• The Transactions of the Korean Institute of Power Electronics
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• v.14 no.1
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• pp.82-88
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• 2009

Low costed position sensor or sensorless control method is generally used in the motor control for home appliance because of the material cost and manufacture standard restriction. In conventional sensorless method, the stator resistance and back-EMF coefficient are varied by the motor speed and load torque variation. Therefore, position error occurred when the motor is operated by sensorless control method because of these variations. In this paper, the compensation method is proposed for sensorless position error using 2 hall sensors.

• Bulletin of the Korean Space Science Society
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• 2010.04a
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• pp.29.2-29.2
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• 2010

항법분야에 있어서 위성항법시스템의 다양한 오차를 제거한 정밀한 위치 정보를 이용하여 이동체에 활용하는 연구가 진행되고 있다. 실제 환경에서 이동체를 이용한 항법실험을 수행하기 전 실제 환경과 유사한 가상의 실시간 테스트베드를 구축하여 알고리즘 테스트 및 검증 실험을 수행하려 한다. 이를 위해 이동체의 운동을 시뮬레이션하는 운동궤적제어시스템과 실제의 항법신호를 시뮬레이션하는 GNSS 시뮬레이터 사이의 시각동기화는 실시간 시뮬레이션을 구현하기 위해 필수적으로 요구된다. 동기화 되지 않은 시각정보는 이동체 운동궤적제어시스템에 의해 생성된 실제의 궤적과 GNSS 시물레이터로부터 생성된 궤적사이의 오차를 유발하여 항법수신기의 부정확한 항법신호를 유발한다. 이 연구는 GNSS 시뮬레이터를 이용한 실시간 테스트베드의 구축에 있어 필요한 이동체 운동궤적의 시각동기화 기술 개발을 목표로 한다. GNSS 시뮬레이터는 Spirent 사의 GPS 시뮬레이터가 사용되었다. 이동체의 위치, 속도, 가속도와 같은 움직임을 나타내는 운동에 관한 명령은 적용되어야 하는 정확한 시각이 함께 전송되므로, 이는 그 시각 이전에 GPS 시뮬레이터에 도달해야 한다. 따라서 1초(1 Hz) 또는 0.1초(10 Hz) 사이에 원격제어시스템과 GPS 시뮬레이터사이의 시각 동기화를 구현하였다. 시뮬레이터와의 시각정보 동기화를 위해 Amplicon사의 PCI-215 타이머카드를 이용하였고, 그 결과, 이동체 운동궤적제어시스템과 시뮬레이터의 시각정보를 $10^{-3}$ 내의 위치오차를 가지는 정밀도로 동기화됨을 확인할 수 있었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.87-91
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• 2004

It is definitely required to control dispersion of the rocket engine performance in order to accomplish the mission of launch vehicle successfully. We performed the dispersion analysis of gas generator cycle LRE (liquid rocket engine) accompanied with ANASYN. As a result, the vacuum thrust dispersion of the engine was $+5.34\%,\;-5.27\%$ and the mixture ratio deviated $+9.07\%,\;-9.82\%$ from the nominal value due to the errors of components and engine inlet condition of propellants. By applying the gas generator regulator only, the dispersion of the engine performance increases. Error in turbine efficiency is the most influential factor to the dispersion of engine performance.

• The Journal of the Korea institute of electronic communication sciences
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• v.11 no.12
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• pp.1209-1218
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• 2016

In order to safely and speedily transport a load such as a large glass plate using four electric cylinders, the synchronous error outside the permitted range should not be continuously generated between the cylinders. In this study, a methodology of synchronous control which can be applied to synchronization of four or more cylinders is developed. The synchronous control system based on the decoupling structure is composed of a reference model, position and synchronous controllers in the respective cylinders. The reference model is used for calculating the decoupled synchronous error and control input for the each cylinder. The position controller of I-PD type is designed in order that the cylinder may follow the reference signal without overshoot and input saturation. And the synchronous controller of lead compensator is designed to achieve stable and accurate synchronization through loop shaping approach. Finally, the simulation results show that the synchronization between the four cylinders can be quickly and stably while each cylinder rod is transferred to the target point under torque disturbance.

