In-flight development of SINS-500NS satellite inertial navigation system at high latitudes

Basic features of implementing the modes of operation of a strapdown inertial navigation system (SINS) under polar conditions are considered. The above-mentioned SINS based on fiber-optic gyros has been the subject of our studies. Approaches to the improvement of the accuracy characteristics of such...

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Bibliographic Details
Published in2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) pp. 1 - 4
Main Authors Chernodarov, A. V., Patrikeev, A. P., Karpov, O. A.
Format Conference Proceeding
LanguageEnglish
Published Concern CSRI Elektropribor, JSC 01.05.2018
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