• 제목/요약/키워드: maneuvering target

검색결과 201건 처리시간 0.029초

IMM Method Using Intelligent Input Estimation for Maneuvering Target Tracking

  • Lee, Bum-Jik;Joo, Young-Hoon;Park, Jin-Bae
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2003년도 ICCAS
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    • pp.1278-1282
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    • 2003
  • A new interacting multiple model (IMM) method using intelligent input estimation (IIE) is proposed to track a maneuvering target. In the proposed method, the acceleration level for each sub-model is determined by IIE-the estimation of the unknown acceleration input by a fuzzy system using the relation between maneuvering filter residual and non-maneuvering one. The genetic algorithm (GA) is utilized to optimize a fuzzy system for a sub-model within a fixed range of acceleration input. Then, multiple models are composed of these fuzzy systems, which are optimized for different ranges of acceleration input. In computer simulation for an incoming ballistic missile, the tracking performance of the proposed method is compared with those of the input estimation (IE) technique and the adaptive interacting multiple model (AIMM) method.

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기동표적 추적을 위한 유전 알고리즘 기반 지능형 입력추정을 이용한 상호작용 다중모델 기법 (IMM Method Using GA-Based Intelligent Input Estimation for Maneuvering target Tracking)

  • 이범직;주영훈;박진배
    • 한국지능시스템학회:학술대회논문집
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    • 한국퍼지및지능시스템학회 2003년도 추계 학술대회 학술발표 논문집
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    • pp.99-102
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    • 2003
  • A new interacting multiple model (IMM) method using genetic algorithm (GA)-based intelligent input estimation(IIE) is proposed to track a maneuvering target. In the proposed method, the acceleration level for each sub-model is determined by IIE-the estimation of the unknown acceleration input by a fuzzy system using the relation between maneuvering filter residual and non-maneuvering one. The GA is utilized to optimize a fuzzy system fur a sub-model within a fixed range of acceleration input. Then, multiple models are composed of these fuzzy systems, which are optimized for different ranges of acceleration input. In computer simulation for an incoming ballistic missile, the tracking performance of the proposed method is compared with those of the input estimation(IE) technique and the adaptive interacting multiple model (AIMM) method.

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기동 표적 추적을 위한 일반화된 입력 추정 기법 (Generalized input estimation for maneuvering target tracking)

  • 황익호;이장규;박용환
    • 대한전기학회논문지
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    • 제45권1호
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    • pp.139-145
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    • 1996
  • The input estimation method estimates maneuvering input acceleration in order to track a maneuvering target. In this paper, the optimal input estimator is derived by choosing the MAP hypothesis among maneuvering input transition hypotheses under the assumption that a maneuvering input acceleration is a semi-Markov process. The optimal input estimation method cannot be realized because the optimal filter should consider every maneuver onset time hypothesis from filter starting time to current time which increase rapidly. Hence the suboptimal filter using a sliding window is proposed. Since the proposed method can consider all hypotheses of input transitions inside the window, it is general enough to include Bogler's input estimation method. Simulation results show, however, that we can obtain a good performance even when the filter considering just one input transition in the window is used. (author). 9 refs., 3 figs., 1 tab.

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연합형 칼만필터를 이용한 다중감지기 환경에서의 기동표적 추적 (Maneuvering-Target Tracking Using the Federated Kalman Filter with Multiple Sensors)

  • 황보승욱;홍금식;최성린
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1995년도 추계학술대회 논문집
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    • pp.598-601
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    • 1995
  • This paper proposes a federated Kalman filter approach which utilizes information from multiple sensors and variable estimation model. Compared with the decentralized Kalman filter, the algorithm proposed in this paper demonstrates much better tracking performance in both maneuvering and constant velocity movement of the target.

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기동입력의 직접추정에 의한 표적상태 추정 (Target State Estimation by Direct Estimation of Maneuvering Input)

  • 김종화;이만형;황장선
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1989년도 하계종합학술대회 논문집
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    • pp.70-74
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    • 1989
  • To track the target trajectory with maneuvers, unknown maneuvering inputs must be estimated. To do this the direct estimation algorithm using generalized least square technique is developed based on the procedure of failure detection and identification(FDI) theory. Through the simulation using maneuvering target scenario, tracking performance and efficiency of the algorithm developed here are investigated.

