• 대한전기학회:학술대회논문집
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• 대한전기학회 2000년도 추계학술대회 논문집 학회본부 D
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• pp.765-768
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• 2000

Linearization of the biped dynamic equations and design of linear controller for the linearized equations are studied in this paper. The biped robot with inverted pendulum type trunk, used to stabilize the dynamic balancing of the biped robot during dynamic walking period, is modelled with 14 DOF and simulated. Despite of well defined linear control theories so far, the linear control methods was limited to the applications for a walking robot, because they have been inherently strong nonlinear properties, such as a modeling parameter uncertainties, external forces as noise, inertial and Coriolis terms by three dimensional modeling and so on. To linearize the nonlinear equations of motion of biped robot on MIMO and time varying linear equations of motion, 1st order Taylor series is used to formulate the linear equation. And a 2nd order numerical perturbation method Is used to approximate partial differential equations. Using the linearized equations of motion, a linear controller is designed by pole placement method with feed forward compensation. Using the obtained linearized equations and linear controller, the continuous walking simulation is performed.

• 전자공학회논문지S
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• 제36S권6호
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• pp.57-66
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• 1999

본 논문에서는 자기부상시스템의 부상제어기 설계방법을 제시한다. 국내에서는 여러 이점을 갖는 상전도부상방식에 관한 연구가 주로 수행되고 있다. 그러나 이 상전도 부상시스템은 높은 비선형성과 불안정성을 갖기 때문에 여러 외부조건에 대해서 견실한 안정도와 높은 정밀도를 유지하는 부상제어기 설계는 매우 어려운 문제이다. 본 논문에서는 극배치방식에 근거한 이득계획제어 설계기법과 LQG방식에 근거한 이득계획제어 설계기법을 제시하고 제어성능을 모의 실험을 통하여 보인다.

• International Journal of Aeronautical and Space Sciences
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• 제12권4호
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• pp.365-370
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• 2011

This paper presents the air-to-air missile autopilot design for a $180^{\circ}$ heading reversal maneuver during boost-phase. The missile's dynamics are linearized at a set of operating points for which angle of attack controllers are designed to cover an extended flight envelope. Then, angle of attack controllers are designed for this set of points, utilizing a pole-placement approach. The controllers' gains in the proposed configuration are computed from aerodynamic coefficients and design parameters in order to satisfy designer-chosen criteria. These design parameters are the closed-loop frequency, damping ratio, and time constant; these represent the characteristics of the control system. To cope with highly nonlinear and rapidly time varying dynamics during boost-phase, the global gain-scheduled controller is obtained by interpolating the controllers' gains over variations of the angle of attack, Mach number, and center of gravity. Simulation results show that the proposed autopilot design provides satisfactory performance and possesses good [ed: or "sufficient" or "excellent"] capabilities.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2006년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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• pp.313-315
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• 2006

Being controlled by a pole placement, levitation system should need many sensors that measure air-gap, velocity, acceleration, and so on. However, these sensors have observational errors by changed temperature. This paper proposed a output compensated command tracking controller for reducing the error and reducing sensors. Simulation results will be provided to show the validity of the proposed scheme.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국제학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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• pp.327-332
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• 1993

One maglev vehicle is composed of 6 r 8 modules. Each module is composed of 4 staggered magnets attached to an aluminum bogie. In the view point of levitation control except propulsion by LIM, 5 is the maximum degrees of freedo to be controlled. But rolling control of the vehicle depends on the bogie structure. We describe just anti-roll type out of bogie structures and 4 degrees of freedom control is sufficient for levitation quality improvement. Multivariable pole-placement concept and the decentralized control concept are used for controller design. Computer simulation and control experiment are performed on a specially designed test module.

