Influence of Interference Effects of the Rotor on the Launch Dynamics of Gliding Unmanned Aerial Vehicle
- Авторы: Grumondz V.1, Al’bokrinova A.1, Noskov S.2
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Sukhoi Design Bureau
- Выпуск: Том 61, № 3 (2018)
- Страницы: 363-370
- Раздел: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230587
- DOI: https://doi.org/10.3103/S1068799818030078
- ID: 230587
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Аннотация
A mathematical model of the gliding unmanned aerial vehicle (UAV) motion is performed taking into account the interference effect of the main rotor on the UAV. Calculated values are presented for the interference addition to the aerodynamic coefficients of forces and moments on the UAV path section close to the carrier. The problems of stabilization and control are solved, providing stability of the UAV motion at the launch with due account of the aerodynamic interference and the effect of short-term upper stage engine operation, as well as a safe distance between the carrier and the UAV during their simultaneous motion.
Об авторах
V. Grumondz
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: v.grumondz@gmail.com
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Al’bokrinova
Moscow Aviation Institute (National Research University)
Email: v.grumondz@gmail.com
Россия, Volokolamskoe sh. 4, Moscow, 125993
S. Noskov
Sukhoi Design Bureau
Email: v.grumondz@gmail.com
Россия, ul. Polikarpova 23b, Moscow, 125284