Specific Features in Identification of Instrument Errors of Strapdown Inertial Navigation Systems for Apparatus with Short Phase of Active Flight
The article is devoted to the problem of identification of the instrument errors of the strapdown inertial navigation systems for the apparatus with a short phase of active flight by the difference between the navigation parameters and the data of the satellite navigation equipment. The suggested algorithm makes it possible to a certain degree overcome the difficulties connected with the absence of the data from the satellite navigation equipment during the active flight phase that produces maximum data for the problem to be solved.