• 대한전기학회논문지
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• 제37권6호
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• pp.376-382
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• 1988

A small-signal low-frequency disturbance of the input line affects the regulated-output voltage of the series resonant converter. To mitigate the detrimental effect, the output feedback PI-controller is employed. Small-signal linear models are represented to characterize the closed loop series resonant converter system. Design equations for the PI-controller which satisfy stability and percent ripple conditions are derived from the closed-loop linear model. Experimental results are presented which show excellent correlation with theory.

• Advances in aircraft and spacecraft science
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• 제4권2호
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• pp.145-167
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• 2017

The presented paper gives an overview of several projects addressing the experimental characterization and control of the buffet phenomenon on 3D turbulent wings in transonic flow conditions. This aerodynamic instability induces strong wall pressure fluctuations and therefore limits flight domain. Consequently, to enlarge the latter but also to provide more flexibility during the design phase, it is interesting to try to delay the buffet onset. This paper summarizes the main investigations leading to the achievement of open and closed-loop buffet control and its experimental demonstration. Several wind tunnel tests campaigns, performed on a 3D half wing/fuselage body, enabled to characterize the buffet aerodynamic instability and to study the efficiency of innovative fluidic control devices designed and manufactured by ONERA. The analysis of the open-loop databases demonstrated the effects on the usual buffet characteristics, especially on the shock location and the separation areas on the wing suction side. Using these results, a closed-loop control methodology based on a quasi-steady approach was defined and several architectures were tested for various parameters such as the input signal, the objective function, the tuning of the feedback gain. All closed-loop methods were implemented on a dSPACE device able to estimate in real time the fluidic actuators command calculated mainly from the unsteady pressure sensors data. The efficiency of delaying the buffet onset or limiting its effects was demonstrated using the quasi-steady closed-loop approach and tested in both research and industrial wind tunnel environments.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1995년도 가을 학술발표회 논문집
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• pp.242-249
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• 1995

In order to search more efficient structural control algorithm, several closed-loop algorithm are developed. Among those, feedback control algorithm using parameters as displacement velocity, and acceleration has been studied. In this paper, especially the characteristics of accleration feedback is studied as more efficient control algorithm than any others. Furthermore the fact that ATMD with acceleration feedback system further reduce the variance of structural displacement rather than with displacement or velocity feedback system will be examined and proved.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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• pp.907-912
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• 1989

A new procedure is presented for optimally placing closed-loop poles of multivariable continuous-time systems in specified regions via linear-quadratic(LQ) state-feedback design. This method has the advantages of pole-placement and LQ-design. In addition, it provides minimum feedback gains in the control law.

• 한국통신학회논문지
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• 제29권4A호
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• pp.429-438
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• 2004

본 논문에서는 WCDMA 시스템을 위한 판정궤환 동기식 동기추적 회로 (decision-feedback coherent code tracking loop)를 설계하고 AWGN 환경과 페이딩 환경에서 위상 에러와 심볼 에러의 영향을 고려하여 지터 분산을 해석한다. 먼저, AWGN 환경에서의 지터 분산을 위상 에러와 비트 오율을 포함하여 펄스성형 필터(pulse-shaping filter), 타이밍 오프셋 (timing offset), 신호 대 잡음비 (signal-to-interferences ratio), 루우프 대역폭(loop-bandwidth)에 대한 일반식으로 유도하고 페이딩 환경에서 지터 분산의 상한치 (upper bonnd)를 유도한다. 끝으로, WCDMA 순방향 링크의 DPCH 프레임 포맷 #13을 목표 시스템(target system)으로 설정하여 2차 동기식 등기추적 회로를 설계하고 AWGN 환경과 Rayleigh 페이딩 환경에서 지터 분산의 이론치와 시뮬레이션 결과를 비교, 분석한다.

