• Transactions of the Korean Society of Mechanical Engineers A
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• v.41 no.9
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• pp.869-876
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• 2017

Analysis of actuating forces and joint reaction forces are essential to determine the capacity of actuators, to control the mechanical system and to design its components. This paper presents an algorithm that calculates actuating forces(or torques), depending on the various types of driving constraints, in order to produce a given system motion in the joint coordinate space. The joint coordinates are used as the generalized coordinates of a kinematic system. System equations of motion and constraint acceleration equations are transformed from the Cartesian coordinate space to the joint coordinate space using the velocity transformation method. A numerical example is carried out to verify the algorithm proposed.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.923_924
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• 2009

본 논문에서는 소용량의 직류단 캐패시터를 가지는 교류전동기 구동 시스템의 전류 주입 방식 기반의 새로운 입력 전류 고조파 저감 방법에 대해 논의한다. 소용량 직류단 캐패시터를 가지는 전동기 구동 시스템의 가격 및 부피의 경쟁력을 유지하면서 주어진 고조파 규제를 만족시킬 수 있도록, 최소의 비용 추가로 입력 전류의 고조파를 저감하기 위한 새로운 회로를 제안하고, 제안된 회로를 이용하여 최적의 성능을 얻을 수 있는 제어 방법을 소개한다. 제안된 회로 구성 및 제어 방법의 타당성은 실험을 통하여 검증한다.

• Transactions of the Korean Society of Automotive Engineers
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• v.6 no.5
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• pp.138-145
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• 1998

Recently, TCS(Traction Control System) is attracting attention, because it maintains traction ability and steerability of vehicles on low-$\mu$ surface roads by controlling the slip rate between tire and road surface. The development of TCS control law is difficult due to the highly nonlinearity and uncertainty involved in TCS. A fuzzy logic approach is appealing for TCS. In this paper, fuzzy logic controller for TCS is introduced and evaluated by the computer simulation with 8 DOF vehicle model. The result indicate that the fuzzy logic TCS improves vehicle's stability and steerability.

• Proceedings of the KIPE Conference
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• 2017.07a
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• pp.395-396
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• 2017

차세대 고속 이동수단에 필요한 고전력 전동기에 대한 관심이 꾸준히 증가하는 추세이다. 본 논문에서는 고전력 동기전동기(PMSM) 구동에 필요한 전력 인버터의 제어 및 센서리스 제어기법을 적용한 자속 기준 제어(Field-oriented control)를 시뮬레이션을 통해 입증하였다. 고전력에서 인버터 스위치의 전력부담을 줄이기 위해 3-레벨 인버터를 설계하고, 벡터 제어 SVPWM 방식을 적용하였으며 고전력 및 고속 PMSM의 파라미터에 맞추어 센서리스(sensorless) 제어기를 설계하였다. 센서리스 제어에는 모델 기준 적응 시스템(MRAS)을 통해 속도 및 위치를 예측하여 모터를 제어하는 방식을 적용하였다. 가속시 5초간 가가속도 값을 적용하여 필요 토크 및 속도제어를 Matlab/Simulink에서 설계 및 구현하고, 예측속도와 실제 모터속도는 최대 0.01 rad의 오차를 나타났고, 67초 동안 목표 속도 500 rad/s까지 가속함을 확인하였다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.7 no.1
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• pp.83-95
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• 1983

원판의 진동은 위치 좌표에 따라 진동변위 및 속도가 달라질 뿐 아니라, 또한 여러 진동모우드를 포함하고 있다. 이러한 특성을 갖는 시스템의 진동을 감소시키기 위해서는 진동 제어력을 발생시 켜주는 구동장치와 진동변수를 측정하는 측정장치를 어느 위치에 두느냐가 무엇보다도 중요하다. 더구나 여러 진동 모우드를 동시에 최적으로 제어하기 위해서는 진동 모우드 개수 만큼의 많은 측정장치가 필요하게 되는데 이러한 난점을 해결하기 위해서 본 논문에서는 측정장치의 역할을 대신해 주는 관측기(observer)를 부착하여 측정장치의 필요 개수를 줄였다. 최적제어 이론을 바탕 으로 구동 장치와 측정장치의 위치를 최적으로 결정하였고, 제어기의 제어상수를 최적으로 설계 하였다. 이와 같이 설계된 최적 제어 시스템의 제어효과를 평가해 보기 위해서 원판의 진동을 예 를 들어 시뮬레이션해 보았는데 그 결과를 자세히 기술하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.2
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• pp.144-152
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• 2011

This paper presents a new scheme for fault detection and isolation in the satellite system. The purpose of this paper is to develop a fault detection, isolation and diagnosis algorithm based on the bank of interacting multiple model (IMM) filter for both total and partial faults in a satellite attitude control system (ACS). In this paper, IMM are utilized for detection and diagnosis of anticipated actuator faults in a satellite ACS. Other fault detection, isolation (FDI) schemes using conventional IMM are compared with the proposed FDI scheme. The FDI procedure is developed in two stages. In the first stage, 11 EKFs actuator fault models are designed to detect wherever actuator faults occur. In the second stage of the FDI scheme, two filters are designed to identify the fault type which is either the total or partial fault. An important feature of the proposed FDI scheme can decrease fault isolation time and figure out not only fault detection and isolation but also fault type identification.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.28 no.8 s.227
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• pp.1203-1211
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• 2004

A traction control systems (TCSs) composed of either a wheel slip controller or a throttle valve controller or an integrated controller of both systems are proposed in this study. To validatethe dynamic characteristics of a vehicle and TCS, a full car model that can simulate the responses of both front wheel drive (2WD) and four wheel drive (4WD) vehicle is also developed. The wheel slip controller uses a sliding mode control scheme and the throttle valve is controlled by a PID controller. The results shows that tHe brake TCS and the engine TCS achieve rapid acceleration, and reduce slip angle on slippery road. When a vehicle is cornering and accelerating maneuver with the brake or engine TCS, understeer or oversteer occur, depending on the driving conditions. The integrated TCS prevents most of these problems and improves the stability and controllability of the vehicle.

• The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.9 no.6
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• pp.57-64
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• 1995

This paper deals with the modeling and simulation to control the torque and speed of an induction motor using field-oriented control methods. Rotor flux is estimated using the indirect sensing method based on the rotor circuit equation in the synchronously rotation reference frame, and slip angle and rotor position are calculated from rotor angular velocity and stator current. As results of modeling and digital simulation with a voltage source inverter, it is shown that the proposed scheme gives good static and dynamic performance to the induction motor drive.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.913-914
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• 2017

Structural analyses of a engine system is required in development stage for increasing structural reliability and reducing weight. Attitude of a launch vehicle during flight is controlled by combustion chamber rotation varying with TVC (thrust vector control) actuator displacements. In this study nonlinear static analysis is performed for a 75 tonf-class liquid rocket engine using before and after the TVC actuation.

• Journal of Biomedical Engineering Research
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• v.24 no.2
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• pp.127-132
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• 2003

In this paper. the pneumatic service robot with a hybrid type is developed. A pneumatic has the advantages of good compliance , high Payload-to-weight and payload-to-volume ratios. high speed and force capabilities. Using pneumatic actuators. which have low stiffness. the service robot can guarantee safety. By suggesting a new serial-parallel hybrid type for the service robot which separates into Positioning motion and orienting motion, we can achieve large workspace and high strength-to-moving-weight ratio at the same time. A sliding mode controller can be designed for tracking the desired output using the Lyapunov stability theory and structural properties of pneumatic servo systems. Through many experiments of circular trajectory. the Pneumatic service robot is evaluated and verified.