• International Journal of Internet, Broadcasting and Communication
• /
• 제13권2호
• /
• pp.76-81
• /
• 2021

This study proposes a method to reduce the phase error of the received signal to detect the object bearing. The phase shift of the received signal occurs due to the multipath of the signal by natural structure or artificial structures. When detecting the direction of the object using radio waves, the phase of the received signal cannot be accurately detected because of the phase bearing error in the object detection direction. The object detection direction estimation depends on the phase difference, antenna installation distance, signal source wavelength, frequency band and bearing angle. This study reduces the error of the phase bearing by using the phase delay of the relative phase difference for the signals incident on the two antennas. Through simulation, we analyzed the object direction detection performance of the proposed method and the existing method. Three targets are detected from the [-15°, 0°, 15°] direction. The existing method detects the target at [-13°, 3°, 17°], and the proposed method detects the at [-15°, 0°, 15°]. As a result of the simulation, the target detection direction of the proposed method is improved by 2 degrees compared to the existing method.

• 방송공학회논문지
• /
• 제17권1호
• /
• pp.81-94
• /
• 2012

본 논문에서는 두 영상간의 회전각도를 추정하는 방법들 중에서, 정확도에서 높은 성능을 제공하는 저니키 모멘트의 위상을 이용한 방법들의 회전각도 추정 결과의 정확도를 비교하여 제시하고, 기존의 방법들보다 정확하게 각도를 추정하는 angular radial transform(ART) 계수들의 위상성분을 이용한 회전각도 추정방법을 제안한다. 제안하는 방법은 Revaud가 제안한 저니키 모멘트를 이용한 회전각도 추정 방법[1]을 ART로 확장한 방법이다. ART는 저니키 모멘트에 비해서 회전에 의한 영상의 변화를 보다 효과적으로 서술할 수 있는 기저함수의 생성이 가능하기 때문에 저니키 모멘트보다 두 영상간의 회전각도를 정확히 추정하는 것을 가능하게 한다. MPEG-7 데이터셋을 이용한 실험 결과, 제안하는 방법이 제곱평균제곱근오차(root mean square error) 대 커버리지(coverage)를 기준으로한 성능비교에서 가장 우수한 성능을 보였다.

• Journal of Power Electronics
• /
• 제18권5호
• /
• pp.1347-1356
• /
• 2018

In a three-phase system, three-phase AC signals can be translated into two-phase DC signals through a coordinate transformation. Thus, the PI regulator can realize a zero steady-state error for the DC signals. In the control of a three-phase grid-connected inverter, the phase angle of grid is normally detected by a phase-locked loop (PLL) and takes part in a coordinate transformation. A novel control strategy for a three-phase grid-connected inverter with a frequency-locked loop (FLL) based on coordinate transformation is proposed in this paper. The inverter is controlled as a current supply. The grid angle, which takes part in the coordinate transformation, is replaced by a periodic linear changing angle from $-{\pi}$ to ${\pi}$. The changing angle has the same frequency but a different phase than the grid angle. The frequency of the changing angle tracks the grid frequency by the negative feedback of the reactive power, which forms a FLL. The control strategy applies to non-ideal grids and it is a lot simpler than the control strategies with a PLL that are applied to non-ideal grids. The structure of the FLL is established. The principle and advantages of the proposed control strategy are discussed. The theoretical analysis is confirmed by experimental results.

• 한국항해항만학회:학술대회논문집
• /
• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
• /
• pp.535-540
• /
• 2006

The relationship between the observable noise model and the satellite elevation angle can be modeled quite well by an exponential function.[Jin, 1996] Noise size and dependence on the elevation angle are, however, different for each observation and receiver type. Therefore, the coefficient determination of this model is an issue, and various methods including PR-CP, single difference, and time difference have been suggested. The limitations of them are difficulty to model the carrier phase noise and to eliminate bias. To overcome these disadvantages for using Jin's model, we suggest zero baseline double difference (DD) and noise sorting algorithm. Data DD technique in zero baseline is useful to eliminate all the troublesome GPS biases, and the remaining error is the sum of GPS measurement noises from two satellites. These DD residuals for hours should be sorted by the combination of satellite elevation angles, and then variance value of the residual for each combination can be estimated. Using these values, we construct an over-determined linear equation whose solution is a set of noise variance for each satellite elevation angle. With 24hr Trimble 4000ssi data, we easily worked out the coefficients of the noise model not only for pseudorange but also for carrier phase. We estimated the standard deviation of the measurement DD using our model, and plotted 1 and 3 sigma lines for every epoch to verify the representation of the residual error. 63.3% of pseudorange residual and 65.9% of phase error did not exceed the 1 sigma lines. Additionally, 99.2% and 99.5% of them lied within 3sigma line. These figures prove that the Gaussian property of measurement noise, and that the suggested model by our algorithm corresponds to the observable noise information.

