Abstract: The statistical estimates based RMS coordinate deviation from the initial conditions and the absolute values of angular velocity and the apparent acceleration produced mathematical modeling to determine the coordinates of strapdown inertial navigation system with different standard deviation of the initial conditions.
Keywords: strapdown inertial navigation system, quaternions, the error standard deviation
Authors and copyright holders:
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For citation:
Konakov A. S., Shavrin V. V., Tislenko V. I., Savin A. A. Effect of initial conditions on the RMS estimates of coordinates in strapdown inertial navigation system with quaternion method of transition between the bases. Doklady Tomskogo gosudarstvennogo universiteta sistem upravleniya i radioelektroniki, 2012, no. 1(25), – p. 1. pp. 10–14.
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