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Possibilities of defense from a missile attacking from the back hemisphere by a vertical maneuver. (English) Zbl 1260.93015

J. Comput. Syst. Sci. Int. 45, No. 1, 120-127 (2006); translation from Izv. Ross. Akad. Nauk, Teor. Sist. Upr. 2006, No. 1, 125-132 (2006).
Summary: The possibilities to defend an aircraft attacked from the back hemisphere by an air-air missile are investigated. A model problem of determining an optimal vertical maneuver of the aircraft evading a missile that moves in the exponential atmosphere according to a given law of approach subject to aerodynamic drag forces and the Earth’s gravitation is studied.

MSC:

93A30 Mathematical modelling of systems (MSC2010)
93C95 Application models in control theory

Software:

KONUS
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References:

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