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Seamless global positioning system/inertial navigation system navigation method based on square-root cubature Kalman
Yufeng Xiong1, Yu Zhang1, Xiaoting Guo1
1Key Laboratory of Instrumentation and Science and Dynamic Measurement, Ministry of Education, North University of China, Taiyuan 030051, People's Republic of China.
This study introduces a novel dual-model for seamless navigation, enhancing Global Positioning System (GPS)/Inertial Navigation System (INS) performance during GPS outages. The method improves navigation accuracy by effectively correcting INS errors when GPS signals are unavailable.
Area of Science:
- Navigation Systems Engineering
- Signal Processing
- Machine Learning
Background:
- Global Positioning System (GPS) and Inertial Navigation System (INS) integration is crucial for accurate positioning.
- GPS signal outages significantly degrade the performance of integrated navigation systems.
- Existing methods often struggle to maintain accuracy during prolonged GPS signal loss.
Purpose of the Study:
- To develop a seamless navigation dual-model for robust GPS/INS integration.
- To enhance navigation accuracy and reliability during GPS signal outages.
- To outperform traditional single-model approaches in correcting INS errors.
Main Methods:
- A dual-model approach combining Square-Root Cubature Kalman Filter (SRCKF) and Random Forest Regression (RFR).
- Sub-model 1: Relates INS specific force to filter measurements.
- Sub-model 2: Relates SRCKF cubature points and innovation to filter-induced errors.
Main Results:
- The proposed dual-model ensures seamless navigation capabilities even with complete GPS signal loss.
- Experimental results demonstrate significant improvements in navigation accuracy compared to traditional methods.
- The SRCKF and RFR combination shows superior performance in predicting INS errors.
Conclusions:
- The developed dual-model effectively corrects standalone INS during GPS outages, outperforming single models.
- The integration of SRCKF and RFR provides a more accurate prediction of INS errors.
- This seamless navigation method offers a significant advancement for navigation systems operating in challenging environments.
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