Solution of the problem of close integration of inertial-satellite navigation systems, complexed with odometer

Abstract

Solution of the problem of close integration of inertial-satellite navigation systems, complexed with odometer

Sinyutin S.A., Socolov S.V.

Incoming article date: 01.12.2014

The solution of the navigation problem on the basis of integration of inertial-satellite navigation systems, complexed with odometer, in the general case - without simplifying assumptions about the object model of its trajectory, etc. The effectiveness of the solution with the loss of satellite signals is illustrated by numerical experiment.

Keywords: tight integration, inertial - satellite navigation systems, odometer, nonlinear Kalman filter, continuous-discrete filtering