Simulation results of the error identification problem of inertial navigation system

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The results of numerical simulation of calibration of inertial navigation system on a moving target are given. As criterion of accuracy the fractional error of calibration of platform and acceleration indicator was taken. The influence of the source information about object kinematics, time of calibration, moments of reading the sensory data, position of reference and calibrated inertial navigation systems on the object upon this error was researched.

Error, calibration, moving base, inertial navigation system, ins, strapdown inertial navigation system (sins)

Короткий адрес: https://sciup.org/147154677

IDR: 147154677

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