Skip to main navigation Skip to search Skip to main content

Error analysis and application of a nonlinear filter

  • Jing Yang*
  • , Hongxia Ji
  • , Mingkun Wei
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journal › Article › peer-review

Abstract

A nonlinear filtering algorithm with online model error estimation and compensation is proposed for a nonlinear system with uncertain model errors and disturbances. The model error is estimated by minimizing the variance of the predictive output residual based on the nonlinear predictive filter (NPF) principle, and then the system state is estimated by the extended Kalman filter (EKF) principle based on the compensated model. Detailed propagation formula of the state estimation error and its variance matrix are derived. Simulation results show the effectiveness of the proposed algorithm on a satellite attitude determination system with uncertain model errors. The simulation shows the robustness of the proposed algorithm for both the initial state error and uncertain model error, and the increasing filtering period may decrease the estimation accuracy. Compared with EKF and NPF, the proposed nonlinear filtering algorithm has the advantage of both improved estimation accuracy and faster convergence.

Original languageEnglish
Pages (from-to)1469-1477
Number of pages9
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume32
Issue number8
StatePublished - Aug 2011

Keywords

  • Attitude control
  • Error analysis
  • Error compensation
  • Nonlinear filtering
  • State estimation

Fingerprint

Dive into the research topics of 'Error analysis and application of a nonlinear filter'. Together they form a unique fingerprint.

Cite this