COORDINATES CORRECTION METHOD FOR AIMING MARK OF SPACE ROCKET
A. F. Mozhaysky Military Spaсe Academy, Department of Onboard Information and Measuring Complexes; Professor
D. A. Bulekbaev
Mozhaysky Military Space Academy, Department of Higher Mathematics, St. Petersburg;
S. B. Silantev
Mozhaysky Military Space Academy, Department of Independent Control Systems;
Abstract. The problem of aiming mark choice to ensure the rocket separated part fall in a given Earth surface area is considered. Analytical solution is presented which allows for determination of aiming mark with minimal prestarting correction of flight program.
Keywords: space rocket, aiming mark, separated part, dispersion ellipse, impact area