• The Transactions of the Korean Institute of Power Electronics
• /
• v.5 no.2
• /
• pp.163-169
• /
• 2000

From the viewpoint of the cost effective design of power conversion systems, it is very important to fully u utilize the CillTent capacity of power devices over all circumstances. Therefore this paper deals with the l practical design of digital CillTent controller to meet the requirements of fast and overshoot free control r response over the varying control voltage bOlmds, the accompanied computational delay, and the system U W1certainties. The proposed controller consists of high gain PI control schemes using both the conditional i integrator and the modified delay compensator. The simulation and experimental results show the validity of t the proposed controller.

• Journal of Power System Engineering
• /
• v.3 no.1
• /
• pp.50-54
• /
• 1999

In order to reject the steady-state tracking error, it is common to introduce integral compensators in servosystems for constant reference signals. However, if the mathematical model of the plant is exact and no disturbance input exists, the integral compensation is not necessary. From this point of view, a two-degree-of-freedom(2DOF) servosystem has been proposed, in which integral compensation is effective only when there is modeling error for disturbance input. The present paper considers the design problem of 2DOF servosystem incorporating an observer. It is shown that if a state feedback gain and a observer gain satisfy a condition, the integral effect does not appear when modeling error or disturbance input exists. This result means that the servosystem does not behave as a 2DOF servosystem.

• Journal of Institute of Control, Robotics and Systems
• /
• v.17 no.4
• /
• pp.299-303
• /
• 2011

In this paper, we propose an output feedback controller for a chain of integrators system compensating measurement noise of feedback sensor. Measurement noise makes feedback signals distorted, and results in performance degradation or even system failure. Therefore, we need to design a robust controller to accommodate the possible measurement noise in the feedback information. Our controller is equipped with a gain-scaling factor to reject or minimize the effect of measurement noise in output feedback information. We give a theoretical analysis of the controlled system and illustrate the improved control performance via an example.

• Proceedings of the KIPE Conference
• /
• 2019.11a
• /
• pp.10-12
• /
• 2019

영구자석 동기 전동기는 높은 효율과 전력 밀도 등의 장점때문에 자동차나 엘리베이터 등 다양한 산업 분야에서 사용되고 있다. 영구자석 동기 전동기의 구동에는 여러가지 이유로 인해 고조파 토크 리플이 존재한다. 이러한 토크 리플은 속도 리플을 유발하여 소음이나 진동의 원인이 되며, 그 분포가 전동기의 구조나 운전점에 따라 변화하기 때문에 제어 성능에 매우 큰 영향을 준다. 본 연구에서는 영구자석 동기 전동기의 운전점에 따라 변화하는 토크 리플을 상쇄하기 위해 주입할 최적의 고조파 토크를 실시간으로 추적하는 방법을 제안한다. 제안된 방법에서는 속도 제어 중 토크 리플에 의해 발생하는 속도 리플을 적분하여 평가지표로 삼고, 속도 리플이 감소하는 방향으로 주입할 고조파 토크의 크기와 위상을 조정한다. 이 방법은 제정수 추출이나 회전자의 위치 별 토크 테이블 없이 운전 조건의 변화에 따라 토크 리플의 최적 보상점을 추적한다는 장점이 있다. 제안된 방법의 효과는 시뮬레이션을 통해 검증되었다.

• Proceedings of the Korean Society of Machine Tool Engineers Conference
• /
• 1999.05a
• /
• pp.205-209
• /
• 1999

This paper proposes a variable structure position controller for an induction motor(IM) which uses a reaching law and an integral compensating nonlinear switching function. With the reaching law, reaching mode can be established quantitatively during transient state so that dynamic control performance is improved. With the integral compensating nonlinear switching function, both very low overshoot and high steady state control accuracy can be obtained by compensating the states chattering problem due to the unmodelled dynamics of inverter and feedback sensors. For experiment a digital servo driver which consists of a DSP and an IPM inverter was developed. With the various experimental results, IM position control performance was verified.

