Journal
Scientific and technical journal «Priborostroenie»
UDK629.78 (075.8)
Issue:7 (57)
Download PDF346 Kbyte
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.