• 제목/요약/키워드: Phase margin

검색결과 267건 처리시간 0.031초

회로 최적화를 위한 외부 커패시터가 없는 LDO 레귤레이터의 안정도와 PSR 성능 모델 (Stability and PSR(Power-Supply Rejection) Models for Design Optimization of Capacitor-less LDO Regulators)

  • 주소연;김진태;김소영
    • 한국전자파학회논문지
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    • 제26권1호
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    • pp.71-80
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    • 2015
  • 한정된 배터리 용량으로 장시간 모바일 시스템을 구동시키기 위하여 저전력 설계에 대한 요구가 높아지면서 PMIC(Power Management IC)의 핵심 부분인 LDO(Low Drop-Out) 레귤레이터의 설계에 대한 관심이 증가하고 있다. 본 논문에서는 Dongbu HiTek $0.5{\mu}m$ BCDMOS 공정을 이용하여 최적화 기법 중 하나인 기하 프로그래밍(Geometric Programming: GP)을 통해 외부 커패시터가 없는 LDO 레귤레이터의 성능을 최적화하였다. 계수가 양수인 단항식 (monomial)으로 모델링된 트랜지스터의 특성 파라미터들을 이용하여 안정도(stability)와 PSR(Power-Supply Rejection)과 같은 LDO 레귤레이터의 특성을 기하 프로그래밍(Geometric Programming: GP)에 적용 가능한 형태로 유도하였다. 위상 마진(phase margin)과 PSR 모델은 시뮬레이션 결과와 비교하였을 때 각각 평균 9.3 %와 13.1 %의 오차를 보였다. 제안한 모델을 사용하여 PSR 제약 조건이 바뀔 경우, 자동화된 회로 설계를 수행하였고, 모델의 정확도를 검증하였다. 본 논문에서 유도된 안정도와 PSR 모델을 이용하면 회로의 목표 성능이 변화하더라도 부가적인 설계 시간을 줄이면서 목표 성능을 가진 회로를 재설계하는 것이 가능할 것이다.

안정성 영역(Stability Area) 판별법을 이용한 발사체 자세제어 이득 설계 및 자세 안정성 분석 (A Study of Attitude Control and Stability Analysis Using D-Decomposition Stability Area Technique for Launch Vehicle)

  • 박용규;선병찬;노웅래;오충석
    • 한국항공우주학회지
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    • 제37권6호
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    • pp.537-544
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    • 2009
  • 본 논문에서는 안정성 영역 판별법(stability area) 기반 발사체의 자세제어기 이득결정과정에 대한 내용을 기술하였다. 안정성 영역 판별법은 D-Decomposition 기법으로부터 정의되는 것으로 본 논문에서는 D-Decomposition 기본 이론과 이로부터 산출된 발사체의 자세 안정성 영역을 도시하고, 적용 예로써 일반적인 발사체의 1단 추력 비행구간에서 자세제어기 설계과정을 제시하였다. 제어이득 결정을 위해서 중첩된 안정성 영역을 바탕으로 시스템 파라미터 불확실성을 고려 안정성 영역 경계(stability area boundary)를 설정하고, 선정된 제어이득을 발사체 선형모델에 적용, 자세 안정성 분석 수행 결과를 나타냈다.

지간 신경종 발생 위치와 심부 횡 중족 골간 인대의 해부학적 연구 (Anatomical Study of Interdigital Neuroma Occurring Site and the Deep Transverse Metatarsal Ligament (DTML))

  • 김재영;최재혁;이경태;양기원;박정민
    • 대한족부족관절학회지
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    • 제11권2호
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    • pp.182-186
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    • 2007
  • Purpose: We examined the relationship of interdigital neuroma occurring site and the surrounding structures, including the deep transverse metatarsal ligament (DTML) by cadaver study and clinical results. Materials and Methods: Seventeen fresh frozen cadavers study were done to evaluate the relationship of interdigital neuroma occuring site and the DTML at two phase of the gait cycle with 60 degree of metatarsophalangeal dorsiflexion and with 15 degrees of ankle dorsiflexion. We measured the distance from interdigital nerve bifurcation of the common digital nerve to anterior margin of the DTML and longitudinal length of DTML itself. Clinically, we checked the location of interdigital neuroma and DTML length during surgery in 32 feet. Results: In the second and third web space, the mean distance from bifurcation of the common digital nerve of foot to the anterior margin of DTML was 16.7 mm, 15.1 mm in the mid-stance position, and 15.9 mm. 14.6 mm in heel-off position. Second, Third web space ligament itself length were average 12.8 mm, 10.6 mm. Clinically, all of the cases of interdigital neuroma started at the bifurcation area of the common digital nerve and interdigital neuroma was average 7.5 mm (range; 6-11 mm). Conclusion: Interdigital neuroma were located more distally than DTML in both the mid-stance and heel off stage. The main lesion was located between metatarsal head and metatarsophalangeal joint and more distal than the DTML anterior margin.

