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  • Revisiting the filtering problem

    Paper number

    IAC-19,A6,7,6,x50344

    Author

    Mr. Shambo Bhattacharjee, United Kingdom, University of Leeds

    Coauthor

    Prof. John T Kent, United Kingdom, University of Leeds

    Coauthor

    Mr. Weston Faber, United States, Applied Defense Solutions, Inc.

    Coauthor

    Dr. Islam Hussein, United States, Applied Defense Solutions, Inc.

    Year

    2019

    Abstract
    Consider a space object in orbit about the earth and suppose a
    sequence of angles only measurements is available at known times. The
    objective of the filtering problem is to successively update the
    predicted distribution of the state of the orbiting object.  Each
    overall step of the filtering algorithm includes two parts: a
    propagation step and an update step.  These tasks are simplest if the
    distribution of the propagated state vector and the measurement can be
    described in terms of Gaussian distributions, so that a variant of the
    classic Kalman filter can be used.  It is well-known that ECI
    coordinates are unsuited for this purpose since the distribution of
    propagated position vector can have a pronounced banana shape (and
    hence is non-Gaussian) for large propagation times.  A better
    coordinate system is given by equinoctial coordinates, which perform
    well in many (but not all) circumstances.  Equinoctial coordinates
    depend on a ``reference plane'', typically taken to be the equatorial
    plane.
    
    In this paper, we explore the use of a recently developed new set of
    coordinates called ``Adapted STtructural (AST)'' coordinates.  They are
    essentially a ``local'' or adapted version of equinoctical coordinates.
    The main difference from equinoctial coordinates is that the 
    reference plane is now taken to be the orbital plane of the
    current best estimate of the state.  There are also a few other
    differences between AST and equinoctial coordinates.
    
    One of the benefits of AST coordinates is that a version of an
    extended Kalman filter (EKF) can be developed to simplify the update
    step, in contrast to the more typically used update based on the
    unscented Kalman filter (UKF).  In this paper, we give a detailed
    investigation of the AST-EKF algorithm.  In particular, we show that
    in certain circumstances under high ellipticity and using AST
    coordinates, the EKF update step can outperform the more conventional
    UKF update step.
    Abstract document

    IAC-19,A6,7,6,x50344.brief.pdf

    Manuscript document

    IAC-19,A6,7,6,x50344.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.