Email this article Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft
- Authors: Bykov L.V.1, Pashkov O.A.1, Pravidlo M.N.2, Tishkov V.V.1, Yanyshev D.S.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Toropov State Machine Building Design Bureau “Vympel”
- Issue: Vol 61, No 2 (2018)
- Pages: 194-200
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230483
- DOI: https://doi.org/10.3103/S1068799818020071
- ID: 230483
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Abstract
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.
About the authors
L. V. Bykov
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: bykov@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
O. A. Pashkov
Moscow Aviation Institute (National Research University)
Email: bykov@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
M. N. Pravidlo
Toropov State Machine Building Design Bureau “Vympel”
Email: bykov@mai.ru
Russian Federation, Volokolamskoe sh. 90, Moscow, 125424
V. V. Tishkov
Moscow Aviation Institute (National Research University)
Email: bykov@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
D. S. Yanyshev
Moscow Aviation Institute (National Research University)
Email: bykov@mai.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
