• 제어로봇시스템학회논문지
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• 제20권4호
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• pp.468-473
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• 2014

This paper describes the in-flight alignment of SDINS (Strapdown Inertial Navigation Systems) using an EKF (Extended Kalman Filter) and a UKF (Unscented Kalam Filter), which allow large initial attitude error uncertainty. Regardless of the inertial sensors, there are nonlinear error dynamics of SDINS in cases of large initial attitude errors. A UKF that is one of the nonlinear filtering approaches for IFA (In-Flight Alignment) are used to estimate the attitude errors. Even though the EKF linearized model makes velocity errors when predicting incorrectly in case of large attitude errors, a UKF can represent correctly the velocity errors variations of attitude errors with nonlinear attitude error components. Simulation results and analyses show that a UKF works well to handle large initial attitude errors of SDINS and the alignment error attitude estimation performance are quite improved.

• International Journal of Aeronautical and Space Sciences
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• 제17권2호
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• pp.222-231
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• 2016

This paper proposes a new method achieving computationally efficient attitude reference system for low cost strapdown sensors and microprocessor platform. The main idea in this method is to define and compare velocity differential vectors, geometrically computed from INS and GPS data with different update rate, for generating attitude error measurements which is further used for filter construction. A quaternion based Kalman filter configuration is applied for the attitude estimation with the adapted measurement model of differential vector comparison. Linearized model for Extended Kalman Filter and low pass filtered characteristics of measurement greatly extend the affordability of the proposed algorithm to the field of simple low cost embedded systems. For performance verification, experiment are done employing a practical low cost MEMS IMU and GPS receiver specification. Performance comparison with a high grade navigation system demonstrated good estimation result.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제31회 추계학술대회논문집
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• pp.192-195
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• 2008

다중 트림 상태에서 헬리콥터용 소형 터보샤프트 엔진에 부착된 센서의 고장을 검출하기 위한 방법을 제시한다. 먼저 헬리곱터의 엔진, 로터, 되먹임(feedback) 제어루프가 포함된 비선형 모델을 구하고 다중 트림 상태에서의 선형 모델을 추출하였다. 고장 검출 방법은 칼만필터에 기반한 방법을 채용하였는데 트림 상태가 변화할 때에 필터의 추정값이 연속적으로 변화하도록 상태변수 초기값을 재구성하였다. 또한 어떠한 센서가 고장이 일어났는지 구분할 수 있도록 어떤 센서의 고장을 검출한 다음 문제가 없는 경우 다음 센서의 고장 검출을 수행하는 단계적인 방법을 사용하였다. 시뮬레이션을 통하여 제시한 방법이 다중 트림 상태에서 각 센서의 고장을 잘 검출함을 보였다.

• 대한전자공학회논문지TC
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• 제37권3호
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• pp.28-34
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• 2000

본 논문에서는 선형화된 리카티(Riccati) 방정식에 후리에 변환을 적용하여 주파수 특성함수와 불균일 테이퍼 전송선상의 새로운 임피던스 분포를 구한다. 리카티 방정식을 선형화 함으로써 발생할 수 있는 오차를 보상하기 위해 임의의 Taylor 급수를 임피던스 항에 추가한다. 추가된 항은 불균일 전송선 양단의 임피던스 불연속을 제거하는 역할을 한다. 설계과정을 통해서 여파기의 과녁 주파수 특성에 접근해 가는 것을 축차법을 통해서 보이며, 위상함수의 역할을 예제를 통해서 보인다. 본 논문에서 제시한 설계법은 불균일 테이퍼 전송선의 설계에 뛰어난 융통성을 제공하므로, 임의의 주파수 대역특성을 만족시키는 여파기 및 임피던스 정합회로 설계에 응용할 수 있다.

