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An Online Gravity Modeling Method Applied for High Precision Free-INS.

Jing Wang1,2, Gongliu Yang3,4, Jing Li5,6

  • 1School of Instrument Science and Opto-electronics Engineering, Beihang University, Beijing 100083, China. by1217133@buaa.edu.cn.

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|September 27, 2016
PubMed
Summary
This summary is machine-generated.

A new polynomial gravity model offers a faster, more accurate solution for inertial navigation systems (INS) by simplifying complex spherical harmonic models. This method improves real-time gravity compensation for high-precision INS applications.

Keywords:
complexity analysishigh precision free-INSonline modelingpolynomial model

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Area of Science:

  • Geodesy
  • Navigation Systems

Background:

  • High-degree spherical harmonic models (SHM) are computationally intensive for real-time inertial navigation system (INS) applications.
  • Traditional normal gravity models (NGM) are often used but lack sufficient accuracy for high-precision INS.

Purpose of the Study:

  • To develop a computationally efficient and accurate gravity compensation model for real-time INS.
  • To improve upon the limitations of both SHM and NGM in INS applications.

Main Methods:

  • Derived a two-dimensional second-order polynomial model from SHM based on regional disturbing potential characteristics.
  • Calculated deflections of vertical (DOVs) using SHM on dense grids to obtain polynomial coefficients.
  • Synchronously updated polynomial coefficients and applicable regions for global navigation.

Main Results:

  • The polynomial model requires less storage and computational time than high-degree SHM, with only minor precision loss.
  • The proposed polynomial model demonstrates higher accuracy compared to the traditional NGM.
  • Numerical tests and INS experiments confirmed the superiority of the proposed method over traditional gravity models for high-precision free-INS.

Conclusions:

  • The developed polynomial gravity model provides an effective balance between computational efficiency and accuracy for real-time INS.
  • This method enhances the performance of high-precision inertial navigation systems by offering improved gravity compensation.