Patents by Inventor Robert E. Yang

Robert E. Yang has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 8149159
    Abstract: A method for rapid convergence of radar target state includes the steps of using range acceleration to estimate perpendicular velocity and jump-starting a Cartesian state filter with the estimated perpendicular velocity. The improved estimate in the Cartesian state filter allows improved coasting of the range-state.
    Type: Grant
    Filed: October 13, 2008
    Date of Patent: April 3, 2012
    Assignee: Lockheed Martin Corporation
    Inventor: Robert E. Yang
  • Patent number: 7574057
    Abstract: An improved covariance matrix encoding scheme wherein a covariance matrix is described in terms of Euler angles and eigenvalues. A covariance matrix, P, is decomposed into its eigenvalues and eigenvectors. The eigenvalues and their corresponding eigenvectors are arranged starting with the smallest value, and the next two ordered such that, the eigenvector set comprises a right-handed coordinate system. Each eigenvalue is then encoded with a logarithmic or other compression scheme. Euler angles are calculated and angle is compressed and an offset is added to each angle. The covariance matrix is then reconstructed from the encoded values to test if the encoded matrix completely covers the original matrix. If necessary, a scale factor is applied to all reconstructed eigenvalues and the scaled versions are then re-encoded as described above. The scaling and re-encoding process ensures that the encoded matrix covers the original matrix.
    Type: Grant
    Filed: March 23, 2005
    Date of Patent: August 11, 2009
    Assignee: Lockheed Martin Corporation
    Inventor: Robert E. Yang
  • Patent number: 7187320
    Abstract: A target tracking arrangement predicts the state of a target. The predictor may be a Kalman filter. In the presence of a target which is maneuvering, the prediction may be in error. A maneuver detector is coupled to receive residuals representing the difference between the predictions and the target state. The maneuver detector is matched to the predictor or Kalman filter to thereby tend to reduce the undesirable effects of system noise. The matching may be of the frequency response.
    Type: Grant
    Filed: August 27, 2004
    Date of Patent: March 6, 2007
    Assignee: Lockheed Martin Corporation
    Inventor: Robert E. Yang