• 제목/요약/키워드: Angle Calculation

검색결과 715건 처리시간 0.035초

The Iron loss Estimation of IPMSM According to Current Phase Angle

  • Cho, Gyu-Won;Kim, Dong-Yeong;Kim, Gyu-Tak
    • Journal of Electrical Engineering and Technology
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    • 제8권6호
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    • pp.1345-1351
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    • 2013
  • Variable iron loss as function of current phase angle of Interior Permanent Magnet Synchronous Motor(IPMSM) was calculated through Curve Fitting Method(CFM). Also, a magnetic flux density distribution of iron core according to current phase angle was analyzed, and an iron loss calculation was performed including harmonic distortion. The experiment was performed by production of non-magnetizing model for the separation of mechanical loss, and the iron loss was calculated by the measurement of input using power analyzer and output power using dynamometer. Some error was generated between experimental results and calculation value, but an iron loss diminution according to current phase angle followed a same pattern. So, errors were generated by measurement, vibration, noise, harmonic distortion loss, etc.

투과일사의 유입길이에 따른 Tilt 창호의 적정 기울기 산정 (The Calculation on the Optimum Angle of Tilt Type Window by Length of Transmitted Solar Radiation)

  • 조성우
    • 설비공학논문집
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    • 제22권9호
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    • pp.635-640
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    • 2010
  • This study is suggested tilt window type to be restrained solar radiation through vertical window type in buildings. The shading and aesthetical effect of buildings would be solved by installation of tilt window type. For investigate optimum an angle of tilt window and building azimuth in reference region, the distance of transmitted solar radiation is calculated. The results of calculation showed optimum an angle of tilt window is obtained $7^{\circ}$ that the distance of transmitted solar radiation is 20% of 1.5m of balcony width. In case of an tilt window angle of $7^{\circ}$, the optimum building azimuth is showed $SW15^{\circ}{\sim}SE15$.

IPMSM의 쇄교자속 계산을 통한 릴럭턴스 토크 산정 (The Reluctance Torque Estimate by Linkage Flux Calculation of IPMSM)

  • 조규원;김철민;;김규탁
    • 전기학회논문지
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    • 제62권2호
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    • pp.171-176
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    • 2013
  • Classically, reluctance torque of IPMSM(Interior Permanent Magnet Synchronous Motor) by using inductance according to current phase angle generates an error. This error is affected by total torque. From current phase angle $0^{\circ}$ to large errors will occur, because reluctance torque include current phase angle. But, reluctance torque from steady-state voltage equation of IPMSM is represented by linkage flux. So, reluctance torque is unrelated to the current phase angle formula can be derived. In this paper, operating torque was analyzed by d, q-axis linkage flux of IPMSM and reluctance torque to perform calculations reduced the error of the total torque calculation.

위성통신 안테나의 위성 지향각도 해석적 모델의 실증 (Proof of SATCOM Antenna Heading Angle's Analytical Model)

  • 조규한
    • 한국시뮬레이션학회논문지
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    • 제28권3호
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    • pp.75-82
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    • 2019
  • 유선통신의 사용이 제한되는 상황에서의 통신방법으로 널리 활용되는 위성통신(SATCOM)은 정지궤도위성을 사용하여 통신하기 때문에, 우주 공간의 크게 변하지 않는 한 지점으로 통신용 안테나를 지향시킴으로써 통신할 수 있다. 지상에 설치되어 움직이지 않는 안테나를 위성에 지향시키기 위해서는 안테나가 위치한 위도, 경도, 고도에서 앙각, 방위각과 같은 위성지향각도를 아는 것이 중요하다. 더욱이 비행기와 같이 움직이는 물체위에 탑재된 안테나를 이용하여 위성을 지향 할 경우 지향각도의 계산은 필수적이다. 본 연구는 정지궤도 위성을 지향하기 위해 필요한 안테나 앙각과 방위각의 계산방법을 제시하고 그 방법에 따라서 한반도 지표상의 위경도에 따라서 어떤 지향각도가 요구되는지 시뮬레이션을 수행하였다. 그리고 시뮬레이션 결과를 검증하기 위하여 모노펄스 신호(Monopulse Signal)를 이용하여 위성을 지향하는 위성통신 안테나를 비행기에 탑재하여 안테나의 위치에 따라서 지향각도가 어떻게 변하는지 실험적으로 확인하였다. 이 결과를 시뮬레이션과 비교해 봄으로써 위성통신 안테나의 지향에 필요한 앙각과 방위각의 시뮬레이션의 정확도를 확인하였고, 추가적으로 필요한 안테나 편파각의 계산에 대한 방향을 제시하였다.

