• Title/Summary/Keyword: extended Kalman filter

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Design of State-estimator using Extended Kalman Filter for Magnetic Levitation System (자기부상시스템에서의 확장칼만필터를 이용한 상태추정자 설계)

  • Sung H.K.;Jung B.S.;Cho J.M.;Jang S.M.;Kim D.S.;Yu M.H.
    • Proceedings of the KIEE Conference
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    • summer
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    • pp.1334-1336
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    • 2004
  • The existing problems of the Electro-Magnetic Suspension system such as air-gap disturbance, mass variation and actuator/sensor failure are described in amore specific manner. These problem can not be solved by conventional state-feedback and output-feedback control. Extended Kalman Filter is to linearize about a trajectory that is continually updated with the state estimates resulting from the measurements. In this paper, first, the physical properties of the EMS system are described. second, Extended Kalman Filer designed as form appliable EMS system. It is shown that state estimation performance can be obtained with the use of Extended Kalman filter, and that results from simulation, stability analyze.

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Comparison of Extended Kalman Filter and Constraint Propagation Technique to Localize Multiple Mobile Robots (다중 이동 로봇의 위치 추정을 위한 확장 칼만 필터와 제약 만족 기법의 성능 비교)

  • Jo, Kyaung-Hwan;Lee, Hang-Ki;Lee, Ji-Hong
    • Proceedings of the KIEE Conference
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    • 2008.10b
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    • pp.323-324
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    • 2008
  • In this paper, we present performance comparison of two methods to localize multiple robots. One is extended Kalman filter and the other is constraint propagation technique. Extended Kalman filter is conventional probabilistic method which gives the sub-optimal estimation rather than guarantee any boundary for true position of robot. In case of constraint propagation, it can give a boundary containing true robot position value. Especially, we deal with cooperative localization problem in outdoor environment for multiple robots equipped with GPS, gyro meter, wheel encoder. In simulation results, we present strength and weakness for localization methods based on extend Kalman filter and constraint propagation technique.

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The development of a visual tracking system for the stable grasping of a moving object (움직이는 물체의 안정한 Grasping을 위한 시각추적 시스템 개발)

  • 차인혁;손영갑;한창수
    • 제어로봇시스템학회:학술대회논문집
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    • 1996.10b
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    • pp.543-546
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    • 1996
  • We propose a new visual tracking system for grasping which can find grasping points of an unknown polygonal object. We construct the system with the image prediction technique and Extended Kalman Filter algorithm. The Extended Kalman Filter(EKF) based on the SVD can improve the accuracy and processing time for the estimation of the nonlinear state variables. By using it, we can solve the numerical unstability problem that can occur in the visual tracking system based on Kalman filter. The image prediction algorithm can reduce the effect of noise and the image processing time. In the processing of a visual tracking, we can construct the parameterized family and can found the grasping points of unknown object through the geometric properties of the parameterized family.

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Equalization of Time-Varying Channels using a Recurrent Neural Network Trained with Kalman Filters (칼만필터로 훈련되는 순환신경망을 이용한 시변채널 등화)

  • 최종수;권오신
    • Journal of Institute of Control, Robotics and Systems
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    • v.9 no.11
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    • pp.917-924
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    • 2003
  • Recurrent neural networks have been successfully applied to communications channel equalization. Major disadvantages of gradient-based learning algorithms commonly employed to train recurrent neural networks are slow convergence rates and long training sequences required for satisfactory performance. In a high-speed communications system, fast convergence speed and short training symbols are essential. We propose decision feedback equalizers using a recurrent neural network trained with Kalman filtering algorithms. The main features of the proposed recurrent neural equalizers, utilizing extended Kalman filter (EKF) and unscented Kalman filter (UKF), are fast convergence rates and good performance using relatively short training symbols. Experimental results for two time-varying channels are presented to evaluate the performance of the proposed approaches over a conventional recurrent neural equalizer.

Filtering Performance Analyizing for Relative Navigation Using Single Difference Carrier-Phase GPS (GPS 신호의 단일차분을 이용한 편대위성의 상대위치 결정을 위한 필터링 성능 분석)

  • Park, In-Kwan;Park, Sang-Young;Choi, Kyu-Hong;Choi, Sung-Ki;Park, Jong-Uk
    • Journal of Astronomy and Space Sciences
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    • v.25 no.3
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    • pp.283-290
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    • 2008
  • Satellite formation flying can provide the platform for interferometric observation to acquire the precise data and ensure the flexibility for space mission. This paper presents development and verification of an algorithm to estimate the baseline between formation flying satellites. To estimate a baseline(relative navigation) in real time, EKF(Extended Kalman Filter) and UKF(Unscented Kalman Filter) are used. Measurements for updating a state-vector in Kalman Filter are GPS single difference data. In results, The position errors in estimated baseline are converged to less than ${\pm}1m$ in both EKF and UKF. And as using the two types of Kalman filter, it is clear that the unscented Kalman filter shows a relatively better performance than the extended Kalman filter by comparing an efficiency to the model which has a non-linearity.

