SEARCH METHOD FOR OPTIMAL PROGRAM OF LAUNCHER MOVEMENT TO MINIMIZE JETTISONABLE ELEMENTS SCATTERING AREA
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;
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Abstract. The problem of synthesis of the optimal launcher movement control program for active trajectory part is considered. The area of scattering ellipse of jettisonable elements is taken as the functional to be optimized. A method of deliberate replacement of optimizable functional is used for development of the control program.
Keywords:
launcher, jettisonable element, impact area, scattering ellipse, functional
