Analysis of the Strapdown Inertial Navigation System (SINS) Error Genesis

Pjotrs Trifonovs-Bogdanovs, Anvar Zabirov

Abstract


Analysis and simulation of the Strapdown Inertial Navigation System (SINS) error genesis revealed that the East Feedback Contour has the greatest influence on the development of an error in this model, and angular velocity sensor is the critical element. In order to prevent the development of an error, structural correction in the East Feedback Contour, and elements that are more critical, namely in angular velocity measurement sensors is the best option.

Keywords:
Feedback loops; inertial reference system (IRS); SINS error model simulation; SINS simulink analysis; strapdown inertial navigation system (SINS)

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DOI: 10.2478/tae-2018-0006

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