An improved self-alignment method for strapdown inertial navigation system based on gravitational apparent motion and dual-vector
Author:
Affiliation:
1. School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China and Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology, Ministry of Education, Nanjing 210096, China
Funder
National Natural Science Foundation of China (NSFC)
Publisher
AIP Publishing
Subject
Instrumentation
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4903196
Reference16 articles.
1. Strapdown Inertial Navigation Technology
2. A fast compass alignment method for SINS based on saved data and repeated navigation solution
3. Observability analysis of piece-wise constant systems. II. Application to inertial navigation in-flight alignment (military applications)
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