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 language | English |
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Pages (from-to) | 2226-2230 |
Number of pages | 5 |
Journal | Yuhang Xuebao/Journal of Astronautics |
Volume | 30 |
Issue number | 6 |
DOIs | |
State | Published - Nov 2009 |
Keywords
- Autonomous navigation
- Mean value theorem
- Nonlinear estimation
- Smoothing