Email this article Influence of Interference Effects of the Rotor on the Launch Dynamics of Gliding Unmanned Aerial Vehicle
- Authors: Grumondz V.T.1, Al’bokrinova A.S.1, Noskov S.V.2
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Sukhoi Design Bureau
- Issue: Vol 61, No 3 (2018)
- Pages: 363-370
- Section: 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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Abstract
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.
About the authors
V. T. Grumondz
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: v.grumondz@gmail.com
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
A. S. Al’bokrinova
Moscow Aviation Institute (National Research University)
Email: v.grumondz@gmail.com
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
S. V. Noskov
Sukhoi Design Bureau
Email: v.grumondz@gmail.com
Russian Federation, ul. Polikarpova 23b, Moscow, 125284
