Numerical research of the space vehicle transfer problem in circular orbit

There are results of numerical research of the space vehicle transfer problem in circular orbit in the article. For the solution of a problem the method of the moments of N.N.Krasovsky is used. During research following results are received: set of the compromise between propellant consumption and time of response; relations of time of response to various initial deviations on an angle, an eccentricity and cycle time. Results of calculations are processed and deduced simple relations for an estimation of minimally necessary time of control in a problem of transfer.