• 조명전기설비학회논문지
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• 제28권12호
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• pp.95-102
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• 2014

This paper proposes a coordinated control for an independent multi-phase transverse flux linear synchronous motor (IM-TFLSM) based on magnetic levitation. The stator structures of the IM-TFLSM are composed of a two set, which has independent three-phase windings and a double-sided air-gap as opposed to the conventional Y-connected three-phase linear motors. A suitable control algorithm is necessary to operate the applied linear machine. This study proposes a coordinated control algorithm for adjusting the mover air-gap and thrust force of the IM-TFLSM in order to maintain air-gap and phase shifted current control of the independent 3-phase modules. In addition, the principle of operation and its special structures are described in detail and the validity and effectiveness of the control algorithm is verified through multiple experimental results.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2000년도 하계학술대회 논문집 B
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• pp.653-655
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• 2000

A moving-coil-type linear oscillatory actuator(LOA) consists of the NdFeB permanent magnets with high specific energy as the stator. a coil-wrapped nonmagnetic hollow rectangular structure. LOA system have the push/pull effect caused by the unbalanced magnetic field. In order to eliminate the unbalanced thrust, we propose the control algorithm and construct the LOA driver. As a results, we obtain the balanced oscillating thrust.

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제55권1호
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• pp.21-26
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• 2006

This paper deals with the dynamic analysis and experiments of moving-magnet linear actuator with/without spring. On the basis of two dimensional (2-D) analytical solutions and experiments, control parameters such as thrust constant, back-emf constant, inductance and resistance are obtained. And then, dynamic simulation algorithm is established from the voltage and motion equation. Finally, for various values of frequency, dynamic simulation results for characteristics of current and displacement of moving-magnet linear actuator with and without spring are presented and confirmed through the experiments. In particular, This paper applies the PWM voltage waveform obtained from a DSP for bidirectional voltage drive to the actuator.

• 대한조선학회논문집
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• 제54권2호
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• pp.102-112
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• 2017

Many studies on dynamic positioning control algorithms using fixed feedback gains have been carried out to improve station keeping performance of dynamically positioned vessels. However, the control algorithms have disadvantages in that it can not cope with changes in environmental disturbances and response characteristics of vessels motion in real time. In this paper, the Fuzzy Gain Scheduling - PID(FGS - PID) control algorithm that can tune PID gains in real time was proposed. The FGS - PID controller that consists of fuzzy system and a PID controller uses weighted values of PID gains from fuzzy system and fixed PID gains from Ziegler - Nichols method to tune final PID gains in real time. Firstly, FGS - PID controller, control allocation algorithm, FPSO and environmental disturbances were modeled using Matlab/Simulink to evaluate station keeping performance of the proposed control algorithm. In addition, simulations that keep positions and a heading angle of vessel with wind, wave, current disturbances were carried out. From simulation results, the FGS - PID controller was confirmed to have better performances of keeping positions and a heading angle and consuming power than those of the PID controller. As a consequence, the proposed FGS - PID controller in this paper was validated to have more effectiveness to keep position and heading angle than that of PID controller.

• 한국추진공학회지
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• 제11권4호
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• pp.52-58
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• 2007

하이브리드 로켓의 연소 가시화에 의하면 연소 후 연료 표면이 고르게 연소되지 못한 것을 확인할 수 있었다. 검은색의 불규칙한 연료 표면은 국부적으로 산화제가 부족해서 생긴 현상이다. 실험조건은 산화제 공급이 충분히 이루어진 상태였으므로 불완전 연소가 산화제 유동 조건과 관련이 있는가를 검증하기 위하여 여러 가지의 산화제 유동 환경을 설정하여 실험하였다. 실험결과에 의하면, 산화제 유동이 불안정한 연료표면에 영향을 줄 수 있지만 근본적인 발생 원인이 아닌 것을 알 수 있었다. 또한 다른 추진제를 사용하는 하이브리드 로켓 실험에서도 비슷한 현상이 발견되고 있는 점을 볼 때 이러한 불안정한 연소는 하이브리드 로켓의 연소에서 발생하는 공통적인 현상임을 확인하였다. 이는 연료가 기화하는 분출 유동과 산화제 유동이 혼합할 때 경계층이 교란되어 나타난 결과로 판단된다.

