• 제목/요약/키워드: Nonlinear switching control

검색결과 185건 처리시간 0.023초

낮은 스위칭 주파수를 갖는 대용량 무정전전원장치를 위한 협대역 전압제어기 설계 (Design of Narrowband Voltage Controller for Large Capacity Uninterruptible Power Supply with Low Switching Frequency)

  • 윤춘기;조영훈;임승범
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2015년도 추계학술대회 논문집
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    • pp.149-150
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    • 2015
  • This paper presents narrowband voltage controller for large capacity UPS system with low switching frequency. The proposed controller is repetitive controller applicable to low sampling. The controller reduces the control error for nonlinear load and improve efficiency. The proposed controller is verified through the experiment using 40kW UPS inverter.

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신경회로망을 이용한 SRM의 토크 추정과 스위칭 각 제어 (A Torque Estimation and Switching Angle Control of SRM using Neural Network)

  • 백원식;김민회;김남훈;최경호;김동희
    • 전력전자학회논문지
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    • 제7권6호
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    • pp.509-516
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    • 2002
  • 본 논문에서는 신경회로망을 이용한 스위치드 릴럭턴스 전동기(Switched Reluctance Motor, SRM)의 간편한 순시토크 추정기법과 스위칭 각 제어에 관해 연구하였다. 간단한 구조와 높은 효율 등의 많은 장점을 가지고 있는 SRM은 부하토크와 회전속도에 따라 운전특성이 달라지므로 최적운전을 위해서는 스위칭 각 제어가 필수적이다. 이러한 스위칭 각은 고정자 및 회전자 극호각, 토크 및 속도 능의 여러 변수들에 따라 달라지기 때문에 적정 스위칭 시점을 결정하는데 있어서 어려움이 있다. 따라서 본 논문에서는 부하토크 및 회전속도에 따라 효율이 가장 높은 적정 스위칭 각을 실험을 통해 선정한 후 신경회로망(Neural Network, NN)을 이용하여 전동기 제어에 적용하는 방안에 관해 고찰하였다. 또한 스위칭 각 제어에 있어서 필수적인 순시토크의 추정에 있어서도 신경회로망을 이용하여 인덕턴스의 비선형적인 특성이 고려되도록 하였다. 구현된 스위칭 각 제어기를 실제 시스템에 적용하였으며, 고효율 측면에서 선정된 스위칭 각 제어기의 동특성을 확인함으로써 스위칭 각 제어기의 적합성을 검증하였다.

Sliding Mode Control of Spacecraft with Actuator Dynamics

  • Cheon, Yee-Jin
    • Transactions on Control, Automation and Systems Engineering
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    • 제4권2호
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    • pp.169-175
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    • 2002
  • A sliding mode control of spacecraft attitude tracking with actuator, especially reaction wheel, is presented. The sliding mode controller is derived based on quaternion parameterization for the kinematic equations of motion. The reaction wheel dynamic equations represented by wheel input voltage are presented. The input voltage to wheel is calculated from the sliding mode controller and reaction wheel dynamics. The global asymptotic stability is shown using a Lyapunov analysis. In addition the robustness analysis is performed for nonlinear system with parameter variations and disturbances. It is shown that the controller ensures control objectives for the spacecraft with reaction wheels.

차량 성능 및 안정성 향상을 위한 $H_{\infty}$ 요 모멘트 강인제어 ($H_{\infty}$ Robust Yaw-Moment Control Based on Brake Switching for the Enhancement of Vehicle Performance and Stability)

  • 안우성;박종현
    • 대한기계학회논문집A
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    • 제24권8호
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    • pp.1899-1909
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    • 2000
  • This paper proposes a new $H_{\infty}$ yaw moment control scheme using brake torque switching for improving vehicle performance and stability especially in high speed driving. In the scheme, one wheel is selected, depending on the vehicle states, at which a brake torque for control is applied. Steering angles are modeled as a disturbance to the system and the $H_{\infty}$ controller is designed to minimize the difference between the performance of the vehicle and that of the desired model. Its performance robustness as well as stability robustness to system parameter variations is assured through ${\mu}$-analysis. Various simulations with a nonlinear 8-DOF vehicle model show that proposed controller enhances the vehicle performance and stability under disturbances and parameter variations as well as under the normal driving condition.

Improved Sliding Mode Controller for Shunt Active Power Filter

  • Sahara, Attia;Kessal, Abdelhalim;Rahmani, Lazhar;Gaubert, Jean-Paul
    • Journal of Electrical Engineering and Technology
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    • 제11권3호
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    • pp.662-669
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    • 2016
  • In this work, nonlinear control of a three-phase shunt active power filter (SAPF) has been studied and compared to classical control based on proportional integral regulator. The control strategy is based on the direct current method using sliding mode control (SMC), where the aim is to regulate the average voltage across the dc bus of the inverter. Details are given for the control algorithm; the controller is comprised of a current loop which utilizes a hysteresis controller to generate the gating signals for the switching devices, and a nonlinear controller based on SMC law which is different from classical laws based on error between reference and measured output voltage of the inverter. Sliding surface applied in this work contains the whole of state variables, in order to ensure full control of the system behavior in the presence of disturbances that affect the supply source, the load parameters or the reference value. The designed controller offers advantage that it can gives the improvement of dynamic and static performances in cases of large disturbances. A comparison of the effects of PI control and SMC on the APF response in steady stat, under line variations, load variations, and different component variations is performed.

