• Advances in aircraft and spacecraft science
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• 제5권2호
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• pp.205-223
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• 2018

During launch a spacecraft is subjected to a variety of dynamical loads transmitted through the launcher to spacecraft interface or air-born transmission excitations in the acoustic pressure field inside the fairing. As a result, spacecraft are tested on ground to ensure and demonstrate the global integrity of the structure against these loads, to screen the flight hardware for quality of workmanship and to validate mathematical models. This paper addresses the numerical modelling and simulation of the low frequency sine and random vibration tests performed on electrodynamic shaker facilities to comprise the mechanical-borne transmission loads through the launcher to spacecraft interface. Consequently, the paper reviews techniques and methodologies to derive a reliable and representative coupled virtual vibration testing simulation environment based on experimental data. These technologies are explored with the main objectives to ensure a stable, reliable and accurate control while testing. As a result, the use of the derived simulation models in combination with the added value of improved control and signal processing algorithms can lead to a safer and smoother vibration test control of the entire environmental test campaign.

• 자원환경지질
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• 제34권5호
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• pp.499-506
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• 2001

연안지역에서 해수의 지하 유동현상을 효과적이고 경제적으로 파악하기 위하여 등위치 송수신루프배열의 시간영역 전자탐사법(Time-domain Electromagnetic :TEM)을 이용한 지구물리모니터링을 적용하였다. TEM 모니터링은 전기 비저항 모니터링과 비교하여 해수유동에 대한 TEM반응의 민감도는 떨어진다. 그러나, 광범위한 조사지역에 대한 담수-해수 전이대의 공간적인 분포를 파악하는데 있어서는 측정시간을 포함한 탐사경비 그리고 현장에서 자료처리 측면에서 볼 때 매우 효율적이다.

• Wind and Structures
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• 제26권5호
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• pp.317-329
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• 2018

Wake characteristics of the flow over a finite square prism at different incidence angles were experimentally investigated using an open-loop wind tunnel. A finite square prism with a width D = 15 mm and a height H = 7D was vertically mounted on a horizontal flat plate. The Reynolds number was varied from $6.5{\times}10^3$ to $28.5{\times}10^3$ and the incidence angle ${\alpha}$ was changed from $0^{\circ}$ to $45^{\circ}$. The ratio of boundary layer thickness to the prism height was about ${\delta}/H=7%$. The time-averaged velocity, turbulence intensity and the vortex shedding frequency were obtained through a single-component hotwire probe. Power spectrum of the streamwise velocity fluctuations revealed that the tip and base vortices shed at the same frequency as that ofspanwise vortices. Furthermore, the results showed that the critical incidence angle corresponding to the maximum Strouhal number and minimum wake width occurs at ${\alpha}_{cr}=15^{\circ}$ which is equal to that reported for an infinite prism. There is a reduction in the size of the wake region along the height of the prism when moving away from the ground plane towards the free end.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.618-623
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• 2011

가스발생기의 압력 제어기법을 제안하였다. 모델기반 제어법칙을 설계하기 위하여 Robert 식과 보존방정식을 이용하여 가스발생기의 모델을 구성하였고, 연소시험을 통하여 모델의 정확성을 검증하였다. 모델은 연소 공간이 증가함에 따라 시스템의 고유 특성이 변화하게 되는데, 이러한 특성으로 인한 폐루프 구조에서 나타나는 응답특성을 평가하기 위하여 PID 및 비선형 적응 제어법칙을 설계하였다. 수치 시뮬레이션 결과 두 방법이 각각 제어 성능과 실제 시스템 적용에 문제가 있음을 알 수 있었고, 이를 극복하기 위한 새로운 제어기법을 제안하였다. 새롭게 제안된 이득계획 제어기법의 수치 시뮬레이션 결과 외란 및 측정 잡음의 영향에서도 우수한 제어 응답성능을 보였다.

• Structural Engineering and Mechanics
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• 제17권3_4호
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• pp.539-556
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• 2004

In this paper, the design, fabrication and characterization of a piezoelectric friction damper are presented. It was sized with the proposed practical procedure to minimize the story drift and floor acceleration of an existing 1/4-scale, three-story frame structure under both near-fault and far-field earthquakes. The design operation friction force in kip was numerically determined to range from 2.2 to 3.3 times the value of the peak ground acceleration in g (gravitational acceleration). Experimental results indicated that the load-displacement loop of the damper is nearly rectangular in shape and independent of the excitation frequency. The coefficient of friction of the damper is approximately 0.85 when the clamping force on the damper is above 400 lbs. It was found that the friction force variation of the damper generated by piezoelectric actuators with 1000 Volts is approximately 90% of the expected value. The properties of the damper are insensitive to its ambient temperature and remain almost the same after being tested for more than 12,000 cycles.

