Mathematical Simulation with Providing Precision of Information Problem Solution in Modernized Onboard Complexes of Highly-Maneuvering Flying Vehicles

Aspects of mathematical simulation, as applied to a problem of data integration of a commercial inertial navigation system of medium precision with a high-precision receiver of satellite navigation, are discussed. The problem is considered within the framework of modernization of onboard complexes of combatant highly-maneuvering flying vehicles. Particular emphasis has been placed on aspects of compensation of the gyroscope dynamical drift influence on the system accuracy.