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가스수화물 BSR을 이용한 남극반도 남쉐틀랜드 대륙주변부의 지열류량 변화 (Gas Hydrate BSR-derived Heat Flow Variations on the South Shetland Continental Margin, Antarctic Peninsula)

  • 진영근;남상헌;김예동;김규중;이주한
    • Ocean and Polar Research
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    • 제25권2호
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    • pp.201-211
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    • 2003
  • Bottom simulating reflectors (BSR), representing the base of the gas hydrate stability field, are widespread on the South Shetland continental margin (SSM), Antarctic Peninsula. With the phase diagram fur the gas hydrate stability field, heat flow can be derived from the BSR depth beneath the seafloor determined on multichannel seismic profiles. The heat flow values in the study area range from $50mW/m^2$ to $85mW/m^2$, averaging to $65mW/m^2$. Small deviation from the average heat flow values suggests that heat flow regime of the study area is relatively stable. The landward decrease of heat flow from the South Shetland Trench to the continental shelf would be attributed to the landward thickening of the accretionary prism and the upward advection of heat associated with fluid expulsion. The continental slope 1500m to 3000m deep, where BSRs are most distinguished in the SSM, shows relatively large variation of heat flow possibly due to complex tectonic activities in the study area. The local high heat flow anomalies observed along the slope may be caused by heat transport mechanisms along a NW-SE trending large-scale fault.

복합재 샌드위치 구조의 개선된 확률론적 설계 및 신뢰성 기반 최적설계 (Advance Probabilistic Design and Reliability-Based Design Optimization for Composite Sandwich Structure)

  • 이석제;김인걸;조우제;설창원
    • Composites Research
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    • 제26권1호
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    • pp.29-35
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    • 2013
  • 복합재료 샌드위치 구조는 굽힘 강성을 향상시키고 복합재 적층판에 비해 30% 이상의 무게를 절감할 수 있다. 그러나 일반 금속에 비해 제작과정에서 발생되는 재료물성의 불확실성이 많이 내재되어 있으므로 신뢰성 기반 확률론적 설계방법이 요구된다. 본 논문에서는 안전계수를 이용한 고전적인 설계 방법이 구조물의 안전을 보장하지 않는다는 확률론적 증거를 제시하기 위하여 단순화된 복합재 샌드위치 동체에 대해 PMS(Probabilistic Margin of Safety)를 계산하였다. 이 과정에서 CMCS(Crude Monte-Carlo Simulation)에 의해 계산된 확률밀도함수를 이용하였다. 더 나아가 신뢰성 기반 최적설계를 수행하고 효율적인 계산을 위해 RBDO-MPDF(RBDO by Moving PDF) 방법을 제시하였다. 본 논문의 결과는 구조물의 신뢰성을 보장하기 위한 개선된 설계 방법과 효율적인 신뢰성 기반 최적설계 방법 연구에 유용할 것이다.

항공기 세로축 무게중심의 변화에 따른 민감도 해석에 관한 연구 (A Study on Aircraft Sensitivity Analysis for C.G Variation of Longitudinal Axis)

  • 김종섭
    • 한국항공우주학회지
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    • 제34권6호
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    • pp.83-91
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    • 2006
  • 현대의 고성능 전투기는 공력성능 및 조종성능의 향상을 위하여 대부분 세로축 방향으로 항공기를 불안정하게 설계하는 정안정성 완화 개념을 채택하고 있다. 비행제어법칙의 설계 작업은 불안정하게 설계된 항공기에 안정성을 부여하고, 주어진 비행임무에 대하여 만족스런 조종성능을 발휘할 수 있도록 비행성능을 조작하는 일련의 과정이다. 세로축 무게중심은 무장형상, 연료상태 및 착륙장치의 위치에 영향을 받으며 항공기 안정성에 많은 영향을 미친다. 따라서 무게중심의 이동은 세로축 안정도 여유에 영향을 미친다. 본 논문에서는 운용 시에 발생 가능한 최대 후방 무게중심에 대해 항공기 안정성을 해석하였고, 비행시험을 통해 최종적으로 검증하였다. 선형해석 항목은 세로축 단주기 모드 특성 및 안정도 여유에 관하여 행하였으며, 비선형 해석 항목은 단주기 모드를 해석하기 위해 세로축 가진 입력에 대한 항공기 응답특성을 분석하였다. 또한, 최대 후방 무게중심에서 수행된 고받음각 비행시험 자료를 제시함으로써 T-50 고등훈련기의 비행 안정성을 제시하였다.

