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;
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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
