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Linearized In-Motion Alignment for a Low-Cost INS

  • Kedong Wang*
  • , Xiaohan Xu
  • , Wei Gao
  • , Jinling Wang
  • *Corresponding author for this work
  • Beihang University
  • University of New South Wales

Research output: Contribution to journalArticlepeer-review

Abstract

An accurately linearized in-motion alignment with a large heading error is proposed for a low-cost inertial navigation system with the aiding of global positioning system. The linearization is designed for both the coarse and the fine stages in the local level frame. A criterion is constructed to determine the time to switch the alignment from the coarse stage to the fine one automatically. A vehicle test demonstrates that the proposed alignment converges fast and accurately.

Original languageEnglish
Article number8809209
Pages (from-to)1917-1925
Number of pages9
JournalIEEE Transactions on Aerospace and Electronic Systems
Volume56
Issue number3
DOIs
StatePublished - Jun 2020

Keywords

  • Global positioning system (GPS)
  • Kalman filter (KF)
  • inertial navigation system (INS)
  • initial alignment

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