. The graphene on Cu was grown by the diffusion and precipitation mode not by the surface adsorption mode, because similar results were observed in graphene/Ni system. The carbon-diffused Cu layer was also observed after graphene growth under high CH4 pressure. Our findings may facilitate both the large-area synthesis of well-controlled graphene features and wide range of applications of graphene.

• 한국음향학회지
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• 제15권5호
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• pp.99-106
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• 1996

컴프레서의 소음은 냉장고로부터 발생하는 전체 소음레벨중 높은 기여를 나타낸다. 그리고, 컴프레서로부터 방사되는 소음의 상당부분이 컴프레서 쉘의 진동에 의해 방사되는 소음이다. 본 연구에서는 컴프레서 쉘의 동특성을 규명하기 위하여 범용 구조해석 패키지인 MSC/NASTRAN을 이용하여 컴프레서 쉘을 여러 분계로 분리하여 해석한 뒤, 부분구조 합성법을 이용하여 전계의 동특성을 규명하였다. 그리고 각 분계의 변형 에너지와 운동에너지를 산정하여 각 분계가 전계에 기여하는 정도를 파악하였다. 컴프레서 소음에 가장 높은 영향을 미치는 1차모드를 고주파로 이동시키기 위하여, 1차 모드에 기여가 높은 분계의 질량과 강성을 변경하여 컴프레서 쉘의 동특성 개선 방향을 제시하였다.