• 한국통신학회논문지
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• 제30권10A호
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• pp.906-911
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• 2005

본 논문에서는 제한된 피드백 정보를 사용하는 공간 다중화 기법에 사용될 수 있는 부 공간 방식 기반 preceding 기법을 제안한다. 제안된 preceding 기법은 수신기에서 다수의 공통 기저 집합(common basis sets)으로 부터 용량을 최대로 하는 기저들을 선택하고, 선택된 기저들은 feedback 정보를 통해 송신기에 전달되곤 송신기에서는 선택된 기저들로 이루처진 preceding 행렬을 구성한다. 선택된 기저들은 해당 기저들이 속한 기저 집합의 index에 대한 feedback 정보와 선택된 기저 집합에서 각 기저들의 선택 여부에 대한 feedback 정보를 통해 송신기로 feedback된다. 선택된 기저 집합 index는 송수신기가 약속한 공통 기저 집합 중에서 해당 MIMP 채널의 부 공간의 좌표(coordinate)에 가장 적합한 좌표를 나타내고, 해당 좌표에서 상당한 양의 에너지를 포함하는 기저들을 선택함으로써 적은 feedback 정보량으로 MIMO 채널을 묘사한다. 시뮬레이션을 통해 제안된 부 공간 방식 기반 preceding 기법이 적은 feedback 정보량을 사용하면서 폐루프 MIMO 용량 (closed-loop MIMO capacity)에 근접하는 용량을 제공함을 보인다.

• 로봇학회논문지
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• 제15권1호
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• pp.77-89
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• 2020

This paper proposes a simple and intuitive model-free torque-tracking control for rotary electro-hydraulic actuators. The undesirable natural-velocity-feedback effect is discussed by introducing mechanical impedance into the electro-hydraulic actuation system. The proposed model-free torque control comprises inner- and outer-loop control to achieve two control objectives. Inner-loop control reduces the mechanical impedance passively and optimally. To improve the tracking accuracy, a certain form of proportional-integral-derivative control is applied to the outer loop. The robustness of the proposed closed-loop system against external disturbances is demonstrated by transforming the two-loop control structure into a disturbance observer form. The proposed method is validated on a single joint electro-hydraulic actuator.

• 한국정밀공학회지
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• 제12권10호
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• pp.157-165
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• 1995

The new formulation of designing the two degree of freedom(TDF) robust controller is proposed using $H_{\infty}$optimization and model matching method. In this formulation the feedback controller and feedforward controller are designed in a single step using $H_{\infty}$optimization procedure. Roughly speaking, the feedback controller is designed to meet robust stability and disturbance rejection specifications, while the feedforward controller is used to improve the robust model matching properties of the closed loop system. The proposed formulation will be illustrated and evaluated on a seeker scan-loop. And the performances of TDF robust controller are compared with those of the $H_{\infty}$ controller designed using Loop Shaping Design Procedure proposed by McFarlane and Glover.lover.

• International Journal of Naval Architecture and Ocean Engineering
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• 제9권5호
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• pp.525-536
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• 2017

Course keeping is hard to implement under the condition of the propeller stopping or reversing at slow speed for berthing due to the ship's dynamic motion becoming highly nonlinear. To solve this problem, a practical Maneuvering Modeling Group (MMG) ship mathematic model with propeller reversing transverse forces and low speed correction is first discussed to be applied for the right-handed single-screw ship. Secondly, a novel PID-based nonlinear feedback algorithm driven by bipolar sigmoid function is proposed. The PID parameters are determined by a closed-loop gain shaping algorithm directly, while the closed-loop gain shaping theory was employed for effects analysis of this algorithm. Finally, simulation experiments were carried out on an LPG ship. It is shown that the energy consumption and the smoothness performance of the nonlinear feedback control are reduced by 4.2% and 14.6% with satisfactory control effects; the proposed algorithm has the advantages of robustness, energy saving and safety in berthing practice.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 하계종합학술대회 논문집 V
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• pp.2589-2592
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• 2003

In this paper, a robust mixed H$_2$/H$\_$$\infty$/ output feedback control method is applied to the design of loop filter for PLL carrier phase tracking. The proposed method successfully copes with large S-curve slope uncertainty and a significant decision delay in the closed-loop that may exist In modern receivers due to a convolutional decoder or an equalizer. The objective is to design an output feedback controller which minimizes the H$_2$performance while satisfying the H$\_$$\infty$/ performance to guarantee the gain margin and phase margin for linear time invariant(LTI) polytopic uncertain systems. LMIs based approach is given to solve this problem. We can verify the H$\_$$\infty$/ performance satisfaction and minimize the phase detector error through the simulation result.