Universalization of mathematical model trajectory managements of aeroballistic flying devices in a vicinity of small normal overloads
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Description: 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.
Reference:
Fomenko, O.N. and Zhuravlev, A.A. (2003), “Universalizatsiia matematicheskoi modeli traektornogo upravleniia aeroballisticheskikh letatelnykh apparatov v okrestnosti malykh normalnykh peregruzok”, Information Processing Systems, Vol. 5(27), pp. 18-27.
Fomenko, O.N. and Zhuravlev, A.A. (2003), “Universalizatsiia matematicheskoi modeli traektornogo upravleniia aeroballisticheskikh letatelnykh apparatov v okrestnosti malykh normalnykh peregruzok”, Information Processing Systems, Vol. 5(27), pp. 18-27.