• 한국지능시스템학회:학술대회논문집
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• 한국퍼지및지능시스템학회 1998년도 The Third Asian Fuzzy Systems Symposium
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• pp.331-336
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• 1998

A systematic design method for PDC(Parallel Distributed Compensation)-type continuous time Takagi-Sugeno(T-S in short) fuzzy control systems which have inaccessible states is developed in this paper. Reduced-dimensional fuzzy state estimator is introduced from existing T-S fuzzy model using the PDC structure of Wang et al. [1] LMI(Linear Matrix Inequalities) problems which represent the stabililty of the reduced-dimensional fuzzy state estimator are derived. Pole placement constraints idea for each rules is adopted to determine the estimator gains and they are also revealed as LMI problems. these LMI problems are combined with Joh et al's [7][8] LMI problems for PDC -type continuous time T-S fuzzy controller design to yield a systematic design method for PDC -type continuous time T-S fuzzy control systems which have inaccessible states.

• 전력전자학회논문지
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• 제5권1호
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• pp.1-10
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• 2000

본 논문에서는 무정전전원장치(UPS)에 사용되는 3상 PWM 인버터의 정전압 제어특성 향상을 위해 개선된 형태의 데드비트 제어방식을 제안하고 이의 설계를 수행한다. 일반적으로 UPS는 전압제어 루프 안에 전류제어기를 두는 형태의 이중 제어 루프 구조를 가지며, 빠른 과도응답 제어 특성을 얻기 위해 데드비트 제어기가 많이 적용되어 왔다. 그러나 전압, 전류의 이중 제어구조를 갖는 데드비트 제어기의 경우 동일한 극배치 특성으로 인해 기존의 제어 시스템은 불안정한 측면을 갖게된다. 이러한 제어특성의 개선을 위하여 분리된 극배치를 가지는 제어기구조를 제안하며, 이는 전압제어기 출력으로 1차 지수함수 응답을 사용하는 변형된 형태의 데드비트 제어기로 구성된다. 아울러 부하 변동에 따른 부하전류의 외란성분을 전향보상하기 위하여 전차원 외란 관측기를 설계하고 시뮬레이션 및 실험을 통하여 제안된 시스템의 우수성을 확인한다.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2008년도 하계학술대회 논문집
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• pp.607-609
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• 2008

본 논문에서는 태양광 발전 및 연료전지 시스템에서 사용되는 계통 연계형 인버터에 적용 가능한 새로운 전류제어기 설계방법을 제안한다. 제안된 상태궤환 전류제어기는 극점배치기법을 이용하여 주어진 시스템 요구사항에 따른 체계적인 제어기설계가 가능하며, 계통 전압과 동상을 가지도록 계통 주입전류를 제어한다. 이에 따라, 사인입력 기준전압을 추적할 수 있는 상태궤환 제어 알고리즘을 인버터의 대신호 평균 모델을 이용하여 설계하고, 200W급 계통 연계형 2단 구조 태양광 발전 전력변환 축소 시스템의 실험을 통하여 그 성능을 검증한다.

• International Journal of Internet, Broadcasting and Communication
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• 제9권1호
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• pp.1-8
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• 2017

Nowadays many articles describe the controlling models for four rotor flying vehicle. Basic approaches to the problem of these articles are mathematical expressions describing dynamics of the models of the vehicle and PID control for manipulating the object in 3 dimensional space. Design of control systems is usually started by careful consideration of its mathematical model description. We present a detailed mathematical model for a quad rotor. This paper first considers simulation of quadcopter control based on full state feedback technique with linearization in MATLAB environment and shows the results of the simulations. Finally will be shown experimental results of the state feedback control implemented in real model.

• 한국조명전기설비학회:학술대회논문집
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• 한국조명전기설비학회 2000년도 학술대회논문집
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• pp.199-204
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• 2000

Generally, The systems are so complex that it not possible to obtain reasonable model using physical insight. Also a model based on physical insight contains a number of unknown parameters even if the structure is derived from physical laws. To solve these problems, the systems identification is described in this paper. So, AC servo motor system which has both open loop and closed loop is selected as an example for identification. A state-space model of AC servo motor system is identified through open loop experiment and identified through closed loop experiment and using pole placement integral controller to open loop system. As the results, From ARMA model, We have obtained continuous-time state space model.