• 대한조선학회논문집
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• 제35권1호
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• pp.54-60
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• 1998

일반적으로 선박의 보침성능을 평가하기 위해서 spiral test가 이용되고 있다. 그러나 spiral curve를 얻기 위한 spiral시험 및 역spiral시험에 있어서 바람과 파도 등의 영향으로 많은 어려움이 따른다. 따라서 spiral 시험을 하지 않고도, zig-zag test의 overshoot angle을 이용하여 선박의 보침성능을 판정하는 방법이 시도되고 있다. 본 연구에서는 실선의 spiral 시험결과를 대상으로, K-T 조종수학모델을 적용하여 zig-zag 운동을 계산하고, overshoot angle과 보침성능과의 상관관계를 조사하였다.

• 대한전기학회논문지:시스템및제어부문D
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• 제51권11호
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• pp.483-493
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• 2002

The damping ratio ${\xi}$ of the unit-step response of a second-order discrete system is a function of only the location of the closed-loop poles and is not directly related to the location of the system zero. However, the peak overshoot of the response is the function of both the damping ratio ${\xi}$ and an angle ${\alpha}$, which is the phasor angle of the damped sinusoidal response and is determined by the relative location of the zero with respect to the closed-loop poles. Therefore, if the zero and the open-loop poles are relatively adjusted, through pole-zero cancellation, to maintain the desired (or designed) closed-loop poles, the damping ratio ${\xi}$ will also be maintained, while the angle ${\alpha}$ changes. Accordingly, when the closed-loop system poles are fixed, the peak overshoot is considered as a function of the angle ${\alpha}$ or the system zero location. In this paper the effects of the relative location of the zero on the system performance of a second-order discrete system is studied, and a design method of digital compensator which achieves a minimum peak overshoot while maintaining the desired system mode and the damping ratio of the unit step response is presented.

• Journal of Electrical Engineering and Technology
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• 제12권2호
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• pp.674-682
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• 2017

This paper presents an optimal initial firing angle control based on the energy consumption and regenerative energy of a parallel multi-pulse thyristor dual converter for urban railway power substations. To prevent short circuiting the thyristor dual converter, a hysteresis band for maintaining a zero-current discontinuous section (ZCDS) is essential during mode changes. During conversion from the ZCDS to forward or reverse mode, the DC trolley voltage can be stabilized by selecting the optimal initial firing angle without an overshoot and slow response. However, the optimal initial firing angle is different depending on the line impedance of each converter. Therefore, the control algorithm for tracking the optimal initial firing angle is proposed to eliminate the overshoot and slow response of DC trolley voltage. Simulations and experiments show that the proposed algorithm yields the fastest DC voltage control performance in the transient state by tracking the optimal firing angle.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1999년도 추계학술대회 논문집 학회본부 B
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• pp.512-514
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• 1999

The damping ratio $\zeta$ of a continuous 2nd order response which passes all the points of the discrete response of a 2nd order discrete system(envelope curve) is a function of only the location of the closed-loop pole and ie not at all related to the location of the zero. And the peak overshoot of the envelope curve is uniquely specified by the damping ratio $\zeta$, which is a function of solely the closed-loop pole location, and the angle $\alpha$ which is determined by the relative location of the zero with respect to the closed-loop complex pole. Therefore, if the zero slides on the real axis with the closed-loop complex poles being fixed, then the angle $\alpha$ changes however the damping ratio $\zeta$ does not. Accordingly, when the closed-loop system poles are fixed, the peak overshoot is function of $\alpha$ or the system zero. In this thesis the effects of the relative location of the zero on the system performance of a second order discrete system is studied.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 합동 추계학술대회 논문집 정보 및 제어부문
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• pp.382-386
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• 2002

The damping ratio $\zeta$ of the unit-step response of a second-order discrete system is a function of only the location of the closed-loop poles and is not directly related to the location of the system zero. However, the peak overshoot of the response is the function of both the damping ratio $\zeta$ and an angle $\alpha$, which is the phasor angle of the damped sinusoidal response and is determined by the relative location of the zero with respect to the closed-loop poles. Accordingly, when the closed-loop system poles are fixed, the peak overshoot is considered as a function of the angle $\alpha$ or the system zero location. In this paper the effects of the relative location of the zero on the system performance of a second-order discrete system is studied, and a design method of digital compensator which achieves arbitrary steady-state response with minimum peak overshoot while maintaining the desired system mode and the damping ratio of the unit step response is presented.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1993년도 춘계학술대회 논문집
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• pp.185-191
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• 1993

A flexible nanipulator can move in the high speed even with the small driving torque. The dynamic equations of flexible manipulator whichinclude 2 vibrationalmodes are derived using the clamped-free boundarycondition. Simulation results of the 6th order modelare well matched with experimental results. The hub angle of the flexible manipulator can be controlled without vibration of beam by the feedback of both hub angle and strain. The overshoot of the hub angle in the step resonse is reduced without sacrificing the rise time using the cycloidal function instead of the step function as the reference input.

