• 제목/요약/키워드: initial control

검색결과 4,119건 처리시간 0.028초

신경회로망과 유전알고리즘에 기초한 이동로봇의 제어 이득 최적화 (Control Gain Optimization for Mobile Robots Using Neural Networks and Genetic Algorithms)

  • 최영규;박진현
    • 한국정보통신학회논문지
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    • 제20권4호
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    • pp.698-706
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    • 2016
  • 이동로봇을 원하는 위치로 최단시간 안에 이동시키기 위해 최적제어문제를 풀어야 하지만 비선형시스템이므로 해석적 접근이 매우 어렵다. 본 논문에서 유전알고리즘을 사용하여 이동로봇의 최적제어이득을 구한다. 로봇 방정식이 비선형식이므로 초기치에 따라 최적제어이득은 다르게 결정된다. 따라서 초기치 범위를 적절한 개수의 격자점으로 이산화시킨 뒤 해당 격자점에서 유전알고리즘으로 최적제어이득을 구한다. 일반적인 초기치에 대한 제어이득은 신경회로망으로 구하며 해당 격자점의 초기치와 그에 대한 최적제어이득을 신경회로망 학습데이터로 사용하고 학습시킨다. 이산화된 격자점이 아닌 다른 초기치에 대한 제어이득은 신경회로망으로부터 구한다. 마지막으로 본 논문의 제어방법의 유용성을 시뮬레이션 연구로 확인하고자 한다.

파라미터 보상기를 가지는 비대칭 SRM의 센서리스 속도제어 (A Sensorless Speed Control of 2-Phase Asymmetric SRM with Parameter Compensator)

  • 임근민;안진우;이동희
    • 전력전자학회논문지
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    • 제17권3호
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    • pp.238-245
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    • 2012
  • This paper presents a sensorless speed control of a 2-phase switch reluctance motor(SRM). The proposed sensorless control scheme is based on the slide mode observer with parameter compensator to improve the estimation performance. In the stand still position, the initial rotor position is determined by pulse current responses of each phase windings and the current difference. In order to determine an accurate initial rotor position, the two initial rotor positions are estimated by the difference of the pulse currents. From the stand still to the operating region, a simple open loop control which determines the commutation sequence by the pulse current of the unexcited phase winding is used. When the motor speed is reached to the sensorless control region, the estimated rotor position and speed by the slide mode observer are used to control the SRM. The flux calculator used in the slide mode observer is designed by phase voltage and the voltage drops in the phase resistance of the winding. The accuracy of the flux calculator is dependent on the phase resistance. For the continuous update of the phase resistance, current gradient at the inductance break point is used in this paper. The error of the estimated rotor position at the current gradient position is used to update the phase resistance to improve the sensorless scheme. The proposed sensorless speed control scheme is verified with a practical compressor used in home appliances. And the results show the effectiveness of the proposed control scheme.

불확실 일반 선형 시스템의 레귤레이션 제어를 위한 사전 제어 성능을 갖는 개선된 연속 적분 가변구조 시스템 (An Improved Continuous Integral Variable Structure Systems with Prescribed Control Performance for Regulation Controls of Uncertain General Linear Systems)

  • 이정훈
    • 전기학회논문지
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    • 제66권12호
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    • pp.1759-1771
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    • 2017
  • In this paper, an improved continuous integral variable structure systems(ICIVSS) with the prescribed control performance is designed for simple regulation controls of uncertain general linear systems. An integral sliding surface with an integral state having a special initial condition is adopted for removing the reaching phase and predetermining the ideal sliding trajectory from a given initial state to the origin in the state space. The ideal sliding dynamics of the integral sliding surface is analytically obtained and the solution of the ideal sliding dynamics can predetermine the ideal sliding trajectory(integral sliding surface) from the given initial state to the origin. Provided that the value of the integral sliding surface is bounded by certain value by means of the continuous input, the norm of the state error to the ideal sliding trajectory is analyzed and obtained in Theorem 1. A corresponding discontinuous control input with the exponential stability is proposed to generate the perfect sliding mode on the every point of the pre-selected sliding surface. For practical applications, the discontinuity of the VSS control input is approximated to be continuous based on the proposed modified fixed boundary layer method. The bounded stability by the continuous input is investigated in Theorem 3. With combining the results of Theorem 1 and Theorem 3, as the prescribed control performance, the pre specification on the error to the ideal sliding trajectory is possible by means of the boundary layer continuous input with the integral sliding surface. The suggested algorithm with the continuous input can provide the effective method to increase the control accuracy within the boundary layer by means of the increase of the $G_1$ gain. Through an illustrative design example and simulation study, the usefulness of the main results is verified.

정수압 저어널 베어링의 동특성 향상에 관한 연구

  • 양문호;이기영;안유민;한동철
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 1996년도 제24회 추계학술대회
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    • pp.195-201
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    • 1996
  • The dynamic characteristics of externally pressurized journal bearing have been studied theoretically. The Reynolds' equation has been solved by FDM, and the dynamic coefficients have been calculated by using perturbation method. The bearing is compensated by orifice or double-pad diaphragm control valve. The effects of diaphragm initial gap and stiffness are considered. As the results of analysis, it is shown that a control valve has better performance than orifice.

