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Reverse Attitude Statistics Based Star Map Identification Method

Shunmei Dong, Qinglong Wang, Haiqing Wang, Qianqian Wang

TL;DR

This work proposes a reverse attitude statistics-based method for star map identification that is validated in simulation, field test, and on-orbit experiment and improves the identification rate by more than 14.3%, and the solving time is reduced by over 28.5%.

Abstract

The star tracker is generally affected by the atmospheric background light and the aerodynamic environment when working in near space, which results in missing stars or false stars. Moreover, high-speed maneuvering may cause star trailing, which reduces the accuracy of the star position. To address the challenges for starmap identification, a reverse attitude statistics based method is proposed to handle position noise, false stars, and missing stars. Conversely to existing methods which match before solving for attitude, this method introduces attitude solving into the matching process, and obtains the final match and the correct attitude simultaneously by frequency statistics. Firstly, based on stable angular distance features, the initial matching is obtained by utilizing spatial hash indexing. Then, the dual-vector attitude determination is introduced to calculate potential attitude. Finally, the star pairs are accurately matched by applying a frequency statistics filtering method. In addition, Bayesian optimization is employed to find optimal parameters under the impact of noises, which is able to enhance the algorithm performance further. In this work, the proposed method is validated in simulation, field test and on-orbit experiment. Compared with the state-of-the-art, the identification rate is improved by more than 14.3%, and the solving time is reduced by over 28.5%.

Reverse Attitude Statistics Based Star Map Identification Method

TL;DR

This work proposes a reverse attitude statistics-based method for star map identification that is validated in simulation, field test, and on-orbit experiment and improves the identification rate by more than 14.3%, and the solving time is reduced by over 28.5%.

Abstract

The star tracker is generally affected by the atmospheric background light and the aerodynamic environment when working in near space, which results in missing stars or false stars. Moreover, high-speed maneuvering may cause star trailing, which reduces the accuracy of the star position. To address the challenges for starmap identification, a reverse attitude statistics based method is proposed to handle position noise, false stars, and missing stars. Conversely to existing methods which match before solving for attitude, this method introduces attitude solving into the matching process, and obtains the final match and the correct attitude simultaneously by frequency statistics. Firstly, based on stable angular distance features, the initial matching is obtained by utilizing spatial hash indexing. Then, the dual-vector attitude determination is introduced to calculate potential attitude. Finally, the star pairs are accurately matched by applying a frequency statistics filtering method. In addition, Bayesian optimization is employed to find optimal parameters under the impact of noises, which is able to enhance the algorithm performance further. In this work, the proposed method is validated in simulation, field test and on-orbit experiment. Compared with the state-of-the-art, the identification rate is improved by more than 14.3%, and the solving time is reduced by over 28.5%.

Paper Structure

This paper contains 26 sections, 12 equations, 18 figures, 4 tables.

Figures (18)

  • Figure 1: The framework of reverse attitude statistics based star map identification method.
  • Figure 2: The process of constructing a catalog star pairs database based on spatial hash.
  • Figure 3: The distribution of potential attitude, where each dot represents a potential attitude, with the size and color depth of the dot being proportional to the frequency.
  • Figure 4: The angular distance distribution of the whole celestial sphere.
  • Figure 5: Attitude error caused by star position noise at different angular distances.
  • ...and 13 more figures