• 제목/요약/키워드: unscented transform

검색결과 9건 처리시간 0.022초

무향 변환 기반 필터링을 이용한 전술표적 추적 성능 연구 (Study on Tactical Target Tracking Performance Using Unscented Transform-based Filtering)

  • 변재욱;정효영;이새움;김기성;김기선
    • 한국군사과학기술학회지
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    • 제17권1호
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    • pp.96-107
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    • 2014
  • Tracking the tactical object is a fundamental affair in network-equipped modern warfare. Geodetic coordinate system based on longitude, latitude, and height is suitable to represent the location of tactical objects considering multi platform data fusion. The motion of tactical object described as a dynamic model requires an appropriate filtering to overcome the system and measurement noise in acquiring information from multiple sensors. This paper introduces the filter suitable for multi-sensor data fusion and tactical object tracking, particularly the unscented transform(UT) and its detail. The UT in Unscented Kalman Filter(UKF) uses a few samples to estimate nonlinear-propagated statistic parameters, and UT has better performance and complexity than the conventional linearization method. We show the effects of UT-based filtering via simulation considering practical tactical object tracking scenario.

GPS를 이용한 자세결정에서 Unscented Kalman Filter를 이용한 성능 향상 (Performance Improvement in GPS Attitude Determination Using Unscented Kalman Filters)

  • 천세범;이은성;강태삼;지규인;이영재
    • 제어로봇시스템학회논문지
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    • 제11권7호
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    • pp.621-626
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    • 2005
  • With precise GPS carrier positioning result, we can get attitude information if GPS antenna has adequate attaching position on the vehicle. In this case, baseline length information can be bandied as an additional measurement or constraint. In this paper, we have proposed a method to improve the attitude accuracy. To overcome nonlinearity of baseline observation model, we analyze attitude estimation result using existing estimation method like a least square method and Kalman filter, and apply a new nonlinear estimation method an unscented Kalman filter Finally we confirm the improvement of attitude estimation result in the case of appling the unscented Kalman filter.

INS/GPS 강결합 기법에 대한 EKF 와 UKF의 성능 비교 (A Performance Comparison of Extended and Unscented Kalman Filters for INS/GPS Tightly Coupled Approach)

  • 김광진;유명종;박영범;박찬국
    • 제어로봇시스템학회논문지
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    • 제12권8호
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    • pp.780-788
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    • 2006
  • This paper deals with INS/GPS tightly coupled integration algorithms using extend Kalman filter (EKF) and unscented Kalman filter (UKF). In the tightly coupled approach, nonlinear pseudorange measurement models are used for the INS/GPS integration Kalman filter. Usually, an EKF is applied for this task, but it may diverge due to poor functional linearization of the nonlinear measurement. The UKF approximates a distribution about the mean using a set of calculated sigma points and achieves an accurate approximation to at least second-order. We introduce the generalized scaled unscented transformation which modifies the sigma points themselves rather than the nonlinear transformation. The generalized scaled method is used to transform the pseudo range measurement of the tightly coupled approach. To compare the performance of the EKF- and UKF-based tightly coupled approach, real van test and simulation have been carried out with feedforward and feedback indirect Kalman filter forms. The results show that the UKF and EKF have an identical performance in case of the feedback filter form, but the superiority of the UKF is demonstrated in case of the feedforward filer form.

Precise Orbit Determination Based on the Unscented Transform for Optical Observations

  • Hwang, Hyewon;Lee, Eunji;Park, Sang-Young
    • Journal of Astronomy and Space Sciences
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    • 제36권4호
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    • pp.249-264
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    • 2019
  • In this study, the precise orbit determination (POD) software is developed for optical observation. To improve the performance of the estimation algorithm, a nonlinear batch filter, based on the unscented transform (UT) that overcomes the disadvantages of the least-squares (LS) batch filter, is utilized. The LS and UT batch filter algorithms are verified through numerical simulation analysis using artificial optical measurements. We use the real optical observation data of a low Earth orbit (LEO) satellite, Cryosat-2, observed from optical wide-field patrol network (OWL-Net), to verify the performance of the POD software developed. The effects of light travel time, annual aberration, and diurnal aberration are considered as error models to correct OWL-Net data. As a result of POD, measurement residual and estimated state vector of the LS batch filter converge to the local minimum when the initial orbit error is large or the initial covariance matrix is smaller than the initial error level. However, UT batch filter converges to the global minimum, irrespective of the initial orbit error and the initial covariance matrix.

심층 신경망을 이용한 실시간 유도탄 파편 탄착점 및 분산 추정 (Real-Time Estimation of Missile Debris Predicted Impact Point and Dispersion Using Deep Neural Network)

  • 강태영;박국권;김정훈;유창경
    • 한국항공우주학회지
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    • 제49권3호
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    • pp.197-204
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    • 2021
  • 유도탄의 비행 시험 중 고장 또는 비정상적인 기동이 발생하는 경우 비행을 계속하지 않도록 의도적으로 자폭한다. 이때 파편이 발생하며 안전 지역을 벗어났는지 여부를 실시간으로 추정하는 것이 중요하다. 본 논문에서는 Fully-Connected Neural Network(FCNN)를 이용하여 실시간으로 파편의 예상 낙하 영역 및 낙하 시간을 추정하는 방법을 제안한다. 많은 양의 학습 데이터 생성을 위해 Unscented Transform(UT)를 적용하였으며 신뢰도 확보를 위해 Monte-Carlo(MC) 시뮬레이션과 비교하여 파라미터를 선정하였다. 또한 제안한 방법의 추정 결과를 MC와 비교하여 성능을 분석하였다.

