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Algorithm to Estimate Parameters of Flying Vehicle Motion

Authors: Asaturov S.M., Zelentsov V.V. Published: 03.05.2014
Published in issue: #1(58)/2005  
DOI:

 
Category: Control Systems  
Keywords:

An algorithm of restrictive filtering of navigation errors in stochastic and uncertain disturbance models of the inertial navigation system for a flying vehicle is studied. Drifts of gyroscopic unit axes, accelerometer errors, wind disturbance and gravitation anomalies have been considered in the disturbance models. Characteristics of the restrictive filtering precision are examined by computer-aided simulation.