A Novel Tightly-Coupled SINS/RCNS Integrated Navigation Method Considering Atmospheric Density Error
Author:
Affiliation:
1. College of Aerospace and Engineering, National University of Defense Technology, Changsha, China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Instrumentation
Link
http://xplorestaging.ieee.org/ielx7/19/10012124/10121389.pdf?arnumber=10121389
Reference34 articles.
1. A Lie Group Manifold-Based Nonlinear Estimation Algorithm and Its Application to Low-Accuracy SINS/GNSS Integrated Navigation
2. A Quasi-Newton Quaternions Calibration Method for DVL Error Aided GNSS
3. A novel navigation method used in a ballistic missile
4. Autonomous satellite navigation using starlight refraction angle measurements
5. High-precision navigation approach of high-orbit spacecraft based on retransmission communication satellites;wen;J Navigat,2012
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