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    Alternating Direction Implicit Method-Based Nonlinear Filtering for Relative Orbit Estimation

    Source: Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 003
    Author:
    J. Yoon
    ,
    Y. Xu
    DOI: 10.1061/(ASCE)AS.1943-5525.0000024
    Publisher: American Society of Civil Engineers
    Abstract: Nonlinear filtering theory, based upon the Fokker-Planck equation and Bayes’ rule, has been around since the 1970s. This method does not require linearized dynamics and/or measurement models, and also the assumption of the Gaussian process is not necessary. However, it is extremely difficult to obtain an analytical solution of the Fokker-Planck equation with only a few exceptions, and normally the solution is obtained through numerical approaches. In this paper, this type of nonlinear filtering method is reinvestigated and applied to a relative orbit estimation problem. The time evolution of the state conditional probability density function between measurements is obtained by solving the associated Fokker-Planck equation numerically using the numerical scheme called the alternating direction implicit method. To further mitigate the computational load, an enhanced moving domain technique is employed and the probability distribution function is partitioned.
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      Alternating Direction Implicit Method-Based Nonlinear Filtering for Relative Orbit Estimation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56162
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    contributor authorJ. Yoon
    contributor authorY. Xu
    date accessioned2017-05-08T21:33:38Z
    date available2017-05-08T21:33:38Z
    date copyrightJuly 2010
    date issued2010
    identifier other%28asce%29as%2E1943-5525%2E0000024.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56162
    description abstractNonlinear filtering theory, based upon the Fokker-Planck equation and Bayes’ rule, has been around since the 1970s. This method does not require linearized dynamics and/or measurement models, and also the assumption of the Gaussian process is not necessary. However, it is extremely difficult to obtain an analytical solution of the Fokker-Planck equation with only a few exceptions, and normally the solution is obtained through numerical approaches. In this paper, this type of nonlinear filtering method is reinvestigated and applied to a relative orbit estimation problem. The time evolution of the state conditional probability density function between measurements is obtained by solving the associated Fokker-Planck equation numerically using the numerical scheme called the alternating direction implicit method. To further mitigate the computational load, an enhanced moving domain technique is employed and the probability distribution function is partitioned.
    publisherAmerican Society of Civil Engineers
    titleAlternating Direction Implicit Method-Based Nonlinear Filtering for Relative Orbit Estimation
    typeJournal Paper
    journal volume23
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000024
    treeJournal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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