• Title/Summary/Keyword: Phase plane switching control

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Hybrid Control Strategy of Phase-Shifted Full-Bridge LLC Converter Based on Digital Direct Phase-Shift Control

  • Guo, Bing;Zhang, Yiming;Zhang, Jialin;Gao, Junxia
    • Journal of Power Electronics
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    • v.18 no.3
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    • pp.802-816
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    • 2018
  • A digital direct phase-shift control (DDPSC) method based on the phase-shifted full-bridge LLC (PSFB-LLC) converter is presented. This work combines DDPSC with the conventional linear control to obtain a hybrid control strategy that has the advantages of linear control and DDPSC control. The strategy is easy to realize and has good dynamic responses. The PSFB-LLC circuit structure is simple and works in the fixed frequency mode, which is beneficial to magnetic component design; it can realize the ZVS of the switch and the ZCS of the rectifier diode in a wide load range. In this work, the PSFB-LLC converter resonator is analyzed in detail, and the concrete realization scheme of the hybrid control strategy is provided by analyzing the state-plane trajectory and the time-domain model. Finally, a 3 kW prototype is developed, and the feasibility and effectiveness of the DDPSC controller and the hybrid strategy are verified by experimental results.

High Speed Position Control Method of a Linear DC Motor (리니어 직류 모터의 고속 위치 제어방식)

  • 엄기환;선동설;김주홍
    • The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.7 no.4
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    • pp.51-58
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    • 1993
  • This paper proposed a minmum time control method by a parabolic switching function to high speed position control, with high accuracy, of a Linear OC Motor A proposed method is organized simply and a bang-bang control's signal switched on a parabola type switching function in the phase for a minimum time control realization. However, a sliding mode occurs owing to system's modelling errors, so the minimum time control is realized a once switching bang-bang control by repeating trial experiments. Next time, in a neighborhood of the origin in the phase plane, a Linear OC Motor is stopped at the origin by the linear feedback control.

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Reduction of Reaching Time on Phase Plane in Variable Structure Control System (가변구조 제어시스템에 있어서 위상면상에의 도달시간 감소)

  • 이주장;황동환
    • The Transactions of the Korean Institute of Electrical Engineers
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    • v.39 no.1
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    • pp.51-59
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    • 1990
  • In this paper, a new variable structure control algorithm is proposed to reduce the reaching time on a phase plane. In the new method, a term proportional to the magnitude of the switching variables is added to the Morgan and Ozguners algorithm. When this algorithm is applied to second order systems the simulation results show that the new approach of the control algorithm is more effective than morgan's algorithm.

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Control Method for Fault-Tolerant Active Power Filters

  • Zhang, Chenyu;Zheng, Jianyong;Mei, Jun;Deng, Kai;Zhou, Fuju
    • Journal of Power Electronics
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    • v.15 no.3
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    • pp.796-805
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    • 2015
  • New direct and indirect current control methods for a fault-tolerant active power filter topology are presented in this paper. Since a three-phase four-switch topology has a phase bridge current which cannot be directly controlled, a hysteresis control method in the α-β plane which controls the three-phase current in the two-phase stationary coordinate system is proposed. The improved SVPWM algorithm is able to eliminate the operation of the trigonometric functions in the traditional algorithm by rotating the α-β coordinates and alternating the sequence of the output vectors, which in turn simplifies the algorithm and reduces the switching frequency. The selection of the DC-side reference voltage and DC-side capacitor equalization strategy are also discussed. Simulation and experiments demonstrate that the proposed control method is correct and feasible.

Integrated Simulation of Descent Phase using the RCS jet for a Lunar Lander (RCS jet을 고려한 달착륙선의 Descent phase 통합 시뮬레이션)

  • Min, Chan-Oh;Jeong, Seun-Woo;Lee, Dae-Woo;Cho, Keum-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.6
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    • pp.473-480
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    • 2013
  • Researches for various lunar landing technologies are in progress for the lunar exploration program planned for early 2020s in Korea. This paper shows the integrated simulation for safe lunar landing guidance/control system in powered descent phase. Generally, the lunar lander uses on/off(bang-bang) controller to control the RCS jet thrusters instead of proportional controller. In this paper, the on/off controller using phase-plane switching function, and thruster selection algorithm to control sixteen thrusters are applied. Also additional guidance commands are calculated by a proposed fuzzy logic guidance algorithm. The simulation results show that lunar lander can follow a reference trajectory which is generated by optimization method, then land on the surface safely.