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An IMM Approach for Tracking a Maneuvering Target with Kinematic Constraints Based on the Square Root Information Filter

  • Kim, Kyung-Youn;Kim, Joong-Soo
    • Journal of Electrical Engineering and information Science
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    • 제1권2호
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    • pp.39-44
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    • 1996
  • An efficient interacting multiple mode(IMM) approach for tracking a maneuvering target with kinematic constraints is described based on the square root information filter(SRIF). The SRIF is employed instead of the conventional Kalman filter since it exhibits more efficient features in handling the kinematic constraints and improved numerical characteristics. The kinematic constraints are considered in the filtering process as pseudomeasurements where the degree of uncertainty is represented by the magnitude of the pseudomeasurement noise variance. The Monte Carlo simulations for the constant speed, maneuvering target are provided to demonstrate the improved tracking performance of the proposed algorithm.

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Tracking Error Performance of Tracking Filters Based on IMM for Threatening Target to Navel Vessel

  • Fang, Tae-Hyun;Choi, Jae-Weon
    • International Journal of Control, Automation, and Systems
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    • 제5권4호
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    • pp.456-462
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    • 2007
  • Tracking error performance is investigated for the typical maneuvering pattern of the anti-ship missile for tracking filters based on IMM filter in both clear and cluttered environments. Threatening targets to a navel vessel can be categorized into having three kinds of maneuvering patterns such as Waver, Pop-Up, and High-Diver maneuvers, which are classified according to launching platform or acceleration input to be applied. In this paper, the tracking errors for three kinds of maneuvering targets are represented and are investigated through simulation results. Studying estimation errors for each maneuvering target allows us to have insight into the most threatening maneuvering pattern and to construct the test maneuvering scenario for radar system validation.

기동하는 표적의 추적을 위한 연합형 가변차원 입력추정필터 (Federated Variable Dimension Kalman Filters with Input Estimation for Maneuvering Target Tracking)

  • 황보승욱;홍금식;최성린;최재원
    • 제어로봇시스템학회논문지
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    • 제5권6호
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    • pp.764-776
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    • 1999
  • In this paper, a tracking algorithm for a maneuvering single target in the presence of multiple data from multiple sensors is investigated. Allowing individual sensors to function by themselves, the estimates from individual sensors on the same target are fused for the purpose of improving the state estimate. The filtering method adopted in the local sensors is the variable dimensional filter with input estimatio technique, which consists of a constant velocity model and a constant acceleration model. A posteriori probability for the maneuvering hypothesis is newly derived. It is shown that the relation function of the a posteriori probability is a function of only the covariance of the fused estimates. Simulation results are provided.

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Design of Adaptive Fuzzy IMM Algorithm for Tracking the Maneuvering Target with Time-varying Measurement Noise

  • Kim, Hyun-Sik;Kim, In-Ho
    • International Journal of Control, Automation, and Systems
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    • 제5권3호
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    • pp.307-316
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    • 2007
  • In real system application, the interacting multiple model (IMM) based algorithm operates with the following problems: it requires less computing resources as well as a good performance with respect to the various target maneuvering, it requires a robust performance with respect to the time-varying measurement noise, and further, it requires an easy design procedure in terms of its structures and parameters. To solve these problems, an adaptive fuzzy interacting multiple model (AFIMM) algorithm, which is based on the basis sub-models defined by considering the maneuvering property and the time-varying mode transition probabilities designed by using the mode probabilities as the inputs of the fuzzy decision maker whose widths are adjusted, is proposed. To verify the performance of the proposed algorithm, a radar target tracking is performed. Simulation results show that the proposed AFIMM algorithm solves all problems in the real system application of the IMM based algorithm.

곡률을 이용한 기동표적 추적용 회전가속도 추정기 설계 (An Estimator Design of Turning Acceleration for Tracking a Maneuvering Target using Curvature)

  • 주재석;박제홍;임상석
    • 한국항행학회논문지
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    • 제4권2호
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    • pp.162-170
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    • 2000
  • 기동표적의 추적은 실재의 표적 궤적과 기둥의 통계적 특성을 미리 알 수 없기 때문에 매우 어려운 일이다. 이를 해결하기 위한 여러 가지 기법들이 제안되었고 이들 방식은 과거의 고전적인 방법에 비해 상당한 성능향상을 가져왔다. 본 논문에서는 칼만필터를 기본으로 한 회전가속도 추정기를 포함하는 필터를 제안한다. 제안된 방법은 인노베이션(innovation)을 사용하는 입력 추정법과는 달리 기동표적의 궤적의 모양으로부터 직접 가속도 입력벡터를 추정하여 필터를 갱신하는 방식이다. 가속도 모델 칼만필터 및 입력추정 기법(Input estimation)과의 성능을 비교하기 위해 3가지 종류의 기동표적 운동에 대하여 Monte Carlo 시뮬레이션을 수행하고 그 결과를 분석한다.

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