Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft


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This paper presents the numerical simulation of detachment dynamics of a payload from its parent aircraft. The simulation allowed obtaining the free motion parameters of the payload taking into account its mass and momentum characteristics, aerodynamic forces and moments as well as gravity.

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L. Bykov

Moscow Aviation Institute (National Research University)

编辑信件的主要联系方式.
Email: bykov@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

O. Pashkov

Moscow Aviation Institute (National Research University)

Email: bykov@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

M. Pravidlo

Toropov State Machine Building Design Bureau “Vympel”

Email: bykov@mai.ru
俄罗斯联邦, Volokolamskoe sh. 90, Moscow, 125424

V. Tishkov

Moscow Aviation Institute (National Research University)

Email: bykov@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

D. Yanyshev

Moscow Aviation Institute (National Research University)

Email: bykov@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

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