비용함수와 서브 골을 이용한 비선형 최적화 방법 기반의 이동로봇 장애물 회피 주행 (Mobile Robot Navigation with Obstacle Avoidance based on the Nonlinear Least Squares Optimization Method using the Cost Function and the Sub-Goal Switching)

  • 정영종;김곤우
    • 전기학회논문지
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    • 제63권9호
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    • pp.1266-1272
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    • 2014
  • We define the mobile robot navigation problem as an optimization problem to minimize the cost function with the pose error between the goal position and the position of a mobile robot. Using Gauss-Newton method for the optimization, the optimal speeds of the left and right wheels can be found as the solution of the optimization problem. Especially, the rotational speed of wheels of a mobile robot can be directly related to the overall speed of a mobile robot using the Jacobian derived from the kinematic model. When the robot detects the obstacle using sensors, the sub-goal switching method is adopted for the efficient obstacle avoidance during the navigation. The performance was evaluated using the simulation and the simulation results show the validity of the proposed method.

WAETER LEVEL CONTROL USING Z-80 MICROOMPUTER

  • Sugisaka, Masanori
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국제학술편); KOEX, Seoul; 22-24 Oct. 1991
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    • pp.1899-1903
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    • 1991
  • This paper presents a water level control method using Z-80 microcomputer. The process considered in this paper is one tank system which is described by an unknown nonlinear differential equation. The water level is measured by the end of bar installed at a float passing through 8 pair of photointerrupters located at equal distance. Therefore, the input data to 8255 which is interface between Z-80 and photointerrupters is discrete value, namely, value under 1. values from 1 to 8, and value upper 8. The water is pumped into the tank from a reservoir by switching on a relay connected to a moter and pump driving system. The pumping is stopped by switching off the relay. Experimental studies for two types of controllers are performed in order to investigate the control performance of water level of the water pumping system.

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시변절환면을 갖는 슬라이딩 모드에 의한 차량의 요-모멘트 제어 (Control of Vehicle Yaw Moment using Sliding Mode with Time-Varying Switching Surface)

  • 이창노;양현석;박영필
    • 대한기계학회논문집A
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    • 제27권5호
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    • pp.666-672
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    • 2003
  • This paper presents a design of the controller for vehicle lateral dynamics using active yaw moment. Vehicle lateral motion is incorporated with directional controllability and stability. These are conflicting each other from the view of vehicle handling performance. To compromise the trade-off between these two aspects, we suggest a new control algorithm based on the sliding mode with time-varying switching surface according to the body side slip angle. The controller can deal with the nonlinear region in vehicle driving condition and be robust to the parameter uncertainties in the plant model. Control performance is evaluated from the simulation for the vehicle of real parameters on the road with various tire-road frictions.

LQ비행제어를 위한 무충돌 전환 구현 알고리즘 (Bumpless Transfer Implementation Algorithm for LQ Flight Control)

  • 김태신;박종후;권오규;박춘배
    • 한국항공우주학회지
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    • 제34권11호
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    • pp.35-41
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    • 2006
  • 이 논문에서는 항공기의 비행제어에 적용하기 위해 각각의 비행영역에서 설계된 LQ(Linear Quadratic)제어기를 비행영역이 바뀜에도 충돌 없이 교체할 수 있는 알고리즘을 제안한다. 이 알고리즘은 기존의 구현 알고리즘에 비해 LQ제어기에 적용하기 편리하게 유도되었고, 비선형 모델에도 적용할 수 있도록 트림점을 포함한 식으로 제시된다. 제안된 알고리즘의 성능을 확인하기 위해 시험표준 문제로 초음속 시험 항공기의 LQ제어문제에 적용하는 모의실험을 수행하고 제어성능이 우수함을 예시한다.

입력과 매칭되지 않는 외란을 갖는 시스템에 대한 가변구조제어 (Variable Structure Control for a System with Mismatched Disturbances)

  • 최윤종;박부견
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2007년도 심포지엄 논문집 정보 및 제어부문
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    • pp.149-151
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    • 2007
  • For several decades, VSC has gained much attention as one of the useful design tools for handling the practical system with uncertainties or disturbances. Generally, the disturbances in the matching condition can be perfectly rejected via VSC; however, these in the mismatching condition are known to be hardly rejected. There have been some trials on it, in which the resulting controls in fact belong to the class of robust control guaranteeing disturbance ${\gamma}$-attenuation. Therefore, in this paper, we propose a new Variable Structure Control (VSC) for a system with mismatched disturbances. The proposed controller is composed of linear and nonlinear parts; the former plays a role in stabilizing the system and the latter takes care of attenuating the disturbances. The main contribution is to introduce the concept of switching-zone, rather than switching-surface, that is designed through piece-wise Lyapunov functions. The resulting non-convex conditions are formulated with an iterative linear programming algorithm, which provides an excellent performance of almost rejecting the disturbances.

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