An algorithm for controlling the spatial motion of a spacecraft with an imperfectly reflecting solar sail based on the laws of locally optimal control for Earth — Mars heliocentric flight
Published: 09.08.2020
Authors: Khabibullin R.M., Starinova O.L.
Published in issue: #8(104)/2020
DOI: 10.18698/2308-6033-2020-8-2006
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control