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Volume 27 Issue 9
Sep.  2005
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Fan ShiWei, Zhang Tao, Zhou BaiZhao. The Trajectory Estimation in Boost-Phase Using Pseudolinear Estimator[J]. Journal of Electronics & Information Technology, 2005, 27(9): 1503-1506.
Citation: Fan ShiWei, Zhang Tao, Zhou BaiZhao. The Trajectory Estimation in Boost-Phase Using Pseudolinear Estimator[J]. Journal of Electronics & Information Technology, 2005, 27(9): 1503-1506.

The Trajectory Estimation in Boost-Phase Using Pseudolinear Estimator

  • Received Date: 2004-04-02
  • Rev Recd Date: 2004-10-08
  • Publish Date: 2005-09-19
  • Trajectory estimation using the measurement of arrival angles from space-based infrared sensors is one of the key technologies in the space early warning system. This paper presents a pseudolinear measure-Kalman estimator for trajectory estimation in boost-phase. Compared with EKF and CRLB, this estimator is more precise.
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  • Li Yicong, Bar-Shalom Y. Trajectory and launch point estimation for ballistic missiles from boost phase LOS measurements. IEEE Aerospace Conference Proceedings, 1999, Vol. 4:425 - 442.[2]Danis J. Space-based tactical missile launch parameter estimation.IEEE Trans. onAES, 1993,29(2): 412 - 424.[3]李盾.空间预警系统对+目标的定位与预报.[博士论文],国防科技大学,2001年.[4]Taylor H. The Cramer-Rao estimation error lower bound computation for deterministic nonlinear systems. IEEE Trans. on AC, 1979, AC-24(2): 343 - 344.
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