• 제목/요약/키워드: High control margin

검색결과 152건 처리시간 0.029초

회전자 위치 추정 PI 제어기를 이용한 PMSM 센서리스 제어 (Sensorless Control of PMSM using Rotor Position Tracking PI Controller)

  • 이종건;석줄기;이동춘
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2003년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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    • pp.176-178
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    • 2003
  • This paper presents a new velocity estimation strategy of a non-salient permanent magnet synchronous motor(PMSM) drive without high frequency signal injection or special PWM pattern. This approach is based on the d-axis current regulator output voltage of the drive system which has the information of rotor position error. The rotor velocity can be estimated through a rotor position tracking PI controller that controls the position error to aero. For zero and low speed operation, the PI gains of rotor position tracking controller have a variable structure. The PI tuning formulas are derived by analyzing this control system using the frequency domain specifications such as phase margin and bandwidth assignment.

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웨이브 파이프라인 클럭 제어에 의한 1V-2.7ns 32비트 자체동기방식 병렬처리 덧셈기의 설계 (1V-2.7ns 32b self-timed parallel carry look-ahead adder with wave pipeline dclock control)

  • 임정식;조제영;손일헌
    • 전자공학회논문지C
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    • 제35C권7호
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    • pp.37-45
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    • 1998
  • A 32-b self-timed parallel carry look-ahead adder (PCLA) designed for 0.5.mum. single threshold low power CMOS technology is demonstrated to operate with 2.7nsec delay at 8mW under 1V power supply. Compared to static PCLA and DPL adder, the self-timed PCLA designed with NORA logic provides the best performance at the power consumption comparable to other adder structures. The wave pipelined clock control play a crucial role in achieving the low power, high performance of this adder by eliminating the unnecessary power consumption due to the short-circuit current during the precharge phase. Th enoise margin has been improved by adopting the physical design of staic CMOS logic structure with controlled transistor sizes.

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자속축 전류제어기 출력전압를 이용한 PMSM 센서리스 제어 (Senseless Control of PMSM using Current Regulator Output Voltage in the Synchronous D-axis)

  • 이종건;석줄기;이동춘
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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    • pp.147-149
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    • 2004
  • This paper presents a new velocity estimation strategy of a non-salient permanent magnet synchronous motor(PMSM) drive without high frequency signal injection or special PWM pattern. This approach is based on the d-axis current regulator output voltage of the drive system which has the information of rotor position error. The rotor velocity can be estimated through a rotor position tracking PI controller that controls the position error to zero. For zero and low speed operation, the PI gains of rotor position tracking controller have a variable structure. The PI tuning formulas are derived by analyzing this control system using the frequency domain specifications such as phase margin and bandwidth assignment.

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Development of a Bio-mimetic Quadruped Walking Robot with Waist Joint

  • Kim, Dong-Sik;Park, Se-Hoon;Kim, Kyung-Ho;Lee, Yun-Jung
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.1530-1534
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    • 2004
  • This paper presents a novel bio-mimetic quadruped walking robot with a waist joint, which connects the front and the rear parts of the body. The new robot, called ELIRO-1(Eating LIzard RObot version 1), can bend its body while the legs is transferred, thereby increasing the stride and speed of the robot. The waist-jointed walking robot can move easily from side to side, which is an important feature to guarantee a larger gait stability margin than that of a conventional single rigid-body walking robot. We design the mechanical structure of the robot, which is small and light to have high movability and high degree of human friendship. In this paper, we describe characteristics of the waist joint and leg mechanism as well as the analysis using ADAMS to select appropriate actuators. In addition, a hardware and software of the controller of ELIRO-1 are described.

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통신위성 전력제어 및 분배장치 설계 및 해석

  • 최재동
    • 항공우주기술
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    • 제2권1호
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    • pp.108-116
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    • 2003
  • 본 연구는 통신위성 전력제어장치(Power control&Distribution Unit)의 설계 및 해석에 관한 내용을 기술한다. 위성체 전력제어장치는 임무기간동안 각 서브시스템과 탑재체에 충분한 전력을 공급하여야 하며, 또한 우주환경 하에서 높은 신뢰성 및 성능이 요구된다. 전력제어 및 분배장치의 제어회로를 위해 버스전압검출 및 필터회로, 오차신호 증폭회로 그리고 SAS 및 BPC 오차신호 회로가 포함되었다. 설계된 제어보상회로에 대한 주파수 응답특성분석을 통해 각 회로의 위상여유와 이득이 분석되었다. 또한 배터리 충/방전을 위한 BPC회로 분석을 통해 배터리 충전 연속모드, 배터리 방전 연속/불연속 모드에서의 입출력 전달함수가 제시되었다.