A study on the Parameter Identification for a Mechanical Dynamic System Using a Time-Domain Extened Kalman Filter Algorithm (시간 영역에서의 Extended Kalman Filter 알고리즘을 이용한 동적 기계 시스템의 파라미터 추정에 관한 연구)

  • 이용복;김창호;사종성;김광식
    • Journal of KSNVE
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    • v.2 no.2
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    • pp.135-140
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    • 1992
  • The Extended Kalman Filter(EKF) algorithm estimates variables and unknown parameters simultaneously and is applied to parameter identification of linear and nonlinear mechanical systems. In this paper, an EKF algorithm was developed through a computer simulation and then applied to a sealing test system as a practical example. Comparing with the frequency domain analysis, it was proved to be a useful alternative for the parameter identification.

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Comparison of Attitude Estimation Methods for DVL Navigation of a UUV (UUV의 DVL 항법을 위한 자세 추정 방법 비교)

  • Jeong, Seokki;Ko, Nak Yong;Choi, Hyun-Taek
    • The Journal of Korea Robotics Society
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    • v.9 no.4
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    • pp.216-224
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    • 2014
  • This paper compares methods for attitude estimation of a UUV(Unmanned Underwater Vehicle). Attitude estimation plays a key role in underwater navigation using DVL(Doppler Velocity Log). The paper proposes attitude estimation methods using EKF(Extended Kalman Filter), UKF(Unscented Kalman Filter), and CF(Complementary Filter). It derives methods using the measurements from MEMS-AHRS(Microelectromechanical Systems-Attitude Heading Reference System) and DVL. The methods are used for navigation in a test pool and their navigation performance is compared. The results suggest that even if there is no measurement relative to some absolute landmarks, DVL-only navigation can be useful for navigation in a limited time and range.

Advanced Kalman filter - a survey (칼만필터의 최근 동향 및 발전)

  • 이장규;이연석
    • 제어로봇시스템학회:학술대회논문집
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    • 1987.10b
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    • pp.464-469
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    • 1987
  • The Kalman filter is an optimal linear estimator that has been an active research topic for the past three decades. The scheme has become the milestone of modern filtering, and it is applied to many areas including navigations and controls of free vehicle. The Kalman filter technique is matured. But some problems are still remained to be resolved. The prevention of divergence induced by digital implementation, nonoptimal application for nonlinear system, and application to non-Gaussian processes are some of the problems. This paper surveys the problems. The square root filtering is suggested to prevent the divergence. The extended Kalman filter is used for nonlinear systems. And, many other approaches to Kalman-like optimal estimators are also investigated.

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Application of Recurrent Neural-Network based Kalman Filter for Uncertain Target Models (불확정 표적 모델에 대한 순환 신경망 기반 칼만 필터 설계)

  • DongBeom Kim;Daekyo Jeong;Jaehyuk Lim;Sawon Min;Jun Moon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.26 no.1
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    • pp.10-21
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    • 2023
  • For various target tracking applications, it is well known that the Kalman filter is the optimal estimator(in the minimum mean-square sense) to predict and estimate the state(position and/or velocity) of linear dynamical systems driven by Gaussian stochastic noise. In the case of nonlinear systems, Extended Kalman filter(EKF) and/or Unscented Kalman filter(UKF) are widely used, which can be viewed as approximations of the(linear) Kalman filter in the sense of the conditional expectation. However, to implement EKF and UKF, the exact dynamical model information and the statistical information of noise are still required. In this paper, we propose the recurrent neural-network based Kalman filter, where its Kalman gain is obtained via the proposed GRU-LSTM based neural-network framework that does not need the precise model information as well as the noise covariance information. By the proposed neural-network based Kalman filter, the state estimation performance is enhanced in terms of the tracking error, which is verified through various linear and nonlinear tracking problems with incomplete model and statistical covariance information.

Scalar Adaptive Kalman Filtering for Stellar Inertia! Attitude Determination

  • Jung, Jae-Woo;Cho, Yun-Cheol;Bang, Hyo-Choong;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
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    • v.3 no.2
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    • pp.88-94
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    • 2002
  • This paper describes attitude determination algorithm for the low earth orbit(LEO) spacecraft using stellar inertial sensors. The cascaded gyro/star tracker extended Kalman filter is constructed to fuse two sensor data. And then the smoothing of the measurement are proposed for an unreasonable jump of star tracker. The smoothing algorithm for the rejection of star tracker error jumps is designed by scalar adaptive filter. The proposed algorithms operate to process the measurement of gyro/star tracker Kalman filter, therefore, it is comparatively simple to apply these methods to other integration systems. Simulations to gyro/star tracker integrated system show that the proposed method is effective.