• 한국산학기술학회논문지
• /
• 제10권5호
• /
• pp.909-916
• /
• 2009

본 연구는 위상천이 영사식 모아레 측정기의 기준 위상 측정단계에서 기준 위상의 검출 정확도를 높이기 위한 방안으로, 일반적인 N-bucket 방법이 아닌, 줄무늬 패턴 투사 영상의 직접적인 영상처리를 기반으로, 노이즈가 포함된 영상으로부터 기준 위상을 자동으로 검출하고 보정하는 방법을 다룬다. 일반적으로 기준위상을 정확히 구하기 위해서는 상대적으로 노이즈가 원천적으로 적은 고정밀도의 교정 시편과 이에 맞는 세분화된 교정방법이 필요하다. 하지만, 고가의 시편 제작비용 절감과 고정도 교정을 위한 교정시간의 단축을 위해, 상대적으로 일반 정밀도등급의 제작된 시편으로부터 획득된 영상을 이용하여, 효율적인 기준위상 교정 방법을 제안한다. 투사된 평행 라인 띠가 시편에서 반사되어 카메라로 입력되는 영상으로부터, 영상처리 라인마스크를 이용하여 격자 라인들의 중심점을 정밀하게 추출하고, 각 라인들에서 추출된 샘플링점 기반의 최소자승법을 이용하여, 라인 특징치인 기울기와 절편을 추출함으로써 실제 관측되는 격자 라인의 중심선을 획득하였으며, 획득된 중심선들을 이용하여 N-bucket 알고리즘에 적용할 수 있도록 위상을 추출한 후, 기준위상을 자동으로 생성하였다. 본 연구를 통하여 고가의 시편 제작 없이 빠르게 자동으로 기준위상을 추출할 수 있었다.

• 대한전자공학회논문지TC
• /
• 제48권2호
• /
• pp.95-104
• /
• 2011

본 논문에서는 complementary 나선형 공진 구조와 인터디지털 구조 기반의 메타물질 전송 선로가 전압 제어 발진기의 위상 잡음을 줄이기 위해서 제안되었다. 이와 같은 메타물질 전송 선로는 접지 면에 식각된 complementary 나선형 공진 구조의 배열과 신호 면의 인터디지털 전송 선로를 적용하여 구현되었다. 신호 면의 인터디지털 전송 선로는 인터디지털 구조가 없는 일반적인 전송 선로보다 더 높은 공진 Q 특성을 얻기 위해서 사용되었다. 제안된 메타물질 전송 선로의 공진 특성과 Q 특성의 고유 포화 특성이 신호 면의 전송 선로의 폭, complementary 나선형 공진 구조의 크기, complementary 나선형 공진 구조 사이의 전류 방향, complementary 나선형 공진 구조의 단위 셀 쌍의 수를 변화시킴으로써, 그리고 인터디지털 구조의 유무에 의해서 분석되어졌다. 제안된 전압 제어 발진기의 위상 잡음과 주파수 조절 범위는 -127.50~-125.33 dBc/Hz @ 100 kHz와 5.744~5.852 GHz이다.

• 대한기계학회논문집B
• /
• 제20권11호
• /
• pp.3598-3606
• /
• 1996

The finite volume method for radiation is applied to investigate a radiative heating of rocket base plane due to searchlight and plume emissions. Exhaust plume is assumed to absorb, emit and scatter the radiant energy isotropically as well as anisotropically, while the medium between plume boundary and base plane is cold and nonparticipating. Scattering phase function is modelled by a finite series of Legendre polynomials. After validating benchmark solution by comparison with that of previous works obtained by the Monte-Carlo method, further investigations have been done by changing such various parameters as plume cone angle, scattering albedo, scattering phase function, optical radius and nozzle exit temperature. The results show that the base plane is predominantly heated by the plume emission rather than the searchlight emission when the nozzle exit temperature is the same as that of plume.

• 대한기계학회논문집B
• /
• 제24권6호
• /
• pp.792-801
• /
• 2000

The problem of phase change from liquid to solid in the inviscid plane-stagnation flow is theoretically investigated. The solution at the initial stage of freezing is obtained by expanding it in powers of time, and the final equilibrium state is determined from the steady-state governing equations. The transient solution is dependent on the three dimensionless parameters, but the equilibrium state is determined by one parameter of (temperature ratio/conductivity ratio). The effect of the fluid flow on the growth rate of the solid in the pure conduction problem can be clearly seen from the solution of the initial stage and the final equilibrium state. The characteristics of the transient heat transfer at the surface of the solid and the liquid side of the solid-liquid interface for all the dimensionless parameters are elucidated.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2001년도 하계학술대회 논문집 A
• /
• pp.243-245
• /
• 2001

This paper presents a new classification method for high impedance faults in power systems. Results of phase plane trajectory with Clarke modal transformation using postfault current and voltage are utilized to classify types of arcing faults. The performance of the proposed method is tested on a typical 154 kV korean transmission system under various fault conditions using EMTP. As can be seen from results, phase plane trajectory of postfault current should be combined with that of o component from Clarke modal transformation to give reliability of clear fault classification. Thus the proposed method can classify arcing faults including LIFs and HIFs accurately in power systems.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2003년도 추계학술대회
• /
• pp.759-764
• /
• 2003

