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Global Positioning System (GPS) technology has revolutionized navigation and positioning, but its accuracy is often compromised by various errors. These errors, stemming from environmental, satellite, and receiver-related factors, require careful mitigation to ensure reliable performance across applications.Atmospheric ErrorsGPS signals travel through the Earth’s ionosphere and troposphere, introducing delays which affect accuracy. The ionosphere is strongly influenced by charged particles,...
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Optimization Algorithm for Kalman Filter Exploiting the Numerical Characteristics of SINS/GPS Integrated Navigation

Shaoxing Hu1, Shike Xu2, Duhu Wang3

  • 1School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China. husx@buaa.edu.cn.

Sensors (Basel, Switzerland)
|November 17, 2015
PubMed
Summary

This study introduces an optimized Kalman filter algorithm for SINS/GPS systems, significantly reducing computational costs. The new method enhances efficiency by 90% in CPU time and 66% in memory usage without sacrificing accuracy.

Keywords:
SINS/GPSaccuracy-lossless decouplingblock matrixclosed-loop Kalman filtercomputational optimizationoffline-derivationparallel processingsymbol operation

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Area of Science:

  • Navigation Systems
  • Computational Optimization
  • Signal Processing

Background:

  • Traditional Kalman filters for SINS/GPS integration face high computational demands.
  • Existing methods often involve approximations or complex matrix theories, limiting efficiency and applicability.

Purpose of the Study:

  • To develop a computationally efficient Kalman filter optimization algorithm for SINS/GPS.
  • To reduce CPU time and memory usage while maintaining filter accuracy.
  • To create an easily transplantable optimization method for other filters.

Main Methods:

  • Exploiting matrix sparseness and symmetry for computational simplification via offline derivation and block matrix techniques.
  • Implementing a parallel computational mechanism through subdivision and restructuring of calculations based on "useful" data.
  • Utilizing numerical approaches that avoid precise-loss transformations or approximations of system modules.

Main Results:

  • Achieved approximately 90% savings in CPU processing time compared to classical Kalman filters.
  • Reduced memory usage by approximately 66%.
  • Maintained high accuracy, with minimal loss compared to the unoptimized filter.

Conclusions:

  • The proposed algorithm offers significant computational efficiency for SINS/GPS Kalman filtering.
  • The method is accurate, requires no complex matrix theories, and is easily adaptable to other filters.
  • This optimization strategy enhances practical implementation of integrated navigation systems.