On a scheme integration of inertial primary information sensors with on-board navigation correctors aircraft

The new version notinvariant compensation scheme integration inertial sensors with the primary data onboard navigation correctors proposed in this article. Procedure nonlinear discrete filtering to refine estimates of navigation options (using information from the navigation correction and extrapolation of these estimates on the basis of indications of inertial sensors) and linear regression procedure parameter identification model systematic errors inertial sensors (at a given initial time interval using information from navigation correction, built using the apparatus of the theory of sensitivity) form the basis of the proposed scheme.