Universalization of mathematical model trajectory managements of aeroballistic flying devices in a vicinity of small normal overloads
О.N. Fomenko, А.А. Ghuravlev
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For a class of trajectories of zero normal overloads analytical expressions are received, statement of a problem is carried out and results of optimization of orientation of a longitudinal axis of aeroballistic flying devices are resulted at the moment of the beginning of movement at start of the engine by criterion of the maximal full range of flight.
