FORMULATION OF MATHEMATICAL MODELING PROBLEMS OF AERIAL VEHICLE WITH VARIABLE INERTIAL CHARACTERISTICS

Abstract

In article problems of land-based testing of aeroballistic flying machines
with variable inertial characteristics and their navigating systems are considered.
The integrated approach to the decision of a problem of definition of errors of
angular position strapdown inertial navigation system (SINS) on the stand
of defining inertial characteristics is formulated. Advantages of such approach
are shown.