• Journal of Power Electronics
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• 제19권5호
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• pp.1224-1234
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• 2019

Hybrid rotor position estimation methods that integrate a fundamental model and high frequency (HF) signal injection are widely used for the wide speed-range sensorless control of interior permanent-magnet synchronous machines (IPMSMs). However, the direct transition of two different schemes may lead to system fluctuations or system instability since two estimated rotor positions based on two different schemes are always unequal due to the effects of parameter variations, system delays and inverter nonlinearities. In order to avoid these problems, a seamless transition strategy to define and construct a virtual q-axis inductance is proposed in this paper. With the proposed seamless transition strategy, an estimated rotor position based on a fundamental model is forced to track that based on HF signal injection before the transition by adjusting the constructed virtual q-axis inductance. Meanwhile, considering that the virtual q-axis inductance changes with rotor position estimation errors, a new observer with a two-phase phase-locked loop (TP-PLL) is developed to accurately obtain the virtual q-axis inductance online. Furthermore, IPMSM sensorless control with maximum torque per ampere (MTPA) operations can be tracked automatically by selecting the proper virtual q-axis inductance. Finally, experimental results obtained from an IPMSM demonstrate the feasibility of the proposed seamless transition strategy.

• 한국항공우주학회지
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• 제47권3호
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• pp.187-194
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• 2019

비축 적외선 탐색기는 공력 가열에 의한 열 차폐 효과를 완화시키기 위해 대공 고속 유도탄의 노즈콘 측면에 장착된다. 탐색기 출력은 표적을 지속적으로 추적하기 위한 유도탄의 롤 기동이 관여되었을 때 더 이상 시선각속도로 간주할 수 없다. 본 논문에서는 2축 김발 위에 장착된 비축탐색기를 위한 시선각속도 계산 방식을 제안한다. 첫째로, 실제 시선각속도 방정식은 해석적으로 도출되지만 조준각 오차 변화율을 측정할 수 없어 구현할 수 없다. 그에 따라 조준각 오차 변화율을 획득하기 위해 1차 지연 근사화를 제안한다. 제안한 시선각속도 계산 방식은 유도탄과 김발의 회전을 고려하여 커플링 효과를 보상할 수 있다. 제안한 방식의 성능을 비선형 6 자유도 시뮬레이션을 통해 검증하였다.

• 한국측량학회지
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• 제26권2호
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• pp.111-116
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• 2008

본 연구는 무선조정 헬리콥터에 1000만 화소 카메라인 비측량용 카메라를 장착하였다. 그리고 상공에서 촬영되는 영상을 지상에서 제어하면서 중복도를 고려하여 촬영하였다. 획득된 영상으로부터 영상정합에 의해 불규칙 삼각망을 추출하여 수치표고모형(DEM)을 나타낼 수가 있었으며, 재래적인 측량방식인 Total Station에 의해 관측된 기준점 및 검사점과의 정확도를 비교 검토한 결과 X방향으로는 $-0.194{\sim}0.224m$, Y축으로는 $-0.088{\sim}0.180m$, Z축으로는 $-0.286{\sim}0.285m$ 정도의 오차를 얻을 수 있었다. 또한, 검사점에 대한 오차의 RMSE를 표현하면, X축 방향으로 0.021388m, Y축 방향으로 0.015285m, Z축 방향으로 0.041872m로 나타났다. 이러한 사진촬영 및 분석방법으로 기존의 Total Station 측량방법보다 더 많은 지형표고자료를 취득하는데 좋은 방법이라 판단된다.

• 대한의용생체공학회:의공학회지
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• 제22권6호
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• pp.543-550
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• 2001

본 연구에서는 하퇴 절단환자에서 고정형. 단축형, 다축형 인공족관절 장착시 지면반발력과 에너지 소비량을 측정하여 하퇴의지에 대한 생체역학적 평가를 하였다. 실험에는 각각 2명의 남성과 여성 하퇴 절단 환자가 3종류의 의지를 착용하고 참여하였으며. 3차원 보행분석은 7개의 기준점에 대하여 전체 입각기에 대한 지면 반발력의 체중에 대한 비율로 나타내었다. 하퇴의지 에너지 소비량은 피 실험자들이 각각 2km/h, 3km/h 그리고 가장 걷기 편한 속도로 런닝머신 위에서 보행하게 하면서 측정하였다 실험결과는 지면반발력에서 다축형 인공족관절 장착시 추진력과 후진력의 보행특성에 대하여 우위를 보이며, 고정형 인공족관절 장착시에는 보행균형과 무게중심의 이동에 대해 상대적인 우위를 보였다. 에너지 소비량은 2.3km/h 이상의 보행속도에서 단축형 인공족관절 장착시 다른 두 의지에 비해 적은량의 에너지 소비를 보였다.