• 한국신재생에너지학회:학술대회논문집
• /
• 2006.06a
• /
• pp.265-268
• /
• 2006

인버터의 개발에 앞서 살펴야 할 것 중 하나로 부하의 종류이다 여기에서는 유체부하를 가지는 경우이다 경제적인 측면과 성능을 고려하여 마이크로컨트롤러(PIC18F4431)를 결정하였다. 또한 여기에서는 전반적인 인버터의 제어를 다루기보다는 유체부하에서 발생하기 쉬운 과부하상태시의 간단한 제어방안을 다루었다 유도기제어에 있어서 유체부하를 가지는 경우 갑작스러운 유체부하의 증가가 발생할 수 있다. 유도기에서 이와 같은 과부하가 발생할 경우 전압과 전류의 위상차는 줄어들게 되고 전류는 증가하게 되며 유도기의 실제 속도와 인버터의 지령치는 벌어지게 된다. 지속적으로 위상차를 감시하여 과부하 상태를 판별할 수 있으며 과부하 상태 시 속도를 변화시켜 실제 속도를 정상상태와 비슷하게 유지시켜준다.

• Journal of Advanced Marine Engineering and Technology
• /
• v.33 no.8
• /
• pp.1268-1274
• /
• 2009

Various evaluation systems using simulators have been adopted widely for the purpose of training and examination, including marine engineering education area. This paper suggests a PC based evaluation scoring system for simulators where the operation ability of machineries and background knowledges of trainees or examinees are able to be assessed relatively. The scores are based on the 100 point resulted from their responses for a given evaluation scenario under a PID tuning simulation. The mistakes they make during the operation time are integrated firstly to get error sum, and the error sum is transformed secondly to 100 point score according to a formula where the knowledge level of examinee's groups can be compensated and considered reasonably. The implementation result of evaluation system for the given control loop is described and analyzed to show the effectiveness of the suggested configuration as an evaluation tool.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.37 no.7
• /
• pp.851-856
• /
• 2013

Recently, as the tactical environment has changedto one of network-centric warfare, where all components are connected through a network, much emphasis has been placed on the use of an artificial satellite for achieving high communication speeds. To provide a high-quality artificial satellite link, stabilization is very important in a platform. Previous stabilization control techniques used PI control, which is commonly used for vessels. However, for ground terminals that require a higher communication speed, the antenna should move faster to track an artificial satellite within a short period of time. Moreover, the terminals must be equipped with proper sensors and algorithms so that they can detect and compensate for external disturbances while tracking the artificial satellite. In this study, through the analysis of the dynamic model of an antenna system, a stabilization algorithm for ground terminals was proposed;this algorithm shows high isolation performance in the low-frequency range and includes $PI^2$ control.

• Journal of the Korea Institute of Information and Communication Engineering
• /
• v.15 no.8
• /
• pp.1797-1804
• /
• 2011

In this paper, I analyzed array organization of MIMO channel antenna and effect of operation environment by evaluating average BER from linear Space-Time Block Code orthogonal design and suggests designing condition of MT antenna for improved BER and the fading index m. To analyze system performance, I used M-PSK and M-QAM modulation, and to use analysis equations I used integrated by Nakagami fading variable, non-integrated Nakagami fading variable. We can get the organization of channel array by using mathematical calculation on matrix. STBE BER performance will decrease as AOA spreading decrease and such loss can be compensated from extending antenna spacing, and changing array organization.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.50 no.10
• /
• pp.709-716
• /
• 2022

In this paper the Gamma guidance law, which was used for IUS (Inertial Upper Stage), is applied for solid-motor guidance of a upper stage of a satellite launch vehicle. The RCS (Reaction Control System), which activates after burnout of the upper stage, is employed for the convergence of the guidance algorithm and compensation of velocity errors induced by the solid motor. The algorithm is also simplified by replacing the time-consuming numerical integration process to predict final vehicle states with Keplerian trajectories. The performance of the algorithm is evaluated by conducting 3-DOF computer simulations for off-nominal flight conditions. The numerical results show that Gamma guidance can reduce the orbit injection accuracy in comparison with that obtained by applying open-loop commands.