• 전력전자학회논문지
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• 제7권4호
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• pp.332-338
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• 2002

토카막 장치의 초전도 코일에 사용되는 전원 공급장치는 초대형급(20kA) 직류 전원 공급기로서 빠른 전류제어 응답성과 매우 작은 정상상태 리플이 필수적이다. 특히 역전류 공급이 가능한 회생형 컨버터의 운전중 전류 방향이 바뀌는 순간에도 전류기준값을 잘 추종하는 것이 중요하다. 이러한 조건들을 만족시키기 위하여 입력측에 2중 출력($\Delta$, Y)를 갖는 변압기와 출력단에 상간변압기(interphase transformer, IPT)를 이용한 12펄스 싸이리스터 듀얼 컨버터를 설계, 제작하였다. 각 컨버터에서 출력되는 전류의 합이 부하전류 지령치를 따르도록 제어하는 동시에 차 전류의 평균값이 영이 되도록 함으로써 각 컨버터의 부하 분담율을 일정하게 하여 상간 변압기의 포화를 방지한다. 대전류 코일 전류 공급장치의 양방향 전류 제어 성능을 높이기 위하여 위상각 검출 및 게이팅 지연각 구현을 디지털화하고 컨버터 전류방향 정역절환시 초기 응답특성을 개선하는 방법을 제안하였다. 또한 시뮬레이션과 실부하 전류실험을 통해 제안된 제어기의 동작성능을 확인하였다.

• 한국항행학회논문지
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• 제20권3호
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• pp.226-231
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• 2016

이동로봇의 제어는 로봇 분야에 있어 중요한 이슈이다. 이동로봇의 자율주행은 다양한 작업 환경에서 중시되고 있다. 자율 주행을 위해 이동로봇은 장애물을 감지, 회피하며 지능시스템을 도입한 제어 방식들을 사용해 충돌회피의 성능을 보완하는 연구가 활발히 진행되고 있다. 본 논문에서는 이동 로봇의 기구학적 모델을 분석하고 조향각 제어를 위한 type-2 fuzzy self-tuning PID 제어기를 설계하였다. Type-2 fuzzy 제어기는 type-1 fuzzy 제어기와 달리 복수 개의 값을 가지므로 언어표현의 모호함의 자유도가 높다. 본 논문에서는 설계된 제어기와 기존의 PID 제어기, type-1 fuzzy self-tuning PID 제어기를 비교하기 위한 방법으로 MATLAB Simulink를 사용하여 시뮬레이션을 하였다. 시뮬레이션 비교 결과 기존의 PID제어기와 type-1 fuzzy self-tuning PID 제어기의 성능보다 type-2 fuzzy self-tuning PID 제어기의 성능이 우수하다는 것을 확인하였다.

• 한국산학기술학회논문지
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• 제19권10호
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• pp.330-338
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• 2018

비례-적분-미분(PID) 제어기는 단순한 구조와 넓은 범위의 운전영역에서 견고한 성능으로 인해 산업계에서 널리 사용되고 있다. 그러나 제어대상으로서 AVR(Automatic Voltage Regulator)은 전력 시스템의 파라미터의 변동에 강인하지 않다. 따라서 PID 제어기를 사용하여 AVR 시스템의 안정성과 성능을 향상시키는 것이 필요하다. 본 논문에서는 PSO(Partial Swarm Optimization) 알고리즘을 사용하여 AVR 시스템을 위한 최적 PID 제어기 파라미터를 결정하는 새로운 설계 방법을 제시한다. 제안하는 접근법은 쉬운 구현뿐만 아니라 안정된 수렴 특성 및 양호한 계산 효율과 우수한 특성을 갖는다. 또한, 제안 된 PSO-PID 제어기의 성능을 평가하기 위해 새로운 목적함수를 정의한다. 이 목적함수는 최대백분율 오버슈트와 정정시간이 설계사양으로 주어진 경우 이를 반영하기 위한 것이다. 이를 위해 ITAE 평가함수에 제약 조건을 위반하면 벌점을 부과하도록 하여 PSO 알고리즘이 PID 제어기 파라미터를 탐색할 때 설계사양을 만족하도록 하게 한다. 최종적으로 컴퓨터 시뮬레이션을 통해 제안한 PSO-PID 제어기는 단자전압 계단응답에 대해 주어진 설계사양을 만족할 뿐만 아니라 다른 유사한 최근의 연구보다 더 우수한 제어 성능을 보임을 확인하였다.