• 제어로봇시스템학회논문지
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• 제1권2호
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• pp.94-98
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• 1995

This paper proposes an optimal design method for the weight and cost of a moving magnet typer linear DC motor (MM-LDM). The optimal design condition such as type and size of MM-LDM were determined by the trinary search algorithm after adjusting a standard function and its related parameters. In order to verigy results of the optimal design by the computer simulation, the designed values such as a thrust, a current, a velocity, and etc. of the fabricated MM-LDM were measured. And the measurement results are in good agreement with the designed ones.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.1095-1098
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• 2005

Most electronic chassis control systems until today have been designed with optimization on its own performance. However, According to the increase of the interest regarding a vehicle safety and development of information technique, the integration technique of current chassis systems is being emphasized. Each enterprise proposed it with name of GCC(Global Chassis Control) or UCC(Unified Chassis Control). This study realizes control algorithm of suspension and brake by using the vehicle model of low degree of freedom as the primary stage of realization of integrated chassis control system. The proposed algorithm build the simulation environment connected to the CarSim having full vehicle model of 27 degree of freedom for raising the thrust of results

• 한국추진공학회지
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• 제15권4호
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• pp.73-78
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• 2011

가스발생기 사이클 액체로켓 엔진의 보정이나 제어를 위해 제어밸브를 적용하는 경우 제어밸브의 고유유량특성을 제어 대상값인 추력이나 혼합비와 선형적인 관계를 가지도록 선정함으로써 제어를 간단하면서도 예측가능한 형태로 가져갈 수 있다. 이에 본 연구에서는 기존에 개발된 엔진 모드해석 프로그램을 응용하여 추력 제어밸브와 혼합비 제어밸브의 고유유량특성을 계산하기 위한 알고리즘을 제안하였으며, 제어밸브의 스로틀 각에 따른 민감도를 계산하였다. 계산된 제어밸브의 고유유량특성을 해외사례와 운용범위에서 그 곡선의 형태를 비교하여 결과의 타당성을 검토하였다.

• 전자공학회논문지CI
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• 제41권2호
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• pp.103-112
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• 2004

본 논문에서는 터널 굴진기의 모든 조작이 시스템 운용자에 의해 수동으로 운용 되고 있는 방법을 개선하여 터널 굴진기의 토크/추력 및 송/배니압을 자동으로 제어하는 방법을 제안한다. 이를 위하여 본 연구에서는 굴진 운용자의 토크/추력 및 송/배니압의 수동 제어 방법에 대해 체계적인 분석을 하였고 이를 바탕으로 퍼지 제어기와 경고 및 긴급 정지를 위한 제어기를 설계하였다. 제안된 시스템은 전문가 규칙으로부터 퍼지 규칙을 추출하였기 때문에 시스템 운용자들의 숙련된 제어 방법을 그대로 따르면서 시스템의 변화에 신속하게 대응할 수 있다. 따라서 복잡한 환경에서 전문가의 역할을 대신할 수 있으며 기존에 운용자의 인지능력의 한계로 인해 시스템의 상태 변화에 빠르게 대응하기 어려웠던 점을 해결할 수 있다.

• Advances in aircraft and spacecraft science
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• 제9권5호
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• pp.433-447
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• 2022

This work deals with an explicit guidance and control architecture for autonomous lunar ascent and orbit injection, i.e., the locally-flat near-optimal guidance, accompanied by nonlinear reduced-attitude control. This is a new explicit guidance scheme, based on the local projection of the position and velocity variables, in conjunction with the real-time solution of the associated minimum-time problem. A recently-introduced quaternion-based reduced-attitude control algorithm, which enjoys quasi-global stability properties, is employed to drive the longitudinal axis of the ascent vehicle toward the desired direction. Actuation, based on thrust vectoring, is modeled as well. Extensive Monte Carlo simulations prove the effectiveness of the guidance, control, and actuation architecture proposed in this study for precise lunar orbit insertion, in the presence of nonnominal flight conditions.