• 전기학회논문지
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• 제61권2호
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• pp.284-290
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• 2012

This paper addresses a new passive target tracking problem using the range differences measured by cooperative UAVs. In order to solve the range difference based passive target tracking problem within the framework of linear robust state estimation, the uncertain linear measurement model which contains the stochastic parameter uncertainty is derived by using the noisy range difference measurements. To cope with the performance degradation due to the stochastic parameter uncertainty, the recently developed non-conservative robust Kalman filtering technique [1] is applied. For the cruciform formation flying UAVs, the relationship between the target tracking performance and the measurement errors is quantitatively analyzed. The proposed filter has practical advantages over the classical nonlinear filters because, for its recursive linear structure, it can provide satisfactory convergence properties and is suitable for real-time multiple UAVs applications. Through the simulations, the usefulness of the proposed method is demonstrated.

• Journal of Astronomy and Space Sciences
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• 제29권4호
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• pp.363-374
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• 2012

This paper studies the problem of tracking a re-entry vehicle (RV) in order to predict its impact point on the ground. Re-entry target dynamics combined with super-high speed has a complex non-linearity due to ballistic coefficient variations. However, it is difficult to construct a database for the ballistic coefficient of a unknown vehicle for a wide range of variations, thus the reliability of target tracking performance cannot be guaranteed if accurate ballistic coefficient estimation is not achieved. Various techniques for ballistic coefficient estimation have been previously proposed, but limitations exist for the estimation of non-linear parts accurately without obtaining prior information. In this paper we propose the ballistic coefficient ${\beta}$ model-based interacting multiple model-extended Kalman filter (${\beta}$-IMM-EKF) for precise tracking of an RV. To evaluate the performance, other ballistic coefficient model based filters, which are gamma augmented filter, gamma bootstrapped filter were compared and assessed with the proposed ${\beta}$-IMM-EKF for precise tracking of an RV.

• 한국음향학회지
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• 제21권1호
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• pp.11-18
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• 2002

본 논문에서는 부가 잡음에 오염된 음성신호에 이득 적응을 가지는 음성인식을 시간 영역에서 다루었다. 잡음은 유색잡음이라고 가정한다. 전화망에서 마찰음 (fricative), 운음 (glides), 유음 (liquds), 그리고 천이영역(transition region)과 같은 음성 신호의 뚜렷한 비정상상태를 극복하기 위해서 NAR-HMM (nonstationary autoregressive HMM)7을 제안하였다. 비정상상태 AR 처리는 M개의 알고 있는 기저 함수 (basis function)의 선형 결합으로 이루어진 다항 함수 (polynomial function)로 나타낼 수 있다. 오염된 신호만을 이용할 수 있을 때, 잡음의 추정 (estimation)문제는 필연적으로 발생한다. 다중 Kalman 필터를 사용함으로써, 잡음모델의 추정과 음성의 이득곡선 (gain contour)을 수행하였다. 제안한방법의 잡음 추정은 오염된 신호로부터 효과적으로 잡음을 제거하여 깨끗한 음성신호를 얻을 수 있었다. 또한 잡음 추정을 하는 일반적인 ARHMM보다 제안한 NAR-HMM이 약 2-3%의 인식성능을 향상시켰다.

• Advances in aircraft and spacecraft science
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• 제4권2호
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• pp.185-202
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• 2017

In a flexible airvehicle, an assessment of the structural coupling levels through analysis and experiments provides structural data for the design of notch filters which are generally utilized in the flight control system to attenuate the flexible response pickup. This is necessitated as during flight, closed loop control actuation driven with flexible response inputs could lead to stability and performance related problems. In the present work, critical parameters influencing servoelastic response have been identified. A sensitivity study has been carried out to assess the extent of influence of each parameter. A multi-parameter tuning approach has been implemented to achieve an enhanced analytical model for improved predictions of aircraft servoelastic response. To illustrate the model updation approach, initial and improved test analysis correlation of lateral servoelastic responses for a generic flexible airvehicle are presented.

• 한국통신학회논문지
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• 제40권7호
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• pp.1239-1247
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• 2015

Frequency-division duplex (FDD) massive multiple-input multiple-output (MIMO) 시스템에서 하향 링크 채널 추정의 계산 복잡도는 기지국의 안테나 개수와 비례한다. 그러므로 이러한 시스템에서의 효율적인 채널 추정 방식이 연구 될 필요가 있다. 본 논문에서는 채널이 시간적, 공간적 상관관계를 가지는 모델에서 Kalman 필터와 least mean square (LMS) 등과 같은 적응 신호처리 기법을 이용한 채널 추정 방식을 제안한다.

• 한국산업정보학회논문지
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• 제22권5호
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• pp.39-49
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• 2017

인공위성 발사를 위한 우주발사체는 효율적인 비행을 위하여 다단으로 구성이 되며 단분리, 연료점화 및 연소종료 등의 비행이벤트를 거쳐서 임무를 완수하게 된다. 이 과정에서 발사체는 추력이 발생하는 동력비행구간과 추력이 없는 탄도비행구간의 과정을 반복하여 겪게 된다. 이러한 우주 발사체의 비행특성을 하나의 동력학 모델로 표현하기는 어렵기 때문에 다중모델을 사용하는 추적 알고리즘에 대한 연구가 많이 진행되어 왔다. 다중모델 추적 알고리즘을 사용하는 경우에는 추적 성능의 개선을 기대할 수 있지만, 사용할 각 동력학 모델들을 적절히 선정해야 하는 어려움이 있으며 또한 다중모델 사용으로 인해 계산양이 증가하는 단점이 있다. 본 논문에서는 등가속도 모델과 적응형 Singer 모델을 사용하는 두 개의 칼만필터만으로 다양한 비행특성을 가지는 우주발사체를 효과적으로 추적하는 방법을 제안한다.

