Applying of forecast-revise EKF algorithm in autonomous navigation system

Gong Yuan Zhang, Yong Mei Cheng, Feng Yang, Quan Pan, Cong Gu

Research output: Contribution to journalArticlepeer-review

9 Scopus citations

Abstract

In order to improve the nonlinear estimation accuracy in autonomous navigation of spacecraft, via analyzing the drawbacks of linearization in EKF(Extended Kalman Filter), the influence of the difference expansion point in linearization of nonlinear function and the difference valued point in Jacobin matrix to the accuracy of linearization was studied based on the theory of mathematics analyzing. Then the linearization expansion way of generic EKF was improved, and a new algorithm called Forecast-Revise EKF (FR-EKF) based on mean value theorem and the smoothing estimation was proposed. Simulation result shows that the new algorithm is prior to EKF regard to accuracy.

Original languageEnglish
Pages (from-to)2226-2230
Number of pages5
JournalYuhang Xuebao/Journal of Astronautics
Volume30
Issue number6
DOIs
StatePublished - Nov 2009

Keywords

  • Autonomous navigation
  • Mean value theorem
  • Nonlinear estimation
  • Smoothing

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