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<pubDate>Thu, 21 Aug 2008 15:16:44 BST</pubDate>


	<title>CiteULike: bsilverthorn kalman_filters</title>
	<description>CiteULike: bsilverthorn kalman_filters</description>


	<link>http://www.citeulike.org/user/bsilverthorn/tag/kalman_filters</link>
	<dc:publisher>CiteULike.org</dc:publisher>
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	<dc:rights>Copyright &#169; 2004-2008 citeulike.org</dc:rights>
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        <rdf:li rdf:resource="http://www.citeulike.org/user/bsilverthorn/article/3124262"/>
        <rdf:li rdf:resource="http://www.citeulike.org/user/bsilverthorn/article/3116050"/>
        <rdf:li rdf:resource="http://www.citeulike.org/user/bsilverthorn/article/3112551"/>
        <rdf:li rdf:resource="http://www.citeulike.org/user/bsilverthorn/article/2675803"/>

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<item rdf:about="http://www.citeulike.org/user/bsilverthorn/article/3126328">
    <title>Unscented Filtering in a Unit Quaternion Space for Spacecraft Attitude Estimation</title>
    <link>http://www.citeulike.org/user/bsilverthorn/article/3126328</link>
    <description>&lt;i&gt;Industrial Electronics, 2007. ISIE 2007. IEEE International Symposium on (2007), pp. 66-71.&lt;/i&gt;&lt;br /&gt;&lt;br /&gt;A novel approach to the straightforward implementation of unscented filtering in a unit quaternion space is proposed for spacecraft attitude estimation. A method of weighted mean computation for quaternions is derived in a rotational space, leading to a quaternion with a unit norm. Quaternion multiplication, which allows a quaternion in the filter to lie in the unit quaternion space, is then used for predicted covariance computations and quaternion updates. In this study, quaternion process noise, which increases the uncertainty in attitude orientation, is either modeled as the vector part of the quaternion or as a rotation vector. Simulation results indicate that the proposed approach successfully estimates spacecraft attitude.</description>
    <dc:title>Unscented Filtering in a Unit Quaternion Space for Spacecraft Attitude Estimation</dc:title>

    <dc:creator>Yee-Jin Cheon</dc:creator>
    <dc:creator>Jong-Hwan Kim</dc:creator>
    <dc:identifier>doi:10.1109/ISIE.2007.4374575</dc:identifier>
    <dc:source>Industrial Electronics, 2007. ISIE 2007. IEEE International Symposium on (2007), pp. 66-71.</dc:source>
    <dc:date>2008-08-15T21:17:16-00:00</dc:date>
    <prism:publicationYear>2007</prism:publicationYear>
    <prism:publicationName>Industrial Electronics, 2007. ISIE 2007. IEEE International Symposium on</prism:publicationName>
    <prism:startingPage>66</prism:startingPage>
    <prism:endingPage>71</prism:endingPage>
    <prism:category>bayes_filtering</prism:category>
    <prism:category>kalman_filters</prism:category>
    <prism:category>pose_estimation</prism:category>
    <prism:category>quaternions</prism:category>
    <prism:category>spacecraft</prism:category>
    <prism:category>unscented_kalman</prism:category>
</item>