• 한국전자파학회논문지
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• 제7권2호
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• pp.139-146
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• 1996

본 논문에서 MSA(Microstrip Antenna)의 변형인 QMSA(Quarter-wavelength Microstrip Antenna)에 용량을 장하한 미소 루프 구조와 용량을 장하시킨 부분에서 방사하는 개구 구조에 의한 합성 전계 안테나를 제안 하였다. 그리고 합성 전제 특성은 계산된 값과 실험 값이 양호하게 일치함을 보였다. 제안된 안테나는 그라운드판과 방사 소자의 폭이 같은 소형화된 안테나이다. 설계.제작된 안테나는 동작 주파수 1.5GHz에서 수직.수평 편파를 각각 수신할 수 있다. 그리므로 이 안테나는 무선 전화를 위한 소형화된 안테나로써 이용할 수 있고, 실내 통신을 위해 아주 유용하다. 또한, 전송 선로 모델의 안테나 등가 회로는 정확한 공진 주파수를 찾기 위해 설계되었고, 리턴로스 값을 계산했다. 계산된 값은 실험값과 양호하게 일치되었다.

• 한국철도학회논문집
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• 제4권3호
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• pp.102-109
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• 2001

In this paper, it has a proposal of the RFID reader antenna design that expand the dedicated short-range communication distance between a static object on the ground and a mobile object attached on the moving article. The static reader equipped with micro-processor makes it possible to have a serial communication with a main system, so that much data can be transfer to the main system. An antenna is adjusted in order to a communication, the scale is designed by results values of simulation using matlab. It is achieved to systematically manage logistics, person resource and security system by grasping the information and location of mobile object on the basis that this system receives the information between a static reader and a mobile object tag at 134.2kHz band on real time, also to make it possible the main system to process. Therefore, the reader antenna scale is controlled on the foundation of a magnetic field theory in order to expand a recognition distance of reader and tag, so that can be optimistically recognized with minimizing the direction influence of reader and tag.

• International Journal of Control, Automation, and Systems
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• 제6권4호
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• pp.506-514
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• 2008

This paper presents an intelligent model; named as free model, approach for a closed-loop system identification using input and output data and its application to design a power system stabilizer (PSS). The free model concept is introduced as an alternative intelligent system technique to design a controller for such dynamic system, which is complex, difficult to know, or unknown, with input and output data only, and it does not require the detail knowledge of mathematical model for the system. In the free model, the data used has incremental forms using backward difference operators. The parameters of the free model can be obtained by simultaneous perturbation stochastic approximation (SPSA) method. A linear transformation is introduced to convert the free model into a linear model so that a conventional linear controller design method can be applied. In this paper, the feasibility of the proposed method is demonstrated in a one-machine infinite bus power system. The linear quadratic regulator (LQR) method is applied to the free model to design a PSS for the system, and compared with the conventional PSS. The proposed SPSA-based LQR controller is robust in different loading conditions and system failures such as the outage of a major transmission line or a three phase to ground fault which causes the change of the system structure.

• 한국전자파학회논문지
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• 제8권1호
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• pp.83-93
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• 1997

본 논문은 고전압 실험실에서 시변성 전자계의 측정 및 평가에 관한 것으로 전자적 외란은 주로 전력장비의 지락고장 및 개폐조작에 의해 기인되며, 전자회로와 제어장비틀은 전자방해작용에 매우 민감하다. 주어진 전자환 경에 대한 전자방해작용의 레벨을 평가하는 것은 필수적이다. 전계는 40 Hz-2oo MHz 범위의 대역폭을 갖는 전계센서로 관측되었으며, 시변성 자계는 출력이 입사신호에 직접적으로 비례하는 루프형 센서로 측정되었다. 또한 진동성 과도전류와 차단파 임펄스전압에 의해 유도된 전자방해작용의 레벨파 전자 차폐의 외함설계에 관한 정보를 주는 사변성 전자계의 주파수 성분을 고속프리에변환으로 분석하였다.

• Earthquakes and Structures
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• 제3권5호
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• pp.749-766
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• 2012

Structural control through integration of passive damping devices within the building structure has been increasingly implemented internationally in the last years and has proven to be a most promising strategy for earthquake safety. In the present paper an alternative configuration of an innovative energy dissipation mechanism that consists of slender tension only bracing members with closed loop and a hysteretic damper is investigated in its dynamic behavior. The implementation of the adaptable dual control system, ADCS, in frame structures enables a dual function of the component members, leading to two practically uncoupled systems, i.e., the primary frame, responsible for the normal vertical and horizontal forces and the closed bracing-damper mechanism, for the earthquake forces and the necessary energy dissipation. Three representative international earthquake motions of differing frequency contents, duration and peak ground acceleration have been considered for the numerical verification of the effectiveness and properties of the SDOF systems with the proposed ADCS-configuration. The control mechanism may result in significant energy dissipation, when the geometrical and mechanical properties, i.e., stiffness and yield force of the integrated damper, are predefined. An optimum damper ratio, DR, defined as the ratio of the stiffness to the yield force of the hysteretic damper, is proposed to be used along with the stiffness factor of the damper's- to the primary frame's stiffness, in order for the control mechanism to achieve high energy dissipation and at the same time to prevent any increase of the system's maximum base shear and relative displacements. The results are summarized in a preliminary design methodology for ADCS.