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A Kalman Filtering Algorithm for Measurement Interruption Based on Polynomial Interpolation and Taylor Expansion.

Jianhua Cheng1, Zili Wang1, Bing Qi1

  • 1College of Intelligent Systems Science and Engineering, Harbin Engineering University, Harbin 150001, China.

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Summary

This study introduces an adaptive Kalman filtering algorithm to improve navigation accuracy during GPS signal loss. The method enhances accuracy in attitude, velocity, and position estimation for combined SINS/GPS systems.

Keywords:
Taylor expansionadaptive filteringmeasurement interruptionpolynomial fittingvirtual measurement

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Area of Science:

  • Navigation Systems Engineering
  • Signal Processing
  • Control Theory

Background:

  • Combined Strapdown Inertial Navigation System (SINS) and Global Positioning System (GPS) navigation systems are widely used but suffer from GPS signal blockage in urban canyons, tunnels, and under foliage.
  • GPS signal interruption causes SINS/GPS systems to degrade to pure inertial navigation, leading to significant accumulated errors.

Purpose of the Study:

  • To propose an adaptive Kalman filtering algorithm to mitigate navigation errors caused by GPS signal interruption in combined SINS/GPS systems.
  • To enhance the accuracy and stability of navigation solutions when GPS signals are temporarily unavailable.

Main Methods:

  • Developed an adaptive Kalman filtering algorithm incorporating polynomial fitting and Taylor expansion.
  • Utilized inertial guidance system data for polynomial interpolation to construct virtual velocity and position measurements during GPS outages.
  • Employed Taylor expansion to create virtual measurements, compensating for the lack of GPS data.

Main Results:

  • Computer simulations and road tests demonstrated improved performance compared to standard algorithms without rescue measures.
  • The proposed algorithm significantly enhanced accuracy in attitude angle estimation.
  • The algorithm also improved velocity estimation accuracy and positional localization precision.
  • The system exhibited higher overall stability during GPS signal interruptions.

Conclusions:

  • The proposed adaptive Kalman filtering algorithm effectively compensates for GPS signal loss in combined SINS/GPS navigation.
  • This method significantly improves navigation accuracy and system stability in challenging environments.
  • The technique offers a robust solution for maintaining reliable navigation performance when GPS is intermittently unavailable.