• 제목/요약/키워드: 3-loop controller

검색결과 301건 처리시간 0.029초

Intelligent Digital Redesign for Nonlinear Interconnected Systems using Decentralized Fuzzy Control

  • Koo, Geun-Bum;Park, Jin-Bae;Joo, Young-Hoon
    • Journal of Electrical Engineering and Technology
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    • 제7권3호
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    • pp.420-428
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    • 2012
  • In this paper, a novel intelligent digital redesign (IDR) technique is proposed for the nonlinear interconnected systems which can be represented by a Takagi-Sugeno (T-S) fuzzy model. The IDR technique is to convert a pre-designed analog controller into an equivalent digital one. To develop this method, the discretized models of the analog and digital closed-loop system with the decentralized controller are presented, respectively. Using these discretized models, the digital decentralized control gain is obtained to minimize the norm between the state variables of the analog and digital closed-loop systems and stabilize the digital closed-loop system. Its sufficient conditions are derived in terms of linear matrix inequalities (LMIs). Finally, a numerical example is provided to verify the effectiveness of the proposed technique.

분산제어 기반 직류 마이크로그리드 전력관리시스템의 HIL 시뮬레이션 적용 연구 (Development of Hardware In-the-Loop Simulation System for Testing Power Management of DC Microgrids Based on Decentralized Control)

  • 투딘두;리덕중;이동춘
    • 전력전자학회논문지
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    • 제24권3호
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    • pp.191-200
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    • 2019
  • This study proposes a hardware-in-the-loop simulation (HILS) system based on National Instruments' PXI platform to test power management and operation strategies for DC microgrids (MGs). The HILS system is developed based on the controller HIL prototype, which involves testing the controller board in hardware with a real-time simulation model of the plant in a real-time digital simulator. The system provides an economical and effective testing function for research on MG systems. The decentralized power management strategy based on the DC bus signaling method for DC MGs has been developed and implemented on the HILS platform. HILS results are determined to be similar to those of the off-line simulation in PSIM software.

주기 조정과 커널 자동 생성을 통한 다중 루프 시스템의 구현 (Synthesizing multi-loop control systems with period adjustment and Kernel compilation)

  • 홍성수;최종호;박홍성
    • 제어로봇시스템학회논문지
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    • 제3권2호
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    • pp.187-196
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    • 1997
  • This paper presents a semi-automatic methodology to synthesize executable digital controller saftware in a multi-loop control system. A digital controller is described by a task graph and end-to-end timing requirements. A task graph denotes the software structure of the controller, and the end-to-end requirements establish timing relationships between external inputs and outputs. Our approach translates the end-to-end requirements into a set of task attributes such as task periods and deadlines using nonlinear optimization techniques. Such attributes are essential for control engineers to implement control programs and schedule them in a control system with limited resources. In current engineering practice, human programmers manually derive those attributes in an ad hoc manner: they often resort to radical over-sampling to safely guarantee the given timing requirements, and thus render the resultant system poorly utilized. After task-specific attributes are derived, the tasks are scheduled on a single CPU and the compiled kernel is synthesized. We illustrate this process with a non-trivial servo motor control system.

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Development of a Hardware-in-the-loop Simulator for Spacecraft Attitude Control Using Thrusters

  • Koh, Dong-Wook;Park, Sang-Young;Kim, Do-Hee;Choi, Kyu-Hong
    • Journal of Astronomy and Space Sciences
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    • 제26권1호
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    • pp.47-58
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    • 2009
  • In this study, a Hardware-In-the-Loop (HIL) simulator using thrusters is developed to validate the spacecraft attitude system. To control the attitude of the simulator, eight cold gas thrusters are aligned with roll, pitch and yaw axis. Also linear actuators are applied to the HIL simulator for automatic mass balancing to compensate the center of mass offset from the center of rotation. The HIL simulator consists of an embedded computer (Onboard PC) for simulator system control, a wireless adapter for wireless network, a rate gyro sensor to measure 3-axis attitude of the simulator, an inclinometer to measure horizontal attitude, and a battery set to supply power for the simulator independently. For the performance test of the HIL simulator, a bang-bang controller and Pulse-Width Pulse-Frequency (PWPF) modulator are evaluated successfully. The maneuver of 68 deg. in yaw axis is tested for the comparison of the both controllers. The settling time of the bang -bang controller is faster than that of the PWPF modulator by six seconds in the experiment. The required fuel of the PWPF modulator is used as much as 51% of bang-bang controller in the experiment. Overall, the HIL simulator is appropriately developed to validate the control algorithms using thrusters.

Output feedback receding horizon control for uncertain LTV systems

  • Seuncheol Jeong;Park, Poo-Gyeon
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.27.3-27
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    • 2001
  • In this paper, a robust receding horizon controller for uncertain linear time-varying systems is presented in the dynamic output-feedback form. The existing output-feedback receding horizon controller in the literature is composed of a state observer and a static controller associated with the observer states (similar to LQC control), where the fundamental assumption is that the state observer will supply the exact states as time goes up. The performance of those controllers may be much degraded and even the closed-loop stability may not be guaranteed when the system suffers from disturbances and uncertainties or is time-varying. The proposed controller, which is not necessary to have the state-observer, overcomes such difficulties. Using matrix inequality conditions on the terminal weighting matrix, the closed-loop system stability is guaranteed. Numerical examples are ...