• 해양환경안전학회지
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• 제21권5호
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• pp.552-557
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• 2015

본 연구에서는 선미형상을 고려한 조종성능을 심수역 뿐만 아니라 천수역에 대해서 수치 시뮬레이션을 통해 검토하였다. 선미형상을 나타내는 파라메터 중 $C_{wa}$를 미소(${\pm}2%$)하게 변화시킴으로써 각 수역에서의 침로안정성, 선회 및 지그재그 성능이 어떤 변화를 보이고 그 경향이 어떻게 변화하는 지를 검토하였다. 선박의 조종성능 관점에서 흘수 대 수심의 비(=d/H)가 0.5 부근에서의 조종성에 큰 변화를 가져오는 중요 지점임을 알 수 있었고, 비대선(VLCC, 탱커 등)과 세장선(컨테이너)의 경우 선미형상의 변화에 따라 조종성능의 변화 정도가 많은 차이를 가질 수 있음을 알 수 있었다. 또한, $C_{wa}$를 감소(U형에 근접)시키면 선회운동에 있어서 advance 및 tactical diameter가 증가하고, 지그재그 운동에서는 track reach는 증가하지만 각 overshoot angle들은 감소한다. 이와 반대로, $C_{wa}$를 증가(V형에 근접)시키면 선회운동에 있어서 advance 및 tactical diameter는 감소, 지그재그 운동에서는 track reach는 감소, 각 overshoot angle 들은 증가함을 알 수 있었다.

• 해양환경안전학회:학술대회논문집
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• 해양환경안전학회 2003년도 추계학술발표회
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• pp.141-148
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• 2003

본 연구에서는 선박의 안전항해의 관점에서 IMO조종성기준 중 변침 및 보침 성능에 관해 검토하였다. 침로불안정의 정도가 각각 다른 세척의 시리즈선박을 채택하여 지그재그시험에 관한 수치시뮬레이션을 수행하여 침로불안정의 정도와 오버슈트각 사이의 관계를 규명하였다. 그 결과 오버슈트각은 변침 및 보침 성능의 기준이 될 수 있음을 확인하였다. 그리고 자체개발한 시뮬레이터를 활용하여 시리즈선박의 항로항행에 관한 실시간 시뮬레이션 실험을 수행하여 선박의 조종난이도와 침로불안정의 정도 사이의 관계를 규명하였다. 아울러 수치시뮬레이션과 시뮬레이션실험 결과를 토대로 IMO조종성기준의 변침 및 보침 성능에 관한 새로운 안을 제시하였다.

• 수산해양기술연구
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• 제56권2호
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• pp.172-182
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• 2020

In order to offer specific information needed to assist in operation of a ship with same type rudder through evaluating the maneuverability of training ship A-Ra with flapped rudder, sea trials based full scale for turning test, zig-zag test with rudder angle 10° and 20°, and spiral test at service condition were carried out on starboard and port sides around Jeju Island according to the standards of maneuverability of IMO. As a result, the angular velocity of port turn was higher than that of starboard turn. Therefore, the size of turning circle was longer on the starboard side. In addition, variation of the transfer due to various factors was more stable than those of the others. In the Z-test results, the mean of 1st and 2nd overshoot angles were 9.8°, 6.3° and 15.3°, 9.2° respectively when the port and starboard was 10°; the 1st overshoot angle were 18°, 13.7° when using 20°. Her maneuverability index T' and K' can be easily determined by using a computer with the data obtained from Z-test where K' and T' are dimensionless constants representing turning ability and responsiveness to the helm, respectively. In the Z-test under flap rudder angle 10°, the obtained K' value covered the range of 2.37-2.87 and T' was 1.74-3.45. Under the flap rudder angle 20°, K' and T' value showed 1.43-1.63, 1.0-1.73, respectively. In the spiral test, the loop width was unstable at +0.3° and -0.5°-0.9° around the midship of flap rudder. As a result, course stability was comparatively good. From the sea trial results, training ship ARA met the present criterion in the standards of maneuverability of IMO.

• 한국정밀공학회지
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• 제10권4호
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• pp.163-169
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• 1993

A flexible manipulator can move in the high speed even with the small driving torque. The dymanic equations of flexible manipulator which include 2 vibrational modes are derived using the clamped-free boundary condition. Simulation results of the 6th order model are well matched with experimental results. The hub angle of the flexible mainpulator can be controlled without vibration of the beam by the feedback of both hub angle and strain. The overshoot of the hub angle in the step response is reduced without sacrificing the rise time using the cycloidal function instead of the step function as the referenmce input.