• 조명전기설비학회논문지
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• 제23권4호
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• pp.72-78
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• 2009

이 논문은 국내 원자력 발전소에서 급수펌프 구동용 소형 터빈의 아날로그 제어시스템을 디지털 방식으로 교체한 후 발전소를 기동하기 전에 최초 제어 파라미터를 설정하는 방법에 대하여 기술하고 있다. 기존 제어시스템의 제어상수가 알려져 있는 경우에는 초기 제어상수를 쉽게 결정할 수 있으나 보통은 아날로그 시스템의 제어상수를 파악할 수 없는 경우가 많으며 이 때 초기 제어상수와 최적 제어상수는 크게 차이가 날 수도 있다. 이런 경우에는 발전소 자체의 기동이 위험한 경우도 발생할 수 있다. 매우 간단한 실험이지만 제어기술자가 플랜트를 기동하기 위해서 매우 유용한 방법과 실제로 이를 적용한 사례에 대하여 기술한다.

• 제어로봇시스템학회논문지
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• 제19권4호
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• pp.285-289
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• 2013

In switching from the track-seeking or track-jumping control mode to track-following control mode in hard disk drives or optical disk drives, initial values of the feedback controller are tuned to improve the transient response. In general, all the initial values of the controller have been compensated for this purpose. In this paper, by partially compensating initial values of digital controllers, we achieve a good performance of the transient response. In the proposed method for IVC (Intial Value Compensation), LMIs (Linear Matrix Inequalities) are used, which includes conditions for improving the performance of the transient response such as reducing a tracking error and control efforts. We obtain optimal initial values of the controller by solving an optimization problem with constraints represented by only one LMI. Although initial values of the controller are partially compensated, we can show that not only a sufficient performance of the transient response is obtained but also control efforts are diminished. The feasibility of the method is verified by simulation studies.

• 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.

• 전기학회논문지
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• 제66권10호
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• pp.1523-1531
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• 2017

In general, the thrust vector control should be fast and stable in the initial launch phase. Two types of conventional controllers, one is for pitch angle control and the other is for pitch rate control, are designed based on the equation of motion without aerodynamics and are compared in the viewpoints of the stability margin and the time response performance. Also analyzed are the rejection capabilities to cope with high aerodynamic disturbances caused by high angle of attacks in initial booting phase. Additionally, time response features at actuator saturation are investigated. Based on those results, we suggest a controller structure which is more suitable for thrust vector control of missiles at initial booting phase.

• 제어로봇시스템학회논문지
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• 제4권5호
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• pp.608-615
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• 1998

In this paper a second-order iterative learning control algorithm with feedback is proposed for the trajectory-tracking control of nonlinear dynamic systems with unidentified parameters. In contrast to other known methods, the proposed teaming control scheme utilize more than one past error history contained in the trajectories generated at prior iterations, and a feedback term is added in the learning control scheme for the enhancement of convergence speed and robustness to disturbances or system parameter variations. The convergence proof of the proposed algorithm is given in detail, and the sufficient condition for the convergence of the algorithm is provided. We also discuss the convergence performance of the algorithm when the initial condition at the beginning of each iteration differs from the previous value of the initial condition. The effectiveness of the proposed algorithm is shown by computer simulation result. It is shown that, by adding a feedback term in teaming control algorithm, convergence speed, robustness to disturbances and robustness to unmatched initial conditions can be improved.

• Journal of Power Electronics
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• 제9권3호
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• pp.499-506
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• 2009

In this paper, the initial pole-position estimation of a surface (non-salient) permanent magnet synchronous motor is mathematically analyzed and surveyed on the basis of simulation analysis, and developed for accurate servo motor drive. This algorithm is well carried out under the full closed-loop position control without any pole sensors and is completely insensitive to any motor parameters. This estimation is based on the principle that the initial pole-position is simply calculated by the reverse trigonometric function using the two feedback currents in the full closed-loop position control. The proposed algorithm consists of the predefined reference position profile, the information of feedback currents, speed, and relative position, and the reverse trigonometric function for the initial-pole position estimation. Comparing with the existing researches, the mathematical analysis is introduced to get a more accurate initial pole-position of the surface permanent magnet motor under the closed-loop position control. It is found that the proposed algorithm can be easily applied in servo drive applications because it satisfies the following user's specifications; accuracy and moving distance.

