ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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3
Issue
vol 60 / MARCH, 2017
Article
UDC 629.78 (075.8)

MODIFICATION OF BALLISTIC STRUCTURE OF ORBITAL CONSTELLATION OF SPACECRAFT ON THE BASE OF THE OPTIMAL CONTROL PRINCIPLE

N. F. Averkiev
Mozhaysky Military Space Academy, Department of Navigation and Ballistic Support in Aerospace Means Application and Aircraft Flight Theory, St. Petersburg; Professor


V. V. Salov
Mozhaysky Military Space Academy, Department of Navigation and Ballistic Support in Aerospace Means Application and Aircraft Flight Theory, St. Petersburg;


A. T. Zhatkin
Mozhaysky Military Space Academy, Department of Navigation and Ballistic Support in Aerospace Means Application and Aircraft Flight Theory, St. Petersburg; Cand. Techn. Sci.


V. V. Kiselev
Mozhaysky Military Space Academy, Department of Navigation and Ballistic Support in Aerospace Means Application and Aircraft Flight Theory, St. Petersburg; Graduate Student


Abstract. The problem of synthesis of a ballistic structure of orbital constellation of spacecraft is considered as a problem of optimal control over a dynamic system. The problem is formalized and reduced to the traditional formulation of the problem of optimal control over a dynamical system with a free right end, the methods for solving the later problem being known.
Keywords: ballistic structure synthesis, optimal control over dynamic system, efficiency rate