Numerical simulations are conducted to investigate the mechanism of hovering flight by single flapping wing, and to examine the effect of the phase difference between the fore- and hindwings in hovering flight by two flapping wings. The numerical method used is based on an immersed boundary method in Cartesian coordinates. The Reynolds number considered is Re=150 based on the maximum translational velocity and chord length of the wing. For single flapping wing, the stroke plane angles are $0^{\circ}$, $30^{\circ}$, $60^{\circ}$, $75^{\circ}$ and $90^{\circ}$ and the downstroke angles of attack are varied for each stroke angle. Results show that for each stroke plane angle, there is an optimal angle of attack to maximize the vertical force. Below the stroke angle of $60^{\circ}$, wake capturing reduces the negative vertical force during the upstroke. For two flapping wings, The phase lags of the hindwing are $0^{\circ}$, $90^{\circ}$, $180^{\circ}$ and $270^{\circ}$. The amplitudes of the stroke are 2.5 and 4.0 times the chord length at each phase lag. The results show that maximum vertical force is generated when the phase lag is zero, and the amplitude of the vertical force is minimum at the phase lag of $180^{\circ}$.

• 한국가시화정보학회지
• /
• 제7권2호
• /
• pp.28-34
• /
• 2010

Two turbulent jet with different sinusoidal nozzle exit configurations of in-phase and $180^{\circ}$ out-of-phase were investigated experimentally using a smoke-wire method and a hot-wire anemometry. Mean velocity and turbulence intensity were measured at several downstream locations under $Re_D\;=\;5000$. For the case of in-phase nozzle configuration, the length of potential core exhibits negligible difference with respect to the transverse locations (0, $\lambda/4$ and $\lambda/2$), similar to that of a plane jet. On the other hand, a maximum difference of 30% in the potential-core length occurs for the $180^{\circ}$ out-of-phase configuration. The spatial distributions of turbulence intensities also show significant difference for the nozzle of $180^{\circ}$ out-of-phase, whereas non-symmetric distribution is observed in the near-exit region(x/D = 1) for the in-phase sinusoidal nozzle jet. Compared to a slit planc jet, the sinusoidal nozzle jets seem to suppress the velocity deficit as the flow goes downstream. The sinusoidal nozzle jet was found to decrease turbulent intensity dramatically. The flow visualization results show that the flow characteristics of the sinusoidal nozzle jet are quite different from those of the slit plane jet.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2005년도 추계학술대회 논문집
• /
• pp.926-929
• /
• 2005

Recently, laser interferometer is widely used as a measuring system in many fields because of its high resolution and its ability to measure a board area in real-time ail at once. In conventional laser interferometer, for examples Out of plane ESPI, In plane ESPI, Shearography and Holography, it uses PZT or other components as a phase shift instrumentation to extract 3-D deformation data, vibration mode and others. However, in most cases PZT has some disadvantages, which include noli-linear errors and limited time of use. In present study, a new type of laser interferometer using a laser diode(LD) is proposed. Using Laser Diode Sinusoidal Phase Modulating(LD-SPM) interferometer, the phase modulation can be directly modulated by controlling the LD injection current thereby eliminating the need for PZT components.

• Transactions on Electrical and Electronic Materials
• /
• 제7권1호
• /
• pp.30-35
• /
• 2006

We have studied the motion of charged micro-particles that are immersed in a nematic liquid crystal (LC) and controlled by in-plane field. The LC is an anisotropic liquid such that the viscosity of the LC depends on flow direction, phase of the LC, and temperature, which affects the motion of the charged particles under the influence of electric field. This study shows that the motion of charged particles mainly depends on the applied voltage and the LC phase, but does not show any significant influence from the initial alignment of LC, although one may expect directional difference in drag force due to interaction between LC and particle. The viscosity changes due to temperature variations in nematic phase also show no signification influence on particle velocity when compared to the effect from varying in-plane field strength.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2005년도 춘계학술대회논문집
• /
• pp.572-575
• /
• 2005

A novel pneumatic artificial muscle actuator (PAM actuator), which has achieved increased popularity to provide the advantages such as high strength and high power/weight ratio, low cost, compactness, ease of maintenance, cleanliness, readily available and cheap power source, inherent safety and mobility assistance to humans performing tasks, has been regarded during the recent decades as an interesting alternative to hydraulic and electric actuators. In order to realize satisfactory control performance, a variable damper Magneto Rheological Brake (MRB), Is equipped to the Joint of the manipulator. Superb mixture of conventional PID controller and a phase plane switching control method brings us a novel controller. This proposed controller is appropriate for a kind of plants with nonlinearity, uncertainties and disturbances. The experiments were carried out in practical PAM manipulator and the effectiveness of the proposed control algorithm was demonstrated through experiments, which had proved that the stability of the manipulator can be improved greatly in a high gain control by using MRB with phase plane switching control method and without regard for the changes of external inertia loads.