A Fast Continuous Self-Calibration Method for FOG Rotational Inertial Navigation System Based on Invariant Extended Kalman Filter
Author:
Affiliation:
1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Instrumentation
Link
http://xplorestaging.ieee.org/ielx7/7361/10032973/09975260.pdf?arnumber=9975260
Reference26 articles.
1. The Invariant Extended Kalman Filter as a Stable Observer
2. Anin situhand calibration method using a pseudo-observation scheme for low-end inertial measurement units
3. Left-invariant extended Kalman filter and attitude estimation
4. Invariant Kalman Filtering
5. A new continuous self-calibration scheme for a gimbaled inertial measurement unit
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