• Journal of the Institute of Electronics Engineers of Korea TC
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• v.37 no.2
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• pp.91-97
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• 2000

Tn this paper, a novel control circuit applicable to the error sensor loop block in the feedforward linearizer system is proposed. The proposed control circuit is applied to the error sensor loop block, where in the 11dB power range, it operates stably, and makes main carrier signals to be eliminated more than 40dB below 3$\^$rd/ order IM level. In the operating point, the amplitude control error is 0.05∼0.12dB, and the phase control error is smaller than 0.02。. It is verified theoretically as well as experimentally that the control circuit can precisely compensate the variation of nonlinear characteristics in a high power amplifier, due to the variations of input power, operating temperature, humidity and the other system environments.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.10
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• pp.1171-1179
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• 2012

In this study, we consider a dynamic positioning system (DPS) design problem that can be extended to many application fields. Toward this end, tracking and positioning control problems are discussed. In particular, we design a tracking control system that incorporates an observer based on the 2-DOF servo system design approach in order to obtain the desired state information. In the case of observer design, a weighted $H_{\infty}$ error bound approach for a state estimator is considered. Based on an algebraic Riccati equation (inequality) approach, a necessary and sufficient condition for the existence of a full-order estimator that satisfies the weighted $H_{\infty}$ error bound is introduced. The condition for the existence of the estimator is denoted by a linear matrix inequality (LMI) that yields an optimized solution and the observer gain.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.36 no.3
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• pp.257-265
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• 2000

Brushless DC(BLDC) motors are widely used as AC servo motors in factory automation fields because of their quick instantaneous mobility, good energy saving efficiency and easiness of design for control system comparing with induction motors. Recently, a Two-Degree-of-Freedom(2DOF) PI control law has been adopted to some application parts to accomplish an advanced speed control of BLDC motors. The method can treat the two conflicting performances, minimum tracking errors versus reference inputs without large overshoot and rejection of some disturbances including modeling errors, independently. However, the method can not design the optimal system which is able to minimize tracking errors and energy consumption simultaneously. In this paper, a 2DOF integral type optimal servo control method is investigated to promote the speed control performances of BLDC motors considering energy consumption. In order to applicate the method to the speed servo system of the BLDC motor, the motor is modeled in the state space using the vector control and decoupling technique. To verify the validity of the suggested method, some simulations and experiments are performed.

• Journal of IKEEE
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• v.13 no.1
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• pp.36-40
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• 2009

In control of time delay systems, if the informations about the system model and the disturbance can be estimated exactly, the ideal response can be achieved by using Smith predictor controller. Therefore, in this paper, an adaptive algorithm is proposed to control time delay systems existing modelling errors and disturbance. An adaptive observer to estimate disturbance and system model is designed and adaptive laws adjusting the observer are proposed. The new Smith predictor controller is designed using the proposed adaptive observer. As a result, the proposed controller can eliminate the effects of the disturbance and the modelling error. The effectiveness and the improved performance of the proposed system are verified by computer simulation.

• The Journal of the Korea institute of electronic communication sciences
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• v.7 no.4
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• pp.839-848
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• 2012

In this paper, we propose a robust control scheme of AC servo motors to suppress disturbance torques effectively. The proposed controller consists of both a model based feed-forward controller and a stabilizing feedback controller. The feed-forward controller is designed such that the output of the nominal plant tracks perfectly the reference velocity command with desired dynamic characteristics. The feedback controller stabilizes the overall closed loop system. Furthermore, the feedback controller contains a free function that can be chosen arbitrarily. The free function can be designed so as to achieve both suppression of disturbances and robustness to model uncertainties. In order to illuminate the superior performance of the proposed control scheme to the conventional ones, we present some simulation results.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.4
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• pp.34-42
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• 2004

In this paper, a double gimbal is used for roll/yaw attitude control of spacecraft and two feedback controllers are designed. One is a PD controller of no phase difference between roll and yaw control input. The other is a PD controller with a phase lag compensator about the yaw control input. The phase lag compensator is designed a first order system and a lag parameter is designed for the control of yaw angle. There are two case simulations for each of controllers; constant disturbance torques and initial errors of nutation. We obtain the results through simulations that a steady-state error and a rising time of yaw angle are developed by the compensator. In this paper, simulation parameters use the values of KOREASAT 1.