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Multi-Sensor Optimal Data Fusion Based on the Adaptive Fading Unscented Kalman Filter
Bingbing Gao1, Gaoge Hu2, Shesheng Gao3
1School of Automatics, Northwestern Polytechnical University, Xi'an 710072, China. nwpugbb0826@126.com.
A novel data fusion method using an adaptive fading unscented Kalman filter enhances multi-sensor nonlinear system accuracy. This approach improves adaptability and robustness against modeling errors for optimal state estimation in integrated navigation systems.
Area of Science:
- Control Engineering
- Signal Processing
- Estimation Theory
Background:
- Multi-sensor systems often face challenges with nonlinear dynamics and stochastic noise.
- Process-modeling errors can significantly degrade the performance of traditional data fusion techniques.
- Accurate state estimation is crucial for applications like integrated navigation.
Purpose of the Study:
- To develop an optimal data fusion methodology for multi-sensor nonlinear stochastic systems.
- To enhance the adaptability and robustness of state estimation against process-modeling errors.
- To achieve globally optimal state estimation using a two-level fusion structure.
Main Methods:
- Implementation of an adaptive fading unscented Kalman filter (AFUKF) with Mahalanobis distance for local filters.
- Development of a two-level fusion structure with local AFUKFs and a top-level unscented transformation-based fusion.
- Application of the principle of linear minimum variance for optimal fusion of local estimations.
Main Results:
- The proposed methodology effectively mitigates the influence of process-modeling errors on data fusion.
- Improved adaptability and robustness in state estimation for multi-sensor nonlinear stochastic systems were achieved.
- Globally optimal fusion results were obtained, validated by simulations and experiments.
Conclusions:
- The novel data fusion methodology provides superior performance for multi-sensor nonlinear stochastic systems.
- The approach demonstrates significant improvements in adaptability, robustness, and accuracy.
- The method is validated for integrated navigation systems, including Inertial Navigation System/Global Navigation Satellite System/Celestial Navigation System (INS/GNSS/CNS).
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