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A new direct filtering approach to INS/GNSS integration

  • Published:2018-06 Issue: Volume:77 Page:755-764
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Hu Gaoge,Wang Wei,Zhong Yongmin,Gao Bingbing,Gu Chengfan

Funder

National Natural Science Foundation of China

Specialized Research Funds for the Doctoral Program of Higher Education

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference47 articles.

1. An adaptive sensor fusion method with applications in integrated navigation;Jwo;J. Navig.,2008

2. Random weighting method for estimation of error characteristics in SINS/GPS/SAR integrated navigation system;Gao;Aerosp. Sci. Technol.,2015

3. Modified federated Kalman filter for INS/GNSS/CNS integration;Hu;Proc. Inst. Mech. Eng, Part G J. Aerosp. Eng.,2016

4. Principles of GNSS, Inertial, and Multisensor Integrated Navigation Systems;Groves,2008

5. Quadratic extended Kalman filter approach to GPS/INS integration;Wang;Aerosp. Sci. Technol.,2006
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