SYNTHESIS OF SPACE ROCKET MOTION PROGRAM TO MINIMIZE PAYLOAD LAUNCH COST
Mozhaysky Military Space Academy, Department of Navigation and Ballistic Support in Aerospace Means Application and Aircraft Flight Theory, St. Petersburg; Professor
D. A. Bulekbaev
Mozhaysky Military Space Academy, Department of Higher Mathematics, St. Petersburg;
Abstract. The problem of synthesis of the optimal motion program of a space rocket in order to minimize orbital injection cost per kilogram of payload is considered. The problem is formalized and reduced to a standard optimal control problem with constraints. The method of purposeful replacement of optimization functional is applied to solve the problem.
Keywords: space rocket, spacecraft, detachable part, impact area, functional, payload