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안정적인 조동 검색을 위한 강인 트랙 추종 제어 (A Robust Track-following Control for the Stable Coarse Seek)

  • 이문노;진경복
    • 한국소음진동공학회논문집
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    • 제20권3호
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    • pp.279-286
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    • 2010
  • In this paper, we provide a robust track-following controller design method for the stable coarse seek control. Due to the inaccurate velocity control during a coarse seek, the shake of fine actuator is generated and thus a gain-up track-following control is required to complete stably the coarse seek. To this end, a loop gain adjustment algorithm is introduced to estimate accurately the shake of fine actuator. A weighting function can be properly selected from a minimum tracking gain-up open-loop gain, calculated from the estimated shake quantity of fine actuator. A robust tracking gain-up controller is designed by considering a robust $H_{\infty}$ control problem using the weighting function. The proposed design method is applied to the coarse seek control system of an optical rewritable drive and is evaluated through the experimental results.

Enhanced Dynamic Response of SRF-PLL System for High Dynamic Performance during Voltage Disturbance

  • Choi, Hyeong-Jin;Song, Seung-Ho;Jeong, Seung-Gi;Choi, Ju-Yeop;Choy, Ick
    • Journal of Power Electronics
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    • 제11권3호
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    • pp.369-374
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    • 2011
  • Usually, a LPF (low pass filter) is used in the feedback loop of a SRF (synchronous reference frame) - PLL (phase locked loop) system because the measured grid voltage contains harmonic distortions and sensor noises. In this paper, it is shown that the cut-off frequency of the LPF should be designed to suppress the harmonic ripples contained in the measured voltage. Also, a new design method for the loop gain of the PI-type controller in the SRF-PLL is proposed with consideration of the dynamics of the LPF. As a result, a better transient response can be obtained with the proposed design method. The LPF frequency and the PI controller gain are designed in coordination according to the steady state and dynamic performance requirements. Furthermore, in the proposed method, the controller gain and the LPF cut-off frequency are changed from their normal value to a transient value when a voltage disturbance is detected. This paper shows the feasibility and usefulness of the proposed methods through the computer simulations and experimental results.

마이크로 자이로스코프를 위한 PD 제어기 설계 및 성능시험 (PD controller design for Micro Gyroscope and Its Performance Test)

  • 성운탁;송진우;이장규;강태삼
    • 한국항공우주학회지
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    • 제33권3호
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    • pp.47-56
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    • 2005
  • 본 논문에서는 마이크로 자이로스코프를 위한 폐루프 제어기를 설계하여 그 성능이 개선됨을 보였다. 마이크로 자이로스코프는 높은 Q값을 가지는 시스템으로 그 특성상 공진 영역에서 동작하게 되는데, 개루프로 동작할 경우 선형성, 대역폭 등의 성능에 제약이 있게 된다. 폐루프 제어기는 개루프 동작시의 이러한 제약을 극복하고 성능을 개선할 수 있도록 한다. 본 연구에서는 PD 제어기를 적용하였으며 실험 대상이 된 마이크로 자이로스코프는 서울대에서 설계하고 Bosch foundry에서 제작한 SNU-Bosch MEMS 자이로스코프를 사용하였다. 실험을 통해 폐루프 제어기의 성능을 검증한 결과 대역폭은 35Hz에서 78Hz로, 선형성은 2.07%에서 0.504%로, 바이어스 안정도는 0.066deg/sec에서 0.043deg/sec로 개선되는 것을 확인할 수 있었다.

Rough Fuzzy Control of SVC for Power System Stability Enhancement

  • Mishra, Yateendra;Mishra, Sukumar;Dong, Zhao Yang
    • Journal of Electrical Engineering and Technology
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    • 제3권3호
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    • pp.337-345
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    • 2008
  • This paper presents a new approach to the design of a rough fuzzy controller for the control loop of the SVC (static VAR system) in a two area power system for stability enhancement with particular emphasis on providing effective damping for oscillatory instabilities. The performances of the rough fuzzy and the conventional fuzzy controller are compared with that of the conventional PI controller for a variety of transient disturbances, highlighting the effectiveness of the rough fuzzy controller in damping the inter-area oscillations. The effect of the rough fuzzy controller in improving the CCT (critical clearing time) of the two area system is elaborated in this paper as well.

신경회로망을 이용한 공압구동기의 위치 추종제어에 관한 연구 (A Study on Tracking Position Control of Pneumatic Actuators Using Neural Network)

  • Gi Heung Choi
    • 한국안전학회지
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    • 제15권3호
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    • pp.115-123
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    • 2000
  • 공압구동기는 다양한 형태의 위험작업 환경하에서 사용되고 있다. 또한, 공압구동기를 적용한 공정은 일반적으로 환경친화적인 것으로 인식되고 있다. 대부분의 경우, 공압구동기는 point to point 제어에 사용된다. 그러나, 최근 공압구동기의 정밀 위치제어에 관한 많은 연구가 수행되고 있다. 본 연구에서는 비례밸브로 구성된 공압구동기의 추종위치제어에 관하여 논의한다. 제안되는 제어기는 압력제어 루프와 위치제어 루프로 구성된다. 공기의 압축성에 기인한 비선형성을 상쇄하기 위하여 되먹임선형화에 의한 PID제어기가 압력제어 루프에 사용된다. 위치제어에는 신경회로망을 사용하여 비선형성을 보상한 PID제어기가 사용된다. 실험결과에 의하면, 제안된 제어기는 공압구동기의 추종성능을 대폭 향상시킬 수 있는 것으로 나타났다.

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