Mathematical model of deceleration of landing object by means of parachute-jet system

Aviation technics and technology


Tryamkin A. V.1, Emelyanov U. N.2

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Moscow State Institute of Radio Engineering, Electronics and Automation (Technical University),


The subject of this article is the mathematical model of deceleration process of landing object by a parachute-jet system. The obtained model allows to determine motion characteristics of the object during its deceleration, to analyze the effect of unstability of parameters parachute-jet system and meteorological conditions on motion characteristics of touching down object.

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