• Journal of Electrical Engineering and Technology
• /
• 제8권5호
• /
• pp.1221-1226
• /
• 2013

In this paper, the equivalent circuit for the efficiency calculation by precise estimation of the linkage flux, inductance and iron loss resistance was calculated accurately. In addition, the driving characteristics according to the current phase angle are analyzed and the maximum efficiency point is calculated. And then, analyzed and experimental values of the efficiency were compared. So, causes of error were expected to be vibration and noise by harmonic distortion of the voltage and current, and mechanical loss of dynamometer. In addition, the driving characteristics according to the current phase angle are analyzed and the maximum efficiency point is calculated.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2008년도 추계학술대회 논문집 전기설비전문위원
• /
• pp.61-63
• /
• 2008

We established a system to evaluate the ratio error and phase angle error of electronic voltage transformer using high voltage capacitance bridge and standard capacitors. The uncertainty of evaluation system is about 0.005% in ratio error and 1.5 min in phase angel error.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
• /
• pp.1099-1102
• /
• 1996

In this paper, roll/yaw attitude control of spacecraft using a double gimbaled wheel is discussed with two feedback controllers designed. One is a PD controller with no phase difference between roll and yaw control input. The other is a PD controller with a phase lag compensator about the yaw control input. The phase lag compensator is designed as a first order system and a lag parameter is designed for the yaw angle control. There are two case simulations for each controller ; constant disturbance torques and initial errors of nutation at motion. We obtain the results through simulations that steady-state error and rising time of yaw angle are determined by the compensator. Simulation parameters used in this study are the values of KOREASAT F1.

• 한국전자파학회논문지
• /
• 제29권11호
• /
• pp.828-833
• /
• 2018

일반적으로 반사파 및 공진이 위상 왜곡에 영향을 준다고 많이 알려져 있지만, 그 두 가지 이유 이외에 안테나 임피던스 변화에 따라서도 위상 지연을 왜곡시킬 수 있다는 것을 확인하였다. 본 논문에서는 상호 결합 영향을 모두 고려한 안테나 임피던스 $Z_A$에 따른 위상 지연 오차를 분석하고, 이에 따른 빔조향 특성을 확인하였다. 안테나 임피던스에 대한 반사손실의 최대값($RL_{max}$)이 -10 dB와 -7 dB일 때 모든 주파수에서 각각 $0.051{\lambda}$에 해당하는 $18.5^{\circ}$와 $0.074{\lambda}$에 해당하는 $26.5^{\circ}$의 최대 위상 지연 오차가 발생하는 것을 확인하였다. 8개의 선형 배열 안테나를 통해 몬테 카를로 시뮬레이션을 진행한 결과, $18.5^{\circ}$와 $26.5^{\circ}$의 균등 분포 위상 오차를 갖는 상황에서 각각 $0{\sim}30^{\circ}$의 빔조향을 했을 때 목표 빔조향각과 해당 위상 오차에 의해 틀어져서 관측되는 조향각 사이의 RMS 오차는 $0.19{\sim}0.4^{\circ}$이고, 표준편차는 $0.14{\sim}0.33^{\circ}$이다. 이때 사이드 로브 레벨은 -12.8 dB의 이론치로부터 위상 오차에 의해 0.74~1.21 dB 만큼 증가하고 사이드 로브 레벨 증가량의 표준 편차는 0.31~0.51 dB를 갖는다. 이를 스파이럴 안테나 8개 배열 구조를 설계하여 검증하였다.

• Journal of Electrical Engineering and Technology
• /
• 제9권2호
• /
• pp.478-488
• /
• 2014

Torque pulsation mechanism and highly nonlinear magnetic characterization of switched reluctance motors(SRM) lead to unfavorable torque ripple and limit the variety of applications in industry. In this paper, a modification method proposed for torque ripple minimization of SRM based on conventional torque sharing functions(TSF) to improve maximum speed of torque ripple-free operation considering converter limitations. Due to increasing phase inductance in outgoing phase during the commutation region, reference current tracking can be deteriorated especially when the speed increased. Moreover, phase torque production in incoming phase may not be reached to the reference value near the turn-on angle in which the incremental inductance would be dramatically decreased. Torque error for outgoing phase can cause increasing the resultant motor torque while it would be negative for incoming phase and yields reducing the motor torque. In this paper, a modification method is proposed in which phase torque tracking error for each phase under the commutation added to the other phase so that the resultant torque remained in constant level. This yields to extend constant torque region and reduce peak phase current when the speed increased. Simulation and experimental results for four phase 4 KW, 8/6 SRM validate the effectiveness of the proposed scheme.

• 한국전자파학회논문지
• /
• 제29권9호
• /
• pp.735-738
• /
• 2018

항공용 안테나 하이브리드 모노펄스 레이다 시스템을 이용하여 지상 이동표적 탐지 시, 표적의 방위각 정확도는 시스템 내 채널 간 위상 불균형에 따른 모노펄스 기울기 추정 정확도에 지배적으로 영향을 받는다. 본 논문에서는 안테나와 180도 하이브리드의 물리적 길이 차이에 의한 위상 불균형을 효과적으로 보상할 수 있는 방법을 제안 하였다. 비행시험을 통하여 제안된 방법의 성능을 검증한 결과, 보상 전보다 유의한 성능개선 효과를 확인할 수 있었다.