A study on the trajectory control of SCARA robot using sliding mode (슬라이딩 모드를 이용한 SCARA 로보트의 궤적제어에 관한 연구)

  • 진상영;이민철;이만형
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10a
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    • pp.1031-1035
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    • 1993
  • In this paper, we suggest a new algorithm diminishing the chattering in sliding mode control by setting a dead-band along the switching line on the phase plane although nonlinear terms of an nonlinear system are regarded as disturbances and apply this algorithm to the trajectory control of SCARA robot By this algorithm, we can expect the high performance of the trajectory trajet of an industrial robot which needs a robust and simple algorithm.

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A Study of Optimal Impact Angle Control Laws (최적 충돌각 제어법칙에 관한 연구)

  • 송택렬;신상진
    • Journal of the Korea Institute of Military Science and Technology
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    • v.1 no.1
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    • pp.211-218
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    • 1998
  • As a part of trajectory modulation to increase system survivability and terminal effectiveness, impact angle control is required in the terminal phase of tactical missile systems. The missile systems are not allowed to have high altitude to reduce probability of detection by sensors of missile defense systems. In this paper, an analytic form of a time-optimal control law is suggested in the case of constrained missile maneuverability and impact angle under the assumption of a zero-lag autopilot. The control law is obtained by establishing optimal missile-target engagement geometry in the vertical plane. Extension of the law for missiles with autopilot response lags requiring a numerical solution is studied by introducing an iterative algorithm for optimal switching time determination of which the initial switching instants are obtained from the analytic solution. Also suggested is a closed-form impact angle control law derived by an energy-optimal approach. The performances of the proposed guidance laws are evaluated by a series of computer runs.

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The Tracking Control of Manipulator using Sliding Modea (슬라이딩 모드를 이용한 매니퓰레이터의 궤적추종제어)

  • 전희영;박귀태;김동식
    • 제어로봇시스템학회:학술대회논문집
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    • 1987.10b
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    • pp.41-46
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    • 1987
  • A new control scheme is developed to achieve fast and accurate decoupled tracking for an n-Joint robotic manipulator In the Presence of disturbances and unknown Parameter variations. The control system is designed so that a new type of state trajectories called sliding mode may exist in a phase plane. In order to remove the reaching Phase and high frequency chattering phenomenon which ate the common shortcomings of variable structure control(VSC) scheme, this paper presents the new switching line which is composed of three segments and the continuous control law which is derived from the existence condition of a sliding mode. The Proposed methods in this Paper are applied to a 3-Joint robotic manipulator as a numerical example-The digital simulation results which are compared with those of typical VSC scheme show the validity of accurate tracking capability and robust Performance of the system.

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Design of a Variable Structure Adaptive Model Following Controller (可變 構造適應모델 追從 制御器의 設計)

  • Lee, Kang-Woong;Choi, Keh-Kun
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.26 no.4
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    • pp.27-34
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    • 1989
  • An adaptive model following controller is designed using the theory of variable structure systems. The proposed method based on the modified condition for the sliding mode allows the designer to satisfy the requirements to speed up the reaching phase and for the magnitude of the chattering to be reduced in the sliding mode. Chattering reduction is obtained by the replacement of control input in the neighborhood of the sliding plane. The results of computer simulation show that state trajectories reach switching plane fast and chattering is reduced.

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DEVELOPMENT OF X-Y PLANE DRIVING CONTROL SYSTEM BY STEPPING MOTOR (스텝 모터에 의한 X-Y 평면 구동 제어 시스템 개발)

  • Lee, S.Y.;Kim, B.H.;Park, S.D.;Kim, H.C.;Kim, W.C.;Hong, I.S.;Woo, C.H.;Oh, B.W.;Lee, B.K.
    • Proceedings of the KIEE Conference
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    • 1998.07f
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    • pp.2166-2168
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    • 1998
  • A PWM inverter using power FET is developed to switch the excitation current of 5 phase hybrid stepping motor for the use of driving X, Y table. A micro processor based controller is also developed to control the excitation current switching of X, Y axis stepping motor as well as synchronizing operation of Z-axis servo motor. The developed driving control system is applied to the industrial embroidery sewing machine.

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