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Continuous self‐calibration of platform inertial navigation system based on attitude quaternion model

  • Published:2019-08 Issue:8 Volume:13 Page:1256-1263
  • ISSN:1751-8792
  • Container-title:IET Radar, Sonar & Navigation
  • language:en
  • Short-container-title:IET Radar, Sonar & Navigation

Author:

Qi Wang1,Weiwei Qin1,Lixin Wang1,Qiang Shen1

Affiliation:

1. 3rd DepartmentXi'an High‐tech InstitutionXi'anPeople's Republic of China

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shaanxi Province

Aeronautical Science Foundation of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering

Reference21 articles.

1. Estimation of information sharing error by dynamic deformation between inertial navigation systems;Wang B.;IEEE Trans. Ind. Electron.,2014

2. Continuous self‐calibration of inertial platform based on dual extend Kalman filter;Wang Q.;J. Astronaut.,2017

3. A new continuous self‐calibration scheme for a gimbaled inertial measurement unit;Cao Y.;Meas. Sci. Technol.,2012

4. Continuous self‐calibration and self‐alignment method for floated inertial platform;Ding Z.J.;J. Natl. Univ. Def. Technol.,2015

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