Aspects of applying combined mass–time functional in solving the problem of optimizing the multiple-burn transfer of a spacecraft into a high-energy orbit
Authors: Kiriliuk E.V., Stepanov M.N.
Published in issue: #3(123)/2022
DOI: 10.18698/2308-6033-2022-3-2164
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control