• 한국군사과학기술학회지
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• 제18권5호
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• pp.498-509
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• 2015

The existing mobile antenna networks in the military use have been operated by the manual pointing between two antennas. The work presented here describes the study of ATPC(Automatic Tracking and Pointing Control) system between facing antennas and the related tracking and pointing performances. This system is able to automatically track the maximum RSSI(Received Signal Strength Indication) value from the source's RF(Radio Frequency) signal and then control for maintaining the LOS(Line of Sight) between two antennas. The system has three major units; the driving unit consisting of motors, harmonic drives and encoders, the sensor unit with a GPS(Global Positioning System) and AHRS(Attitude and Heading Reference System) and the control unit regulating all the tracking and pointing events. By using PI(Proportional and Integral) controller, this system is able to properly track and point the other antenna under the external disturbance like the wind load. Both the simulation and the experimental works have been successively carried out to prove the performances of the system.

• International Journal of Aeronautical and Space Sciences
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• 제11권3호
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• pp.167-174
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• 2010

The design, dynamics, and control allocation of tri-rotor unmanned aerial vehicles (UAVs) are introduced in this paper. A trirotor UAV has three rotor axes that are equidistant from its center of gravity. Two designs of tri-rotor UAV are introduced in this paper. The single tri-rotor UAV has a servo-motor that is installed on one of the three rotors, which enables rapid control of its motion and its various attitude changes-unlike a quad-rotor UAV that depends only on the angular velocities of four rotors for control. The other design is called 'coaxial tri-rotor UAV,' which has two rotors installed on each rotor axis. Since the tri-rotor type of UAV has the yawing problem induced from an unpaired rotor's reaction torque, it is necessary to derive accurate dynamic and design control logic for both single and coaxial tri-rotors. For that reason, a control strategy is proposed for each type of tri-rotor, and nonlinear simulations of the altitude, Euler angle, and angular velocity responses are conducted by using a classical proportional-integral-derivative controller. Simulation results show that the proposed control strategies are appropriate for the control of single and coaxial tri-rotor UAVs.

• Journal of Electrical Engineering and Technology
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• 제8권3호
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• pp.544-558
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• 2013

This paper proposes a simplified and efficient control scheme for Unified Power Quality Conditioner (UPQC) based on three-level (NPC) inverter capable to mitigate source current harmonics and compensate all voltage disturbances perturbations such us, voltage sags, swells, unbalances and harmonics. The UPQC is designed by the integration of series and shunt active filters (AFs) sharing a common dc bus capacitor. The dc voltage is maintained constant using proportional integral voltage controller. The shunt and series AF are designed using a three-phase three-level (NPC) inverter. The synchronous reference frame (SRF) theory is used to get the reference signals for shunt and the power reactive theory (PQ) for a series APFs. The reference signals for the shunt and series APF are derived from the control algorithm and sensed signals are injected in tow controllers to generate switching signals for series and shunt APFs. The performance of proposed UPQC system is evaluated in terms of power factor correction and mitigation of voltage, current harmonics and all voltage disturbances compensation in three-phase, three-wire power system using MATLAB-Simulink software and SimPowerSystem Toolbox. The simulation results demonstrate that the proposed UPQC system can improve the power quality at the common connection point of the non-linear load.