• 전력전자학회논문지
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• 제27권6호
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• pp.481-488
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• 2022

This study proposes compensation methods for the initial position error and torque ripple in vector control of two-phase hybrid stepping motors. Stepping motors have an asymmetrical structure due to misalignment, such as the eccentricity generated by the manufacturing and assembly process. When vector control is applied using the position information measured by an incremental encoder attached to the rotor shaft of such stepping motors, the following problems occur. First, an initial position error occurs during the forced excitation process for the initial rotor position alignment. Second, torque ripple corresponding to the mechanical rotation frequency is generated. In this study, these non-ideal phenomena that occur in vector control of the stepping motor are analyzed, and compensation methods are proposed to eliminate them. The validity of the proposed initial position error and torque ripple compensation methods is verified through experiments on a two-phase hybrid stepping motor drive system.

• 산업경영시스템학회지
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• 제32권1호
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• pp.94-101
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• 2009

Complex Products may present more than one type of defects and these defects are not always of equal severity. These defects are classified according to their seriousness and effect on product quality and performance. Demerit systems are very effective systems to monitoring the different types of defects. So, classical demerit control chart used to monitor counts of several different types of defects simultaneously in complex products. S.M. Na et al.(2003) proposed the Demerit-CUSUM for the improvement of the demerit control chart performance and Nembhard, D. A. et al.(2001) and G.Y Cho et al.(2004) developed a Demerit control chart using the EWMA technique and evaluated the performance of the control chart. In this paper, we present an effective method for process control using the Demerit-CUSUM with fast initial response. Moreover, we evaluate exact performance of the Demerit-CUSUM control chart with fast initial response, Demerit-CUSUM and Demerit-EWMA according to changing sample size or parameters.

• 대한공업교육학회지
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• 제32권2호
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• pp.199-216
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• 2007

SCTP(stream control transmission protocol)는 데이터 전송을 위한 전송 계층 프로토콜로서, 많은 부분에서 TCP(transmission control protocol) 방식을 따른다. 하지만 멀티 호밍(multi-homing)과 멀티 스트리밍(multi-streaming)의 특징을 가짐으로 성능의 차이를 갖는다. 이 논문에서는 SCTP 혼잡제어 중에서 초기 슬로우 스타트 단계에 초점을 맞추어 데이터 전송을 분석하고, 대역폭, 지연시간 및 데이터 크기에 따른 SCTP와 TCP 평균 전송 시간을 측정하고 비교하였다. 아울러 SCTP와 TCP의 평균 전송시간에 영향을 미치는 요인인 초기 윈도우 크기를 데이터 크기에 따라 측정하였다. 실험을 위한 서버와 클라이언트 프로그램은 SCTP socket API를 이용하여 C 언어로 작성되었고, 전송 시간은 이더리얼 프로그램을 사용하여 측정되었다. 서버와 클라이언트 사이의 데이터 전송 방법은 라운드 로빈(round robin) 방법을 사용하였다. 실험 결과, SCTP는 초기 슬로우 스타트 단계에서 TCP 보다 평균 전송 시간에 있어 약 15% 정도 향상된 성능을 보였으며, 그 이유는 SCTP 초기 윈도우 크기가 TCP 보다 크기 때문으로 확인되었다.

• 한국군사과학기술학회지
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• 제16권2호
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• pp.101-110
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• 2013

This paper considers the many kinds of attitude control systems including launcher. JVC(Jet vane control), Jet tap, Jetvator and Movable nozzles are used to control the initial attitude of a missile only. Recently side jet thruster and it's applications to control initial turn and to maneuver at high altitude have been increased. How to design and develop the missile for an initial turn and a high maneuver at high altitude using side jet thrust were described in this paper.