• International Journal of Aeronautical and Space Sciences
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• 제15권1호
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• pp.82-90
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• 2014

In this paper, the effect of Lorentz force on the stability of attitude orientation of a charged spacecraft moving in an elliptic orbit in the geomagnetic field is considered. Euler equations are used to derive the equations of attitude motion of a charged spacecraft. The equilibrium positions and its stability are investigated separately in the pitch, roll and yaw directions. In each direction, we use the Lorentz force to identify an attitude stabilization parameter. The analytical methods confirm that we can use the Lorentz force as a stabilization method. The charge-to-mass ratio is the main key of control, in addition to the components of the radius vector of the charged center of the spacecraft, relative to the center of mass of the spacecraft. The numerical results determine stable and unstable equilibrium positions. Therefore, in order to generate optimum charge, which may stabilize the attitude motion of a spacecraft, the amount of charge on the surface of spacecraft will need to be monitored for passive control.

• 펄프종이기술
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• 제29권3호
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• pp.7-16
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• 1997

The constituents of deposits on paper machine and holes/spots in paper have been studied by consequently a combination of analytical techniques, such as FTIR, Py-GC-MS, and. EDS. FTIR spectroscopy was used prior to Py-GC-MS and EDS analysis, as preliminary analysis technique. The analysis of organic components were carried out with the use of a pyrolysis unit connected to a GC-MS, and inorganic components in ash were analysed by SEM equipped with an EDS analyzer after pyrolysis at 59$0^{\circ}C$. The deposits on the dryer section were complex pitch, which was the mixture of the organic contents of fatty acid ester and starch, and the inorganic contents of talc, clay, and calcium carbonate. The complex pitch was estimated to come from the coated broke. We knew the deposits on the metering rod of sym-sizer were associated with the interaction of unstable AKD and CaCO$_3$. The compositions of holes or spots varied considerably and were associated with chemical interaction within the system. The holes, spots, and blotches in the finished paper were PE and PP that were streamed out from pulp sources, complex pitch that were caused by the interaction of the different additives in the system, polymer such as flexible PVC that used for the prop of palette, and hot melt as adhesives that came from the inadequate handling of broke. In addition, we identified that poly(caprolactam) which is used for forming fabrics or press felts, could be mixed with the raw materials by accident and results in streak on coating.

• 항공우주시스템공학회지
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• 제13권3호
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• pp.1-8
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• 2019

전자기적 힘에 의해 김블 모터에 토크가 발생하며 코일 전류 변화는 토크 리플을 야기한다. 이는 김블속도에 영향을 주는 동시에 위성의 자세를 불안정하게 한다. 따라서 위성의 자세 제어 정확도 향상을 위해서는 김블 모터의 토크 리플 저감이 필수적이다. 본 논문에서는 일반적인 집중형 권선과 분포형 권선에 대해 모터의 모델링으로부터 발생 토크를 이론적으로 시뮬레이션 분석하였다. 토크 리플을 저감하는 권선을 선정하여 시제품을 설계 및 제작하여 자기장 및 역기전력의 이론적 해석 결과와 측정 결과를 비교하여 설계와 제작의 합치성을 확인하였다. 저속 시험을 통해 전절권 분포형 권선의 속도 안정도가 향상되어 토크 리플이 저감됨을 입증하였다.

• 한국군사과학기술학회지
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• 제22권4호
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• pp.517-526
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• 2019

In the present study, unsteady flows around a projectile ejected from an aircraft platform have been numerically investigated by using a three dimensional compressible RANS flow solver based on unstructured meshes. The relative motion between the platform and projectile was described by six degrees of freedom(6DOF) equations of motion with Euler angles and a chimera technique. Initial behavior of the projectile for varying conditions, such as roll and pitch-yaw command on the control surface of the projectile, flight Mach number, and platform pitch angle, was investigated. The ejection stability of the projectile was degraded as Mach number increases. In the transonic condition, the initial behavior of the projectile was found to be unstable as increase of platform pitch angle. By applying the command to control surfaces of the projectile, initial stability was highly enhanced. It was concluded that the proposed simulation data are useful for estimating the ejection behavior of a projectile in design phase.

• 대한음성학회:학술대회논문집
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• 대한음성학회 1997년도 7월 학술대회지
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• pp.92-114
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• 1997

This study is aimed to grasp the actual problems of the perception of English rhythm and intonation structure by Korean University students who have studied English in the secondary schools for the past six years, and to establish the systems of English rhythm and intonation structure for the Korean students of English. For this study, the listening test is provided, and 100 students are chosen as the subjects of the study. The noticeable findings are summarized as follows: (1) Koreans perceive the words stress comparatively well in nonsense words, unfamiliar place names, and familiar word. (2) Koreans do not perceive the isochrony of English rhythm well enough. The perception of the sentence stress is very unstable, especially in the sentence involved in polysyllabic words, compound words, and 'emphatic stress' pr 'contrastive stress'(or in the different rhythmic patterns). (3) Koreans do not perceive the nucleus well enough. The perception of the nucleus is more stable in content words than in function words, at the end of a sentence than in the middle of a sentence, and in monosyllabic words than in the polysyllabic words. (4) Koreans do not perceive the boundary(or pause) of intonation group well enough. The perception of the pause is unstable in the long or complex sentence. (5) Koreans discriminate the meaning of English word stress comparatively well, especially in disyllabic words. But the discrimination is somewhat unstable in polysyllabic words and between 'adjective' and 'verb' (6) Koreans' discrimination of the intonation meaning is below the level. Koreans do not perceive the differences of intonation meaning according to the pitch accent or the focus. In conclusion, the writer will propose the procedures for the teaching of rhythm and intonation in the following order: word stress drill longrightarrowstressed and reduced syllables drilllongrightarrowrhythm group drilllongrightarrowthe varying rhythm drilllongrightarrowsentence stress drilllongrightarrownucleus drill longrightarrowintonation group drilllongrightarrowlong utterance drill of more than two intonation group.