덕티드-프롭 유동해석 (FLOW SIMULATION AROUND DUCTED-PROP)

  • 최성욱
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2007년도 추계 학술대회논문집
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    • pp.264-271
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    • 2007
  • The flow simulations around ducted-prop of tilt-duct aircraft were conducted in this study. For the investigation of aerodynamic characteristics of various configurations of duct, the axisymmetric flow calculation method combined with actuator disk model for prop were used. The rapid two-dimensional calculation and fast grid generation enable aerodynamic analysis for various duct configurations in a very short time and anticipated to active role in optimal configuration design of duct exposed to various flight modes. For the case of angle of attack or tilt angle, the three dimensional flow calculation is conducted using the three dimensional grid simply generated by just revolving the axisymmetric grid around center axis. Through the three dimensional calculation around duct, the aerodynamic effectiveness of duct as a lifting surface in airplane mode was investigated. The flow calculations around the control vane (wing) installed in the rear section of duct were conducted The aerodynamic data of wing were compared with the data of the ducts to evaluate the aerodynamic effectiveness of ducts.

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전동식 조향 장치의 성능 평가를 위한 신경 근육계 기반 운전자 모델 개발 (Development of Human Driver Model based on Neuromuscular System for Evaluation of Electric Power Steering System)

  • 이성현;이동필;이재풍;채흥석;이명수;이경수
    • 자동차안전학회지
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    • 제9권3호
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    • pp.19-23
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    • 2017
  • This paper presents a lateral driver model with neuromuscular system to evaluate the performance of electric power steering (EPS). Output of most previously developed driver models is steering angle. However, in order to evaluate EPS system, driver model which results in steering torque output is needed. The proposed lateral driver model mainly consists of 2 parts: desired steering angle calculation and conversion of steering angle into steering torque. Desired steering angle calculation part results in steering angle to track desired yaw rate for path tracking. Conversion of steering angle into torque is consideration with neuromuscular system. The proposed driver model is investigated via actual driving data. Compared to other algorithms, the proposed algorithm shows similar pattern of steering angle with human driver. The proposed driver can be utilized to efficiently evaluate EPS system in simulation level.

Theoretical investigation about the hydrodynamic performance of propeller in oblique flow

  • Hou, Lixun;Hu, Ankang
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제11권1호
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    • pp.119-130
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    • 2019
  • This paper establishes an iterative calculation model for the hydrodynamic performance of propeller in oblique flow based on low order potential based surface panel method. The hydrodynamic performance of propeller is calculated through panel method which is also used to calculate the induced velocity. The slipstream of propeller is adjusted according to the inflow velocity and the induced velocity. The oblique flow is defined by the axial inflow velocity and the incident angle. The calculation results of an instance show that the thrust and torque of propeller decrease with the increase of axial inflow velocity but increase with the incident angle. The unsteadiness of loads on the propeller blade surface gets more intensified with the increases of axial inflow velocity and incident angle. However, comparing with the effect of axial inflow velocity on the unsteadiness of the hydrodynamic performance of propeller, the effect of the incident angle is more remarkable.

PDA 응용을 위한 명함 영상의 회전 보정 (Skew Correction of Business Card Images for PDA Application)

