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Comparative study of two velocity update algorithms for SINS

  • Yu Rong Lin*
  • , Liang Chen
  • , Zhen Xian Fu
  • *Corresponding author for this work
  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

Both traditional and dual quaternion-based velocity update algorithms for strapdown inertial navigation system (SINS) are comparatively studied. The leading cause of difference in accuracy between the two algorithms is analyzed and determined in principle. By defining both truncation and approximate integral errors, the difference in accuracy can be not only described qualitatively but also computed quantitatively. The validity of theoretical analysis and derivation is verified through simulation testing. The significant superiority of the dual quaternion algorithm over the traditional one in accuracy is demonstrated through simulation results under highly-dynamic and large-maneuver conditions. Comparison results under both ideal and real dynamic conditions show that the dual quaternion algorithm is superior to the traditional one in overall performance.

Original languageEnglish
Pages (from-to)1185-1193
Number of pages9
JournalBinggong Xuebao/Acta Armamentarii
Volume33
Issue number10
StatePublished - Oct 2012
Externally publishedYes

Keywords

  • Approximate integral error
  • Control and navigation technology of aerocraft
  • Dual quaternion
  • Truncation error
  • Velocity update algorithm

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