Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft
- Авторы: Bykov L.V.1, Pashkov O.A.1, Pravidlo M.N.2, Tishkov V.V.1, Yanyshev D.S.1
-
Учреждения:
- Moscow Aviation Institute (National Research University)
- Toropov State Machine Building Design Bureau “Vympel”
- Выпуск: Том 61, № 2 (2018)
- Страницы: 194-200
- Раздел: 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
Цитировать
Аннотация
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.
Об авторах
L. Bykov
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: bykov@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
O. Pashkov
Moscow Aviation Institute (National Research University)
Email: bykov@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
M. Pravidlo
Toropov State Machine Building Design Bureau “Vympel”
Email: bykov@mai.ru
Россия, Volokolamskoe sh. 90, Moscow, 125424
V. Tishkov
Moscow Aviation Institute (National Research University)
Email: bykov@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
D. Yanyshev
Moscow Aviation Institute (National Research University)
Email: bykov@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
Дополнительные файлы