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엘리베이터용 유도 전동기 벡터 제어시의 초기 시정수 및 자동 조정 (Initial Value Problem and Tuning of Induction Motor parameter in Elevetor vector control)

  • 박상영
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 추계학술대회 논문집 학회본부A
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    • pp.176-178
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    • 1998
  • Recently, Control method of induction Motor is applied in full circuit model, as circular diagram. In Elevetor moderization problem, there is no circuit information. Nothing but, Motor terminal voltage and HP of motor. So, in this study, using KS induction Motor table, try to solve initial valve problem and make some implementations of manual tuning for use of automatic tuning of induction motor parameter.

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Demonstration of Robust Micromachined Jet Technology and Its Application to Realistic Flow Control Problems

  • Chang Sung-Pil
    • Journal of Mechanical Science and Technology
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    • 제20권4호
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    • pp.554-560
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    • 2006
  • This paper describes the demonstration of successful fabrication and initial characterization of micromachined pressure sensors and micromachined jets (microjets) fabricated for use in macro flow control and other applications. In this work, the microfabrication technology was investigated to create a micromachined fluidic control system with a goal of application in practical fluids problems, such as UAV (Unmanned Aerial Vehicle)-scale aerodynamic control. Approaches of this work include: (1) the development of suitable micromachined synthetic jets (microjets) as actuators, which obviate the need to physically extend micromachined structures into an external flow; and (2) a non-silicon alternative micromachining fabrication technology based on metallic substrates and lamination (in addition to traditional MEMS technologies) which will allow the realization of larger scale, more robust structures and larger array active areas for fluidic systems. As an initial study, an array of MEMS pressure sensors and an array of MEMS modulators for orifice-based control of microjets have been fabricated, and characterized. Both pressure sensors and modulators have been built using stainless steel as a substrate and a combination of lamination and traditional micromachining processes as fabrication technologies.

불확실 선형 시스템을 위한 적분 가변구조 지점에서 지점으로 레귤레이션 제어기 (A Variable Structure Point-to-Point Regulation Controller for Uncertain General Linear Systems)

  • 이정훈
    • 전기학회논문지
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    • 제63권4호
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    • pp.519-525
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    • 2014
  • In this paper, an alternative variable structure controller is designed for the point-to-point regulation control of uncertain general linear plants so that the output of plants can be controlled from an arbitrarily given initial point to an arbitrarily given reference point in the state space. By using the error between the steady state value of the output and an arbitrarily given reference point and those integral, a transformed integral sliding surface is defined, in advance, as the surface from an initial state to an arbitrarily given reference point without the reaching phase problems. A corresponding control input is suggested to satisfy the existence condition of the sliding mode on the preselected transformed integral sliding surface against matched uncertainties and disturbances. Therefore, the output controlled by the proposed controller is completely robust and identical to that of the preselected transformed integral sliding surface. Through an example, the effectiveness of the suggested controller is verified.

슬라이딩모드 제어기를 이용한 공기압 실린더 구동장치의 강인제어 (Robust Control of Pneumatic Cylinder Driving System using Sliding Mode Controller)

  • 장지성;한승훈
    • 동력기계공학회지
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    • 제21권6호
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    • pp.101-109
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    • 2017
  • The pneumatic driving system has advantages such as high output power per weight and low heat generation rate. However, it is difficult to control the position because of its strong non-linearity such as large friction forces compared to driving force, and heat transfer characteristics that change during operation. Therefore, in order to achieve the control objectives, a robust controller should be designed considering modeling error and model uncertainty. In this paper, a sliding mode controller is designed to improve the position control performance of pneumatic cylinder driving system. Experimental results show that the designed controller achieves the designed control objectives even if the model of the cylinder driving system, such as the initial pressure inside the cylinder and the initial position of the piston is changed.

HAUSAT-2 자세제어 성능 해석 (ANALYSIS OF THE HAUSAT-2 ATTITUDE CONTROL)

  • 이병훈;김수정;장영근
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2005년도 한국우주과학회보 제14권1호
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    • pp.133-137
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    • 2005
  • 우주시스템 연구실에서 개발 중인 HAUSAT-2의 피치모멘텀 바이어스 시스템을 설계하고 성능을 검증하였다. HAUSAT-2의 자세제어시스템은 초기자세획득모드와 정상모드로 분리되어 궤도에서 운용된다. 본 논문은 피치모멘텀 바이어스 시스템을 사용하여 위성이 운용될 경우 각 모드에 따라 자세제어가 가능한 범위를 해석하였고 ,모멘팀 휠 구동에 의하여 발생되는 모멘팀 덤핑 현상에 대하여 연구하였다.

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더블김벌 모멘텀휠을 이용한 롤/요 제어기 설계 (Roll/yaw controller design using double gimbaled momentum wheel)

  • 박영웅;방효충
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.1099-1102
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    • 1996
  • In this paper, roll/yaw attitude control of spacecraft using a double gimbaled wheel is discussed with two feedback controllers designed. One is a PD controller with no phase difference between roll and yaw control input. The other is a PD controller with a phase lag compensator about the yaw control input. The phase lag compensator is designed as a first order system and a lag parameter is designed for the yaw angle control. There are two case simulations for each controller ; constant disturbance torques and initial errors of nutation at motion. We obtain the results through simulations that steady-state error and rising time of yaw angle are determined by the compensator. Simulation parameters used in this study are the values of KOREASAT F1.

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