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대 전류 응용 위한 유도 부하를 갖는 위상 변이 풀 브릿지 컨버터의 전류 제어기 설계 (Current Controller Design of a Phase Shift Full Bridge Converter for High Current Applications with Inductive Load)

  • 레덧탕;박민원;유인근
    • 한국산업정보학회논문지
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    • 제23권1호
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    • pp.43-52
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    • 2018
  • 본 논문에서는 유도성 부하를 가지는 위상 변위 풀 브릿지 컨버터(PSFB)의 성능과 다양한 유도성 부하를 갖는 출력 전류의 동적 응답을 향상시키는 새로운 전류 제어 기법을 제안하였다. 누설 인덕턴스 및 유도성 부하를 포함하는 향상된 동적 모델을 사용하였으며, 유도 부하의 변화에 대한 영향을 상세히 분석하였다. 제안된 전류 제어 방식은 위상 여유 사양을 기반으로 설계하였다. 결과적으로 제안된 전류 제어 기법은 기존의 전류 제어 기법과 비교하여 동적 응답을 개선시킬 수 있음을 확인하였다. 설계된 컨트롤러의 성능은 500 A PSFB 컨버터 시스템을 통하여 검증하였다. 이 결과는 초전도 장치와 같이 유도성 부하가 큰 고 전류 애플리케이션에 활용할 수 있다.

제논 혼합가스를 이용한 고효율 면광원과 국부적 밝기 제어 방식 (High Luminous Efficiency Flat Light Source with Xe mixture Gas Discharge and Areal Brightness Control Method)

  • 정재철;서인우;오병주;황기웅
    • 한국조명전기설비학회:학술대회논문집
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    • 한국조명전기설비학회 2009년도 추계학술대회 논문집
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    • pp.153-157
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    • 2009
  • A Highly efficient Mercury-free Flat Fluorescent Lamp (MFFL) with dielectric barrier Xe gas discharge was developed for an alternative of conventional line-type Cold Cathode Fluorescent Lamps (CCFLs) which shows a wide voltage margin and a stable discharge operation for diffuse glow discharge with an application of a auxiliary electrode. Electro-optic characteristics of the MFFL were examined through the changes in ambient temperature, total pressure and Xe partial pressure. the single cell is expanded into a multi-structured configuration to realize a large sized lamp by a simple repetition of the single cells, and a new driving scheme is proposed for an adaptive brightness control using dual auxiliary electrodes and bi-polar drive scheme. In addition, interesting application of this ultra high luminance flat lamp by the optimization of the gas condition and the pattern of the rear phosphor layer is suggested as a good alternative of daylight lamp source

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Satellite FEM Validation test for High Frequency Jitter Analysis

  • Oh, Shi-Hwan;Yong, Ki-Lyuk
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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    • pp.28.4-29
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    • 2008
  • The aim of the test is to provide an experimental basis to validate the prediction of the FEM for high frequency jitter analysis due to reaction wheel. The principle is to measure structural transfer functions between the input disturbances at RWA base plate and the accelerations near the end tips of payload, in a configuration close to the operational model. The spacecraft shall have to be suspended, in order to be representative of on-orbit boundary conditions. The results of the test shall be compared to the output of the FEM analysis, and if needed, local upgrades of the FEM and/or margin policy shall be defined in order to guarantee a good test/FEM consistency. Test results were compared with the transfer functions of the FEM, which is globally tuned based on the results of vibration test and consequently have lower damping coefficients values than 1% in the frequency range of 60~200Hz. The damping coefficients estimated from the figures of FRF test results are different from the theoretical FEM, but the magnitude trend of FRF of the test results is somewhat similar with the analytical, it is expected that the overall jitter effect of final estimation is nearly same with the preliminary analysis result in which the damping coefficients were assumed to be 1% for all modes in FEM.

