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R. Zhan and J. Wan, “Iterated Unscented Kalman Filter for Passive Target Tracking,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 3, No. 38, 2007, pp. 1155-1163.

has been cited by the following article:

• TITLE: Error Analysis of Orbit Determination for the Geostationary Satellite with Single Station Antenna Tracking Data

  AUTHORS: Chingiz Hajiyev, Melih Ata

  KEYWORDS: Orbit Determination, Geostationary Satellite, Single Station Antenna, Error Analysis

  JOURNAL NAME: Positioning, Vol.2 No.4, November 3, 2011

  ABSTRACT: In the study, position and velocity values of a geostationary satellite are found. When performing this, a MATLAB algorithm is used for Runge-Kutta Fehlberg orbit integration method to solve spacecraft’s position and velocity. Integrated method is the solution for the systems which mainly work with a single station. Method provides calculation of azimuth, elevation and range data by using the position simulation results found by RKF. Errors of orbit determination are analysed. Variances of orbit parameters are chosen as the accuracy criteria. Analysis results are the indicator of the method’s accuracy