ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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3
Issue
vol 60 / MARCH, 2017
Article
UDC 629.191

COORDINATES CORRECTION METHOD FOR AIMING MARK OF SPACE ROCKET

V. N. Arseniev
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