Analysis of free oscillation of parachute system with payload aerodynamics
Aviation technics and technology
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractWe 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.