• 한국항행학회논문지
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• 제15권4호
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• pp.487-494
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• 2011

레이더를 이용한 항적 융합 알고리즘은 반드시 필요하며, 이를 통해서 높은 신뢰성을 확보할 수 있다. 본 논문에서는 칼만필터 보다 성능이 좋다고 알려진 IMM(Interacting Multiple Model) 필터를 이용하여 다중 레이더 융합 알고리즘을 제안하였다. 분산형 융합 방식을 적용하였고, 부필터 3개, 주필터 1개를 이용하였다. 성능분석은 등속운동, 가속운동, 선회 등 항공기 기동을 묘사한 가상의 레이더 데이터를 이용하여 분석하였다. 성능분석 결과, 항공기가 기동하는 구간에서도 좋은 추적 성능을 보였다.

• Journal of Power Electronics
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• 제15권6호
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• pp.1664-1672
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• 2015

This paper proposes a series arc fault detection algorithm which incorporates peak voltage and harmonic current detectors for single-phase boost power factor correction (PFC) rectifiers. The series arc fault model is also proposed to analyze the phenomenon of the arc fault and detection algorithm. For arc detection, the virtual dq transformation is utilized to detect the peak input voltage. In addition, multiple combinations of low- and high-pass filters are applied to extract the specific harmonic components which show the characteristics of the series arc fault conditions. The proposed model and the arc detection method are experimentally verified through a boost PFC rectifier prototype operating under the grid-tied condition with an artificial arc generator manufactured under the guidelines for the Underwriters Laboratories (UL) 1699 standard.

• 제어로봇시스템학회논문지
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• 제17권11호
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• pp.1117-1124
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• 2011

An integrated fault detection and isolation method is proposed in this paper. The main objective of this paper is development fault detection, isolation and diagnosis algorithm based on the DKF (Decentralized Kalman Filter) and the bank of IMM (Interacting Multiple Model) filters using penalty scalar for both partial and total faults and the outlier detection algorithm for preventing false alarm also included. The proposed FDI (Fault Detection and Isolation) scheme is developed in four phases. In the first phase, the outlier detection filter is designed to prevent false alarm as a pre-filter. In the second phases, two local filters and master filter are designed to detect sensor faults. In the third phases, the proposed FDI scheme checks sensor residual to isolate sensor faults and 11 EKFs actuator fault models are designed to detect wherever actuator faults occur. In the last phases, four filters are designed to identify the fault type which is either the total fault or partial fault. The developed scheme can deal with not only sensor and actuator faults, but also preventing false alarm. An important feature of the proposed FDI scheme can decreases fault isolation time and figure out not only fault detection and isolation but also fault type identification. To verify the proposed FDI algorithm performance, the Simulator is also developed under the Matlab/Simulink environment.

• 한국대기환경학회지
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• 제19권6호
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• pp.701-717
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• 2003

The objective of this study was to extensively estimate the air quality trends of the study area by surveying con-centration trends in months or seasons, after analyzing the mass concentration of PM-10 samples and the inorganic lements, ion, and total carbon in PM-10. Also, the study introduced to apply the PMF (Positive Matrix Factoriza-tion) model that is useful when absence of the source profile. Thus the model was thought to be suitable in Korea that often has few information about pollution sources. After obtaining results from the PMF modeling, the existing sources at the study area were qualitatively identified The PM-10 particles collected on quartz fiber filters by a PM-10 high-vol air sampler for 3 years (Mar. 1999∼Dec.2001) in Kyung Hee University. The 25 chemical species (Al, Mn, Ti, V, Cr, Fe, Ni, Cu, Zn, As, Se, Cd, Ba, Ce, Pb, Si, N $a^{#}$, N $H_4$$^{+}$, $K^{+}$, $Mg^{2+}$, $Ca^{2+}$, C $l^{[-10]}$ , N $O_3$$^{[-10]}$ , S $O_4$$^{2-}$, TC) were analyzed by ICP-AES, IC, and EA after executing proper pre - treatments of each sample filter. The PMF model was intensively applied to estimate the quantitative contribution of air pollution sources based on the chemical information (128 samples and 25 chemical species). Through a case study of the PMF modeling for the PM-10 aerosols. the total of 11 factors were determined. The multiple linear regression analysis between the observed PM-10 mass concentration and the estimated G matrix had been performed following the FPEAK test. Finally the regression analysis provided source profiles (scaled F matrix). So, 11 sources were qualitatively identified, such as secondary aerosol related source, soil related source, waste incineration source, field burning source, fossil fuel combustion source, industry related source, motor vehicle source, oil/coal combustion source, non-ferrous metal source, and aged sea- salt source, respectively.ively.y.