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Spacecraft optimal control in drag braking flight segment during insertion into orbit of Mars artificial satellite
Authors: Sokolov N.L. | Published: 21.12.2015 |
Published in issue: #6(105)/2015 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: spacecraft, insertion into orbit, combined insertion profile, optimal control, research technique, analytical algorithm, implementation efficiency |