• 대한조선학회논문집
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• 제40권5호
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• pp.43-52
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• 2003

Two methods which estimate manoeuvring derivatives in the model of hydrodynamic force and moment acting on a manoeuvring ship using sea trial data were compared. One is the widely used parameter estimation method by using the Extended Kalman Filter (EKF), which estimates state variables of linearized state space model at every instant after dealing with the coefficients as the augmented state variables. The other one is the Estimation-Before-Modeling (EBM) technique, so called the two-step method. In the first step, hydrodynamic force of which dynamic model is assumed the third-order Gauss-Markov process is estimated along with motion variables by the EKF and the modified Bryson-Frazier smoother. Then, in the next step, manoeuvring derivatives are identified through the regression analysis. If the exact structure of hydrodynamic force could be known, which was an ideal case, the EKF method would be regarded as being more superior compared to the EBM technique. However the EBM technique was more robust than the EKF method from a realistic point of view where the assumed model structure was slightly different from the real one.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 춘계학술대회논문집
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• pp.559-564
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• 2002

Cross-talk cancellation, inverse filter design or deconvolution in a generic term, is a vital process for a virtual sound realization in the stereo sound reproduction system. Most, if not all, of the design algorithms available for the inverse filter are based on a linearized model of the real physical plant. The result of such a plant-based design method, which may be referred to here as the indirect method, is biased due to both modelling and inversion errors. This paper presents a novel direct cross-talk cancellation method that may be free from the inversion error. The direct method can directly models the inverse filter by a suitable rearrangement of the input and output ports of the original plant so that no inversion is required here. Advantages are discussed with various experiments in an anechoic chamber using a PC soundcard. Binaural reproduction tests conducted showed that the conventional indirect method yields about 8 % reproduction performance error on both ear positions, whereas the direct method offers about 3 %.

• 전력전자학회논문지
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• 제14권2호
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• pp.134-141
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• 2009

전원사고로 인하여 야기되는 전원급변상황에서 위상각의 새로운 PLL 방법은 추종속도를 개선시키기 위하여 제안되었다. 일반적으로 측정된 전원이 이상적이지 않고 고조파가 포함되어 있으며 센서의 노이즈 때문에 동기좌표계 PLL의 피드백 루프에는 LPF를 사용하고 있다. 그러므로 과도상태의 빠른 동특성을 얻기 위해서 LPF를 고려한 PLL시스템의 모델링을 제안하였다. 또한 전원의 급변 시에 빠른 위상각 검출을 위한 방법으로 자동으로 제어기 대역폭과 LPF의 차단주파수를 변동시키는 가변 파라미터 PLL방법을 제안하였다. 이를 시뮬레이션과 실험을 통해 검증하여 유효성을 보이고자 한다.

• 제어로봇시스템학회논문지
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• 제7권11호
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• pp.953-957
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• 2001

This paper is concerned with a transfer alignment method for the SDINS under ship motions. Major error sources of transfer alignment are data transfer time-delay, lever-arm velocity and ship body flexure. Specifically, to reduce alignment errors induced by measurement time-delay effects, the error compensation method through delay state augmentation is suggested. A linearized error model for the velocity and attitude matching transfer alignment system is first derived by linearizing the nonliner measurement equation with respect to its time delay and augmenting the delay state into the conventional linear state equations. And then it is shown via observability analysis and computer simulations that the delay state can be estimated and compensated during ship motions resulting in considerably less alignment errors.

• 한국군사과학기술학회지
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• 제4권1호
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• pp.225-233
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• 2001

This paper deals with the transfer alignment problem of SDINS(StrapDown Inertial Navigation System) subjected to roll and pitch motions of the ship. Specifically, to reduce alignment errors induced by measurement time-delay and ship body flexure, an error compensation method is suggested based on delay state augmentation and DCM(Direction Cosine Matrix) partial matching. A linearized error model for the velocity and attitude matching transfer alignment system is first derived by linearizing the nonlinear measurement equation with respect to its time delay and augmenting the delay state into the conventional linear state equations. And then DCM partial matching is properly combined to reduce effects of a ship's Y axis flexure. The simulation results show that the suggested method is effective enough resulting in considerably less azimuth alignment errors.

• 한국진공학회지
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• 제12권S1호
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• pp.33-35
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• 2003

The electrooptic properties of the reflected light in a reflective mode, $45^{\circ}C$twisted nematic liquid crystal (TNLC) cell were investigated in the voltage regions near and away from the Freedericksz transition threshold. The measured reflectivity away from the threshold voltage ($V_th$) could not be described by the model which assurnes a constant tilt angle as well as a linearized distribution of twist angle across the cell, although the data are well fitted near $V_th$. We found that in the voltage region away from $V_th$, the model considering the distributions of the tilt angle and the twist angle should be applied for the calculation of the reflectivity. The director-axis distributions were obtained from the numerical integration of the Euler-Lagrange equation.