• 제목/요약/키워드: 전환모드

검색결과 276건 처리시간 0.034초

A Concurrent MCMA-DD Equalizer with Initial Convergence Detection (초기 수렴 검출 기능을 갖는 동시 MCMA-DD 등화기)

  • Kim, Chul-Min;Choi, Ik-Hyun;Oh, Kil-Nam;Choi, Soo-Chul
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 한국해양정보통신학회 2005년도 추계종합학술대회
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    • pp.477-480
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    • 2005
  • CMA-DD is proposed to improve the steady-state performance of CMA and its performance is depending on switching time between two modes of operation. Castro et al. who proposed a concurrent equalizer for solving problem of CMA-DD, which reduced the sensibility of switching time. However, concurrent algorithm has a problem that it keeps working after convergence. In this paper, we propose concurrent MCMA-DD equalizer combined modified CMA(MCMA) and DD mode for making better concurrent algorithm. The proposed equalizer is better than previous algorithm in convergence speed and steady-state performance. Also, the proposed algorithm decides optimum switching time using residual ISI of the equalizer output.

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RBDO of Coil Spring Considering Transversal Direction Mode Tracking (횡방향 모드추적을 고려한 코일스프링의 신뢰성기반 최적설계)

  • Lee, Jin Min;Jang, Junyong;Lee, Tae Hee
    • Transactions of the Korean Society of Mechanical Engineers A
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    • 제37권6호
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    • pp.821-826
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    • 2013
  • When the values of design variables change, mode switching can often occur. If the mode of interest is not tracked, the frequencies and modes for design optimization may be miscalculated owing to modes that differ from the intended ones. Thus, mode tracking must be employed to identify the frequencies and modes of interest whenever the values of design variables change during optimization. Furthermore, reliability-based design optimization (RBDO) must be performed for design problems with design variables containing uncertainty. In this research, we perform RBDO considering the mode tracking of a compressive coil spring, i.e., a component of the joint spring that supports a compressor, with design variables containing uncertainty by using only kriging metamodels based on multiple responses approach (MRA) without existing mode tracking methods. The reliability analyses for RBDO are employed using kriging metamodel-based Monte Carlo simulation.

Diagnosis and Improvement of mode transition delay in Linux 9bit serial communications (리눅스 9비트 시리얼통신에서 모드전환 지연원인의 분석과 개선)

  • Jeong, Seungho;Kim, Sangmin;Ahn, Heejune
    • Journal of Korea Society of Industrial Information Systems
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    • 제20권6호
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    • pp.21-27
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    • 2015
  • We analyze the problem that is occurring when using parity mode transformation required for 9 bit serial communication under Linux environment and propose the solution. The parity mode change is used for 9 bit serial communication in the Linux that by nature supports only 8 bit serial communication. delay (around OS tick) arises. Our analysis shows that the cause is minimum length of waiting time to transmit data remained in Tx FIFO buffers. A modified Linux serial driver proposed in this paper decreases the delay less than 1ms by using accurate time delaying. Despite various system communication interfaces, enormous existing standards and system have adopted RS-232 serial communication, and the part of them have communicated by 9bit serial.

Anti-islanding Method for Indirect Current Control based Utility Interactive Inverter (간접전류제어 기반의 계통연계형 인버터를 위한 단독운전방지 기법)

  • Oh, Hyeongmin;Kim, Youngwoo;Choi, Sewan
    • Proceedings of the KIPE Conference
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    • 전력전자학회 2011년도 추계학술대회
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    • pp.207-208
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    • 2011
  • 중요부하를 갖는 계통연계 인버터에서 계통이상시 독립운전으로 전환하여 중요부하에 지속적인 전력을 공급하여야 한다. 기존의 제어 방식은 독립운전시 전압제어를 계통연계시 전류제어를 하기 때문에 모드전환시 과도상태가 발생하고 단독운전 검출전에도 부하의 전압과 주파수가 변동하여 중요부하에 심각한 영향을 줄 수 있다. 본 논문에서는 모드 전환시 과도상태를 최소화하면서 단독운전 검출전에도 부하 전압과 주파수가 일정하게 유지하는 간접전류제어 기반의 계통연계 인버터에서 전압 고조파를 주입함으로써 NDZ(Non-Detection Zone)를 갖지 않는 단독운전방지 기법을 제안한다.

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Control Method of Utility Interactive PCS Considering Voltage Quality of Critical Load (중요부하의 전압품질을 고려한 계통연계형 PCS의 제어 기법)

  • Oh, Hyeongmin;Choi, Sewan;Yoon, Sunjae
    • Proceedings of the KIPE Conference
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    • 전력전자학회 2011년도 전력전자학술대회
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    • pp.175-176
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    • 2011
  • 중요자체부하를 갖는 분산발전 시스템에서 PCS는 계통이상시 독립운전으로 전환하여 자체 부하(MBOP 등)에 지속적인 전력을 공급하여야 한다. 기존의 제어방식은 계통연계시 전류제어를 독립운전시 전압제어를 하기 때문에 모드 전환시 자체부하 전압의 큰 과도상태가 발생 뿐아니라 단독운전 검출전까지 부하의 조건에 따라 자체부하 전압주파수가 변동되어 자체부하에 심각한 영향을 미칠 수 있다. 본 논문에서는 모드 전환에 따른 전압의 과도상태를 최소화하고 단독운전 검출 전에도 전압 주파수가 변동하지 않는 제어기법을 제안한다.

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A Low Power 3D Graphics Accelerator Considering Both Active and Standby Modes for Mobile Devices (모바일기기의 동작모드와 대기모드를 모두 고려한 저전력 3차원 그래픽 가속기)

  • Kim, Young-Sik
    • Journal of KIISE:Computer Systems and Theory
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    • 제34권2호
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    • pp.57-64
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    • 2007
  • This paper proposed the low power texture cache for mobile 3D graphics accelerators. It is very important to reduce the leakage power in the standby mode for mobile 3D graphics accelerators and the memory access latency of texture mapping in the active mode which needs a large memory bandwidth. The proposed structure reduces the leakage power using variable threshold values of power mode transitions according to the selected texture filtering algorithms of application programs, which has the run time gain for texture mapping. In the trace driven cache simulation the proposed structure shows the best 7% performance gain to the previous MSA cache according to the new performance metric considering both normalized leakage power and run time impact.

Transient performance behaviour of the CRW type UAV propulsion system during flight mode transition considering valve operation (CRW형식 무인항공기 추진시스템의 밸브 작동을 고려한 비행모드 전환에 따른 천이 성능특성 연구)

  • Kong Chanduk;Park Jong-Ha;Yang Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.219-224
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    • 2005
  • In order to investigate transient behaviour of the CRW(Canard Rotor Wing) type UAV(Uninhabited Aerial Vehicle) propulsion system during flight mode transition considering flow control valve operation, the propulsion system was modelled using SIMULINK commercial program. For transient simulation of the main engine system, the ICV(Inter-Component Volume) method was applied. The valve system is to control the gas flow of the rotary duct system and the main duct system, and the analysis was performed with an assumption that the total gas mass flow of the main engine is the same as summation of the rotary duct flow and the main duct flow, and with consideration of valve loss, flow rate and effective area in valve angle variation. The performance analysis was carried out during flight mode transitions from the rotary flight mode to the fixed wing flight mode and vice versa mode at altitude of 1Km, flight Mach number 0.1 and maximum engine rpm.

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