Investigation into SINS/ANS Integrated Navigation System Based on Unscented Kalman Filtering

  • Ali, Jamshaid;Jiancheng, Fang
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2005년도 ICCAS
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    • pp.241-245
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    • 2005
  • Strapdown inertial navigation system (SINS) integrated with astronavigation system (ANS) yields reliable mission capability and enhanced navigational accuracy for spacecrafts. The theory and characteristics of integrated system based on unscented Kalman filtering is investigated in this paper. This Kalman filter structure uses unscented transform to approximate the result of applying a specified nonlinear transformation to a given mean and covariance estimate. The filter implementation subsumed here is in a direct feedback mode. Axes misalignment angles of the SINS are observation to the filter. A simple approach for simulation of axes misalignment using stars observation is presented. The SINS error model required for the filtering algorithm is derived in space-stabilized mechanization. Simulation results of the integrated navigation system using a medium accuracy SINS demonstrates the validity of this method on improving the navigation system accuracy with the estimation and compensation for gyros drift, and the position and velocity errors that occur due to the axes misalignments.

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DWT/UKF를 이용한 수면 BEACON의 위치추정 (Estimated Position of Sea-Surface Beacon Using DWT/UKF)

  • 윤바다;윤하늘;최성희;이장명
    • 제어로봇시스템학회논문지
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    • 제19권4호
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    • pp.341-348
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    • 2013
  • A location estimation algorithm based on the sea-surface beacon is proposed in this paper. The beacon is utilized to provide ultrasonic signals to the underwater vehicles around the beacon to estimate precise position of underwater vehicles (ROV, AUV, Diver robot), which is named as USBL (Ultra Short Baseline) system. It utilizes GPS and INS data for estimating its position and adopts DWT (Discrete Wavelet Transform) de-noising filter and UKF (Unscented KALMAN Filter) elaborating the position estimation. The beacon system aims at estimating the precise position of underwater vehicle by using USBL to receive the tracking signals. The most important one for the precise position estimation of underwater vehicle is estimating the position of the beacon system precisely. Since the beacon is on the sea-waves, the received GPS signals are noisy and unstable most of times. Therefore, the INS data (gyroscope sensor, accelerometer, magnetic compass) are obtained at the beacon on the sea-surface to compensate for the inaccuracy of the GPS data. The noises in the acceleration data from INS data are reduced by using DWT de-noising filter in this research. Finally the UKF localization system is proposed in this paper and the system performance is verified by real experiments.

이산 웨이블릿 변환과 Unscented 파티클 필터를 이용한 GPS-INS 결합 시스템의 실외 정밀 위치 추정 (Precise Outdoor Localization of a GPS-INS Integration System Using Discrete Wavelet Transforms and Unscented Particle Filter)

  • 서원교;이장명
    • 전자공학회논문지SC
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    • 제48권6호
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    • pp.82-90
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    • 2011
  • 본 논문에서는 실외 정밀 위치 추정을 위하여 설계된 GPS(Global positioning system)-INS(Inertial navigation system) 결합 시스템의 잡음 필터링 기법과 데이터 결합을 위한 기법을 소개한다. 실외 이동 항체의 속도 변화에 따라 차등적으로 발생하는 INS의 잡음들을 이산 웨이블릿 변환을 통해 신호를 분석하고 발생하는 잡음들을 데이터의 왜곡을 최소화하며 제거할 수 있는 차등 임계화 기법을 통한 필터링 기법을 제안하였다. 이는 항체의 가/감/등속을 고려하지 않고 특정 로우/하이 필터를 적용하여 데이터의 왜곡이 일어나는 기존 필터링 기법을 개선한 것이다. 또한 UPF를 이용해 비선형 특성과, 비가우시안 잡음의 특성을 가지는 실외 이동 항체의 GPS와 INS의 결합시킴으로서 실외에서 정밀하게 위치를 추정할 수 있게 하였고 이를 설계하여 실험을 통해 성능을 분석하였다.

EKF/UPF필터 변환을 통한 Multi-GPS/INS 융합 시스템의 실외 위치추정 (Outdoor Positioning Estimation of Multi-GPS / INS Integrated System by EKF / UPF Filter Conversion)

  • 최승환;김기정;김윤기;이장명
    • 제어로봇시스템학회논문지
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    • 제20권12호
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    • pp.1284-1289
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    • 2014
  • In this Paper, outdoor position estimation system was implemented using GPS (Global Positioning System) and INS (Inertial Navigation System). GPS position information has lots of errors by interference from obstacles and weather, the surrounding environment. To reduce these errors, multiple GPS system is used. Also, the Discrete Wavelet Transforms was applied to INS data for compensation of its error. In this paper, position estimation of the mobile robot in the straight line is conducted by EKF (Extended Kalman Filter). However, curve running position estimation is less accurate than straight line due to phase change in rotation. The curve is recognized through the rate of change in heading angle and the position estimation precision of the initial curve was improved by UPF (Unscented Particle Filter). In the case of UPF, if the number of particle is so many that big memory gets size is needed and processing speed becomes late. So, it only used the position estimation in the initial curve. Thereafter, the position of mobile robot in curve is estimated through switching from UPF to EKF again. Through the experiments, we verify the superiority of the system and make a conclusion.