• 전자공학회논문지S
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• 제35S권12호
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• pp.36-45
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• 1998

본 논문은 브러시리스 직류 전동기의 속도제어를 위해 파라메타의 추정 없이 입력과 출력의 패턴을 관찰하여 PI 이득을 온라인(On-line)으로 설정하는 방법을 제안한다. 비례이득은 한계입력을 인가하여 가장 빠른 속도 상승을 유도하는 과정에서 설정되고, 적분이득은 비례제어 과정 중에 오버슈트 방지와 안정된 수렴이 적절히 이루어지도록 설정된다. 따라서 제안된 PI이득 조정은 온라인으로 제어와 동시에 수행됨으로써 시스템 파라메타 추정 등의 부가적인 작업이 필요 없다. 본 논문에서 제안하는 PI이득 조절기법은 직류전동기의 속도제어에 있어서 빠른 응답과 오버슈트 문제를 동시에 해결할 수 있고, 기존의 Auto-tuning 방법보다 간편하고 실용적이다. 컴퓨터 시뮬레이션과 실제 실험을 통하여 제안하는 방법의 유용성과 안정성을 보인다.

• International Journal of Aeronautical and Space Sciences
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• 제12권3호
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• pp.274-282
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• 2011

This paper is focused on dynamic modeling and control system design as well as vision based collision avoidance for multi-rotor unmanned aerial vehicles (UAVs). Multi-rotor UAVs are defined as rotary-winged UAVs with multiple rotors. These multi-rotor UAVs can be utilized in various military situations such as surveillance and reconnaissance. They can also be used for obtaining visual information from steep terrains or disaster sites. In this paper, a quad-rotor model is introduced as well as its control system, which is designed based on a proportional-integral-derivative controller and vision-based collision avoidance control system. Additionally, in order for a UAV to navigate safely in areas such as buildings and offices with a number of obstacles, there must be a collision avoidance algorithm installed in the UAV's hardware, which should include the detection of obstacles, avoidance maneuvering, etc. In this paper, the optical flow method, one of the vision-based collision avoidance techniques, is introduced, and multi-rotor UAV's collision avoidance simulations are described in various virtual environments in order to demonstrate its avoidance performance.

• Smart Structures and Systems
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• 제14권3호
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• pp.347-365
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• 2014

The main objective of this paper is to develop an innovative methodology for the vibration suppression control of the multiple degrees-of-freedom (MDOF) flexible structure. The proposed structure represented in this research as a clamped-free-free-free truss type plate is rotated by motors. The controller has two loops for tracking and vibration suppression. In addition to stabilizing the actual system, the proposed feedback control is based on a genetic algorithm (GA) to seek the primary optimal control gain for tracking and stabilization purposes. Moreover, input shaping is introduced for the control scheme that limits motion-induced elastic vibration by shaping the reference command. Experimental results are presented, demonstrating that, in the control loop, roll and yaw angles track control and elastic mode stabilization. It was also demonstrated that combining the input shaper with the proportional-integral-derivative (PID) feedback method has been shown to yield improved performance in controlling the flexible structure system. The broad range of problems discussed in this research is valuable in civil, mechanical, and aerospace engineering for flexible structures with MDOM motion.

• International Journal of Aeronautical and Space Sciences
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• 제12권3호
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• pp.252-259
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• 2011

This paper is focused on dynamic modeling and control system design as well as vision based collision avoidance for multi-rotor unmanned aerial vehicles (UAVs). Multi-rotor UAVs are defined as rotary-winged UAVs with multiple rotors. These multi-rotor UAVs can be utilized in various military situations such as surveillance and reconnaissance. They can also be used for obtaining visual information from steep terrains or disaster sites. In this paper, a quad-rotor model is introduced as well as its control system, which is designed based on a proportional-integral-derivative controller and vision-based collision avoidance control system. Additionally, in order for a UAV to navigate safely in areas such as buildings and offices with a number of obstacles, there must be a collision avoidance algorithm installed in the UAV's hardware, which should include the detection of obstacles, avoidance maneuvering, etc. In this paper, the optical flow method, one of the vision-based collision avoidance techniques, is introduced, and multi-rotor UAV's collision avoidance simulations are described in various virtual environments in order to demonstrate its avoidance performance.