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Kalman Estimation

Given K `affine patches' being tracked through a sequence, eqn (8) is used to obtain estimates of the instantaneous 3-D motion of the surface (or camera) and the 3-D position and surface normal associated with each patch. This is done using an extended Kalman filter [2, 1, 6]. The state vector consists of the 6 motion parameters, the inverse focal length and 3K structure parameters, ie

equation421

where

equation423

The product tex2html_wrap_inline734 is used to reflect the dependence on focal length of the sensitivity to motion along the optical axis [1] and the structure parameters are normalised by tex2html_wrap_inline736 (which will always be significantly greater than zero for visible patches) to minimise the number of state variables by eliminating the redundant degree of freedom. The measurement vector contains the 6K affine parameters and hence the measurement tex2html_wrap_inline740 at time t is related to the state tex2html_wrap_inline744 by

  equation425

where tex2html_wrap_inline746 is zero mean with covariance R. The non-linear observation model tex2html_wrap_inline750 is defined by equation (8), ie for tex2html_wrap_inline752

  equation427

where tex2html_wrap_inline754 and tex2html_wrap_inline756 are evaluated at tex2html_wrap_inline674 .

The state dynamics for the filter are defined by the equation

equation429

where tex2html_wrap_inline760 is zero mean with covariance Q and tex2html_wrap_inline764 is the state transition function. No prior knowledge of the dynamics is assumed and hence an identity transition for the motion and focal length is used, ie tex2html_wrap_inline766 for tex2html_wrap_inline768 . The motion states then define the evolution of the normals and depths as derived by Murray and Shapiro [6]. Details of this are not repeated here; it suffices to note that it yields a non-linear state transition in the state variables. Recursive estimation of the state then proceeds as for a standard EKF [2], with updated estimates of the affine motion for each patch as used in the tracking being obtained at each stage using the measurement equation (15) and the current state estimate. The main complications is the need to compute the Jacobians of the measurement and state models, ie tex2html_wrap_inline770 and tex2html_wrap_inline772 , and to determine suitable values for the model covariances Q and R. Although the former are somewhat involved, they are readily obtained using a mathematical package such as Maple. The resulting filter does not require excessive computation, the main part being the inversion of a tex2html_wrap_inline778 matrix, and hence, since the system is overdetermined for tex2html_wrap_inline780 , real-time implementation is possible on a high-performance workstation. The model covariances were arrived at through empirical means using standard EKF design procedures [2].


next up previous
Next: Experiments Up: 3-D Surface Normals and Previous: Affine Motion Tracking

Andrew Calway
Mon Dec 4 11:27:23 GMT 2000