<item rdf:about="http://www.citeulike.org/user/bsilverthorn/article/2727317">
    <title>The square-root unscented Kalman filter for state and parameter-estimation</title>
    <link>http://www.citeulike.org/user/bsilverthorn/article/2727317</link>
    <description>&lt;i&gt;Acoustics, Speech, and Signal Processing, 2001. Proceedings. (ICASSP '01). 2001 IEEE International Conference on, Vol. 6 (2001), pp. 3461-3464.&lt;/i&gt;&lt;br /&gt;&lt;br /&gt;Over the last 20-30 years, the extended Kalman filter (EKF) has become the algorithm of choice in numerous nonlinear estimation and machine learning applications. These include estimating the state of a nonlinear dynamic system as well estimating parameters for nonlinear system identification (eg, learning the weights of a neural network). The EKF applies the standard linear Kalman filter methodology to a linearization of the true nonlinear system. This approach is sub-optimal, and can easily lead to divergence. Julier et al. (1997), proposed the unscented Kalman filter (UKF) as a derivative-free alternative to the extended Kalman filter in the framework of state estimation. This was extended to parameter estimation by Wan and Van der Merwe et al., (2000). The UKF consistently outperforms the EKF in terms of prediction and estimation error, at an equal computational complexity of (OL&#60;sup&#62;3&#60;/sup&#62;)&#60;sup&#62;l&#60;/sup&#62; for general state-space problems. When the EKF is applied to parameter estimation, the special form of the state-space equations allows for an O(L&#60;sup&#62;2&#60;/sup&#62;) implementation. This paper introduces the square-root unscented Kalman filter (SR-UKF) which is also O(L&#60;sup&#62;3&#60;/sup&#62;) for general state estimation and O(L&#60;sup&#62;2&#60;/sup&#62;) for parameter estimation (note the original formulation of the UKF for parameter-estimation was O(L&#60;sup&#62;3&#60;/sup&#62;)). In addition, the square-root forms have the added benefit of numerical stability and guaranteed positive semi-definiteness of the state covariances</description>
    <dc:title>The square-root unscented Kalman filter for state and parameter-estimation</dc:title>

    <dc:creator>Rudoplh van der Merwe</dc:creator>
    <dc:creator>Eric Wan</dc:creator>
    <dc:identifier>doi:10.1109/ICASSP.2001.940586</dc:identifier>
    <dc:source>Acoustics, Speech, and Signal Processing, 2001. Proceedings. (ICASSP '01). 2001 IEEE International Conference on, Vol. 6 (2001), pp. 3461-3464.</dc:source>
    <dc:date>2008-04-28T05:01:55-00:00</dc:date>
    <prism:publicationYear>2001</prism:publicationYear>
    <prism:publicationName>Acoustics, Speech, and Signal Processing, 2001. Proceedings. (ICASSP '01). 2001 IEEE International Conference on</prism:publicationName>
    <prism:volume>6</prism:volume>
    <prism:startingPage>3461</prism:startingPage>
    <prism:endingPage>3464</prism:endingPage>
    <prism:category>bayes_filtering</prism:category>
    <prism:category>kalman_filters</prism:category>
    <prism:category>pose_estimation</prism:category>
    <prism:category>unscented_kalman</prism:category>
</item>



<item rdf:about="http://www.citeulike.org/user/bsilverthorn/article/3124262">
    <title>The Scaled Unscented Transformation</title>
    <link>http://www.citeulike.org/user/bsilverthorn/article/3124262</link>
    <description>&lt;i&gt;American Control Conference, 2002. Proceedings of the 2002, Vol. 6 (2002), pp. 4555-4559.&lt;/i&gt;&lt;br /&gt;&lt;br /&gt;This paper describes a generalisation of the unscented transformation (UT) which allows sigma points to be scaled to an arbitrary dimension. The UT is a method for predicting means and covariances in nonlinear systems. A set of samples are deterministically chosen which match the mean and covariance of a (not necessarily Gaussian-distributed) probability distribution. These samples can be scaled by an arbitrary constant. The method guarantees that the mean and covariance second order accuracy in mean and covariance, giving the same performance as a second order truncated filter but without the need to calculate any Jacobians or Hessians. The impacts of scaling issues are illustrated by considering conversions from polar to Cartesian coordinates with large angular uncertainties.</description>
    <dc:title>The Scaled Unscented Transformation</dc:title>

    <dc:creator>Simon Julier</dc:creator>
    <dc:identifier>doi:10.1109/ACC.2002.1025369</dc:identifier>
    <dc:source>American Control Conference, 2002. Proceedings of the 2002, Vol. 6 (2002), pp. 4555-4559.</dc:source>
    <dc:date>2008-08-14T17:26:18-00:00</dc:date>
    <prism:publicationYear>2002</prism:publicationYear>
    <prism:publicationName>American Control Conference, 2002. Proceedings of the 2002</prism:publicationName>
    <prism:volume>6</prism:volume>
    <prism:startingPage>4555</prism:startingPage>
    <prism:endingPage>4559</prism:endingPage>
    <prism:category>bayes_filtering</prism:category>
    <prism:category>kalman_filters</prism:category>
    <prism:category>unscented_kalman</prism:category>
</item>