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제52권6호
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• pp.262-270
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• 2003

In this paper, the characteristics of single-phase line-start permanent magnet synchronous motor driven by constant voltage are analyzed on d-q axis vector diagram and compared with that of current controlled motor. The coupled method of symmetrical coordinates and d-q axis voltage equation are applied to the analysis method like the analysis of single-phase induction motor. From the result of the analysis, it is seen that motors driven by constant voltage source have effects on not only the amplitude of current and torque but also current and current phase angle, so overall characteristics such as power factor and load angle are affected by circuit parameters. For precise analysis and design of single-phase line-start synchronous motor, its characteristics should be analyzed on d-q axis vector plan in consideration of the variation of circuit parameters.

• 한국생산제조학회지
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• 제22권3호
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• pp.380-387
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• 2013

In this study, two finite element (FE) models were developed to evaluate the thermal characteristics of a feeding axis of a CNC lathe. One was used for analysis of heat transfer to identify the temperature distribution of the feeding axis and then, the other was used for analysis of thermal deformation to evaluate its structural behavior based on the temperature distribution. The FE models were based on the test standard for the axial thermal displacement. The feeding velocity was composed of three steps: the ascending, constant, and descending velocities. Therefore, the heat generation and convection coefficient were calculated for each velocity and applied to the thermal FE model. The convection coefficient for the ball screw rotation was based on an experimental equation. The result of the analytical thermal displacement was compared with that of the experimental displacement to verify the finite element models.

• International Journal of Automotive Technology
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• 제8권4호
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• pp.455-465
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• 2007

The bushing element shows nonlinear characteristics in both displacements and frequencies, also with hysteretic responses for repeated vibrational excitations. Since the characteristics of the rubber bushing significantly affects the accuracy of the vehicle dynamic simulation result, it should be accurately modeled in the vehicle suspension model. To develop an accurate bushing model for vehicle dynamics analysis, the bushing characteristics under several excitation inputs must be known. In this paper, a 3-axis tester was used to capture the bushing characteristics. The random inputs, sine inputs, and step inputs were imposed on each axis of the bushing. Also, two-axis inputs, the radial-axial and radial-normal inputs, were simultaneously imposed on the tester. Three-axis inputs including the radial-axial-normal direction were supplied to the tester. Bushing characteristics of each case were precisely analyzed. These results could be available for dynamic modeling of bushing.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2001년도 추계학술대회(한국공작기계학회)
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• pp.399-406
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• 2001

This study describes the geometric characteristic and the 5-axis machining method of end mill body with insert tip. The geometry of end mill body is consisted of the flute part and the insert tip part. Thus, this study defines the flute part as ruled surface with constant helix angle and the insert tip part as rectangular plane on general direction. The geometric algorithm and the 5-axis NC part program were calculated by our programmed software and a sampled end mill body was machined on 5-axis machining center equipped with two index tables. The machined end mill body with insert tip was very agreeable to the designed end mill body with insert tip. Thus, the method proposed in this study may be very useful for the machining of end mill body with insert tip.

• 한국자동차공학회논문집
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• 제8권6호
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• pp.267-278
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• 2000

Vehicle dynamic models in handing and stability analysis are divided into three groups: bicycle model, roll axis model and full vehicle model. Bicycle model is a simple linear model, which hag two wheels with load transfer being ignored. Roll axis model treats left and right wheels independently. In this model, load transfer has a great effect on nonlinearity of tire model. Effects of suspension system can be analyzed by using full vehicle model, which is included suspension stroke motions. In this paper, these models are validated and compared through comparison with road test, and the effects of suspension kinematics and compliance characteristics on vehicle motion are analyzed. In handling and stability analysis, roll axis model can simulate the real vehicle motion more accurately than full vehicle model. Compliance steer has a significant effect, but the effect of suspension kinematics is negligible.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.482-485
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• 1996

We design a homing guidance law based on the proportional navigation for the fast-rolling, single-axis control missiles and analyse the misdistance of the designed guidance system. The guidance law includes a compensation scheme which compensates for the phase-shift between the commanded and achieved acceleration which is peculiar to the fast rolling airframe with single-axis control. In the error analysis of the guidance system, we calculate the misdistance with respect to the target maneuver on the 3-dimensional space via direct simulations. Also, we conduct adjoint simulation on the 2-dimensional plane in case that phase-shift is perfectly compensated. Finally we approximate the linear time-varying dynamics of the missile with autopilot to a linear time-invarient system, and as a result we can find the misdistance as a closed-form.