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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Influence of the inertia resultant moments inequality on the aerial vehicle rotational motion

Published: 21.02.2023

Authors: Koryanov V.V., Kukharenko A.S.

Published in issue: #2(134)/2023

DOI: 10.18698/2308-6033-2023-2-2254

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

    inertia tensor, mathematical model, differential equations, hodograph, attack angle, slip angle, aerial vehicle, angular velocity
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