• 한국정밀공학회지
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• 제21권4호
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• pp.103-108
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• 2004

Carbon fiber reinforced composites(CFRP) were fabricated with phenolic resin matrix by hot press molding, and its surface was modified by the ion-assisted reaction process. When we tested the friction coefficient and wear rate variation and observed the effect of fibers with respect to friction and wear characteristics, the amount of pitch based carbon fiber was 45wt% and the average friction coefficient was the lowest at 0.12. When the amount of ion-irradiation was $1\times10^{l6}ions/cm^2$, the friction coefficient of the composites was about 0.12 and the wear mode was stable, whereas, the friction coefficient of the non-treated composites was about 0.16 and the wear mode was very unstable. But if the amount of ion-irradiation was $5\times10^{l6}ions/cm^2$$1\times10^{l6}ions/cm^2$ion-irradiation case.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2000년도 추계학술대회 논문집
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• pp.743-747
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• 2000

The coordinated mechanism of terrestrial vertebrates enables them to maneuver over all of the terrain conditions since they have a distinct ability to adapt to varying conditions. Their locomotions remain infinitely more advanced and elegant than that of present-day existing mechanical walking robots. However, the principles of existing walking robots are based more on technical rather than on biological concepts, yielding unstable locomotion with low speed. In order to apply these advanced biological phenomena to the mechanical design of 4-legged walking robot, modeling methods are introduced and mathematical equations are also introduced.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.206-209
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• 2011

During landing approach, an airplane could experience dynamic unstable motion by the combination of a gust and elevator control to cancel the disturbances. This situation is dangerous and could lead to a loss of an airplane. In this paper, numerical analysis was used to study the effect of pitch oscillating 2-D high lift devices in a landing condition. Experimental data on a pitching naca0012 airfoil was used for code validation. Dynamic characteristics of an airfoil, single slotted flap for mid-class passenger aircraft were analyzed. Unsteady Navier-Stokes analysis was performed with Spalart-Allmaras turbulence model for separation dominant low speed flow. As a result, flow hysteresis of a flapped airfoil was more complex than that of an oscillating airfoil. So, dynamic analysis of a flap in a landing condition is very important for operational safety.

• Journal of the Korean Wood Science and Technology
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• 제40권3호
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• pp.194-203
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• 2012

바이오매스 전처리에 효과적인 이온성 액체로 주목받고 있는 1-ethyl-3- methylimidazolium acetate를 사용하여 리기다소나무(pitch pine)로부터 리그닌을 추출하였고, 추출한 리그닌(Ionic Liquid Lignin : ILL)의 화학구조적 특성을 동일한 수종에서 단리한 milled wood lignin (MWL)과 비교분석하였다. 작용기 분석 결과 ILL과 MWL은 각각 10.0, 7.2%의 페놀성 수산기와 4.9, 11.0%의 메톡실기를 갖는 것으로 나타났다. ILL의 중량평균 분자량(3,995 Da)은 MWL (8,438 Da)에 비해 약 2배 정도 낮았으며, 다분산지수는 1.36으로 MWL (3.18)보다 낮은 값을 보였다. ILL의 열중량 분석 결과에 의하면 최대중량감소율(Vm)이 나타나는 온도(Tm)는 $306.6^{\circ}C$로 MWL ($341.9^{\circ}C$)보다 낮아 ILL이 MWL에 비해 열적으로 불안정하다는 것을 확인할 수 있었다.

• 대한의용생체공학회:의공학회지
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• 제16권1호
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• pp.95-100
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• 1995

본 논문에서는 발성기관인 후두(glottis)의 기능을 평가하기 위하여 후두신호의 주파수 변동과 진폭변동의 영향을 분석하였다. 정상인의 EGG(electroglottograph)신호는 매개변수 방법을 이용하여 최적의 차수가 9차인 자귀회귀형 모델로 설명할 수 있으며, 이것은 전달함수를 결정함으로써 해석이 가능하다. EGG신호의 진푹과 주파수의 변동은 변복조방식의 4전극 EGG 시스템으로 얻어지며, 후두기능 상태식별을 목적으로 개발하였다. EGG를 이용하여 후두의 닫힘구간과 열림구간을 계산함으로써 비정상 EGG신호는 비주기적이며 불안정한 상태라는 것을 구별할 수 있었다. 정상과 비정상의 피검자들을 구분할 수 있는 파라미터인 주파수 변동은 정상인의 m$\pm$0.5*sd이고, 진폭변동은 m$\pm$2*sd가 각각 되었다. 또한 EGG신호를 Hillbert 변환함으로써 얻어진 궤적의 패턴을 이용하여 정상과 비정상의 후두기능상태를 효과적으로 분류할 수 있었다.