  • 박준효;장익훈;김남철
    • 한국통신학회논문지
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    • 제28권12C호
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    • pp.1225-1238
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    • 2003
  • 본 논문에서는 PDA에 장착된 카메라를 사용하여 획득한 명함 영상에 대한 회전 보정 알고리듬을 제안한다. 제안된 방법은 크게 블록적응 이진화부, 스트라이프 생성부, 회전각 계산부, 그리고 영상 회전부로 구성된다. 블록적응 이진화부에서는 입력 영상의 불균일한 조명이나 그림자의 영향을 감소시키기 위하여 입력 영상을 블록별로 이진화한다. 스트라이프 생성부에서는 인접한 문자와 이들로 이루어진 문자열들을 병합하여 문자열 클러스터를 생성하고, 생성된 클러스터 중에서 회전각 계산에 유용한 것들을 스트라이프로 분류한다. 회전각 계산부에서는 스트라이프들의 방향각을 중심 모멘트를 이용하여 계산하고 이들 방향각을 평균하여 입력 영상의 회전각으로 결정한다. 영상 회전부에서는 입력 영상을 계산된 회전각 만큼 회전시킨다. 실험결과 제안된 방법은 여러 종류의 명함을 다양한 주변 여건에서 PDA로 획득한 시험 영상에 대하여 약 93%의 회전 보정률을 보였다.

Numerical investigation on seismic performance of reinforced rib-double steel plate concrete combination shear wall

  • Longyun Zhou;Xiaohu Li;Xiaojun Li
    • Nuclear Engineering and Technology
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    • 제56권1호
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    • pp.78-91
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    • 2024
  • Double steel plate concrete composite shear wall (SCSW) has been widely utilized in nuclear power plants and high-rise structures, and its shear connectors have a substantial impact on the seismic performance of SCSW. Therefore, in this study, the mechanical properties of SCSW with angle stiffening ribs as shear connections were parametrically examined for the reactor containment structure of nuclear power plants. The axial compression ratio of the SCSW, the spacing of the angle stiffening rib arrangement and the thickness of the angle stiffening rib steel plate were selected as the study parameters. Four finite element models were constructed by using the finite element program named ABAQUS to verify the experimental results of our team, and 13 finite element models were established to investigate the selected three parameters. Thus, the shear capacity, deformation capacity, ductility and energy dissipation capacity of SCSW were determined. The research results show that: compared with studs, using stiffened ribs as shear connectors can significantly enhance the mechanical properties of SCSW; When the axial compression ratio is 0.3-0.4, the seismic performance of SCSW can be maximized; with the lowering of stiffener gap, the shear bearing capacity is greatly enhanced, and when the gap is lowered to a specific distance, the shear bearing capacity has no major affect; in addition, increasing the thickness of stiffeners can significantly increase the shear capacity, ductility and energy dissipation capacity of SCSW. With the rise in the thickness of angle stiffening ribs, the improvement rate of each mechanical property index slows down. Finally, the shear bearing capacity calculation formula of SCSW with angle stiffening ribs as shear connectors is derived. The average error between the theoretical calculation formula and the finite element calculation results is 8% demonstrating that the theoretical formula is reliable. This study can provide reference for the design of SCSW.

개선된 위상 측정 알고리즘과 오차 해석 (An Advanced Phase Angle Measurement Algorithm And Error Analysis)

  • 송영석;김재철;최인규;박종식
    • 전자공학회논문지SC
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    • 제41권3호
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    • pp.25-32
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    • 2004
  • 본 논문에서는 두 개의 사인파 신호의 위상 차이를 계산해 내기위한 개선된 위상 측정 알고리즘을 제안하였다. 이 알고리즘은 두 개의 입력신호의 양자화된 샘플링 데이터를 사용하여 위상과 크기를 구해낸다. 측정 알고리즘의 중요 파라메타들은 몇개의 해석식으로 표현되기 때문에 위상을 계산하기 위해 필요한 연산량이 상당히 줄어들고 따라서 더 빠른 속도로 위상을 계산해 낼 수 있게 되었다. 또한 본 논문에서 제시한 알고리즘을 사용하여 입력신호의 한주기 전체를 샘플링할 경우에는 입력신호에 harmonic distortion이 발생하더라도 위상 측정 오차가 전혀 발생하지 않음을 수식으로 증명하였으며 컴퓨터 시뮬레이션을 통하여 이를 확인하였다. 그리고 입력신호에 가우시안 백색 잡음(white gaussian noise)이 발생할 경우에 위상 측정 오차가 얼마나 발생하는 지에 대하여 여러 가지 관점에서 컴퓨터 시뮬레이션을 수행하고 그 결과를 분석하였다.