Early Recurring Hepatocellular Carcinoma after Partial Hepatic Resection: Preoperative CT Findings

  • Jae Hoon Lim;Hyun-Jung Jang;Eung Yeop Kim;Cheol Keun Park;Jae-Won Joh;Yong Il Kim
    • Korean Journal of Radiology
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    • 제1권1호
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    • pp.38-42
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    • 2000
  • Objective: The purpose of this study was to determine the utility of preoperative CT in predicting early recurrence of hepatocellular carcinoma after partial hepatic resection. Materials and Methods: Preoperative three-phase helical CT scans in 53 patients with hepatocellular carcinoma were retrospectively reviewed by two radiologists. In 27 patients (group I), HCC had recurred within six months, while 26 (group II) had remained disease free for at least two years. In each group, preoperative CT findings were evaluated in each group for the tumor size and number, the presence or absence of capsule, distinctness of tumor margin, perinodular extension, and the presence or absence of portal vein thrombosis. Results: In group I, a tumor capsule of tumor was seen in five of 27 patients (19%), and in group II, in 16 of 26 (62%) (p = .001). The tumor margin was distinct in eight patients (30%) in group I and in 20 (77%) in group II (p = .001). Multiple tumors, perinodular extension, and portal vein thrombosis were more frequently seen in group I but the differences were not statistically significant (p > .05). Tumor size was similar in each group (p > .05). Conclusion: Preoperative CT findings that may help predict the early recurrence of hepatocellular carcinoma after surgical resection are an absence of capsule of tumors and an indistinct margin. Reference to these findings during preoperative CT can guide clinicians in their choice of treatment.

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Extreme Learning Machine Approach for Real Time Voltage Stability Monitoring in a Smart Grid System using Synchronized Phasor Measurements

  • Duraipandy, P.;Devaraj, D.
    • Journal of Electrical Engineering and Technology
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    • 제11권6호
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    • pp.1527-1534
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    • 2016
  • Online voltage stability monitoring using real-time measurements is one of the most important tasks in a smart grid system to maintain the grid stability. Loading margin is a good indicator for assessing the voltage stability level. This paper presents an Extreme Learning Machine (ELM) approach for estimation of voltage stability level under credible contingencies using real-time measurements from Phasor Measurement Units (PMUs). PMUs enable a much higher data sampling rate and provide synchronized measurements of real-time phasors of voltages and currents. Depth First (DF) algorithm is used for optimally placing the PMUs. To make the ELM approach applicable for a large scale power system problem, Mutual information (MI)-based feature selection is proposed to achieve the dimensionality reduction. MI-based feature selection reduces the number of network input features which reduces the network training time and improves the generalization capability. Voltage magnitudes and phase angles received from PMUs are fed as inputs to the ELM model. IEEE 30-bus test system is considered for demonstrating the effectiveness of the proposed methodology for estimating the voltage stability level under various loading conditions considering single line contingencies. Simulation results validate the suitability of the technique for fast and accurate online voltage stability assessment using PMU data.

Application of an Adaptive Autopilot Design and Stability Analysis to an Anti-Ship Missile

  • Han, Kwang-Ho;Sung, Jae-Min;Kim, Byoung-Soo
    • International Journal of Aeronautical and Space Sciences
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    • 제12권1호
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    • pp.78-83
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    • 2011
  • Traditional autopilot design requires an accurate aerodynamic model and relies on a gain schedule to account for system nonlinearities. This paper presents the control architecture applied to a dynamic model inversion at a single flight condition with an on-line neural network (NN) in order to regulate errors caused by approximate inversion. This eliminates the need for an extensive design process and accurate aerodynamic data. The simulation results using a developed full nonlinear 6 degree of freedom model are presented. This paper also presents the stability evaluation for control systems to which NNs were applied. Although feedback can accommodate uncertainty to meet system performance specifications, uncertainty can also affect the stability of the control system. The importance of robustness has long been recognized and stability margins were developed to quantify it. However, the traditional stability margin techniques based on linear control theory can not be applied to control systems upon which a representative non-linear control method, such as NNs, has been applied. This paper presents an alternative stability margin technique for NNs applied to control systems based on the system responses to an inserted gain multiplier or time delay element.

척추 융합 수술을 위한 삼차원 척추경 모델을 이용한 자동 수술 계획 시스템 (Automated Surgical Planning System for Spinal Fusion Surgery with Three-Dimensional Pedicle Model)

  • 이종원;김성민;김영수;정완균
    • 제어로봇시스템학회논문지
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    • 제17권8호
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    • pp.807-813
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    • 2011
  • High precision of planning in the preoperative phase can contribute to increase operational safety during computer-aided spinal fusion surgery, which requires extreme caution on the part of the surgeon, due to the complexity and delicacy of the procedure. In this paper, an advanced preoperative planning framework for spinal fusion is presented. The framework is based on spinal pedicle data obtained from CT (Computed Tomography) images, and provides optimal insertion trajectories and pedicle screw sizes. The proposed approach begins with safety margin estimation for each potential insertion trajectory that passes through the pedicle volume, followed by procedures to collect a set of insertion trajectories that satisfy operation safety objectives. The radius of a pedicle screw was chosen as 70% of the pedicle radius. This framework has been tested on 68 spinal pedicles of 8 patients requiring spinal fusion. It was successfully applied, resulting in an average success rate of 100% and a final safety margin of $2.44{\pm}0.51mm$.