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- W2465250485 abstract "When an inertial navigation system regains a valid aiding navigation signal after a long-term outage, normal state feedback correction in the Kalman filter (KF) will cause a large instantaneous jump in the navigation parameters which may severely affect flight control stability. In this paper, we present a partial state feedback correction method in the KF to smooth the navigation parameters to solve this problem. The idea is to partially correct the navigation state in several steps according to the requirement of the guidance and control system. The simplicity of this method lies in the fact that no additional changes of the filter parameters are needed in the algorithm. The capability of residual monitoring and fault detection is the same with normal state feedback correction in the KF. Comparative simulation results show the effectiveness of the proposed method." @default.
- W2465250485 created "2016-07-22" @default.
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- W2465250485 date "2016-01-01" @default.
- W2465250485 modified "2023-10-05" @default.
- W2465250485 title "Partial State Feedback Correction for Smoothing Navigational Parameters" @default.
- W2465250485 cites W102148132 @default.
- W2465250485 doi "https://doi.org/10.1007/978-981-10-0937-2_39" @default.
- W2465250485 hasPublicationYear "2016" @default.
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