Identification of dynamical paramenters for a short-range rocket system firing

Abstract

The method of identifying the various parameters caused by the aerodynamic motion of a rocket system firing has been developed. An open – loop of fin – stabilized short – range rocket system has been investigated. The mathematical analysis of the motion and dispersion of the rockets has been derived. The identification of such parameters as the velocity at the end of burning time and the drag coefficient of a fin-stabilized short – range rocket has been evaluated for practical applications.