Calculation of illumination conditions during putting the spacecraft into geostationary orbit using low thrusters
Published: 28.11.2016
Authors: Kazakovtsev V.P., Koryanov V.V., Prosuntsov P.V., Toporkov A.G.
Published in issue: #12(60)/2016
DOI: 10.18698/2308-6033-2016-12-1568
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control