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초기 자궁경부암의 수술후 방사선치료 결과 (Therapeutic Results of Postoperative Radiation Therapy for Early Stage Uterine Cervical Cancer)

  • 강승희;서현숙
    • Radiation Oncology Journal
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    • 제11권2호
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    • pp.347-354
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    • 1993
  • This is a retrospective analysis of 67 patients with histologically proven invasive carcinoma of uterine cervix treated with surgery followed by adjuvant radiotherapy at Inje University Seoul Paik Hospital between october 1983 and september 1991, Postoperative radiotherapy was carried out in patients with high risks of locoregional recurrence such as positive pelvic lymph node (38 pts), large tumor size more than 3 cm (22 pts), cervical stromal invasion more than 2/3 (46 pts), parametrial involvement (9 pts), positive resection margin (14 pts), endo/myometrial extension (10 pts), and angiolymphatic invasion (13 pts). Stage I A, I B, and IIA were 2 $(3\%),$ 39 $(58.2\%),\;and\;26\;(38.8\%),$ respectively. Median follow-up period was 48 months with ranges from 13 to 115 months. All 67 patients were treated externally with standard pelvic field with radiation dose ranging from 4080 to 6120 cGy in 4~6 weeks period of time. Of these, 45 patients received intracavitary radiotherapy. The overall survival rate and disease free survival rate at 5-year were $88.0\%\;and\;82.1\%,$ respectively. The survival rates by stage were $87.1\%$ in IB and $88.4\%$ in IIA. Local control rate was $80.6\%(58\;pts).$ The treatment failure was noted in 12 of 67 patients $(17.9\%):$ locoregional failure in $7(10.4\%),$ distant metastasis in 3 $(4.5\%),$ and locoregional and distant metastasis in $2(3\%),$ The univariate analysis of prognostic factors disclosed endo/myometrial extension as a significant factor of survival and recurrence $(70.0\%\;vs\;91.1\%\;P<0.05\;&\;30.0\%\;vs\;15.8\%,\;respectively).$ The complication of postoperative radiothrapy was not significant and all patient were well tolerated. In conclusion, postoperative radiotherapy in patients with high risks of locoreginal recurrence is relatively well tolerated and it gives significantly improved survival rate especially in patients with positive lymph nodes, bulky tumor size $(\geqq3\;cm),$ parametrial involvement, cervical stromal invasion more than 2/3, positive resection margin and angiolymphatic invasion.

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고속 측면 충돌 감지 알고리즘의 개발 (Development of Fast Side-impact Sensing Algorithm)

  • 박서욱;김현태
    • 한국자동차공학회논문집
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    • 제8권3호
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    • pp.163-170
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    • 2000
  • Accident statistics shows that the portion of fatal occupant injuries due to side impacts is considerably high. The side impact usually leads to a severe intrusion of side structure into the passenger compartment. Furthermore, the safety zone for the side impact is relatively small compared to the front impact. Those kinds of physics for side impact frequently result in a fatal injury for the occupant. Therefore, NHTSA and EEVC are trying to intensify the regulation for the occupant protection against side impact. Both the regulation and recent market trends are asking for an installation of side airbag. There are several types of system configuration for side impact sensing. In this paper, we adopt the acceleration-based remote sensing method for the side airbag control system. We mainly focus on the development of hardware and crash discrimination algorithm of remote sensing unit. The crash discrimination algorithm needs fast decision of airbag firing especially for high-speed side impact such as FMVSS 214 and EEVC tests. It is also required to distinguish between low-speed fire and no-fire events. The algorithm should have a sufficient safety margin against any misuse situation such as hammer blow, door slam, etc. This paper introduces several firing criteria such as acceleration. velocity and energy criteria that use physical value proportional to crash severity. We have made a simulation program by using Matlab/Simulink to implement the proposed algorithm. We have conducted an algorithm calibration by using real crash data for 2,500cc vehicle. The crash performance obtained by the simulation was verified through a pulse injection method. It turned out that the results satisfied the system requirements well.

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