<item rdf:about="http://www.citeulike.org/user/bsilverthorn/article/3116050">
    <title>A Quaternion-based Unscented Kalman Filter for Orientation Tracking</title>
    <link>http://www.citeulike.org/user/bsilverthorn/article/3116050</link>
    <description>&lt;i&gt;Information Fusion, 2003. Proceedings of the Sixth International Conference of, Vol. 1 (2003), pp. 47-54.&lt;/i&gt;</description>
    <dc:title>A Quaternion-based Unscented Kalman Filter for Orientation Tracking</dc:title>

    <dc:creator>Edgar Kraft</dc:creator>
    <dc:source>Information Fusion, 2003. Proceedings of the Sixth International Conference of, Vol. 1 (2003), pp. 47-54.</dc:source>
    <dc:date>2008-08-13T18:46:34-00:00</dc:date>
    <prism:publicationYear>2003</prism:publicationYear>
    <prism:publicationName>Information Fusion, 2003. Proceedings of the Sixth International Conference of</prism:publicationName>
    <prism:volume>1</prism:volume>
    <prism:startingPage>47</prism:startingPage>
    <prism:endingPage>54</prism:endingPage>
    <prism:category>kalman_filters</prism:category>
    <prism:category>pose_estimation</prism:category>
    <prism:category>quaternions</prism:category>
    <prism:category>unscented_kalman</prism:category>
</item>



<item rdf:about="http://www.citeulike.org/user/bsilverthorn/article/3112551">
    <title>Unscented Filtering for Spacecraft Attitude Estimation</title>
    <link>http://www.citeulike.org/user/bsilverthorn/article/3112551</link>
    <description>&lt;i&gt;Journal of Guidance, Control, and Dynamics, Vol. 26, No. 4. (2003), pp. 536-542.&lt;/i&gt;</description>
    <dc:title>Unscented Filtering for Spacecraft Attitude Estimation</dc:title>

    <dc:creator>John Crassidis</dc:creator>
    <dc:creator>FL Markley</dc:creator>
    <dc:source>Journal of Guidance, Control, and Dynamics, Vol. 26, No. 4. (2003), pp. 536-542.</dc:source>
    <dc:date>2008-08-12T18:27:06-00:00</dc:date>
    <prism:publicationYear>2003</prism:publicationYear>
    <prism:publicationName>Journal of Guidance, Control, and Dynamics</prism:publicationName>
    <prism:volume>26</prism:volume>
    <prism:number>4</prism:number>
    <prism:startingPage>536</prism:startingPage>
    <prism:endingPage>542</prism:endingPage>
    <prism:category>kalman_filters</prism:category>
    <prism:category>pose_estimation</prism:category>
    <prism:category>quaternions</prism:category>
    <prism:category>spacecraft</prism:category>
    <prism:category>unscented_kalman</prism:category>
</item>



<item rdf:about="http://www.citeulike.org/user/bsilverthorn/article/2675803">
    <title>A new approach to linear filtering and prediction problems</title>
    <link>http://www.citeulike.org/user/bsilverthorn/article/2675803</link>
    <description>&lt;i&gt;Journal of Basic Engineering, Vol. 82, No. 1. (1960), pp. 35-45.&lt;/i&gt;</description>
    <dc:title>A new approach to linear filtering and prediction problems</dc:title>

    <dc:creator>Rudolf Kalman</dc:creator>
    <dc:source>Journal of Basic Engineering, Vol. 82, No. 1. (1960), pp. 35-45.</dc:source>
    <dc:date>2008-04-16T01:26:04-00:00</dc:date>
    <prism:publicationYear>1960</prism:publicationYear>
    <prism:publicationName>Journal of Basic Engineering</prism:publicationName>
    <prism:volume>82</prism:volume>
    <prism:number>1</prism:number>
    <prism:startingPage>35</prism:startingPage>
    <prism:endingPage>45</prism:endingPage>
    <prism:category>kalman_filters</prism:category>
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