Deflection of structural elements in estimating parameters of the controlled motion of the descent vehicle with an inflatable braking device
Published: 25.04.2022
Authors: Koryanov V.V., Kukharenko A.S.
Published in issue: #4(124)/2022
DOI: 10.18698/2308-6033-2022-4-2174
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control