Analysis of free oscillation of parachute system with payload aerodynamics

Aviation technics and technology


Churkin V. M.*, Serpicheva E. V., Silantiev V. M.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia



We make non-linear analysis of free oscillation of parachute system (PS) at the stage of descent having respect to payload aerodynamic characteristics. The results of theoretical calculations are compared with results of numerical integration of PS motion equations.

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